B767 Flightdeck And Avionics

767 Flight Deck and Avionics January 2002

767 Size Comparison 767-200ER/-300ER/-400ER

767-200ER 767-300ER 156 ft 1 in (47.57 m)

767-200ER 61 ft 1 in (18.60 m)

52 ft 0 in (15.8 m)

64 ft 7 in (19.6 m) 155 ft 0 in (47.2 m) 767-400ER 170 ft 4 in (51.92 m)

767-300ER 52 ft 0 in (15.8 m)

61 ft 1 in (18.60 m) 74 ft 8 in (22.76 m) 176 ft 1 in (53.67 m) 767-400ER

55 ft 4 in (16.8 m)

85 ft 10 in (26.1 m) 201 ft 4 in (61.37 m) 797-FD-0052C 1-18-2-MT/CF

767 Evolution

767-400ER 450,000 lb (204,120 kg)

(767-400ER covered in separate book)

767-300ER

767-300 Freighter

412,000 lb (186,880 kg)

412,000 lb (186,880 kg)

767-300ER 387,000 lb (175,540 kg)

767-300* 351,000 lb (159,210 kg)

767-200*

767-200*

767-200ER

767-200ER

300,000 lb (136,080 kg)

315,000 lb (142,880 kg)

351,000 lb (159,210 kg)

395,000 lb (179,170 kg)

*No longer offered.

797-FD-0053C 1-18-2-MT/CF

BOEING PROPRIETARY

797-FD-0054C 11/27-0-MT

Boeing Flight Deck Design Philosophy

• The pilot is the final authority for safe airplane operation; the hierarchy of tasks is • Safety • Passenger comfort • Efficiency • Automation is applied as a tool to aid but not replace the pilot • New technology is used only when there is a clear advantage with no adverse impact on human-machine interface • System designs are error tolerant; the hierarchy of design alternatives is • Simplicity • Redundancy • Automation • Designs address fundamental human strengths, limitations, individual differences, and pilots’ past operational experience

797-FD-0055C 1-18-2-whp/CF

757/767 Commonality Design Features

• Similar handling characteristics • Same crew procedures • Identical recall items • Identical aural warnings • Similar checklists • Similar visual alerts • Same flight deck arrangement • Windshield • Main instrument panel • Overhead panel • Aislestand • Glareshield panels • Panels/controls - Location - Arrangement - Nomenclature • Initial and recurring training will qualify crew for both airplanes

Pilots’ main instrument panel No. 1 windshields

Flt kit

Captain’s seat

First Officer’s seat

Flt kit

Aislestand Overhead panel

• Same flight training simulator can be used for both airplanes

797-FD-0056C 1-18-2-whp/CF

767 Flight Deck - General

Flight Deck and Forward Cabin 767-200ER/-300ER Passenger

First Observer First Officer Galley

Closet

Galley

Lavatory Captain

Second Observer (optional) STA 239

797-FD-0058C 1-18-2-MT/CF

Flight Deck and Forward Cabin 767-300 Freighter STA 273.5

Supernumerary seats First Observer (track mounted)

Lavatory

First Officer Rigid barrier

Access door to cargo bay

Captain Galley

Entry door STA 360.7 797-FD-0059C 1-18-2-MT/CF

Flight Deck Accommodations 767-200ER/-300ER Passenger • Emergency evacuation can be accomplished through the no. 2 side windows.

Hat stowage Fire extinguisher, crash axe, and spare bulb stowage

Coat stowage • Flight deck escape ropes are attached to the airplane structure above each sliding window. They are stowed in compartments in the overhead lining above the pilots’ seats.

Portable light First Observer’s seat

• Oxygen mask, smoke goggles, and life vest are located at each crewmember station.

Suitcase stowage

Coat stowage

Second Observer’s seat (optional)

Suitcase stowage Captain’s seat Flight kit stowage (2 places) 797-FD-0067C 1-18-2-whp/PW

Flight Deck Accommodations 767-300 Freighter Overhead stowage Spare bulb stowage Coat and hat stowage

Lavatory

Supernumerary seats (3) Main deck cargo door control panel Galley

First Officer’s seat Captain’s seat

Life raft stowage Fire extinguisher Suitcase stowage (2)

Illuminated step

797-FD-0068 1-18-2-whp/CF

Pilots’ Main Panel 767-200ER/-300ER Standby magnetic compass Mode control panel VOR (2)

Lighting controls (2)

15

12

E

NS

A/T ARM F R E Q

WARNING

C R S

L NAV

3 3 0

VERT SPD

HDG

IAS/MACH

F/D ON

1 2 6

A/P ENGAGE

ALT 3 2 0 0 0

0 0 0 0

L CMD

B CRS

C

R

CMD

CMD

CWS

CWS

F/D ON

F R E Q

OFF SEL

EPR CAUTION

Master caution and warning lights (2)

6

EW

V NAV

OFF

5 NORM

AUTO MAN

SPD

FL CH

SEL

25 BANK LIMIT

DN

CWS

LOC

V/S

HOLD

HOLD

C R S

AUTO MAN

DISENGAGE

UP

VOR/DME

WARNING CAUTION

OFF

APP

VOR/DME

CLOCK

CLOCK

PANEL

PANEL

OFF

OFF

CHART

CHART

FLOOD

Miscellaneous warning, caution, and advisory lights

OFF MAP PTT

PTT

1

Instrument source select (2)

HDG SEL

LAND 3

FD

BRAKE TEMP w

CAUTION

1.63 2

a

1.8 1.47 1.4

TRUE

1.0

D O O R Sa

TAIL SKID

a

NOSE g

G E A R

Altimeter (2)

CLB

CON

CRZ

1

Marker beacon lights (2)

1

PRESS PSI

X 1000

0 2

g

TO GA

AUTOLAND STATUS

BRAKE

4 3

P/RST

LAND 2

TEST

a

1

THR HLD

NO AUTOLND

VNAV PTH

HDG SEL

FD

2

RIGHT

LEFT

1.8 1.47 1.4

1.0

Thrust management

g

2

EPR

ILS OFF B/CRS

MIDDLE

599

5

a

3

TRK

DME-L

OVSPD r

2

6

MA C H

583

LEADING TRAILING EDGE a EDGE a

140

KNOTS

160 180

200

N1

1114 .

650

EGT

650

UP FLAPS

STW

BWZ

SBJ

KILMR 12000

30 190K

1055 . AUTO

CHR

7

V

10

40

IN. HG

5

a

OUTER b

INSTR SOURCE SEL FLT DIR R

a

29 92 4

3

PRESS

118

OIL

TEMP

13

4

4.4 NM

252

TRK

M

0835.4

0

Z

NAV FMC-L CDU-L

6

OFF

DME-L

ALTN GEAR EXTEND 250K-.75M 20

QTY

.5

DME-R

4 1

KTEB

OFF

2

JFK LGA KJFK KLGA

7.0

167 343 AMBO COL

25 30

7.0 LE

SAX

DN

TE

ALTN

MMU

KILMR 12000

40

FF

GND PROX

ALTN w

w

w

w

FLAP OVRD

N1

0.5 VIB

GEAR OVRD

TERR OVRD

STW

BWZ

SBJ

CHR

BLM

ALTN w

60

EFI w

50

REV

10 GMT

HARRY

ET/CHR

OVRD

OVRD

KTTN ARB 12000 KPNE MUI

OVRD

w

w

w

w

w

w

40

ALTN

20 RUN

30

HLD

w

HLD SS

FS

20

ADE ABE

WARNT 12000

FS RESET

AIR DATA w

w

IRS

RUN

HLD SS

RESET

ALTN

FMC-R

1000 FPM

ALTN FLAPS 5 15

NORM

13

OIL N2

0.5 RTO

1

UP

N2

4

KEWP

118

MAX AUTO

OFF

BARO

95

232

OIL

2 VERTICAL SPEED

.5

LOCK OVRD

DN

RUN

30

HLD

MIDDLE

3

IN.HG

29 92 4

1

20

RUN

ABE

a

AUTO BRAKES 2 3 1

DISARM

ALT MB

1013 6 BRAKE SOURCE a

ET/CHR

T K

w

ADE

R ENG OIL PRESS

AUTO BRAKESa

95 232

L ENG OIL PRESS

a

50 GMT

WARNT 12000

2

8

VALVE

60 REV

KTTN

20

1

w

HARRY

ARB 12000 KPNE MUI

IRS

5

BARO

599

EXTEND OR EXTENDED 270K-.82M

162K N2

ON

ON

259

40

EFI

ALTN

.730

C

195K

20 25

T

0

079

SAX

ALTN

700

GS

A S

15

L

1114 .

1055 .

BLM

COL

1013 6

KNOTS

OFF 210K

5

120

9

167 343 AMBO

INNER/ AIRWAYSw

2

MB ALT

IN OP

MO

FLAP LIMIT IAS 220K

EGT

1

RESERVE BKS & STRG

KEWP

MMU

1

NEG

R

584

240K

4 2

8

EPR

IAS

250 240 220

4

OFF

1

w

0

9

a

PROX G/S INHB a

100

300

VERTICAL SPEED

.5 JFK LGA KJFK KLGA KTEB

ALT

RETRACT 270K

UP

N1

r

GND

a

FMC

80

1000 FPM

DME-R

w

88.3

a

60

0

FMC-R

AUTO PILOT

a

0

350

NAV FMC-L

ALT ALERT a A/T DISC

b

400

1

CABIN ALT

OUTER

29 92 4

BARO

.5

SPEED BRAKESa

259

2

MB ALT IN.HG

1013 6

700

GS .730

88.2 r

MACH

8 NEG

R IN OP

AS

r

INNER/ AIRWAYSw

079

MA C H

KNOTS

TEMP SEL r

A/P DISC

PULL UP

r

1

R

w

1.63

CONFIG r

WINDSHEAR

w

0

C

w

CRZ

CANCEL RECALL

FIRE ALT

FLT DIR L

CDU-L

WHL WELL FIRE r

TAT - 46 C

TEST

g

NO LAND 3

9

MACH

MO

INSTR SOURCE SEL

VNAV PTH

Electronic attitude director indicator (EADI)

REG SELCAL

HDG REF NORM AUTOLAND STATUS P/RST

THR HLD

Heading reference

Engine indication and crew alerting system (EICAS)

Standby attitude indicator Autoland status (2)

Mach/airspeed indicator (2)

FLOOD

OFF MAP

AIR DATA

ALTN w

w

w

Radio distance magnetic indicator (RDMI) (2)

Reserve brakes and steering

Vertical speed indicator (2)

Standby airspeed Standby altimeter Standby engine indicator Autobrakes

Clock (2) Alternate gear Alternate flaps Flap position indicator

Enhanced ground proximity warning system (EGPWS) override

Electronic horizontal situation indicator (EHSI)

797-FD-0060C 1-18-2-whp/CF

Pilots’ Main Panel 767-200ER/-300ER Standby magnetic compass Mode control panel VOR (2)

Lighting controls (2)

15

12

E

NS

A/T ARM F R E Q

WARNING

C R S

L NAV

3 3 0

VERT SPD

HDG

IAS/MACH

F/D ON

1 2 6

A/P ENGAGE

ALT 3 2 0 0 0

0 0 0 0

L CMD

B CRS

C

R

CMD

CMD

CWS

CWS

F/D ON

F R E Q

OFF SEL

EPR CAUTION

Master caution and warning lights (2)

6

EW

V NAV

OFF

5 NORM

AUTO MAN

SPD

FL CH

SEL

25 BANK LIMIT

DN

CWS

LOC

V/S

HOLD

HOLD

C R S

AUTO MAN

DISENGAGE

UP

VOR/DME

WARNING CAUTION

OFF

APP

VOR/DME

CLOCK

CLOCK

PANEL

PANEL

OFF

OFF

CHART

CHART

FLOOD

Miscellaneous warning, caution, and advisory lights

OFF MAP PTT

PTT

1

Instrument source select (2)

HDG SEL

LAND 3

FD

BRAKE TEMP w

CAUTION

1.63 2

a

1.8 1.47 1.4

TRUE

1.0

D O O R Sa

TAIL SKID

a

NOSE g

G E A R

Altimeter (2)

CLB

CON

CRZ

1

Marker beacon lights (2)

1

PRESS PSI

X 1000

0 2

g

TO GA

AUTOLAND STATUS

BRAKE

4 3

P/RST

LAND 2

TEST

a

1

THR HLD

NO AUTOLND

VNAV PTH

HDG SEL

FD

2

RIGHT

LEFT

1.8 1.47 1.4

1.0

Thrust management

g

2

EPR

ILS OFF B/CRS

MIDDLE

599

5

a

3

TRK

DME-L

OVSPD r

2

6

MA C H

583

LEADING TRAILING EDGE a EDGE a

140

KNOTS

160 180

200

N1

1114 .

650

EGT

650

UP FLAPS

STW

BWZ

SBJ

KILMR 12000

30 190K

1055 . AUTO

CHR

7

V

10

40

IN. HG

5

a

OUTER b

INSTR SOURCE SEL FLT DIR R

a

29 92 4

3

PRESS

118

OIL

TEMP

13

4

4.4 NM

252

TRK

M

0835.4

0

Z

NAV FMC-L CDU-L

6

OFF

DME-L

ALTN GEAR EXTEND 250K-.75M 20

QTY

.5

DME-R

4 1

KTEB

OFF

2

JFK LGA KJFK KLGA

7.0

167 343 AMBO COL

25 30

7.0 LE

SAX

DN

TE

ALTN

MMU

KILMR 12000

40

FF

GND PROX

ALTN w

w

w

w

FLAP OVRD

N1

0.5 VIB

GEAR OVRD

TERR OVRD

STW

BWZ

SBJ

CHR

BLM

ALTN w

60

EFI w

50

REV

10 GMT

HARRY

ET/CHR

OVRD

OVRD

KTTN ARB 12000 KPNE MUI

OVRD

w

w

w

w

w

w

40

ALTN

20 RUN

30

HLD

w

HLD SS

FS

20

ADE ABE

WARNT 12000

FS RESET

AIR DATA w

w

IRS

RUN

HLD SS

RESET

ALTN

FMC-R

1000 FPM

ALTN FLAPS 5 15

NORM

13

OIL N2

0.5 RTO

1

UP

N2

4

KEWP

118

MAX AUTO

OFF

BARO

95

232

OIL

2 VERTICAL SPEED

.5

LOCK OVRD

DN

RUN

30

HLD

MIDDLE

3

IN.HG

29 92 4

1

20

RUN

ABE

a

AUTO BRAKES 2 3 1

DISARM

ALT MB

1013 6 BRAKE SOURCE a

ET/CHR

T K

w

ADE

R ENG OIL PRESS

AUTO BRAKESa

95 232

L ENG OIL PRESS

a

50 GMT

WARNT 12000

2

8

VALVE

60 REV

KTTN

20

1

w

HARRY

ARB 12000 KPNE MUI

IRS

5

BARO

599

EXTEND OR EXTENDED 270K-.82M

162K N2

ON

ON

259

40

EFI

ALTN

.730

C

195K

20 25

T

0

079

SAX

ALTN

700

GS

A S

15

L

1114 .

1055 .

BLM

COL

1013 6

KNOTS

OFF 210K

5

120

9

167 343 AMBO

INNER/ AIRWAYSw

2

MB ALT

IN OP

MO

FLAP LIMIT IAS 220K

EGT

1

RESERVE BKS & STRG

KEWP

MMU

1

NEG

R

584

240K

4 2

8

EPR

IAS

250 240 220

4

OFF

1

w

0

9

a

PROX G/S INHB a

100

300

VERTICAL SPEED

.5 JFK LGA KJFK KLGA KTEB

ALT

RETRACT 270K

UP

N1

r

GND

a

FMC

80

1000 FPM

DME-R

w

88.3

a

60

0

FMC-R

AUTO PILOT

a

0

350

NAV FMC-L

ALT ALERT a A/T DISC

b

400

1

CABIN ALT

OUTER

29 92 4

BARO

.5

SPEED BRAKESa

259

2

MB ALT IN.HG

1013 6

700

GS .730

88.2 r

MACH

8 NEG

R IN OP

AS

r

INNER/ AIRWAYSw

079

MA C H

KNOTS

TEMP SEL r

A/P DISC

PULL UP

r

1

R

w

1.63

CONFIG r

WINDSHEAR

w

0

C

w

CRZ

CANCEL RECALL

FIRE ALT

FLT DIR L

CDU-L

WHL WELL FIRE r

TAT - 46 C

TEST

g

NO LAND 3

9

MACH

MO

INSTR SOURCE SEL

VNAV PTH

Electronic attitude director indicator (EADI)

REG SELCAL

HDG REF NORM AUTOLAND STATUS P/RST

THR HLD

Heading reference

Engine indication and crew alerting system (EICAS)

Standby attitude indicator Autoland status (2)

Mach/airspeed indicator (2)

FLOOD

OFF MAP

AIR DATA

ALTN w

w

w

Radio distance magnetic indicator (RDMI) (2)

Reserve brakes and steering

Vertical speed indicator (2)

Standby airspeed Standby altimeter Standby engine indicator Autobrakes

Clock (2) Alternate gear Alternate flaps Flap position indicator

Enhanced ground proximity warning system (EGPWS) override

Electronic horizontal situation indicator (EHSI)

797-FD-0060C 1-18-2-whp/CF

Overhead Panel 767-200ER/-300ER Emergency lights Miscellaneous annunciation

Cargo heat

Passenger oxygen*

Engine start Window heat EMER DOORS

CARGO DOORS

ACCESS DOORS

CAPT PITOT

FO PITOT

L AOA

R AOA

L AUX PITOT

R AUX PITOT

TAT

ENTRY DOORS

IRS MODE SEL W

DSPL SEL PPOS WIND TK/GS

Inertial reference

1

N 2

3

W 4

H 5

E 6

7

S 8

9

ENT

0

CLR

HDG

FWD

Yaw damper

STAB TRIM

SPOILERS

UNSCHED STAB TRIM

RUDDER RATIO

ARMED

AUTO SPDBRK

BULK

ON

ON

OVHT

OVHT

ON

ON

WINDOW HEAT L

R FWD

FWD

SIDE

PRESS

ON

ON

ON

ON

UNLKD

INOP

INOP

INOP

INOP

INOP

R

ALIGN

ALIGN

ALIGN

BOTH

L

ON DC

ON DC

ON DC

DC FAIL

DC FAIL

VALVE C

ALIGN NAV ATT

OFF

C

W

AUTO

AUTO

OFF

OFF

GND

ON

CONT

CONT

FLT

FLT

OFF

ON

ON

INOP

INOP

FAULT

ELEC ENG CONT

ALTN

ON D I S C H

NORM ALTN

SYS PRESS

O F F

QTY

QTY

L ENG

APU GEN EXT PWR

QTY

R ENG

C 1-ELEC-2 ON

ON

ON

PRESS

PRESS

PRESS

I

A OVHT

OVHT

Y

R PUMPS

VALVE

PRESS

AIR

ELEC

PRESS

PRESS

PRESS

BUS OFF

R

P R E S S

R BUS

R

ON

ON

OFF

OFF

MANUAL

ON

BUS OFF

P R E S S

DESCEND

034 0

OVHT

MODE SELECT AUTO 2

LB

KG

LB KG FUEL QTY X 1000

M AUTO

AUTO

A OFF

ON

OFF

AUTO ON

OFF

O F F

A ON

N

O F F

ON DRIVE

DRIVE

TEMP

LB

CABIN

WING ANTI-ICE ON START

OFF

FAULT

2

8

4 6

L

R

ON

ON

VALVE

VALVE

R

VALVE

VALVE

PSI

DIFF

DUCT LEAK

ERASE

BLEED

L ENG 1 2

FT X 1000

ALT

Bleed air and pneumatic

FPM X

RATE 1000

O F F

V A L V E

OVHT

ADP

APU

R ENG

Fuel jettison

O F F

EQUIP COOLING VALVE AUTO

PRESS DIFF LIMIT: T/O & LDG .125 PSI

OFF

Electrical

V A L V E

1 2 0

CABIN ALTITUDE

WIPER TEST

VALVE

DL UE CA TK

OVHT

0 2 25 4 20 15 6 10 8

0

10

ENGINE

ON L

RUN

R ISLN

BLEED

C

ON

0

C ISLN

KG

TOTAL

D

APU

80

MAN

AUTO 1

R

DUCT LEAK

GEN CONT

R

E

OVHT

OVHT

GEN DRIVE DISC L

C

L

R

L GEN CONT

60

20

VALVE

AUTO INOP R

S T B Y

W

DUCT PRESS PSI

L ISLN

LDG ALT

L

C

W

MAX

MIN

ON

S T B Y

AUTO RATE

CLIMB

CL

UTILITY BUS L

VALVE OP

FUEL CONFIG

N

OFF C

PRESS

C PUMPS

M

D

M

D

VALVE

PRESS

PACK OFF AUTO

N

AFT

FWD

FWD

INOP

W

MAN

ON

OFF

OFF

ON

ON

ISLN

L BUS

ON

Y ELEC

D

N

BUS TIE

RESET C

PACK OFF

ON

PRESS

AVAIL AUTO

A OVHT

ON

ISLN

R PACK

INOP SEATBELTS AUTO

AUTO

FUEL XFEED

W

AUTO L PACK

CABIN ALTITUDE CONTROL

AUTO

R

ON PRESS OVHT

AFT

P

I

E

Passenger signs*

C

PASS SIGNS

ON

O F F

BUS TIE

PUMPS

HYD

R

INOP

RESET

OFF L PUMPS

GND CALL

ALERT

NO SMOKING AUTO

OFF

SYS PRESS

AFT

ALERT

BAT

OFF

MID

ON

ON VALVE

ON SYS PRESS

FWD

OFF

ON VALVE

STBY POWER AUTO

R

NORM

M

INOP

INOP

CABIN CALL

FUEL JETTISON

L

Hydraulic

ON

R

L–NOZZLE–R

R

ON

FLT DK

BAT

P

Air-conditioning

W

OFF

L - RECIRC FAN - R

YAW DAMPER

Electronic engine control (EEC)

C

W

OFF

TRIM AIR

OFF GND

L

Pilot’s call panel

AFT CAB AUTO

R

2

1

VALVE

FAULT

FAULT ALIGN NAV ATT

INOP

MID CAB AUTO

ENG START

DC FAIL

OFF

INOP

FWD CAB AUTO

C

NAV ATT

COMPT TEMP

AIL LOCK

ANTISKID

Compartment temperature

UNARMED

RAM AIR TURB

L

FAULT ALIGN

CARGO HEAT

PASS OXY

SIDE

SYS DSPL C R

L

OFF

EMER LIGHTS OFF

N

STBY

LOW

OVHT

OVRD SMOKE NO COOLING

HIGH

COCKPIT VOICE RECORDER

HEADPHONE CKT BKR

OVHD PANEL

DOME

Cabin altitude

PANEL/FLOOD

APU

GLARESHIELD

LT OVRD

ANTI COLLISION

POSITION

RED

ON

OFF

Voice recorder

AISLE STAND

OFF

ON

WING OFF

ON

OFF

FLT DK DOOR

ON

UNLKD UNLKD

R

Fuel Equipment cooling

LANDING WING L

NOSE GEAR R

ON

Miscellaneous lighting

LOGO ON

TAXI RUNWAY TURNOFF L

OFF

OFF

WHITE

ON

OFF

OFF

ON

ON

IND LTS DIM

TEST BRT

Wing/engine anti-ice Windshield controls

*Passenger airplanes only. 797-FD-0061C 12-5-1-whp

Center Aislestand 767-200ER/-300ER EICAS control C

VNAV

C MM

PROG

C

SP

INIT REF

RTE

FIX

LEGS

MENU

NAV RAD

BRT

EXEC

E

D

H

I

J

M

N

O

R

S

T

W

X

DEL

/

M S G

D S P Y

O F S T

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0

+/-

Fuel control

RS

MCDU (2) Throttle levers Stab trim switches Flap lever Speed brake lever

TE

EFIS control (2) Stab trim cutout

20 10

PLAN APL NOSE DN

APL NOSE UP

Stab trim indicator (2)

ALTN STAB TRIM

0

APL NOSE ON S T A B

ENG VALVE SPAR VALVE

ENG VALVE SPAR VALVE

2 4

Parking brake

L

6

FUEL CONTROL R RUN

T R I M APL O NOSE F UP F

8 NORM

CUT OFF

10 12

L O E F F

14 CUT OUT L

Weather radar

C STAB TRIM

WX EST

L ENG OVHT

MAP

ATC/TCAS

+5

TILT +10

0 1

-15 -10

VE

ENG BTL 2 DISCH

DISCH

-5

ILS

ENG BTL 1 DISCH

R ENG OVHT

+15

ARMED

FWD

AFT

1

2

A C A R G O

DISCH

2

F I R E DISCH

Radio communications panel (3)

STANDBY VHF C

VHF R

AM

HF R

R

ACTIVE

FLT

VHF

CAB

L

VHF L

VHF C

VHF R

HF L

AM

HF R

HF SOL

PA

L VHF

BOOM R

Engine, cargo, and APU fire control

BTL DISCH

R I G H T

L E F T

O F F

ADF

ARMED

R

C VHF

R VHF

FLT

Audio selector (2)

ALT OFF ALT ON

SAT

OXY

VOR V B R

APP C R L MKR

ATC

ATC 2

TA

STBY TEST

MIC

TA/RA

FAIL

L 1

ATC

2

IDENT

INT

ATC

VOR ADF R L R L

R TONE L R

L

R HF

SAT VOR V B R

F.

F R E Q

C R S TEST

ILS RUDDER TRIM

Fire/overheat test

15

STANDBY VHF C

VHF R

AM

HF R

10

NOSE LEFT

0

5

10

15

UNITS NOSE RIGHT

AILERON NOSE LEFT

FIRE/OVHT TEST ENG/APU CARGO

5

SYS FAIL

LEFT WING DOWN

RIGHT WING DOWN

R U D D E R

NOSE RIGHT

Aileron/rudder trim

FAIL P-RESET

797-FD-0062C 1-18-2-whp

Right Side Panel 767-200ER/-300ER Gasper air

Flight recorder and service interphone Avionics cooling monitor Data loader selector switch AIR DATA L COMPTR R

TEST

FLT REC CONFIG T/O

Miscellaneous test

SERV INTPH

First Observer’s oxygen

TEST

OFF OFF

WING ANTI ICE

TO

ON

ON NORM TEST

GND PROX

LDG

EADI

DUCT LEAK

VOR-L EHIS

E1 / E2

FMCDU-L

IRU-C

IRU-R

E5 IRU-L RESET TEST

YAW DMPR L EQUIP COOL

STRUT LEAK

E / E COOLING MONITOR

Squib test

R

WINDOW/ FUEL QTY PROBE HEAT

SQUIB TEST

TEST

ENG R

L

Generator reset

L

1

DATA LOAD SELECTOR

1

APU

L (k / mgk (k / mgk

EMER ESCAPE R TEST 1 SLIDE TEST 2 SPOILER CARGO 2 2A TEST 1 FWD TEST 2 AFT

C (k / mgkcjcj fg

C

FIELD OFF

Portable data loader connection (shown here) or airborne data loader

R fhfdhfh (k / mgk (k / mgk

Smoke goggles

SYSTEM SELECT (k / mgkzz (k / mgkzz (k / mgkzz (k / mgkzz zzOzz zzOzz (zzhfh / C lknmv zzOzz l zzOzz zzOzz

Flight control shutoff

MO173

OXYGEN MASK

2

APU

FIELD OFF

l zzOzz

zzOzz zzOzz zzOzz zzOzz

GEN FIELD MAN RESET L

N 100% PUSH

HYD GEN

FIELD OFF

lCOC

l zzOzz

lFlS zzOzz zzOzz

DATA TRANSFER UNIT RECEPTICAL

MO173

FLT CONTROL SHUTOFF - GND USE ONLY L

C T A I L

ON OFF

OFF

W I N G

ON OFF

R T A I L

ON

ON OFF

W I N G

ON OFF

ON OFF

EICAS MAINT EVENT READ

DISPLAY SELECT AUTO ECS

ELEC

PERF

MSG

HYD

APU

CONF

ENG

MCDP

EXCD

EEC maintenance

TEST

REC

MAN

ERASE

EPCS

Book stowage

RESERVE BRAKES & STRG RESET/ DISABLE

C HYD SYS ISLN

NORM

FLIGHT RECORDER SYS TEST PLUG

Lighting control

L VHF

C VHF

R VHF

FLT

CAB

PA

EICAS maintenance

EEC MAINT L ENG POWER

R ENG POWER

MIC

BOOM L

TEST

INT

First Observer’s audio First Observer’s jack panel

MAP

R

L

HF

VOR ADF R L R L

NORM

LIGHTING

R SAT

VOR V B R

OXY APP C R L MKR

PANEL BOOM MIC/HEADSET

HEADPHONE

HANDMIC

Flight recorder system test plug

OFF

Reserve brakes and steering test Ashtray/cup holder 797-FD-0063C 2-27-2-whp/CF

767 Flight Deck - EFIS

Electronic Flight Instrument System (EFIS) 767-200ER/-300ER

Captain’s instrument source select panel

Left EADI

Right EHSI

Left EHSI

Left EFIS control panel

Left EFIS symbol generator

• Thrust management system • ILS navigation system • Radio altimeter system

• PWS system • VOR system • DME system

Right EADI

Right EFIS control panel

Center EFIS symbol generator

First Officer’s instrument source select panel

Right EFIS symbol generator

• Autopilot flight director system • Weather radar system • ADC system

• ADF system • EGPWS • FMCS

• TCAS • IRS 797-FD-0069C 2-26-2-whp/CF

797-FD-0071 1-18-2-PW/CF

EFIS/IRS Switching 767-200ER/-300ER Captain’s instruments EADI - Electronic attitude director indicator EHSI - Electronic horizontal situation indicator EFI - Electronic flight instrument IRS - Inertial reference system RDMI - Radio distance magnetic indicator SG - EFIS symbol generator -Vertical speed indicator VSI

First Officer’s instruments

EADI

EADI RDMI

RDMI

EHSI

EHSI

VSI

VSI

N

Capt EFIS control panel

Capt EFI switch

ALTN

Capt IRS switch

ALTN

A

C-SG

L-SG

N

R-SG

1 N

N

F/O EFIS control panel

ALTN

F/O EFI switch

ALTN

F/O IRS switch

A

A

L-IRS 1

A

A

C-IRS

N

R-IRS

This switch remains in the N position when the Capt EFI switch is selected to ALTN. 797-FD-0070 1-18-2-whp/CF

Electronic Attitude Director Indicator 767-200ER/-300ER Attitude comparator annunciations

Pitch limit indicator

PITCH

Ground speed

GS250

20

ROLL

DH100

2500

20

Selected decision height Radio altitude

F 10

Speed deviation scale and pointer

Autothrottle status Autothrottle mode AFDS pitch mode

Localizer deviation scale and pointer

Split axis flight director cue

10

Glideslope deviation scale and pointer

10

S A/T

SPD G/S VNAV

10

WINDSHEAR 20

20

Windshear annunciation

CMD

AFDS status

LOC LNAV

AFDS roll mode

Slip/skid indicator

797-FD-0073 2-26-2-whp/CF

Electronic Horizontal Situation Indicator 767-200ER/-300ER—Expanded Map Mode • Map mode displays include reference data programmed in the FMC, such as • ETA, distance to go, range to altitude • Top-of-climb, step-climb, top-of-descent, and bottom-of-descent points • Holding pattern • Procedure turns

Distance to active waypoint

Magnetic (M) or true (T) reference

L ADF (head) Track-up annunciation Aircraft track

18.3

NM

TRK

252 M

0835.4z VAR/+TWX +12

Selected heading

Aircraft heading ETA at active waypoint Waypoint not on flight plan (selectable) Weather radar mode, gain, and antenna tilt R ADF (head) Compass rose

MLF

Instantaneous track

Airport (selectable)

AST

VORTAC (selectable)

40 STW

Estimated time and altitude at waypoint (selectable)

KILMR 12000 0841Z

Active flight plan

Range scale (number is half selected range)

Range to selected altitude

KTTN 0 32

Weather radar return (selectable)

0 14 WARNT

20

Wind speed and direction

Vertical deviation scale and pointer Waypoint on flight plan Manually selected VOR course

Airplane symbol

Trend vector

797-FD-0074 2-26-2-whp

Electrical Horizontal Situation Indicator 767-200ER/-300ER—Center Map Mode

Current track

Magnetic/true reference ETA at active waypoint

Distance to active waypoint

25.5

TRK

NM

138

1335.4z WX +12

M FGH I J

15

12

Weather radar mode, gain, and tilt Selected heading bug

9

18

Heading pointer

20

KLMNO 35000 1335Z

Active route

6

21

NOP

3

24

Position trend vector Airplane symbol Vertical deviation scale and pointer

20 27

VWXYZ

0

30

33

20

797-FD-0075C 12-4-1-whp

Electronic Horizontal Situation Indicator 767-200ER/-300ER—Expanded VOR/Approach Mode

DME distance to VOR or LOC DME

140

HDG

262 M VAR/WX +T +12

Selected course (VOR mode) or runway heading (approach mode)

Instantaneous track 20

Course deviation scale and pointer (VOR or approach mode)

Glideslope deviation scale and pointer (approach mode only) To-from VOR station (VOR mode only)

System source annunciation (VOR or approach mode)

20

TO

VOR R

110.10

ILS frequency (approach mode only)

797-FD-0076C 1-19-2-whp

Electronic Horizontal Situation Indicator 767-200ER/-300ER—Center VOR/Approach Mode

Drift angle pointer DME

140 HDG 038

To-from VOR station (VOR mode only)

M

Airplane symbol

Glideslope deviation (approach mode only)

20 VOR R

TO

110.10

797-FD-0077C 1-19-2-whp

Electronic Horizontal Situation Indicator 767-200ER/-300ER—Plan Mode

ACT

RTE

1

LEGS

1 / 9

250 • H D G

ACY

028 •

158 /

530A

178 /

FL560

.824 /

FL340

.824 /

FL340

4.4 NM

TRK

252

M

0835.4 Z

2 NM

WTP 08 322 •

1 1 1 NM

SBY 032 •

9 6 NM

WPT 07 055 •

3 9 NM

WPT 06

.824 / FL340 M AP C TR


STEP>

WPT 10 INIT REF

RTE

CLB

CRZ

DES

ACY

BRT

WPT 11

SBY

WPT 08 FLY P1

HAR

N

Plan mode displays active flight plan referenced to true north. Pilots can step through flight plan on MCDU and EHSI by pushing “STEP” line select key.

797-FD-0078C 1-19-2-whp

EFIS Control Panel 767-200ER/-300ER

EHSI brightness control • Outer knob - EHSI display • Inner knob - weather radar return

Decision height alert reset

ADI RST

BRT

DH REF

EADI brightness control

1 0 0

Terrain data displayed when in MAP, CENTER MAP, EXPANDED APPROACH, and EXPANDED VOR modes

Decision height selector

TERR

WXR

BRT

EHSI range selection • Outer knob - selects desired nautical mile display range for MAP, CENTER MAP, EXPANDED APPROACH, and EXPANDED VOR modes • Center switch (TFC) - displays TCAS data when in MAP, CENTER MAP, EXPANDED APPROACH, and EXPANDED VOR modes

NOTE: Terrain data and weather radar cannot be shown on the same EFIS display at the same time. Selection of the TERR switch turns off weather radar display if showing. Selection of the WXR switch turns off terrain display if showing. It is possible, and a common practice, to show weather radar on one pilot’s EFIS display and show terrain data on the other pilot’s EFIS display.

40

80 160

20 10

TFC

320

APP VOR

ON

PLAN CTR

MAP NAVAID ARPT INOP

MAP

ON

DATA

WPT

ON

ON

Weather radar return displayed when in MAP, CENTER MAP, EXPANDED APPROACH, and EXPANDED VOR modes EHSI mode selector • Outer knob - selects VOR, APPROACH, MAP, and PLAN display modes • Center switch (CTR) - alternates display modes between center and expanded formats for VOR, APPROACH, and MAP modes

Map switches - select information to be displayed in MAP or CENTER MAP mode: • NAVAID - displays high altitude navigation aids in FMC database if selected range is 80 nmi or greater • ARPT - displays airports in FMC database • DATA - displays altitude and ETA for each waypoint on the active route • WPT - displays waypoints in the FMC database but not on the active route if selected range is 40 nmi or less 797-FD-0079C 1-19-2-whp

Weather Radar 767-200ER/-300ER ADI RST

BRT

DH REF

Brightness control (inner knob) • Adjusts brightness of WXR return on EHSI

1 0 0

18.3

NM

TRK

252 M

0835.4z VAR/+TWX +12

Weather radar mode, gain, and antenna tilt data displayed on EHSI.

MLF AST

WXR

TERR

40

BRT

40 10

160

TFC

320

APP VOR

ON

0 32

MAP 0 14 WARNT

PLAN CTR

MAP NAVAID ARPT INOP

KILMR 12000 0841Z

KTTN

80

20

STW

ON

20

DATA

WPT

ON

ON

Weather radar switch • Pushing the WXR switch displays returns on the MAP, EXPANDED MAP, EXPANDED APPROACH, and EXPANDED VOR modes of the EHSI.

Weather radar returns • When the WXR switch is pushed on the EFIS control panel, the weather radar returns are displayed on the respective on-side EHSI. • The most intense areas of precipitation are displayed in red, less intense in amber, and least intense in green. • Detected turbulence is displayed in magenta.

Aislestand

WX

Gain control • AUTO presents an optimum receiver sensitivity for best weather radar display. • Preset gain occurs automatically only in WX mode. • Rotate manually to set receiver gain.

TEST

MAP TILT +10 +5

+15

GAIN

Radar mode selector • TEST – displays maintenance test pattern • WX – displays weather radar returns • MAP – displays ground returns

0 -5 AUTO

MAX

-15 -10

Antenna tilt control • Controls antenna tilt angle with reference to horizon

Weather radar panel (representative)

797-FD-0080 C 1-19-2-whp

Flight Instruments 767 ALT

9

MACH

604

8

0

1 3,6 9 5 MB ALT

6 245 4

1013 6

KNOTS

Mach/airspeed indicator • Each Mach/airspeed indicator displays airspeed, Mach, and Vmo data from its on-side air data computer (ADC). • Each indicator displays data from the off-side ADC when the respective air data switch is selected to the ALTN position. • The command speed bug can be moved automatically from the FMC CDU or manually from the IAS/Mach selector on the MCP.

5

IN.HG

2

1

w

1

VERTICAL SPEED

.5 2

4

0 3

29 92 4

6 1000 FPM

.5

4 1

2

BARO

Altimeter • Each primary altimeter displays altitude data from its on-side ADC. • Each indicator displays data from the off-side ADC when the respective air data switch is selected to the ALTN position. • An ALT light on each indicator provides visual indication of altitude alerting.

Vertical speed indicator (VSI) • Each vertical speed indicator displays vertical speed data from its on-side inertial reference unit (IRU) and on-side ADC. • Each indicator displays data from the center IRU when the respective IRS switch is selected to the ALTN position and from the off-side ADC when the respective ADC switch is selected to the ALTN position.

0 3 6.0 0 9 5.7 DME-L

DME-R

CHR

DATE

60 50

10 GMT ET/CHR

40

20

RUN

RUN

30

HLD

HLD SS FS

RESET

Radio distance magnetic indicator (RDMI) • Each indicator displays magnetic heading; VOR and/or ADF bearings; and VOR, ILS, DME, or VORTAC distance. • Each indicator displays magnetic heading data from its on-side IRU. • Each indicator displays magnetic heading data from the center IRU when the respective IRS switch is selected to the ALTN position.

• Both indicators display magnetic heading when the HSI heading reference switch is in the NORM position and the airplane is between 73 N and 60 S latitude (with standard MAGVAR table) or 82 N and 82 S latitude (with extended MAGVAR table). The heading flag is displayed when the switch is in the TRUE position or the airplane is outside of these latitudes.

Clock • Provides Greenwich mean time (GMT) in day, month, and year or hours and minutes on the GMT indicator. Provides elapsed time or chronograph on the ET/CHR indicator. • The chronograph is controlled by the pushbutton on the clock or the remote switch on the glareshield. 797-FD-0081 C 1-18-2-whp/CF

Instrument Source Select Panel 767-200ER/-300ER Flight director selector • Selects the flight control computer (L, C, or R) for flight director command bar operation INSTR SOURCE SEL FLT DIR L C

IRS switch (alternate action) BLANK - selects normal configuration: • L IRS supplies L and C EFIS SG, CAPT VSI, and F/O RDMI • R IRS supplies R and C EFIS SG, F/O VSI, and CAPT RDMI • C IRS is available as the alternate IRS source ALTN - selects center IRS for attitude, heading, and track data for the appropriate systems above Air data switch (alternate action)

R

NAV FMC-L CDU-L

FMC-R

ALTN w

EFI

w

NAV instrument source selector • Selects source supplying FMS information to symbol generators and flight control computers Captain’s side: - FMC-L – supplies L and C EFIS SG, and L and C FCC - FMC-R – supplies L and C EFIS SG, and L and C FCC - CDU-L– supplies L and C EFIS SG First Officer’s side: - FMC-R – supplies R EFIS SG and R FCC - FMC-L – supplies R EFIS SG and R FCC - CDU-R – supplies R EFIS SG

ALTN w

IRS

w

BLANK - selects normal configuration: • L ADC supplies CAPT MACH/AIRSPEED and primary altimeter • R ADC supplies F/O MACH/AIRSPEED and primary altimeter ALTN - selects opposite air data computer to supply above instruments INSTR SWITCH EICAS advisory message • Indicates each pilot has selected ALTN with EFI switch

ALTN w

AIR DATA

w

INSTR SWITCH

EFI switch (alternate action) BLANK - selects normal configuration: • L EFIS SG supplies CAPT ADI and HSI • R EFIS SG supplies F/O ADI and HSI • C EFIS SG is available as the alternate SG ALTN - selects center EFIS SG for ADI and HSI display • CAPT has display control if each pilot has selected ALTN (C-SG) • Causes EICAS message of INSTR SWITCH if each pilot has selected ALTN

EICAS display

797-FD-0082C 1-19-2-whp/CF

Standby Flight Instruments 767-200ER/-300ER

15

Standby attitude indicator • The self-contained standby attitude indicator incorporates an ILS display with backcourse capability.

12

NS

OFF

E

6

Standby magnetic compass • A direct reading compass is installed on the center window post.

EW

ILS B/CRS

0

Standby airspeed indicator • The standby airspeed indicator (pneumatic) receives input from the L AUX pitot and the alternate static system.

60

80

400

100

350

IAS

120

15

12

NS

E

6

EW

300 250 240 220

140

KNOTS

200

160 180

0

Standby altimeter • The standby altimeter (pneumatic) receives input from the alternate static system.

1

9 8

7

03

ALT MB

1013 6 BARO

6 95 IN. HG

2

3

29 92 4 5

Pilots’ main panel

797-FD-0083C 1-19-2-whp/CF

767 Flight Deck - EICAS and Other Alerting Systems

797-FD-0085C 1-19-2-MT/CF

Engine Indication and Crew Alerting System 767-200ER/-300ER (EICAS)

Engine indication and crew alerting system (EICAS) features: • Operational displays: • Primary and secondary engine parameters • Crew alerting messages • Status page provides additional systems data for determining the readiness of the airplane for dispatch • Maintenance pages • Automatic and manual recording of maintenance data • Automatic display of in-flight start envelope

Pilots’ main panel

797-FD-0084C 1-19-2-whp/CF

EICAS Display Upper display

Standby engine indicator EPR

Lower display

EICAS maintenance panel

104.7

N1

104.7

625

EGT

625

102

N2

102 AUTO ON

Analog data Digital data Discrete inputs From airplane subsystems

CAUTION

CANCEL

Warning electronic unit

Speaker Speaker

Speaker Speaker

Dedicated caution and warning lights

RECALL

EICAS fail

Left EICAS computer unit

Right EICAS computer unit

Engine sensors

splay select pa WARNING WARNING CAUTION CAUTION

Master caution/warning switches

797-FD-0086C 1-19-2-whp/CF

EICAS Display Select Panel 767-200ER/-300ER

EICAS display brightness control • Inner knob controls brightness of upper display unit • Outer knob controls brightness of lower display unit

EICAS computer select knob AUTO Selects the left computer and automatically switches to the right computer upon detected failure L, R Manually selects the left or right computer

DISPLAY

COMPUTER

ENGINE STATUS

EVENT RECORD

L

AUTO

R

Aislestand

Engine display switch • Pushing selects or deselects SECONDARY ENGINE display on lower CRT Status display switch • Pushing selects or deselects the STATUS display on lower CRT

BRT

THRUST REF SET L

BOTH

R MAX IND RESET

PULL

Event record switch • Records maintenance data into nonvolatile memory

Maximum indication reset switch • Resets displayed overlimit readouts

Manual thrust set knob • Inner knob • Push - reference thrust automatically set by TMC • Pull and rotate - manually sets reference thrust bug on PRIMARY ENGINE display • Outer knob • Rotate - selects engine(s) for manual thrust reference control 797-FD-0087C 1-19-2-whp/CF

Typical Normal EICAS Formats 767-200ER/-300ER

TAT

-12o C

TAT -12oC 1.63

2.0

1.63

CRZ 2.0

1.32 1.0

1.63 2.0

1.32 1.0

1.5

TAT -12oC

2.0

1.32

1.0

1.5

1.5 EPR

54.2

54.2

55.3

N1

70

OIL PRESSURE

105 OIL TEMP 428

441

1.32

1.0

1.5

N1

428

2.0

EPR

55.3

1.63

CRZ

1.32

1.0

1.5

EPR

54.2

2.0

1.0

1.5

1.63

1.63

CRZ

1.32

441

18

OIL QTY

3.1 VIS

55.3

N2

70 105

528

EGT

528

18

104

N2

104

3.1

15.3

FF

15.3

EGT

EGT

L 0.76

HYD QTY

92 70 OIL

105 OIL

18 OIL

0.6

94

APU

R 0.25RF CABIN ALT AUTO1 CARGO FAN

OXY PRESS 1750

35 PRESS

N2

70 TEMP

12.4

12.6

12 RUD

FF

QTY

2.0

AIL

DISPLAY ENGINE STATUS

C 1.00

EGT 640

COMPUTER EVENT RECORD

L

AUTO

R

BRT

THRUST REF SET L

BOTH

PULL

R

MAX IND RESET

ELEV

AIL

DISPLAY ENGINE STATUS

COMPUTER EVENT RECORD

L

AUTO

R

BRT

THRUST REF SET L

BOTH

R

MAX IND RESET

PULL

797-FD-0088R1C 1-19-2-MT/CF

797-FD-0089C 1-19-2-MT/CF

797-FD-0090C 1-19-2-MT/CF

797-FD-0091C 2-19-2-MT/CF

EICAS Maintenance Displays 767-200ER/-300ER Postflight • Logbook entry of status and maintenance messages and data • MCDP checkout

PERF/APU ________

_______ ECS/MSG

GROSS WT

227.5

CAS L

2 9 1 96 44 171 193 40 62 0.75 0.62

PACK OUT TURB IN SEC HX OUT COMPR OUT PRIM HX OUT PRIM HX IN PRECOOL OUT DUCT PRESS PACK FLOW TEMP VALVE RAM IN DOOR FLT DK TRIM VALVE

3 10 3 98 46 173 196 42 64 0.80 0.71

FWD

30 0.75

DUCT TEMP

28 0.80

R

FWD EQ SUP FAN 1

TAT

MACH

ZONE TEMP BITE

95 130 12

OIL PRESS OIL TEMP OIL QTY

ALT

95 130 12

1.008 1.008

VIB

0.7 0.5

18.8

0.3 0.9

N1 N2

428

APU: BULK CARGO TEMP

AUX FWD

28 0.80

MID

17 0.00

AUX MID

17 0.00

25 AFT

EGT

640

RPM

100

EPR CMD EPR ACT

+15 21030

1.008 1.008 18.8

N1

428

EGT

60.4

N2

60.4

1.013

FF

1.010

86

FP

84

17 0.00

AFT CABIN TEMP

APU OIL QTY

ECS/status messages

STATUS ELEC/HYD ________

A

21.3

TRA

54.2

LOAD

9.3

SVA

12.4

AC-V

12

BVA

102

FREQ

104.2

NC 2 T2

73.2

12

12

IDG OUT

10.5

PS

9.2

IDG RISE

12.3

P2

11.3

-0.2

RP

-12.7

12

OIL T YEL

SCAV

HYD GEN

STBY /BAT

0 0

120 400 +10 28

DC-A DC-V

0

L

R

0.78 120 402 140 28 145 35

0.85 125 398 150 28 150 36

L RSVR PRESS

10

HYD QTY

79

P5

106

HYD PRESS

46

AOC

102

HYD TEMP

4

TCC

6

LOW 0.76 3230 50

C

APU /BAT

GND PWR

0.00 120 400 0 28

0.04 120 400

R RF

Electrical/hydraulics

:06 :12

STATUS

N1 RED EGT START EGT RED

113.9

N2RED

649

NORM HIGH 1.29 OF 0.25 3210 2140 47 115

ENG EXCD ________

116.7 649

MAX

EGT RED

Electronic propulsion control system

EGT RED

Performance APU

PAGE 1

EPCS ____

B

N1 RED

:03

PART NO S242N701-603 ENGINE CONFIGURATION

EICAS

PW 4060

PW 4060

TMC FMC

PW 4060 PW 4060

PW 4060 PW 4060

EPCS A

PW 40603-B5

EPCS B

PW 40603-B5

L EGT START

645 635 625 615 605 595 585 575 565 555 545

:02.7 :03.5 :04.4 :05.2 :06.3 :07.6 :08.5 :09.1 :10.4 :11.3 :12.2

PROG PINS

1

9C23

SUPL PINS

1

1000

EICAS ADC TMC R EGT REDLINE

MAX

MCDP

680 660 640 620

687

AVM

1:09.5 1:11.2 1:13.3 1:15.7

Engine exceedance

PW 40603-B5 PW 40603-B5

6FE8

32

MCDP OFF

16

DSP ON TEST RA ON FMC OFF FUEL ON ON EPCS A ON ON EPCS B ON

ON OFF ON ON

Configuration MCDP

797-FD-0092R1C 1-19-2-MT/CF

Non-Normal EICAS Operation 767-200ER/-300ER

TAT -12oC

TAT

1.50

1.50 2.0

2.0

1.28 1.0

1.28 1.0

1.5

DISPLAY ENGINE STATUS

COMPUTER EVENT RECORD

L

AUTO

R

BRT

-12o C 1.50

THRUST REF SET L

BOTH

R

2.0

MAX IND RESET

1.50

CRZ 2.0

1.28 1.0

1.5

1.28 1.0

1.5

1.5

EPR

EPR PULL

54.2

54.2

54.2

N1

428

N1

428

428

EGT

70

25

OIL

PRESS

70

OIL

TEMP

18

12

OIL

QTY

93 OIL

105 OIL

18 OIL

0.2

Low oil pressure, temperature, and quantity are displayed automatically

428

EGT

70 105

54.2

93

35 PRESS

N2

70 TEMP

12.4

12.4

12 QTY

FF

2.0

Secondary engine parameters selected

797-FD-0093R1C 1-19-2-whp/CF

Standby Engine Indicator 767-200ER/-300ER

The standby engine indicator (SEI) display is in view automatically if • AC power is lost • Either EICAS CRT fails and status is selected on the ground • Both EICAS CRTs fail

EPR

104.7

N1

104.7

625

EGT

625

102

N2

102 AUTO ON

The ON position manually activates the SEI

797-FD-0094C 1-19-2-whp/CF

Crew Alerting Features 767-200ER/-300ER

• Master warning and caution lights in Pilots’ primary field of view • Discrete alert lights repeated by EICAS messages • Consistent use of colors • Red for warnings • Amber for cautions and advisories • White for communications • Reduced number of aurals: bell, siren, beeper, voice, and chime • Sound intensity automatically adjusted to compensate for flight deck background noise • Predictive windshear and reactive windshear detection systems installed • Enhanced ground proximity warning system (EGPWS) installed • Traffic alert and collision avoidance system (TCAS) installed

797-FD-0095C 1-19-2-MT/CF

Crew Warning and Alerting System 767-200ER/-300ER Captain’s warning speaker

First Officer’s warning speaker

Speaker Speaker

Speaker Speaker

CAUTION

CANCEL

RECALL

CONFIG

FIRE

r

r

WINDSHEAR r

PULL UP r

WARNING

SPEED BRAKES

a

CABIN ALT

r

ALT ALERT

a

AUTO PILOT

a

A/P DISC

r

OVSPD r

GND a

CAUTION

Level B aural command Siren/owl modules (L and R)

Master warning module Bell/chime module

Warning electronic unit • • • • •

Master warning module Bell/chime module Siren/owl module (left or right) Takeoff configuration module Landing configuration module

EICAS computers (L and R) • • • • •

A/T DISC

Fire warnings Other warnings Communications system Ground proximity warning system Altitude alert module

Takeoff configuration module

PROX G/S INHB

FMC a

a

a

Landing configuration module

Radio altitude Airplane configuration • Flaps position • Stabilizer position • Parking brake position • Speedbrake handle position • Air/ground

Airplane configuration • Throttle position • Flaps position • Gear position • Speedbrake handle position

797-FD-0096C 1-19-2-whp/CF

Crew Alerting System 767 Discrete alerting lights Warnings CAUTION

TAT

Advisories CANCEL RECALL

Communication CONFIG

FIRE

r

r

WINDSHEAR r

PULL UP r

SPEED BRAKESa

CABIN ALT

r

ALT ALERT a

AUTO PILOT

a

A/P DISC

r

OVSPD r

-15o C

+46C 88.0

CABIN ALTITUDE OVERSPEED R ENG OVHT L FUEL SYS PRESS FMC MESSAGE PASS OXYGEN ON R ENG FUEL VAL AFT CARGO DOOR •SATVOICE AVAIL •PRINTER RECALL PAGE 1

D-TO

88.0

88.0

88.0

N1

760

760

EGT

GND a a

A/T DISC

PROX G/S INHB

FMC a

a

WARNING CAUTION

Speaker Speaker Master warning and caution switch lights

Aural speakers

797-FD-0028 2-26-2-whp/CF

EICAS Message Definitions 767-200ER/-300ER

Warning (red)

An operational or aircraft system condition that requires immediate corrective or compensatory action by the crew • Associated with warning aural or fire bell and red master warning lights and dedicated system warning annunciators

Caution (amber)

An operational or aircraft system condition that requires immediate crew awareness and future compensatory action • Associated with master caution aural and amber master caution lights and dedicated system caution annunciators

Advisory (amber)

An operational or aircraft system condition that requires crew awareness • Associated with system alert annunciators

Communication (white)

A normal communications condition that may require crew attention • Associated with chime aural

Status (white)

An MEL-related aircraft system fault requiring crew awareness prior to dispatch • Displayed on status page

797-FD-0097C 1-19-2-MT/CF

Alerting Inhibits During Takeoff 767-200ER/-300ER

Master warning lights and aural alerts for takeoff configuration are inhibited Master warning lights and aural alerts for fire, cabin altitude, and overspeed are inhibited Master caution lights and aural alerts for all cautions are inhibited

80 knots

V1

Air-ground transition

400-ft radio altitude or 20 seconds after air-ground transition

797-FD-0098C 1-19-2-MT/CF

Altitude Alert System 767-200ER/-300ER

+900 ft

Visual and aural alerts

Visual and aural alerts

+300 ft Selected altitude (MCP) Visual and aural alerts

-300 ft

-900 ft

No indications White light on primary altimeters illuminated EICAS caution message ALTITUDE ALERT Dedicated amber light ALT ALERT Caution aural

Indications and aurals are inhibited when landing gear is down and locked

797-FD-0099C 1-19-02-MT/DD

TCAS EADI Display 767-200ER/-300ER

Resolution advisory (RA) • Displayed automatically when the traffic alert and collision avoidance system (TCAS) calculates a collision threat with another aircraft • Provides vertical guidance for a pitch maneuver to ensure adequate vertical separation with the traffic airplane 797-FD-0100C 1-18-02-MT/DD

TCAS EHSI Display 767-200ER/-300ER Aislestand 4.4nm

TRK

140

M

0325.4z

ADI RST

15

12

BRT

DH REF

1 0 0

DADES

18

TCAS mode annunciation • TFC • TA only • TCAS fail • TCAS test • TCAS off

10

TFC

BRT

HOM

+05

20 10

-11

TFC

Other traffic symbol

160 320

APP VOR

MAP PLAN

CTR

MAP

NAVAID ARPT ON

ON

DATA

WPT

ON

ON

RA

Definition of RA

- Resolution advisory Other aircraft is 15 to 35 seconds from closest point of approach

TA

- Traffic advisory Other aircraft is 20 to 48 seconds from closest point of approach

Proximate traffic

- Other aircraft is less than 6 nmi away and within 앐 1,200 vertical feet from own aircraft and not currently a potential conflict

Other traffic

40 80

INOP

Proximate traffic

WXR

TERR

TRAFFIC

+06

-10

TA display annunciation

TA or RA annunciation (red or amber)

CAMPO

- Other aircraft is more than 6 nmi away or greater than 앐 1,200 vertical feet from own aircraft and not currently a potential conflict

Arrow

- Indicates traffic climbing or descending at a rate greater than or equal to 500 fpm

Altitude

- Number and associated sign (+ or -) indicates altitude of traffic in hundreds of feet relative to the airplane. The number is below the traffic symbol when the traffic is below and above the traffic symbol when the traffic is above

TCAS mode selector (TFC) • Push for TCAS display Traffic symbols are available in the EHSI modes: • Center map • Expanded map • Expanded VOR • Expanded approach

797-FD-0101C 1-19-2-whp

Enhanced Ground Proximity Warning System (EGPWS) 767-200ER/-300ER The enhanced ground proximity warning system (EGPWS) is a basic installation on Boeing airplanes. EGPWS provides caution and warning level alerts to the flight crew about potential terrain conflicts. The alerts are based primarily on airplane position, flight path, and barometric altitude information in conjunction with the EGPWS self-contained worldwide airport and terrain databases.

Master warning lights (2)

ADI RST

Terrain display select switch

BRT

DH REF

1 0 0

TERR

WXR WARNING

BRT

20 10

40 80 TFC

160 320

CAUTION

APP VOR

MAP PLAN

CTR

PU

MAP

NAVAID ARPT

DATA

WPT

I

Aislestand

Terrain display on EHSI (2)

EGPWS flap override switch

EGPWS landing gear override switch

EGPWS terrain override switch

797-FD-0103C 1-19-2-whp

Enhanced Ground Proximity Warning System 767-200ER/-300ER

25.5

Look-ahead distance Speaker

Altitude offset

NM

TRK

136

M

1335.4z

"CAUTION TERRAIN, CAUTION TERRAIN"

Caution

Warning 20 to 30 seconds 40 to 60 seconds

40

GND

TERRAIN

TERR

PROX

The enhanced ground proximity warning system computes two levels of terrain alerting envelopes: caution and warning.

EHSI

The enhanced ground proximity warning system look-ahead caution alert includes unique voice aural, terrain display, and map annunciations. Airplane altitude

25.5

NM

TRK

136

M

1335.4z

+2,000 ft 25.5

Speaker

+1,000 ft

TRK

136

M

1335.4z

"TERRAIN TERRAIN, PULL UP!"

40

0 ft

NM

40

TERRAIN

-500 ft PULL UP

-1,000 ft

WARNING

TERR

TERR

CAUTION

-2,000 ft

EHSI EGPWS display color coding EHSI

Terrain display colors indicate the height of the terrain relative to the current airplane altitude.

The enhanced ground proximity warning system lookahead warning alert aurals are nearly identical to those for the basic GPWS warnings in order to elicit the same pilot response. In addition, threatening terrain is presented on the map display.

797-FD-0102C 1-19-2-whp

Reactive and Predictive Windshear Systems 767-200ER/-300ER Both a reactive windshear system (RWS) and a predictive windshear system (PWS) are basic equipment on Boeing airplanes. The systems provide windshear detection capability during all operations below 1,500 feet (460 m) above ground level.

1,500 AGL (RWS)

RWS WARNING

PWS WARNING

CAUTION

1,200 AGL (PWS)

Leading edge

0.5 nmi

1.5 nmi

3 nmi

797-FD-0104C 19-1-02-MT/DD

Reactive and Predictive Windshear Systems 767-200ER/-300ER • Predictive windshear system • Provides aural and visual alerts of an impending windshear condition based on weather radar returns • Reactive windshear system • Provides recovery guidance and aural and visual alerts when the EGPWS detects the aircraft has entered a windshear condition • The AFDS provides windshear recovery guidance by means of the normal go-around pitch and roll modes when windshear is detected: – If an autopilot is engaged and the go-around mode is armed, the autopilot commands a pitch-up of 15 degrees or slightly below the pitch limit (whichever is lower) when a GA switch is actuated – If an autopilot is not engaged when the go-around is initiated, the pilot must fly the windshear recovery following the flight director commands. If the autothrottle is not armed or engaged, the pilot must advance the throttle levers manually

797-FD-0042 1-19-02-CF/DD

Predictive Windshear System (PWS) 767-200ER/-300ER The predictive windshear system begins the windshear alerting sequence with a caution to the flight crew, including a voice aural alert and an amber WINDSHEAR message on the EHSI. The predictive windshear alerts are generated by the weather radar system.

Speaker Speaker

F

“MONITOR "MONITOR RADAR DISPLAY" DISPLAY”

S

A/P ENGAGE L

0 0

B CRS

LOC

CMD

CWS

C

R

CMD

CMD

CWS

CWS

F/D ON

F R E Q

C R S

OFF AUTO

APP

DISENGAGE

MAN VOR/DME

25.5 NM

TRK

136 M

1335.4z

15

12

40

797-FD-0105C 1-19-2-whp

Predictive Windshear System (PWS) 767-200ER/-300ER The predictive windshear system next generates one of two warning voice aural alerts, as well as a red WINDSHEAR message on the EHSI and EADI, and illumination of the master warning lights. “WINDSHEAR AHEAD” voice aural alert is annunciated during takeoff phase of flight. “GO AROUND, WINDSHEAR AHEAD” voice aural alert is annunciated during the approach phase of flight.

Speaker Speaker F

S

“WINDSHEAR "WINDSHEAR AHEAD WINDSHEAR AHEAD” AHEAD" or “GO "GO AROUND WINDSHEAR AHEAD” AHEAD"

WARNING

WINDSHEAR

A/P ENGAGE L B CRS

LOC

CMD

CWS

C

R

CMD

CMD

CWS

CWS

F/D ON

F R E Q

C R S

OFF AUTO

APP

DISENGAGE

MAN VOR/DME

25.5 NM

TRK

136 M

1335.4z

WINDSHEAR

15

12

40

WINDSHEAR

797-FD-0105 R1C 1-19-2-whp

Reactive Windshear System (RWS) 767-200ER/-300ER The reactive windshear system warning provides a voice aural alert and a red WINDSHEAR message when the airplane enters a performance-decreasing windshear. The reactive windshear alert is generated by the EGPWS.

Speaker Speaker F

S

“WINDSHEAR "WINDSHEAR WINDSHEAR WINDSHEAR" WINDSHEAR”

WARNING

WINDSHEAR

A/P ENGAGE L

0 0

B CRS

LOC

CMD

CWS

C

R

CMD

CMD

CWS

CWS

F/D ON

F R E Q

C R S

OFF AUTO

APP

DISENGAGE

MAN VOR/DME

25.5 NM

TRK

136 M

1335.4z

15

12

WINDSHEAR

40

797-FD-0106C 1-19-2-whp

767 Flight Deck - Autoflight

Autopilot Flight Director System 767-200ER/-300ER (MCP) WARNING

WARNING

CAUTION

CAUTION

Electronic de director

Engine

Thrus mode selec

utoland status (ASA

The autopilot flight director system (AFDS) provides • Triple-redundant flight control computers (FCC), autopilot servos, multi-mode receivers (MMR), and radio altimeters • Autopilot available from 200 ft after takeoff through climb, cruise, descent, landing, and go-around • Category IIIb, 0 ft decision height and 300 ft RVR, approach, landing, and rollout capability

Flight management computer Thrust management computer

• Automatic thrust management through full-flight regime Flight control computer

• Flap placard and alpha floor protection • Optimum vertical and lateral navigation capabilities when coupled to the flight management computer (FMC)

Throttle quadrant Autopilot servo

797-FD-0108C 1-19-02-whp/DD

Autopilot Flight Director System Diagram

Flight management computer A/T ARM

Flight director command bars

L NAV

F/D ON OFF SEL OFF

VERT SPD

HDG

IAS/MACH

V NAV

Roll 1 2 6 Pitch 5

NORM

25 BANK LIMIT

ALT

C

R

CMD

CMD

CMD

DN

V/S

FLT DIR L

F/D ON

F A I L

RTE

DEP ARR

ATC

VNAV

FIX

LEGS

HOLD

FMC COMM

PROG

NAV RAD

PREV PAGE

BRT

EXEC

A

B

F

G

H

I

J

K

L

M

N

O

P

Q

R

S

T

9

U

V

W

X

Y

+/-

Z

SP

DEL

/

CLR

NEXT PAGE

1

2

3

4

5

6

7

8

.

0

C

D

E M S G O F S T

OFF

HOLD

DISENGAGE

UP

INSTR SOURCE SEL

D S P Y

A/P ENGAGE L

INIT REF

MENU

Multipurpose control display unit

Left flight control computer

C R

NAV FMC-L CDU-L

FMC-R

Center flight control computer Right flight control computer Left hyd sys servo Center hyd sys servo Right hyd sys servo

Autoland status annunciator

Flight control actuators Flight controls 797-FD-0044C 1-19-02-whp/DD

Mode Control Panel 767-200ER/-300ER

Vertical navigation switch

IAS/Mach window

Autothrottle arm switch

A/T ARM F/D ON

Heading window

Lateral navigation switch

L NAV

3 3 0

Vertical speed window

VERT SPD

HDG

IAS/MACH

Altitude window

1 2 6

Backcourse switch

A/P ENGAGE

ALT

0 0 0 0

Autopilot engage switches

3 2 0 0 0

B CRS

L

C

R

CMD

CMD

CMD

F/D ON

OFF

Thrust mode switch (EPR on PW and RR powered aircraft or N1 on GE powered aircraft)

SEL OFF

V NAV

EPR

Autothrottle speed mode

Speed select switch • Alternates display between IAS and Mach

5 NORM

FL CH

SPD

SEL

25 BANK LIMIT

DN

LOC

V/S

HOLD

HOLD

APP

OFF DISENGAGE

UP

Flight level change switch Speed select knob

Heading select knob Heading hold switch

Bank-angle limit select knob

Localizer mode select switch

Altitude select knob Vertical speed switch

Altitude hold switch

Flight director on/off switches Autopilot disengage bar

Approach mode select switch

Vertical speed selector

797-FD-0109C 1-19-02-PW/DD

Thrust Management System 767-200ER/-300ER

Mode control panel * Thrust mode select panel

Thrust management computer Autothrottle servo

* Thrust mode select panel Thrust rating • Thrust limit computation • Thrust reduction • Fixed climb derates • Variable reduction by assumed temperature Autothrottle control • Controls to thrust limit • Controls to IAS/Mach or selected thrust setting • Speed protection

Selector switches • TO/GA - Selects takeoff limit while on the ground and go-around limit while in flight • CLB - Selects maximum climb thrust • CON - Selects maximum continuous thrust • CRZ - Selects maximum cruise thrust

TO GA

CLB

CON

CRZ

1

2

Derate switches • Select fixed derate for climb

TEMP SEL

Temperature selector • Selects assumed temperature reduced thrust for takeoff • Reduced thrust assumed temperature shown in degrees Celsius on EICAS primary display • Maximum 25% assumed temperature reduced thrust 797-FD-0110C 1-19-02-MT/DD

Maintenance Control and Display Panel 767-200ER/-300ER Collins GROUND TEST SEL UP

• The maintenance control and display panel (MCDP) provides flight fault recording for the FCC, TMC, and FMC systems and ground test BITE for the flight control and thrust management systems. • The MCDP can store up to 350 faults for up to 99 flights.

01 R/P DISC ROC SYST L

DOWN

POWER OFF

FLT FAULTS

INSTRUCTIONS XXXXXXXXXXXX XXXXXX XXXX

GRD TEST

NO/SKIP

EICAS maintenance panel (P61)

MCDP (located in E/E bay)

GROUND TESTS

XXXXX XXXXX XXXX XXXXXXXXXXXX XXXXXXXXXXX XXXX

YES/ADV

LRU

XXXXXXX

SUPPORT

XXX XXXXXX XXXXXXXXX XXXXXX XXXXXXXXX XXXXX XXXXX XXXXXXXXX

XXXXXXXXXXXX

XXXXXX

XXX

XXXXXX

XX XXXXXXXXXX XXXXXXXX

XXXXXX XXXXXXXXXXX XXXXXXXXXXX

XXXXXXXXXXX

XXXXX XXXXXX XXXXXXXXX

XXX XXXXXX XXXXXX XXXXXX XXX

XXXXXXXXXXXXXXX

XXXXX XXXXXXXXXX XXXX

XXX XXXX XXXXXXXXXX

XXXXX XXXXX XXXX XXXX XXXXX XXX XXXXXXXXX

XXXXXXX

XXXX XXX

XXX XXXX XXXX XXXXXXXX

XXXX

XXXX

XXXX XXXX XXXX XXXX

XXXXXX XXXXXX XXXX

XXX XXXXXXXXX

XXXXXXXX XXXX

XXX XXXXXX XXXXXXXXX X XXXX XXXXX

XXX XXX XXX XXXXXXX

XXXXXXXXXXXX XXXXXX XXXX

XXXXXXX

XXX XXXXXX XXXXXXXXX XXXXXX XXXXXXXXX

XXXXXXX XXX XXX

SYSTEM

XXXXX XXXXX XXXX XXXXXXXX XX XXXXXXXXXXXX XXXX

XXX

XXXX

XXX XXXXXXXX

XXXXX XXX XXX XX

XXXXXXX XXX

XXXXXX XXXXX

XXXX

XXXXX XXXX X

XXXXX XXXXXX XXXXX XXX

XXXXXXX

EICAS computer

XXXXXXX XXXXXX XXXX

XXXXX XXX XXXXX

XXXXXX

XXXXXXX

XXXXX

Flight management computers

Thrust management computer Flight control computers

• Central fault recording and fault isolation • Allow faster airplane turnaround • Ensure that the proper LRU is replaced • Help lower the cost of ownership

Lower EICAS display STATUS

PART NO S242N701-603 ENGINE CONFIGURATION

EICAS

PW 4060

TMC

PW 4060 PW 4060

FMC

PW 4060 PW 4060 PW 4060

EPCS A

PW 40603-B5

EPCS B

PW 40603-B5

PROG PINS

1

9C23

SUPL PINS

1

1000

EICAS ADC TMC MCDP AVM

PW 40603-B5 PW 40603-B5

6FE8

32

MCDP OFF

16

ON DSP RA TEST ON FMC OFF FUEL ON ON EPCS A ON ON EPCS B ON

ON OFF ON ON

Configuration MCDP

MCDP maintenance page

Inertial reference unit

• Faults and diagnostic data are displayed on the MCDP or on the EICAS maintenance page.

Air data computer

Clock

VOR

Airline warning annunciators

Flap position Mode control panel

EFIS CP

Caution/warning system Instrument landing system

Thrust mode select panel

DME EICAS Flight management MCDU

Servos Speed brake handle position

Radio altimeter Stabilizer position 797-FD-0111C 1-19-02-MT/DD

767 Flight Deck - FMS and MCDU

Flight Management Computer System 767-200ER/-300ER LNAV and VNAV engage

VOR/DME tuning

FMC speed low ator

speed mmand g

nate FMC rce select switch

EHSI D S P Y F A I L

MCDU

INIT REF

RTE

DEP ARR

ATC

FIX

LEGS

HOLD

FMC COMM

MENU

NAV RAD

PREV PAGE

A

NEXT PAGE

F

BRT

VNAV

EXEC

PROG

B

C

G

H

D

E

I

J

INIT REF

RTE

DEP ARR

ATC

FIX

LEGS

HOLD

FMC COMM

MENU

NAV RAD

PREV PAGE

A

NEXT PAGE

BRT

VNAV

EXEC

PROG

B

C

D

E

F

I

J

K

G

H

L

M

N

O

L

M

N

O

4

5

6

P

Q

R

S

T

4

5

6

P

Q

R

S

T

7

8

9

U

V

W

X

Y

7

8

9

U

V

W

X

Y

.

0

+/-

Z

SP

DEL

/

CLR

.

0

+/-

Z

SP

DEL

/

CLR

1

2

3

K

M S G

D S P Y

O F S T

F A I L

M S G

1

2

3

O F S T

Flight control computers

Inertial reference units

Left FMC Thrust management

Right FMC Navigation and system sensors 797-FD-0112C 1-19-2-PW-whp

Flight Management Computer System 767-200ER/-300ER Pegasus FMC is basic Pegasus FMC features: • FANS-1 capable • Performance management • Economically efficient flight profiles – Climb – Cruise – Descent – Holding – Nonprecision approach • Cost index selection • Speed schedules • Engine out performance • Clean or speedbrake descent distances displayed • En route winds • Step-climb planning improvements • Flight planning • Range/fuel data • Takeoff and landing • Top of descent • Optimum altitude and step-climb point • Alternate airports • Required navigation performance (RNP) • Route offsets available • Active waypoint distance and predicted fuel displayed

• Navigation/guidance calculations • FMC calculates airplane position using navigation sensor data in the following priority: – GPS/LOC/INERTIAL – DME/DME/LOC/INERTIAL – DME/VOR/LOC/INERTIAL – LOC/INERTIAL – GPS/INERTIAL – DME/DME/INERTIAL – DME/VOR/INERTIAL – INERTIAL ONLY – GPS ONLY – All navigation sensors failed - none • Point-to-point great circle paths • Guidance commands (LNAV, VNAV, and autothrottle) • Auto tuning of DME and VOR for position updating • Database storage • Airplane and engine performance • Navigation data (VHF NAVAIDS, airports, SIDs, STARs, runways, airway approaches, and missed approaches) • Display data processing • Crew alertness monitor

797-FD-0113 1-19-02-MT/DD

Multipurpose Control Display Unit (MCDU) 767-200ER/-300ER

• Keyboard layout similar to 747-400 FANS CDU

D S P Y F A I L

INIT REF

RTE

DEP ARR

ATC

VNAV

FIX

LEGS

HOLD

FMC COMM

PROG

MENU

NAV RAD

A

B

C

D

E

PREV PAGE

NEXT PAGE

F

G

H

I

J

K

L

M

N

O

1

2

3

BRT

EXEC

4

5

6

P

Q

R

S

T

7

8

9

U

V

W

X

Y

.

0

+/-

Z

SP

DEL

/

CLR

M S G O F S T

• NAV RAD key - access to NAV RADIO page – VOR radio tuning • ATC COMM key - access to ATC data link • FMC COMM key - access to ACARS FMC data link • VNAV key - access to active CLB, CRZ, DES page • Alternate navigation function - The MCDUs can be used as an alternate navigation system if both FMCs fail. The MCDUs perform lateral navigation computations. LNAV and VNAV are not available. Each MCDU can display route information on its on-side EHSI.

797-FD-0114C 1-19-02-PW/DD

FMCS Position Updating 767-200ER/-300ER • The FMCS determines aircraft position using the available sources in this priority: 1. GPS/LOC/INERTIAL 2. DME/DME/LOC/INERTIAL 3. DME/VOR/LOC/INERTIAL 4. LOC/INERTIAL 5. GPS/INERTIAL 6. DME/DME/INERTIAL 7. DME/VOR/INERTIAL 8. INERTIAL ONLY 9. GPS ONLY

Multi-mode receivers

IRU

VOR/DME receivers

GPS position

FCC airplane guidance

FMC Radio updating (autotune)

FMCS LNAV guidance

• The FMCS automatically tunes VOR/DME radios. • If both VOR/DMEs are manually tuned, the FMC will use the range/bearing information as long as signal criteria are satisfied.

F R E Q

C R S

AUTO

Nav tuning panels (manual tuning)

MAN

• The frequency of a navigational aid on an active leg will be tuned if it is part of a published terminal area procedure.

VOR/DME

GPS satellites

Waypoint Active leg

VOR/DME VOR/DME

797-FD-0123C 1-19-02-whp/DD

Global Positioning System 767-200ER/-300ER

• Global positioning system (GPS) provides precision navigation for • FMC position • RNP operations • EGPWS • FANS operation • GPS supports required navigation performance (RNP) operations down to 0.2 nmi

Onboard GPS

• FMC automatically selects best sensors (GPS, DME, VOR, LOC)

797-FD-0115C 1-19-02-PW/DD

Global Positioning System With Pegasus FMC 767-200ER/-300ER

EHSI d

splay

GPS antenna POS REF

FMC position

FMC (GPS) N47 32.4 W 122 18.6 IN E R TIAL

Nav sensor positions Multi-mode receiver left

Multi-mode receiver right

Nav performance

2/4

Nav mode

N47 32.4 W 122 18.7 GP S

N47 32.4 W 122 18.6 R AD IO

N47 32.4 W 122 18.6 RNP/ACTUAL 2.00/0.30 NM


FMC (L and R) EFIS SG (L, C, R)

797-FD-0116C 1-19-02-PW/DD

Required Navigation Performance (RNP) 767-200ER/-300ER

Default RNP Values En route domestic

Oceanic remote area

RNP = 2.0 nmi

RNP = 12.0 nmi

Terminal RNP = 1.0 nmi

Takeoff

Approach

RNP = 1.0 nmi

RNP = 0.5 nmi

Note: RNP values shown here are default values and do not reflect the maximum capability of the airplane.

797-FD-0117C 1-19-02-MT/DD

FMCS Databases 767-200ER/-300ER

Performance database

Basic • Engine data • Drag polars • Operational limits Customized • Airplane factors • Cost factors

• Preflight startup • Navigation • Guidance

Navigation database

Operational program configuration (OPC) database

Basic • VHF NAVAID data • Airport and runway data

• Performance management • Map display processing

Customized • Airway data • Terminal area procedures • ILS data • Airline-tailored data

Basic • Default values Modified by Boeing Customized • Customer requested features

Basic • Default values Airplane modifiable information (AMI) database

Specified by customer Customized • Customer tailored parameters

797-FD-0120 1-19-02-whp/DD

FMCS Databases - OPC and AMI 767-200ER/-300ER Operational program configuration (OPC)

Airline modifiable information (AMI) file

• The OPC is a loadable database used to selectively • The AMI is a loadable database that provides for enable those features requested by the customer software designation of various FMC parameters. within the operational program software (OPS). The Each airline has the ability to tailor their AMI to OPC can be changed only by Boeing. This is done suit their specific operations by selecting the AMI during aircraft configuration or with a service bulletin. parameters. In the event the AMI parameters are not modified by the customer or are not available, the • The OPC enables these following optional FMC FMC provides hard-coded default parameters in the features: basic software. • Runway distance and offset position shift in units of feet or meters (must enable either feet or meters) • Some AMI parameters may be viewed by the crew • Crew alertness monitor on the CDU airline policy page. • Non-directional beacon approaches • A summary of types of parameters that can be • Non-precision GPS approaches specified by the AMI are: • Display of vertical bearing, flight path angle (FPA) • Performance, guidance, and takeoff data and vertical speed • Crew alertness monitor configuration data • Scanning DME operations • Alternate function parameters • Altitude intervention • Data link request/report prompt inhibits • Airline operational communications data link • Data link Imbedded element identifier (IEI)/ (AOC DL) response/trigger enables • Air traffic services data link (ATS DL) • Down link trigger for position report enable • Takeoff data link • Down link trigger for progress report enable • Required time of arrival (RTA) • Request uplink Imbedded message identifiers (IMI) • FMC printer interface table • Down link address table

797-FD-0121 1-19-02-whp/DD

Inertial Reference System 767-200ER/-300ER IRS features • Triple-redundant laser gyros • Certified for extended navigation over water • Maximum alignment time of 10 min • 30-sec quick alignment for through-stops • Initial position input through either the inertial reference mode panel or FMS MCDU • Flight crew selectable alternate data sources

EADI

Navigation systems • WXR • EGPWS • FMC • MMR (GPS)

EADI

EHSI

EHSI

VSI

VSI

Autopilot systems • FCC • TMC • Yaw damper

IRS outputs • • • • • • • • •

Antiskid/autobrake system • EICAS

Magnetic/true heading Magnetic/true track Primary attitude Ground speed Wind velocity and direction Vertical speed Navigation position/drift angle Inertial velocity vectors Acceleration and angular rates Air data computers (2) jgiihc oijfod jgiihc oijfod

EFIS symbol generator

Left IRU

Instrument source select switch

Center IRU

Instrument source select switch

Right IRU

Inertial reference mode panel IRS MODE SEL N W

DSPL SEL PPOS WIND TK/GS

HDG

SYS DSPL C L R

1

N 2

3

W 4

H 5

E 6

7

S 8

9

ENT

0

CLR

jgiihc oijfod

L

C

ALIGN

ALIGN OFF

True airspeed Altitude Altitude rate

R

ALIGN

ALIGN

ON DC

ON DC

ON DC

DC FAIL

DC FAIL

DC FAIL

FAULT

FAULT

FAULT

NAV

ATT

ALIGN OFF

NAV

ATT

ALIGN

NAV

ATT

OFF

Initialization control display 797-FD-0122C 1-19-02-whp/DD

767 Flight Deck - Systems

Air-Conditioning and Pneumatics 767-200ER/-300ER Passenger Air-conditioning system • Two independent packs with one-pack dispatch capability • Automatic temperature control for the flight deck, forward, mid, and aft passenger cabin zones

CARGO HEAT FWD

AFT

ON

ON

OVHT

OVHT

Passenger compartment temperature

COMPT TEMP

INOP

INOP

FWD CAB AUTO

Passenger compartment temperature control

INOP AFT CAB AUTO

MID CAB AUTO

Trim air C

OFF

C

W

C

W

OFF

W

OFF

TRIM AIR

L - RECIRC FAN - R

ON

ON

ON

INOP

INOP

OFF

Recirculation fan

Flight deck trim air

FLT DK INOP

Pack reset

C

W

AUTO R PACK

L PACK

Pack control

RESET

RESET INOP

Pneumatic duct pressure

C MAN

PACK OFF

INOP

W

PACK OFF AUTO

AUTO N

OFF

N

OFF

S

S

Pneumatic system • Provides air for • Engine starting • Cabin air-conditioning • Pressurization • Wing and engine anti-icing • Potable water tank and hydraulic reservoir pressurization • TAT probe aspiration • Bleed air normally isolated to its associated pack

C

T

C

Flight deck compartment temperature

T B

B

Y

Y W

W

Isolation valve 60

80

20

0

DUCT PRESS PSI

L ISLN

R ISLN

VALVE

VALVE

C ISLN

APU bleed air

V A L V E

DUCT LEAK

DUCT LEAK

BLEED

Engine bleed air

OVHT

BLEED DL UE CA TK

L ENG O F F

V A L V E

OVHT

ADP

APU

Duct leak Engine bleed valve Engine bleed overheat

R ENG O F F

Normal in-flight procedures: none

797-FD-0124C 1-19-02-whp/DD

Air-Conditioning and Pneumatics 767-300 Freighter Air-conditioning system • Two independent packs with one-pack dispatch capability • Automatic temperature control for the flight deck, forward, and aft main deck cargo zones • Automatic temperature control for forward lower lobe cargo compartment (General Market Freighter)

CARGO HEAT FWD

AFT

ON

ON

OVHT

OVHT

Flight deck temperature

Main deck temperature

COMPT TEMP

AUTO

Fwd Cargo Air Cond

Flight deck trim air

M1819

ON OVHT

INOP

INOP

INOP C

W OFF

TEMP CONTROL

Flight deck temperature control

Main deck temperature control

W

C

FLT DECK AUTO

C

FWD CAB AUTO

AFT CAB AUTO

C

W MAN

W OFF

C

Forward cargo air-conditioning panel (767 General Market Freighter Only)

W OFF

TRIM AIR ON

Pack reset

OFF

Pneumatic duct pressure

L PACK

R PACK

RESET

RESET

INOP

INOP

PACK OFF

PACK OFF

AUTO

Pack control

AUTO N

OFF

N

OFF S C

S

T

C

B W

Pneumatic system • Provides air for • Engine starting • Cabin air-conditioning • Pressurization • Wing and engine anti-icing • Potable water tank and hydraulic reservoir pressurization • TAT probe aspiration • Bleed air normally isolated to its associated pack

T B

Y

W

Y

Isolation valve 60

80

20

0

DUCT PRESS PSI

L ISLN

R ISLN

VALVE

VALVE

C ISLN

APU bleed air

V A L V E

DUCT LEAK

DUCT LEAK

BLEED

BLEED

DL UE CA TK

OVHT

Engine bleed air

L ENG O F F

OVHT ADP

APU V A L V E

Duct leak Engine bleed valve Engine bleed overheat

R ENG O F F

Normal in-flight procedures: none

797-FD-0125C 1-19-02-whp/DD

Cabin Pressure Control 767-200ER/-300ER Cabin altitude manual control • Controls outflow valve with mode selector in manual

CABIN ALTITUDE CONTROL

VALVE

MANUAL

AUTO RATE

CLIMB OP

MAX

MIN

CL DESCEND

Cabin altitude auto rate control • Sets limit for cabin altitude rate of climb or descent during auto control • Establishes approximately 500 ft/min climb and 300 ft/min descent when set on index

LDG ALT AUTO INOP

034 0

MODE SELECT AUTO 2 MAN

AUTO 1

Landing altitude selector • Selects landing altitude from 1,000 ft below sea level up to 14,000 ft

CABIN

0 2 25 4 20 15 6 10 8

0 10

2

8

4 6

DIFF

PSI

ALT

FT X 1000

1 2 0 1

2

RATE

FPM X 1000

Cabin pressurization mode control • Dual automatic system with auto switching in event of failure • Maintains sea level up to 22,500 ft and 8,000 ft up to maximum cruise • Maximum pressure differential 8.6 psi

Cabin rate of climb indicator Differential pressure indicator

Cabin altitude indicator

797-FD-0126C 1-19-2-whp/CF

Cargo and APU Fire Protection 767-200ER/-300ER Passenger • Fire detection and extinguishing systems are installed for both engines, the APU, and cargo compartments. The main wheel wells have detection only. • Two fire extinguisher bottles are installed for engine fire control for General Electric and Pratt & Whitney engines. Four fire extinguishing bottles are installed for engine fire control for Rolls-Royce engines. • One fire extinguisher bottle is installed for APU fire control. • Three fire extinguishing bottles are installed for cargo fire control.

Engine overheat light Engine fire bottle discharge light APU fire bottle discharged light

L ENG OVHT

ENG BTL 1 DISCH

Fire warning light and engine fire switch

ENG BTL 2 DISCH

R ENG OVHT

DISCH 1

L E F T

1

2

R

ARMED

FWD

AFT

FWD-ARM-AFT CARGO FIRE

DISCH

2

ARMED

2

BTL DISCH F I R E

I G H

APU BTL DISCH

C A R G O DISCH

APU

1

DISCH

T

APU fire warning and APU fire switch

Fire/overheat detection test panel FIRE/OVHT TEST WHL WELL

ENG/APU CARGO

SYS FAIL

FAIL P-RESET

Fire test switch for wheel wells

System fail light System fail reset switch

Fire override switch (under fire switch)

Fire/overheat test switch for engines, APU, and cargo 797-FD-0127C 1-19-2-whp/CF

Cargo and APU Fire Protection 767-300 Freighter • Fire detection and extinguishing systems are installed for both engines, the APU, and cargo compartments. The main wheel wells have detection only. • Two fire extinguisher bottles are installed for engine fire control for General Electric and Pratt & Whitney engines. Four fire extinguishing bottles are installed for engine fire control for Rolls-Royce engines. • One fire extinguisher bottle is installed for APU fire control. • Three fire extinguishing bottles are installed for cargo fire control.

General Market Freighter Configuration Engine overheat light Engine fire bottle discharge light APU fire bottle discharged light CARGO FIRE L ENG OVHT

ENG BTL 1 DISCH

R ENG OVHT

ARMED

FWD A R M AFT

FWD

DISCH 1

Fire warning light and engine fire switch

ENG BTL 2 DISCH

2

L E F T

ARMED

DISCH 1

R I G H T

2

A R M

AFT ARMED MAIN

APU BTL DISCH

DEPR/ DISCH 2

DISCH

APU

DISCH

DEPR

1

MAIN

APU fire warning and APU fire switch Fire override switch (under fire switch)

Package Freighter Configuration APU fire bottle discharged light DEPR/ DISCH APU BTL DISCH

DEPR CARGO

Fire/overheat detection test panel FIRE/OVHT TEST WHL WELL

ENG/APU CARGO

SYS FAIL

FAIL P-RESET

Fire test switch for wheel wells

2

System fail light System fail reset switch

Fire/overheat test switch for engines, APU, and cargo

DISCH MAIN FWD

APU

1 AFT

APU fire warning and APU fire switch 797-FD-0127R1C 1-19-2-whp

Fire Protection 767-200ER/-300ER APU Ground Service Control Panel

APU FIRE WARNING HORN

APU fire warning horn

APU fire bottle armed light APU FIRE

Fwd

FIRE BOTTLE ARMED

APU fire bottle discharged light

BOTTLE DISCHARGED

APU bottle discharge switch APU fire light

APU FIRE SHUTDOWN

APU BOTTLE DISCHARGE

APU shutdown switch

APU ground control panel on nose landing gear strut

797-FD-0128C 1-19-2-whp/CF

Equipment Cooling 767-200ER/-300ER Equipment cooling selector EQUIP COOLING

CABIN ALTITUDE

VALVE AUTO

PRESS DIFF LIMIT: T/O & LDG .125 PSI

STBY

OVHT

OVRD

SMOKE NO COOLING

No cooling light

Conditioned pack air

(3)

(4) Flight deck panels

Override valve ( p)

Override valve ( p) (2)

EE equipment

Air cleaner

Supply fan

Manifold interconnect valve

Flight deck panels

Override valve ( p)

EE equipment

Check valves

AUTO – Automatically controls equipment cooling system STBY – Positions equipment cooling system for inboard airflow OVRD – Positions equipment cooling system for reverse airflow Valve light Overheat light Smoke light

Overboard exhaust valve (1) Inboard supply valve

Check valves Supply fan

EE equipment Air cleaner

Air cleaner Exhaust fan (ON)

Flight deck panels

Exhaust fan Overboard exhaust valve

Check valves Supply fan

Exhaust fan Overboard exhaust valve

Inboard supply valve

Inboard supply valve

(5) Bypass valve (1)

Automatic (AUTO) mode

Bypass valve

Standby (STBY) mode

(1) These valves reverse if OAT below 45oF/7oC or in flight or on ground with both engines running. (2) These valves reverse if cargo fire switch is in DEPR (Freighter only).

Bypass valve (2)

Override (OVRD) mode (3) This valve is open on the 767 Freighter only in flight or on the ground with both engines running. (4) This valve is open on the 767 Freighter. (5) This valve is closed during flight. 797-FD-0129C 1-19-2-whp/CF

Auxiliary Power Unit 767-200ER/-300ER

Auxiliary power unit (APU) • Installed in unpressurized tail cone • Ground or in-flight use • 90-kVA electrical generator • Generator power available to airplane’s maximum certified altitude • Bleed air for packs and engine start • Automatic start • Crew monitoring not required • Start up to 35,000 ft • Automatic cooldown on shutdown • Automatic shutdown for fault/fire • EGT readout on EICAS status page

APU

ON OFF

START

RUN FAULT

797-FD-0130C 1-19-2-whp/CF

Fuel System 767-200ER/-300ER • Three-tank system • Independent fuel system for each engine with crossfeed capability • Two boost pumps in each wing tank • Two override pumps in center tank • Automatic scavenge system for center tank • APU supplied from the left fuel manifold • Normal fuel configuration is tank to engine • Solid-state fuel quantity and temperature indication • Fuel configuration alerts for • Fuel imbalance • Low fuel • Center tank pumps off with fuel in tank • Minimum crew workload • All pumps turned on before flight • Center tank pumps turned off when center tank is empty

L PUMPS

FUEL XFEED

R PUMPS

VALVE

PRESS

VALVE

PRESS

ON

ON

AFT

AFT

PRESS

ON

ON

FWD

FWD

767-200ER 138,037 lb (20,450 U.S. gal) 62,600 kg (77,410 liters)

PRESS

C PUMPS

ON

FUEL CONFIG P R E S S

P R E S S

R

L

C

L

LB

TEMP

ON

KG

C

LB KG FUEL QTY X 1000

R

LB

KG

TOTAL

767-200ER*, -300ER 161,700 lb (24,140 U.S. gal) 73,350 kg (91,380 liters)

* Option 797-FD-0131C 1-19-2-whp/CF

Fuel Jettison 767-200ER/-300ER

• A fuel jettison system is installed on 767 airplanes with gross takeoff weights in excess of 360,000 lb.

FUEL JETTISON

FAULT

L–NOZZLE–R

• Fuel is pumped from the center auxiliary tank by dedicated jettison pumps through jettison transfer valves to the jettison nozzles located on the outboard trailing edges of the wings.

OFF ON

ON

ON

VALVE

VALVE

Center auxiliary tank

Jettison and override pumps P P

Jettison nozzle valve

Jettison transfer valve

Jettison nozzle

Left wing shown, right wing identical Existing fuel system Fuel jettison system 797-FD-0132C 1-19-2-whp/CF

Communication Radios and Equipment 767-200ER/-300ER

Left RCP

Right RCP ACTIVE

STANDBY

VHF L

VHF C

VHF R

HF L

AM

HF R

HF SENS O F F

Radio communications panel (representative)

Center RCP NOSE RIGHT

• Three radio communications panels are each capable of tuning the VHF and HF radios. • Radio communications panels support VHF data link, HF data link, 8.33-kHz frequency spacing, VDL mode 2, and voice mode protection. Separate options are available to enable each of these functions. • Separate option is available, contingent on selection of compatible HF and VHF transceivers, to display transceiver fault status on the radio communications panel by monitoring the CMC output bus.

BOEING PROPRIETARY

797-FD-0133C 2-26-2-CF

Pilots’ Call Panel 767-200ER/-300ER

CABIN CALL FWD

MID

AFT

GND ALERT

CALL

ALERT

SELCAL call lights/switches (blue) • Illuminate when attendant at respective station calls flight crew • Accompanied by flight deck high chime • Reset when call is answered or switch is pressed • Sound high-low chime and illuminate pink light at attendant station • Inhibited if handset at selected station is off hook

Alert call light/switch (amber) • Illuminates when cabin attendant activates alert call • Accompanied by flight deck high chime • Resets when call is answered, the calling handset is reset, or when switch is pressed • Sounds high-low chime three times and flashes pink lights at all attendant stations when pressed

Ground call light/switch (blue) • Illuminates when ground personnel at APU ground control panel call the flight crew • Accompanied by flight deck high chime • Press to reset • As long as the switch is held down, a horn sounds in the wheel well to call ground personnel

797-FD-0134C 1-19-2-whp/CF

Audio Selector Panel 767-200ER/-300ER

Microphone selector switches/lights (white) • Illuminate when selected • Select desired transmitting system • Interlocked to permit only one switch to be selected at a time • Automatically activate respective receiver

Ground call light • Ground crew call to pilots • 30-sec reset

MIC

MIC

MIC

MIC

MIC

MIC

CALL

CALL

CALL

CALL

CALL

IN USE

L VHF

Receiver control • Push to select ON/OFF (alternate action) • Rotate for volume control

C VHF

MIC

R VHF

L

CAB

MIC

MIC

MIC

MIC

CALL

CALL

CALL

R

L

VOR

FLT

CALL

L

HF

INT

Push-to-talk switch • Transmits on selected system with boom microphone or oxygen mask microphone • Resets SELCAL light for selected radio

Call lights (9) • VHF, HF, and SATCOM • ACARS call on VHF-C • Flight attendant call on cabin interphone • Resets with transmit switch or PTT activation; SATCOM resets upon termination of call

ADF R L R

PA

Receive light • Indicates respective receiver is selected

BOOM

R SAT

OXY APP

V B R

L

C R

MKR

Boom-oxygen switch • Selects either boom or oxygen mask microphone for use with selected system

Filter selector • Filters audio from VOR, ADF, ILS, DME • VOICE – voice only • RANGE – range (code) only • BOTH – voice and range

797-FD-0135C 2-26-2-whp

Antenna Locations 767-200ER/-300ER

VOR (L, R)

HF

ATC (L) TCAS

ATC (R) GPS (L, R)

SATCOM 2 ADF (L) ADF (R)

VHF (C)

VHF (L) Weather radar Localizer (L, C, R)

Glideslope (L, C, R) Airphone 1 TCAS ATC (L) ATC (R)

VHF (R) Marker beacon DME-R Radio altimeter receiver (L, C, R) Radio altimeter transmitter (L, C, R) DME (L)

1

Structural provisions.

2

Optional installation.

797-FD-0136C 1-19-2-whp/CF

Electrical System 767-200ER/-300ER 90-kVA engine-driven generators • Integrated drive generator (IDG)

BAT

STBY POWER AUTO

ON

90-kVA APU generator • Automatic start/shutdown • Start with separate APU battery • Ground or in-flight use • APU generator allows for dispatch with one engine IDG inoperative

D I S C H

BAT

OFF

OFF O F F

APU GEN EXT PWR ON

O

BUS TIE

One generator can supply all loads except utility

ON

F

BUS TIE AVAIL

F

AUTO

AUTO

ISLN

Nonparallel system • Left and right sides powered by separate power sources

ISLN UTILITY BUS R

ON

ON

OFF

OFF

R BUS BUS

BUS OFF

Automatic load transfer Automatic load shed of utility buses • For generator loss • For overload • For engine start from APU

L

L BUS

OFF

R

L GEN DRIVE DISC

GEN CONT

L

R

DRIVE

DRIVE

GEN CONT

O

Standby ac and dc buses • Powered by main battery • 30-min minimum

F

O ON

F

F

APU

ON OFF

Flight instrument transfer bus • Automatic transfer • No normal in-flight procedures

ON

F

START

RUN FAULT

797-FD-0137C 1-19-2-whp/CF

Electrical Power System 767-200ER/-300ER External ac power APU gen

L IDG L GCB

EPC

APB

R GCB

R BTB

L BTB

Left main ac bus

R IDG

Right main ac bus

AC tie bus

Left utility bus

Right utility bus F/O flight inst transfer bus

Left TRU

Right TRU

Captain flight inst trans bus

Left ac transfer bus

AC gen

Standby ac bus

DC gen

HMG

Flight ac transfer bus

Left dc bus

DC tie bus

Static inverter Center ac bus

Right dc bus

Ground service bus Center dc bus

Standby dc bus Battery bus

Hot battery bus

Main batt chrgr

APU batt chrgr APU battery bus

Main battery

Standby tie bus

APU battery

797-FD-0043 1-21-2-whp/CF

Hydraulic Motor-Driven Generator (HMG) 767-200ER/-300ER

• Backup electrical power source for extended twin-engine operations • Additional generator to supply 5-kVA ac and 50-A dc power • Powered by center hydraulic system air-driven pump • Located in left-hand wheel well on keel beam • An independent power supply for the Captain’s flight instruments as well as selected navigation, communication, lighting, and anti-icing loads • Activated automatically when the airplane is airborne with loss of the engine-driven and APU generators

797-FD-0138C 1-19-2-whp/CF

Hydraulic Motor Generator (HMG) 767-200ER/-300ER ENTRY

EMER

DOORS

CARGO

DOORS

CAPT

ACCESS

DOORS

DOORS

FO L AOA

L AUX

PASS OXY

EMER LIGHTS

FWD

R AUX

BULK

TAT PITOT

PITOT

OFF

ON

ARMED

W

STAB

N 2

3

W 4

H 5

E 6

7

S 8

9

ENT

0

CLR

1

ON

UNARMED

AUTO SPOILERS

ON

SPDBRK

OVHT COMPT TEMP

AIL

RUDDER

UNSCHED

OVHT

ON

TRIM

DSPL SEL PPOS WIND

CARGO HEAT

R AOA

PITOT

PITOT

IRS MODE SEL N

ANTISKID STAB TRIM

LOCK

RATIO

WINDOW HEAT TK/GS

HDG

L

RAM AIR TURB

R FWD

FWD

SIDE

SYS DSPL C L R

SIDE

PRESS

ON

ON

ON

ON

UNLKD

INOP

INOP

INOP

INOP

INOP

INOP

FWD CAB L

C

ALIGN

ON DC

NAV

OFF

NAV

ALIGN

BOTH

OFF

ALIGN

NAV

INOP

AUTO

VALVE

C

FAULT ATT

AFT CAB

R

2

VALVE

DC FAIL

FAULT ATT

1

ON DC

DC FAIL

FAULT

AUTO

ENG START

ALIGN

L ON DC DC FAIL

ALIGN

MID CAB

AUTO

R

ALIGN

C

W

OFF ATT

TRIM AIR

OFF

AUTO

OFF

GND

ON

CONT

CONT

FLT

FLT

OFF

L

FUEL JETTISON

ON

ON

INOP

INOP

BAT L

AUTO ON D

NORM

ON

ON

VALVE

VALVE

FUEL XFEED

QTY

QTY

BUS TIE

PUMPS

HYD

ENG

ON

ON

ON

PRESS

PRESS

PRESS

OVHT

OVHT

OVHT

OVHT

I

A

Y AIR

AUTO

AUTO ISLN

BUS

A

OFF

R BUS

R ON

OFF

L

P

R

R

E

E

S

S

S

S

DESCEND

00340 0 4

AUTO ON

OFF

F

N

VALVE

C ISLN MAN

AUTO 1

R

V A L V E

DUCT LEAK

LB

O ON

F DRIVE

F

DRIVE

ON

KG

LB KG FUEL QTY X 1000

LB

KG

WING

BLEED DL UE CA T K

OVHT

ON

START

OFF

L L

RUN

FAULT

2

8

ENGINE

4

VALVE

6

2 L ENG 1

2

R

R

VALVE

0 2 25 4 20 15 6 10 8

0

10

ANTI-ICE

ON

ON

ON

VALVE

VALVE

DIFF

PSI

ALT

FT X F 1000

RATE

O F F

V A L V E

OVHT

R ENG

O F F

VALVE AUTO

PRESS DIFF LIMIT: T/O & LDG .125 PSI

WIPER OFF

ERASE

F FPM 1000

ADP

APU

EQUIP COOLING CABIN ALTITUDE

TEST

DUCT LEAK

BLEED

TOTAL

C

TEMP

F

D APU

R ISLN

0

MODE SELECT AUTO 2

O

A ON

20

VALVE

AUTO INOP

R

PSI

L ISLN

LDG ALT

ON

C

L

CONT

M OFF

MAX

MIN

CL

FUEL

P

GEN R

L

CONT

E

OVHT

AUTO ON

Y

80 PRESS

R GEN DRIVE DISC

GEN D

OFF

T B

60

OFF

L

D

ON

BUS ON OFF

S C

W

OP

CONFIG

L

AUTO RATE

Battery switch • ON - Provides backup power from the hot battery bus to the battery and standby buses • OFF - Disconnects battery bus from hot battery bus

DUCT

UTILITY BUS

M

PRESS

OVHT

AUTO

A

N

Y W

MANUAL CLIMB

FWD PRESS

VALVE

PRESS

C PUMP L BUS

VALVE

FWD

ELEC

PRESS

OVHT

M

N

ON

ON

Y ELEC PRESS

E

PACK OFF

AUTO OFF T B

CABIN ALTITUDE CONTROL BUS TIE

AVAIL

ISLN

R

D

W MAN

N

C

ON ON

F

R

ON PRESS

INOP

C

AUTO OFF

PRESS

VALVE

P

I

RESET

INOP PACK OFF ON

ON

AFT

R

C 1-ELEC-2

R PACK

L PACK

AUTO

S

F

L

ALERT

OFF F

R PUMPS

AFT PRESS

O

ENG

W

AUTO

RESET

L PUMPS ON

APU GEN EXT PWR

QTY

C

CALL

SEATBELTS

ON

OFF F

F F

H

SYS PRESS

ALERT

NO SMOKING AUTO O

C

SYS PRESS

GND

AFT

PASS SIGNS

BAT

OFF

S

ALTN

CONT

SYS PRESS

MID

OFF

OFF

I

ENG ALTN

R

Battery discharge light illuminated - The main battery is discharging

INOP

ON

STBY POWER

R ELEC

NORM

FWD

FAULT

L–NOZZLE–R

M

ON INOP

R

CABIN CALL

R

ON INOP

FLT DK

YAW DAMPER

P

W

OFF

L - RECIRC FAN - R

AUTO OFF

GND

C

W

OFF

STBY

OVHT

LOW

OVRD SMOKE NO COOLING

HIGH

HEADPHONE COCKPIT VOICE RECORDER

CKT BKR

OVHD PANEL

DOME

PANEL/FLOOD GLARESHIELD

AISLE STAND ANTI

LT OVRD POSITION

WING

COLLISION RED

ON

OFF

ON

OFF

OFF

OFF

WHITE LOGO

OFF

ON

ON

FLT DK DOOR

ON UNLKD

ON

TAXI RUNWAY TURNOFF

Standby power bus off light • Illuminated - standby ac or dc bus not powered

UNLKD

L

OFF

R

LANDING WING L

NOSE GEAR R

IND LTS DIM

TEST BRT

ON OFF

OFF

ON

ON

Battery charger

BAT AUTO ON

Hot bat bus dc

D I S C H

Battery

Flow lines not on panel DC power AC power

DC output Hydraulic motor-driven AC generator output (HMG)

BAT

OFF

OFF

O F F

Battery bus dc

Left dc

Captain flight instrument transfer bus

Left transfer bus

Right transfer bus

Standby dc bus Standby ac bus

Standby power selector • OFF - The standby buses are unpowered • AUTO - The standby buses powered from main ac and dc transfers to battery power if normal ac power is lost • BAT - The standby buses are powered from the main battery 797-FD-0032 1-19-2-whp/CF

Hydraulic Motor Generator System 767-200ER/-300ER Systems powered by battery or hydraulic motor generator if operational • Fire extinguishing systems • Engine, APU, and cargo and wheel well fire detection systems • Spar fuel valves • APU fuel valve • Fueling system • Fuel crossfeed valves • DC fuel pump • Fuel quantity system • Engine fuel control valves • Clock time references • Captain’s clock • IRS (L and C continuous; R 5 minutes) • RAT manual deployment • RAT automatic deployment system • Parking brake valve • Landing gear alternate extension • Passenger address system • Interphone systems • Generator controls • Engine-driven hydraulic pump shutoff valves • Air-driven hydraulic pump control • E/E cooling override system • Antiskid for inboard wheels • Air/ground system • Passenger oxygen deployment system • Standby engine indicating • Engine start controls • Engine ignition system • Engine thrust reverse control • Left and right pack valves • Manual wing anti-ice • Manual engine anti-ice

Additional systems powered by hydraulic motor generator • • • • • • • • • • • • • • • • • • • • • • • • • • •

Alternate stabilizer trim Stab trim shutoff valves Manual cabin altitude control Aislestand floodlight Left yaw damper Three spoiler pairs Left VHF Left stick shaker Standby attitude indicator Left aural warning speaker Rudder trim Main panel floodlights Left VOR/marker beacon Left air data computer Left RDMI Center MMR Duct leak detection E/E cooling standby mode Standby instrument panel lights Right ADF WEU (channel B) Standby electrical power control APU control Cabin altitude indicator Cabin differential pressure indicator Cabin emergency lights Emergency evacuation system (if installed)

• • • • • • • • • • • • • • • • • • • • • • • • • •

Left EADI Left EHSI Left altimeter Left Mach/airspeed indicator Left EFIS symbol generator Center EFIS symbol generator Left EFIS control panel Left VSI Left MMR Left radio altimeter Captain’s instrument and panel lights Left FMC and MCDU Left DME Left HF Flap and rudder trim position indicators Aislestand and overhead panel lights Captain’s pitot heat Right auxiliary pitot heat Left angle of attack heat Left and right pneumatic isolation valve Cabin pressure controller auto 1 and 2 Lavatory lights Left and right engine probe heat Left ATC system Cargo heat override control Passenger cabin ceiling and night lighting • Manual flight deck temperature control • Trim air

Note: Standby altimeter and standby airspeed indicator are pneumatically driven.

797-FD-0139R1C 1-19-2-whp/CF

Flight Controls 767-200ER/-300ER

• The primary flight controls are the ailerons, elevators, and rudder. Flight controls are powered from the three hydraulic systems. There is no manual reversion. • Spoilers assist the ailerons in providing roll control and, in addition, operate as speed brakes. • A variable-pitch stabilizer assists the elevators in providing pitch control. The stabilizer provides trim by varying the horizontal stabilizer angle. • High lift for takeoff and landing is provided by trailing edge flaps and leading edge slats. The flaps and slats can also be operated by an alternate electrical system.

Outboard aileron Inboard leading edge slat

Inboard aileron Rudder

Spoilers Outboard leading edge slats

Elevator Stabilizer

• Two independent yaw damper systems operate continuously in flight to improve the airplane’s directional stability and turn coordination.

Trailing edge flaps

• The EICAS status display of flight control surface positions shows the amount of deflection. L

C

R

HYD QTY 0.76 FULL 0.25 APU EGT 640

CABIN ALT AUTO1 CARGO FAN

OXY PRESS 1750

RUD

AIL

ELEV

AIL

EICAS status page

797-FD-0142C 1-19-2-whp/CF

Hydraulic Power 767-200ER/-300ER Center system

Left system

• The left and right hydraulic systems are each powered by one primary engine-driven pump and one electric demand pump. • The center hydraulic system is normally powered by two electric primary pumps and one air-driven demand pump. • The center system provides power for the hydraulic motor generator during standby electrical power operation. • Each hydraulic system reservoir is equipped with a low-quantity measuring system to provide information to the EICAS status display for quantity and refill indications. • RAT (ram air turbine) provides hydraulic pressure to center hydraulic system when deployed.

Primary pumps Demand pumps

Engine pump

Electric pump Electric pump

Right system

Electric pump

Electric pump

Air-driv pump Valve

Tail * skid

Flaps and slats

HMG

Main gear Left thrust reverser

Engine pump

Check valve

Right thrust reverser

Nose gear

Rudder ratio

PUMPS

HYD

L

R

R

C 1-ELEC-2

ENG

P

ENG

ON

ON

ON

ON

PRESS

PRESS

PRESS

PRESS

Alternate brakes

Normal brakes

OVHT

OVHT

OVHT

OVHT

Spoilers

Spoilers

I M

Spoilers

A

Y

R

AIR

ELEC

PRESS

PRESS

PRESS

OVHT

OVHT

OVHT

Right inboard aileron

Left inboard aileron

Y

ELEC

D

Elevators

D

E

E

M

Rudder

Outboard ailerons

Center autopilot servos

Right autopilot servos

M

AUTO

A N

Elevator feel Stabilizer trim

R

A R

Nose wheel steering

P

I M

Yaw dampers

OFF

AUTO ON

OFF

AUTO ON

OFF

D

A

ON

N D

Left autopilot servos

Hydraulic control panel * 767-300ER models only.

RAT pump

Hydraulic system diagram 797-FD-0144C 1-19-2-whp/CF

Ice and Rain Protection Probe and Window Heat, Windshield Wipers

Probe heat • Operation is fully automatic Window heat • Heat control is automatically provided for both left and right no. 1 and no. 2 windows Windshield wipers • Hydrophobic coating on windshield

Overhead panel Window heat switch • Signals window heat controller to apply heat to associated window WINDOW HEAT R

L SIDE

FWD

SIDE

ON

ON

ON

ON

INOP

INOP

INOP

INOP

Window heat inoperative lights • Associated window is not being heated

Probe locations L

WIPER

OFF INT

Pitot static probes (2 per side) Angle of attack probe (1 per side) Total air temperature probe (left side only)

FWD

LOW HIGH

R OFF INT LOW HIGH

Standard selections baseline is dual three-speed (with intermittent) wiper switches

Windshield wiper selector OFF – Wipers turned off and sequenced to the stowed position INT – Intermittent operation LOW – Low-speed operation HIGH – High-speed operation

797-FD-0145C 1-19-02-whp/DD

Wing and Engine Anti-Ice 767-200ER/-300ER Wing anti-ice switch • In-flight operation only

Overhead panel WING

To right wing anti-ice valve

ANTI-ICE ENGINE L R

ON

Air/gnd logic

R

L VALVE

ON

ON

VALVE

VALVE

D

VALVE

Engine anti-ice switches

Pneumatic manifold T P

Heated slats

Temperature sensor

Wing anti-ice valve

Cowl anti-ice Bleed air manifold PRV LP

P

Wing thermal anti-ice overpressure switch

T

Wing TAI overheat switch

HP

797-FD-0146C 1-19-02-whp/DD

Wheel Braking System 767-200ER/-300ER

• Normal braking is powered for all main wheels by the right hydraulic system. • Alternate braking is powered by the center hydraulic system. • A single brake pressure accumulator is charged from the center hydraulic system.

PARK BRAKE P A R K

• An antiskid system is provided to all main wheel brakes for skid protection, locked wheel, hydroplane, and touchdown protection.

AUTO BRAKES

B R A K E

AUTO BRAKES 2 3 1

a

4

DISARM

MAX AUTO

OFF

RTO

• An autobrake system permits automatic braking at preselected deceleration rates following touchdown. • An RTO (rejected takeoff) feature applies maximum braking if both thrust levers are retarded to idle above 85 knots during takeoff roll.

Altn brake press Accumulator isolation valve

BRAKE

4

PRESS PSI

Park brake valve

X 1000

3

0 2

Hydraulic system

1

Metering valve

Accumulator

Antiskid valves

Auto brake valve

Antiskid return

Metering valve

Antiskid valves

Antiskid controller Antiskid

797-FD-0147C 1-19-02-whp/DD

Landing Gear 767-200ER/-300ER

• The 767 has two main gear and steerable nose gear

D O O R Sa

• Landing gear actuation is powered by the center hydraulic system

TAIL SKID

a

NOSE g

a

RIGHT

LEFT g

• A tailskid is installed on 767-300ER airplanes

G E A R

UP

OFF

g

RETRACT 270K

EXTEND OR EXTENDED 270K-.82M LOCK OVRD

DN

Landing gear level UP – Releases downlocks – Pressurizes upside of gear actuator OFF – Depressurizes landing gear hydraulic system DN – Releases uplocks – Pressurizes downside of gear actuator

Tailskid light (amber) (767-300ER airplanes) • Tailskid disagrees with lever position

Landing lock override switch Push – Manually releases lever lock

ALTN GEAR EXTEND 250K-.75M OFF

DN

Alternate gear extension switch (toggle, guarded) OFF – Resets alternate gear extension system DN – Releases all gear uplocks

797-FD-0148C 1-19-02-whp/DD

Nose Wheel Steering 767-200ER/-300ER

• Nose wheel steering is powered by the center hydraulic system • Steering is controlled primarily through the left-hand tiller wheel • Rudder pedals provide up to 6˚ of steering control

Minimum turning radius

Tiller steering angle 65˚

Minimum width of pavement for 180˚ turn is 129.0 ft (39.32 m) -200 series 146.0 ft (44.50 m) -300 series

Center of turn for minimum turning radius (slow continuous turn, no differential braking)

, Captain s sidewall

Nose wheel steering tiller • Turns nose wheel up to 65˚ in desired direction • Overrides rudder pedal steering

Nose wheel indicator shows direction and angle of nose wheel steering signal

797-FD-0149C 1-19-02-whp/DD

Air Data System 767-200ER/-300ER Flush static ports (2)

Pitot static probes (4) Captain’s auxiliary pitot

First Officer’s main pitot

R-AOA

Right ADC

RAT arm pressure switch

Standby altimeter

Elevator feel computer

Standby airspeed indicator Left ADC

Captain’s main pitot

• • • •

Differential pressure sensor

TAT L-AOA First Officer’s auxiliary pitot

Dual ARINC 706 digital air data computers Independent standby instruments Auto probe heat Dual-level pitot static probe heat

• Dual angle-of-attack (AOA) vanes • Aspirated TAT probe provides certified TAT for takeoff thrust computations • TAT display on EICAS • TAS and SAT available in FMC MCDU

797-FD-0150 C 1-19-02-whp/DD

Flight Crew Oxygen 767-200ER/-300ER Flow indicator • Shows a yellow cross when oxygen is flowing

Release levers Squeeze and pull • Releases mask from stowage box • Oxygen turns on and mask harness inflates RESET PUSH

Stowed oxygen mask regulator (crewmember station)

100% PUSH

OXYGEN BASE

HYD QTY

L 0.76

APU EGT

640

OXY PRESS

1750

C R 1.00 0.25 RF

Oxygen pressure • Pressure at the crew oxygen cylinder

CABIN ALT AUTO 1 CARGO FAN

RUD

AIL

Reset/test slide lever Push • Mask stowed, turns oxygen on momentarily to test regulator

ELEV

AIL

EICAS status display center panel

Normal/100% selector Normal • Air/oxygen mixture on demand • Ratio is dependent on cabin altitude 100% • Pushing selector supplies pure oxygen on demand

Harness (shown inflated) N

Mask

100% PUSH

EMERGENCY

Microphone Regulator

PRESS TO TEST

Emergency/test selector • 100% oxygen is supplied under positive pressure at all cabin altitudes

797-FD-0151 C 1-19-02-whp/DD

Flight Deck and Emergency Lighting 767-200ER/-300ER Panel light control • Regulates the brightness of the internal lighting in the Captain’s and center panels and standby magnetic compass

Chart light control • Regulates the brightness of the Captain’s and First Officer’s chart light

CLOCK PANEL

Map light control • Regulates the brightness of the Captain’s and First Officer’s map light

OFF

Floodlight control • Regulates the brightness of the floodlighting in the Captain’s, center, and First Officer’s panels

CHART FLOOD

OFF MAP PTT

Emergency lights switch (guarded) OFF – Prevents activation of emergency lighting system when electrical power fails or is turned off ARMED – All interior and exterior emergency lights illuminated automatically if dc power fails or is turned off ON – All emergency lights illuminate Lights override switch (alternate action) ON – Turns on the following lights to full brightness: Captain’s, center, and First Officer’s main panel floodlights, forward and aft dome lights, and aislestand floodlight

Emergency lights switch unarmed light (amber)

EMER LIGHTS OFF ARMED

UNARMED

ON

PASS SIGNS NO SMOKING

SEAT BELTS AUTO

AUTO OFF

ON

OFF

ON

LT OVRD ON

No smoking/seat belt selector OFF – Turns off the associated passenger signs AUTO – Selects automatic control of the associated passenger signs • NO SMOKING signs on when landing gear is down • SEAT BELT signs on when landing gear is down or flaps are not up ON – Turns on the associated passenger signs 797-FD-0152 C 1-19-02-DD/DD

Exterior Lighting 767-200ER/-300ER Right position lights (green and white) Taxi runway turnoff lights (left and right) Landing lights (left, right, and nose)

Logo lights (white)

LOGO ON

RUNWAY TURNOFF L

OFF

R

Logo light switch

ON

Runway turnoff light switch Red and white anticollision light switch (alternate action) ON – Turns on the corresponding red or white strobe lights Position light switch (alternate action) ON – Turns on the red, green, and white position lights Wing landing light switch (alternate action) ON – Turns on the corresponding left or right wing landing light – Light intensity is at maximum only when the landing gear lever is down

Taxi lights (optional) Upper anticollision light (red strobe) Wing illumination lights Lower anticollision (red strobe)

Left position lights (red and white) Anticollision lights (left and right) (white strobe)

ANTI COLLISION RED WHITE

POSITION

ON

ON

WING

ON

ON

Wing light switch (alternate action) ON – Turns on the wing leading edge lights – Light intensity is at maximum only when the landing gear lever is down

LANDING WING L

NOSE GEAR R

OFF

OFF

ON

ON

Nose gear landing light switch ON – Turns on the two nose gear landing lights – Inhibited if nose landing gear is retracted 797-FD-0153C 1-19-02-whp/DD

767 Flight Deck and Avionics - Options

767 Options 767-200ER/-300ER

1

Electronic Flight Instrument System

2

Engine Indication and Crew Alerting System

3

Autoflight Systems

4

Flight Management Computer System

5

Communications

6

Navigation System

7

Crew Accommodations

8

Airframe Systems

797-FD-0154 C 2-25-02-PW-whp

Options 1 —Electronic Flight Instrument System 767-200ER/-300ER EADI Feature Flight Mode Annunciation (FMA) Airspeed Tape

Flight Director Command Display and Airplane Symbol

Basic Bottom of EADI Fast/Slow Indicator

Split Axis

Option Top of EADI Airspeed Tape with Rolling Digits and Trend Vector (Contingent on Top FMA) Airspeed Tape with Hollow Cursor and Trend Vector (Contingent on Top FMA) Filled Integrated CueHollow Integrated Cue

Radio Altitude Display

Digital Display

Digital and Round Dial Display

Rising Runway Display

None

Provided on EADI

Radio Altitude Height Alert

None

Shown at 1000 feet Shown at 1500 feet Shown at 2500 feet

ILS Deviation Alert

None

Provided on EADI

EHSI Feature Map Mode Orientation Range Arcs True Airspeed and Ground Speed display Wind Bearing Digital Display

Basic

Option

Track Up

Heading Up

Range Marks

Range Arcs

Ground Speed on EADI only Wind Speed and Direction displayed

Ground Speed on EADI and EHSI. True Airspeed on EHSI Wind Speed, Direction, and Bearing displayed

ADF Pointers

None

Provided on EHSI

TCAS 3nm Range Ring

None

Provided on EHSI

797-FD-0211C 2-25-2-whp

Options 1 —Electronic Flight Instrument System 767-200ER/-300ER Electronic Attitude Director Indicator (EADI) Flight mode annunciation on top of ADI

Airspeed tape

GS138

SPD A/T

DH150 20

LOC ROLLOUT

20

20

10

10

10

10

20

20

CMD

200

20

F 10

G/S FLARE

Integrated cue flight director

160

10

132 120

10

S

10 100

A/T

SPD FLARE G/S

20

20

CMD

ROLLOUT LNAV

ALT

GS 138

200

Radio altitude height alert 1,000, 1,500, or 2,500 ft RA

Rising runway Rolling digits and trend vector

Basic EADI

ILS deviation warning

Round dial radio altitude

Optional EADI features

797-FD-0155 C 2-26-2-whp/CF

Options 1 —Electronic Flight Instrument System 767-200ER/-300ER Electronic Horizontal Situation Indicator (EHSI) True airspeed and ground speed

27.5 NM

TRK 142 M

27.5 NM

0835.4 Z8 WX+T +12

TAS 270 GS 298

HDG 127

M

12

15

12

ADF pointers

DIDES

Heading up

9

0835.4 Z WX+T +12

15 DIDES

CAMP

CAMP

20

20

BUGLE

BUGLE

Range arcs Note: Range arcs are visible full time in map mode and when weather, TCAS, or terrain is displayed in expanded VOR/APP mode.

20

115˚ /20

Digital wind bearing Basic EHSI map mode

Optional EHSI map mode features

El797-FD-0156C 2-26-2-whp

Options 2 —EICAS 767-200ER/-300ER Feature Engine Fuel Flow Display APU Oil Quantity Display Generator Off and Engine Oil Pressure EICAS Messages ECS Parameters

Basic Display when Secondary Engine page is selected Low APU Oil Quantity message on Maintenance page Advisory Level Basic ECS Parameters on Maintenance page

Option Full Time Display APU Oil Quantity Level on Status and Maintenance page Caution Level Basic and Additional ECS Parameters on Maintenance page

Hydraulic Pressure

Display on Maintenance page

Display on Status and Maintenance pages

APU RPM

Display on Maintenance page

Display on Status and Maintenance pages

Bulk Cargo Compartment Temperature

None

Display on Maintenance and Status page

Ram Air Door Outlet Position

None

Display on Maintenance Page

Display on Maintenance page for GE and RR engines

Display on Maintenance page for PW engines

Engine Fuel Pressure EICAS Maintenance Pages Available during flight

Available above 10,000 feet

Not Available during flight

ECS Precooler Outlet Temperature

None

Display on Maintenance page

Brake Temperature Display

None

Display on Status page

Tire Pressure Display

None

Display on Status page

Caution and Warning Options Feature Autopilot Disengage Warning

Firebell Aural Warning Overspeed Aural Warning

Basic Aural Warning Siren - Aural Inhibited when Autopilot Disconnect Switch double pushed

Option Aural Warning Wailer - Aural activated for one second when Autopilot Disconnect Switch double pushed

1 second on, 9 seconds off

2 seconds on, 3 seconds off

Resettable Warning Siren

Non-resettable Warning Siren

797-FD-0212C 2-25-2-whp

Options 2 —EICAS 767-200ER/-300ER

Caution level messages • Generator off • Engine oil pressure

TAT

L GEN OFF R GEN OFF L ENG OIL PRESS R ENG OIL PRESS

(Default selection shows these messages as advisory level)

-12o C 1.50 2.0

1.50

CRZ 2.0

1.28 1.0

1.28 1.0

1.5

1.5 EPR

54.2

54.2

Metric engine parameters • Fuel flow (FF) shows in kilograms per hour • Oil quantity shows in liters

N1

428

428

EGT

95 70

PRESS

105

105

OIL

TEMP

OIL

3.1

95

70

OIL

18

Note: This is part of a broader option to show all instrumentation with metric units.

N2

11.3

Full-time display of fuel flow 11.3

18 QTY

FF

0.9

(Default selection shows this only when secondary engine display is selected)

Primary and secondary displays

797-FD-0157C 1-18-02-CF/DD

Options 2 —EICAS 767-200ER/-300ER Hydraulic pressure indication L HYD QTY HYD PRESS APU

EGT

R

OIL

12.4 FF 15.3 0.25RF 2140 CABIN ALT AUTO 1 CARGO FAN Q 0.75

1750

OXY PRESS

APU oil quantity level indication

RUD

AIL

ELEV

Full-time fuel flow

26

BULK CARGO TEMP

Bulk cargo compartment temperature indication

C

0.76 1.29 3230 3210 640 RPM 103

AIL

160

160

160

2 3

50

160

4 5

160

160

5 1

160

160

2 3

160

APU RPM indication

BRAKE TEMP / TIRE PRESS

Brake temperature indications

Tire pressure indications

Status page

797-FD-0158C 1-19-02-MT/DD

Options 2 —EICAS 767-200ER/-300ER

ECS/MSG maintenance page

PERF/APU maintenance page PERF/APU

ECS/MSG L

PACK OUT TURB IN SEC HX OUT COMPR OUT

Additional ECS parameters

PRIM HX OUT PRIM HX IN PRECOOL OUT DUCT PRESS PACK FLOW TEMP VALVE RAM IN DOOR RAM OUT DOOR

Ram air outlet door position

FLT DK DUCT TEMP TRIM VALVE

30 0.75

2 9 1 96 44 171 193 40 0 0.75 0.62 0.73

3 10 3 98 46 173 196 42 0 0.80 0.71 0.72

FWD

28 0.80

R

FWD EQ FAN 1

CAS

ZONE TEMP BITE

MACH

95 130 12

OIL QTY

0.7 0.5

95 130 12 0.3 0.9

N1 N2

MID

17 0.00

AUX MID

17 0.00

25 AFT

17 0.00

EGT

640

RPM

100 0.25

OIL Q

TAT ALT

1.523

EPR ACT EPR ACT

104.0

N1

1.284

54.2 1.013

APU: BULK CARGO TEMP

187.6

245 0.015

60.4

AFT CABIN TEMP

ECS precooler outlet temperature

OIL TEMP

VIB

AUX FWD

28 0.80

OIL PRESS

GROSS WT

86

EGT

+15 21030

0.902 1.001 104.0 21.3

N2

82.5

FF

1.010

FP N1 RED

EGT RED

84

APU OIL QTY

Bulk cargo compartment temperature

APU oil quantity level

Interstage fuel pump pressure (basic with General Electric and Rolls-Royce engines)

797-FD-0159 C 1-19-02-MT/DD

Options 3 —Autoflight Systems 767-200ER/-300ER

Feature Glideslope Capture Mach Display on Mode Control Panel (MCP)

Basic Inhibit Glideslope Capture prior to Localizer Capture Two-digit Mach display

Autopilot Triple-Channel Selection in Approach Mode

Automatic

Autopilot Command Engage Default Roll Mode

Heading Hold

Flight Director

Mode Control Panel (MCP) Fixed Derates Climb Fixed Derate Washout FCC Software Loading Capability

Part Time Display (Flight Director display inhibited whenautopilot and flight director are referenced to the same FCC) 757/767 Baseline MCP Climb Fixed Derates 10,000 feet to 12,000 feet On-board Software Loadable

Option Enable Glideslope Capture prior to Localizer Capture Three-digit Mach display Manual Bank Angle Hold Full Time Display (Flight Director always displays when selected)

757/767 Baseline MCP without Backcourse Switch747-400 MCP Takeoff and Climb Fixed Derates 10,000 feet to 30,000 feet Not Software Loadable

797-FD-0213C 2-25-2-whp

Options 3 —Autoflight Systems 767-200ER/-300ER 747-400 mode control panel Knob shape modified to provide tactile difference from heading and altitude knobs A/T ARM

VERT SPD

HDG

IAS/MACH

F/D ON

L NAV

2 0 0

1 2 6

1

Backcourse mode deleted A/P ENGAGE

ALT

7 0 0 0

1 7 0 0 0

L

C

R

CMD

CMD

CMD

F/D ON

OFF SEL

V NAV

THR OFF

5 NORM

FL CH

SPD

SEL

25 BANK LIMIT

LOC

DN

V/S

HOLD

HOLD

OFF

APP

DISENGAGE

UP

All pushbutton switches modified to provide positive tactile feel

Changed EPR or N1 nomenclature to THR (provides commonality with all engine types)

Added push action switch to altitude select knob (provides VNAV altitude intervention capability)

757 and 767 mode control panel options Three-digit Mach display A/T ARM F/D ON

.8 0 5

VERT SPD

HDG

IAS/MACH L NAV

Backcourse mode deleted

2 7 0

1

A/P ENGAGE

ALT

7 0 0 0

1 7 0 0 0

L

C

R

CMD

CMD

CMD

F/D ON

OFF SEL EPR

V NAV

OFF

5 NORM

SPD

FL CH

Full-time flight director: Command bars stay in view when same A/P is selected

SEL

25 BANK LIMIT

LOC

DN

V/S

HOLD

HOLD

APP

OFF

DISENGAGE

UP

Bank angle hold on A/P or F/D engagement if bank between 5 and 30

Individual channel selection in approach mode 797-FD-0160C 1-19-02-whp/DD

Options 4 —Flight Management Computer System 767-200ER/-300ER Feature Runway Position Shift Units Flight Crew Alertness Monitor Navigation Database

Basic Feet Inhibited Boeing Supplied

Option Meters Enabled Customer Supplied

Offpath Descent Circles & DME Range Rings

Inhibited

Displayed

Altitude Intervention

Inhibited

Enabled (Contingent on selecting 747-400 MCP)

Airline Modifiable Information (AMI)

Boeing Supplied

Customer Supplied

Required Time of Arrival (RTA)

Inhibited

Enabled

Air Traffic Services Datalink (ATS DL)

Inhibited

Enabled (Contingent on selecting Datalink capability)

Airline Operational Communciations Datalink (AOC DL)

Inhibited

Enabled (Contingent on selecting Datalink capability)

Takeoff Datalink

Inhibited

Enabled (Contingent on selecting AOC DL)

FMC Printer Interface

Inhibited

Enabled (Contingent on selecting a printer)

ADF Approaches

Inhibited

Enabled

GPS Approaches

Inhibited

Enabled

Display of Vertical Bearing, Flight Path Angle, and Vertical Speed

Inhibited

Enabled

797-FD-0214C 2-25-2-whp

Options 4 —Flight Management Computer System 767-200ER/-300ER Future Air Navigation System (FANS) FANS is an International Civil Aviation Organization (ICAO) concept of a phased approach to Communication Navigation Surveillance/Air Traffic Management (CNS/ATM) implementation. FANS 1 allows: • Reduced separations • More timely altitude change authorizations • Flexible routine operations • Dispatch on required navigation performance (RNP) only routes • Efficient crossing track operations

EICAS messages DATALINK LOST UNABLE RNP FMC MESSAGE ATC

MCDU pages ATC LOGON

RTE PROGRESS

ATC INDEX

POS REF

The Pegasus FMC is FANS 1 capable. Global positioning system (GPS) and required navigation performance (RNP) are basic features. These options are required to enable FANS operation: • Air traffic services data link (ATS DL). This option also provides automatic dependent surveillance (ADS) • ACARS or VDL mode 2/AOA data link • SATCOM, if FANS operations are desired outside of VHF data link range These options are available, but not required for FANS operations: • Required time of arrival (RTA) • FMC printer interface

ACT ECON CRZ ACT RTE LEGS

ATC REQUEST ATC REPORT ATC LOG

Printer

EMERGENCY

Communication management units

FMCs

VHF receiver

GPS (MMR) receivers

SATCOM receiver

Air traffic control

797-FD-0166C 1-21-2-whp/cf

Options 4 —Flight Management Computer System 767-200ER/-300ER Crew Alertness Monitor

Master caution/warning

EICAS message

Pilot response

Monitors time since last pilot button-push • Mode control panel • EFIS control panels • EICAS control panel • MCDUs • VHF/HF microphone push-to-talk • VOR control panel

Typical Implementation TIME ALERT - - - - - - - - - - - - Cruise - - - - - - - - - - - 15 min EICAS advisory 20 min EICAS caution EICAS warning 25 min - - - - - - - - - - - Descent- - - - - - - - - - - 5 min EICAS advisory 6 min EICAS caution EICAS warning 7 min

Airline defines criteria in policy file • Entire feature selectable on or off • EICAS alerting levels selectable on or off • Timing criteria selectable within predefined limits • Requires option for customer supplied Airline Modifiable Information (AMI)

797-FD-0163C 1-19-2-whp/CF

Options 4 —Flight Management Computer System 767-200ER/-300ER Required Time of Arrival (RTA) • RTA provides the capability to specify a required time of arrival for an existing flight plan fix Santa Monica (SMO) RTA 1307.5Z FMC computes RTA speed Airplane maintains RTA speed Airplane arrives at SMO 1307.5Z • RTA computed for CRZ segment • CLB and DES are ECON • 앐 30 seconds accuracy

RTA fix • Any waypoint in active flight plan

FIX

RTA PROGRESS

3 /3 RTA

.

AL T / E T A FL- - - /- - - . - z T/O ---- .-Z Maximum speed • Defaults to MMO minus 0.02 • Crew can enter a maximum speed if desired

MAX S P D . 840

Takeoff • Initially displays dashes • Displays recommended takeoff time following entry of RTA time • If no RTA fix or time is entered, expected takeoff time can be entered and all trip predictions will be based on entered takeoff time

- - - - - - - - - - - - - - - - - - - -

797-FD-0164C 1-19-2-whp/CF

Options 4 —Flight Management Computer System 767-200ER/-300ER ACARS Interface Options can be selected for • Airline operations communication data link (AOC DL) • Air traffic services data link (ATS DL) • Takeoff data link • Contingent on installation of ACARS MU/CMU system

MENU C ARS MENU

FMCS/ACARS data link • Access ACARS menu through FMC (MCDU) or multipurpose interactive display unit (MIDU) • Provides adequate message flexibility while minimizing communication load • Mode S function compatibility • SATCOM compatibility • Requires MCDU or MIDU and ACARS or VDL mode 2 • Provisions for ACARS or VDL mode 2 offered that would provide for future implementation of ACARS or VDL mode 2 • Partial provisions offered for future upgrade from ARINC 724B ACARS to ARINC 758 communication management units (CMU) • Voice mode protection available to allow center VHF system to be used for both voice and data transmission

MS DEP

RTE

LEGS NAV RAD NEXT PAGE

F

I

J

3

K

N

O

6

P

S

T

M S G O F S T

9

Multifunction CDU (MCDU)

Airplane Confirmation (FPR)

Flight plan request (FPR)

Route mod Flight plan (FPR)

Confirmation (ATC) Route clearance (ATC)

Airline dispatch office

ATC center

797-FD-0161C 1-19-2-whp/CF

Options 4 —Flight Management Computer System 767-200ER/-300ER ATS Data Link • Air traffic services data link (ATS DL) is an optional feature of the Pegasus FMC. ATS DL is contingent on selection of VDL mode 2/AOA or ACARS data link. • The ATS DL combines the functions of ATS facilities notification (AFN), automatic dependent surveillance (ADS), and air traffic control data link (ATC DL). The AFN notifies air traffic control that the airplane is equipped and ready to receive data link communications. ADS allows for automatic reporting of aircraft position and intent data. The ADS is capable of simultaneously reporting to four ATC facilities and one airline facility. The capability to disable ADS through the multifunction control display unit (MCDU) is provided. • The ATC DL allows two-way text messages to be sent between pilot and controller. The messages are received and created using the MCDU. The capability to store and recall messages and to load rate information into the flight plan is provided.

ATC LOGON/STATUS

ATC INDEX

L O G O N TO

<EMERGENCY

POS REPORT> FL T


N O

WHEN CAN WE>

BOE001

FREE TEXT>

N757BB

T AI L


A C T C TR

N O

KOAK

A T C C O M M


CLEARANCE>

N EX T C TR

<SELECT OFF A D S ( A C T)


AD S

< O F F < > ARM

VOICE>

EM E R

O FF <

>

ON

DA TA LINK



RTE

CLB

CRZ

DES

BRT

INIT REF

RTE

READY CLB

CRZ

DES

BRT

797-FD-0167C 1-19-2-MT-CF

Options 4 —Flight Management Computer System 767-200ER/-300ER Airline Operational Communications Data Link (AOC DL)

FMC COMM < RTE 1 POS REPORT rel="nofollow"> < ALTN < PERF < TAKEOFF < WIND DATA LINK < DES FORECAST READY INIT REF

RTE

CRZ

CLB

• AOC data link is an optional feature of the Pegasus FMC. AOC data link is contingent on selection of VDL mode 2 or ACARS data link. BRT

DES

• This feature provides data link communication of performance, takeoff route, waypoint winds, reporting waypoints, descent forecasts, route modifications, and alternate airport information directly into the FMC.

PERF INIT UPLINK

< REJECT ACCEPT > < INDEX POS INIT > PERF INIT UPLINK

ALTN UPLINK

< REJECT ACCEPT > ALTN UPLINK INIT REF

RTE

CLB

CRZ

DES

BRT

797-FD-0168C 1-19-2-whp/CF

Options 4 —Flight Management Computer System 767-200ER/-300ER Takeoff Data Link • FMCS takeoff data link (shown below) is a separate option contingent on selection of AOC DL. This feature allows uplinks of takeoff data to the FMC.

TAKEOFF REF UPLINK 1/2

TAKEOFF REF UPLINK 1/2

V1

V1

134

134

VR

VR

140

140

V2

V2

147 GRWT

197.2

147

TOGW

GRWT

198.6

197.2

TAKEOFF DATA

< REJECT ACCEPT > < INDEX POS INIT > TAKEOFF DATA UPLINK

TOGW

198.6

TAKEOFF DATA

< REJECT ACCEPT > < INDEX POS INIT > TAKEOFF DATA LOADED INIT REF

RTE

CLB

CRZ

DES

BRT

797-FD-0168 R1C 1-19-2-whp/CF

Options 4 —Flight Management Computer System 767-200ER/-300ER Printer Interface • Provides for the printing of the FMC flight plan and ATC data link messages ------ CURRENT AIRCRAFT DATA --------LAST POS: YKM ATA AT LAST POS: 1328Z FUEL AT LAST POS: 131.7 FMC LAT/LON: N4700.0W12516.4 NAV SOURCE: INERTIAL RNP/ACTUAL: 2.0/0.4 FLT PHASE: CRZ ALT: 21100 TAS: 405KT GS: 425KT WIND: 270T/14KT OAT: -38C CURRENT FUEL: 128.7 ORIGIN/ATD: KBFI/1300Z DEST/ETA: KMWH/1610Z CO ROUTE: BFIMWH CRZ ALT: FL210 ZFW: 300.0 RESERVES: 25.0 CRZ CG: 30.0% COST INDEX: 90 ------------- ACT RTE 1 -------------VIA/TO SPD/ALT ETA/FUEL -------------------------------------LACRE3.VAMPS 080 1199NM 1320Z/141.3 VAM01 250/FL270AFL290B V2 070 30NM 1325Z/140.3 ELN (305)/(FL210) DIRECT 120 40NM 1330Z/139.3 ----------- ENTERED WINDS -----------FIX ALT DIR/SPD ALT/OAT -------------------------------------VAM01 FL270 240/130 FL210/-44C FL250 240/120 FL230 230/ 80 FL210 220/ 30 ---------- DESCENT FORECAST ---------ALT WIND DIR/SPD FL210 180/ 30KT 17000 170/ 20KT 13000 150/ 10KT 9000 120/ 5KT

• Option available for FMC printer interface • FMC prints uplinked and downlinked ATC messages
• FMC interfaces with an ARINC 740, 744 or 744A printer

1/3

A CT R TE 1 OR IGIN

DEST

K MW H

K B FI

FLT NO

RUN WA Y

R W 13R

AB 345 CO ROUTE

REQUEST

<SEN D

B F IM W H

REPORT

<SEN D ROUTE

< P R IN T

R TE C O PY> - - - - - - - - - - - - A L TN > OFFSE T

- - -

< IN D E X INIT REF

RTE

CLB

CRZ

DES

BRT

---------- RTA FIX/TIME -------------YKM/1329.1Z --------- ALTERNATE AIRPORTS --------KRNT 1335Z 132.2 KSEA <SEL> 1333Z 130.2 KPDX 1334Z 131.2 KPWT 1336Z 133.2 797-FD-0169C 1-19-2-whp/CF

Options 4 —Flight Management Computer System 767-200ER/-300ER GPS and NDB Approaches

• Option available for selection of FMC nondirectional radio beacon (ADF) approaches in the NAV database • Separate option available for selection of FMC GPS “nonprecision” approaches in the NAV database

KBLI ARRIVALS S TA R S

<SEL> GPS34 ILS16 NDB16 R UNW AYS

16
RTE

TUBTY INTC>

CLB

CRZ

DES

BRT

APPRO A C H E S

TUBTY

170 / 3100

345 ˚

5 NM 170 / 2200 G P 3.00˚

OHADO 345 ˚

5 NM

RW34

155 / 0050


RTE DATA>

INIT REF

NDB and GPS approaches are selected on arrivals page on MCDU

GPS16

1/1

5 NM

345 ˚

A P P R OACHES

- NONE -

INIT REF

ACT RTE 1 LEGS

1/2

RTE

CLB

CRZ

DES

GPS final approach and any approach with a specified vertical angle (on which the VNAV approach path is based) results in display of angle on RTE LEGS page BRT

797-FD-0171 C 1-19-2-MT/CF

Options 4 —Flight Management Computer System 767-200ER/-300ER Flight Path Angle—Vertical Bearing—Vertical Speed

3 / 3

AC T D E S E / D

A T

AT

E C O N

N OLLA

2200A

2200 RW13R

• Flight path angle • Actual

S P D

• Vertical bearing

320 SP D T R A N S

W P T / A L T

NOLL A / 2200

240 / 10000 FPA

SP D REST R

V / B

V / S

2.9 3.1 1754 - --/- - - - - - - - - - - - - - - - - - - - - - - < OFFPATH

DES

FORECAST> DES DIR>

• To waypoint and altitude in 3R

• Vertical speed • Required to maintain vertical bearing

797-FD-0162C 1-19-2-PW/CF

Options 5 —Communications 767-200ER/-300ER

Feature

Basic

Option

HF Data Link

None

Installation and Activation of HF Data LinkPartial Provisions

8.33 kHz VHF Channel

None

Activation

Spacing

Partial Provisions

SATCOM

None

SATCOM System Installation Partial Provisions

ACARS/Data Link

None

VDL Mode 2/AOA Installation Level 0A CMU InstallationARINC 724B ACARS InstallationPartial Provisions

Voice Mode Protection

None

Provided

Emergency Locator Transmitter (ELT)

None

ELT InstallationPartial Provisions

Pilots Call Panel

PA-in-Use Light not included

PA-in-Use Light included

Boom Microphone Headset Jacks

Two Pin Jacks

Five Pin Jacks

Push to Talk Switch on Glareshield

None

Provided

Cockpit Voice Recorder Monitor Jack

None

Provided

797-FD-0215C 2-25-2-whp

Options 5 —Communications 767-200ER/-300ER Satellite Communications (SATCOM) • Options available for SATCOM system, or partial provisions for SATCOM • SATCOM provides two-way voice/data communication for the flight crew and cabin passengers anywhere in the world covered by INMARSAT global/spot beam • The services include • Flight deck voice, allowing instantaneous communication with Operations, Maintenance and Air Traffic Control • Flight deck data link data communication • 64 kbps circuit mode PC data communication planned for future with AERO-H+ system • A SATCOM installation consists of the following equipment • Avionics equipment — Satellite data unit (SDU) — Radio frequency unit (RFU) – not required on all SATCOM systems — High power amplifier (HPA) • Antenna systems – customers can select either an AERO-H+ or AERO-I system — High-gain antenna (HGA) – AERO-H+ system — Intermediate-gain antenna (IGA) – AERO-I system • Pilot interface — Multipurpose control and display unit (MCDU) – basic feature – no option required — Audio control panel (ACP) – basic feature — EICAS (communication messages) – basic features – no option required

797-FD-0033 1-19-02-PW/DD

Options 5 —Communications 767-200ER/-300ER Satellite Communications (SATCOM) INMARSAT 3

L-band digital link 1.5/1.6 GHz

RF C-band 4/6 GHz

Airborne earth station (AES)

Ground earth station (GES)

• PSTN - Publish switched telephone network • PSTDN - Publish switched telephone data network • Private networks • Aeronautical fixed network (AFTN, CIDN, SITA, ATN)

Airline operational control (AOC) or air traffic control (ATC)

Service provider network 797-FD-0034 1-19-02-whp/DD

Options 5 —Communications 767-200ER/-300ER Data Link • Data link provides a high-speed digital data transmission between the airplane and ground facilities. By transmitting and receiving data automatically, without the flight crew intervening, data link reduces flight crew workload. Pilots use the MCDU or an optional MIDU to interface with the data link system. Data link is used to exchange airline operations information and airplane operating data. • Options are available for installation of a flight deck printer. • Options are available for airline operational control data link (AOC DL) and air traffic services data link (ATS DL). See FMC system options 4 for further information on these optional features. • Three levels of data link provisions/installations are available: ARINC 724B ACARS, ARINC 758 level 0A, and ARINC 758 VDL mode 2/AOA. ARINC 724B ACARS • ARINC 724B aircraft communications addressing and reporting system (ACARS) transmits character-oriented data at 2.4 kbits/second. The modem, converting data to/from VHF sound transmission, is contained in the ACARS management unit. • The following options are required for ARINC 724B ACARS operations: • Partial provisions for a single ARINC 724B ACARS management unit. • Installation of an ARINC 724B ACARS management unit into partial provisions.

797-FD-0035C 1-19-02-PW/DD

Options 5 —Communications 767-200ER/-300ER Data Link ARINC 758 level 0A data link • Level 0A data link transmits character-oriented data at 2.4 kbits/second. The modem is contained in the communications management unit (CMU). • The following options are required for level 0A data link operation. • Partial provisions for a single ARINC 724B ACARS management unit • Limited partial provisions for dual ARINC 758 CMUs compatible with existing single ARINC 724B ACARS provisions • Installation of an ARINC 758 CMU into partial provisions ARINC 758 VDL mode 2/AOA data link • VDL mode 2/AOA (VHF data link mode 2/aircraft communications addressing and reporting system over aviation VHF link control) transmits high-speed character-oriented data at 31.5 kbits/second to suitably equipped ground stations. VDL model 2/AOA transmits character-oriented data at 2.4 kbits/second to ground stations not equipped for VDL mode 2/AOA high-speed data. The modem is contained in the VHF data radio transceivers (VDR). • The following options are required for VDL mode 2/AOA operation. • Partial provisions for a single ARINC 758 CMU. Partial provisions are also available for dual ARINC 758 CMUs to provide a possible future installation of a second CMU • Installation of an ARINC 758 CMU into partial provisions • Installation of ARINC 716/750 capable VHF data radio (VDR) transceivers

797-FD-0036C 1-19-02-PW/DD

Options 5 —Communications 767-200ER/-300ER - Data Link Installations ARINC 724B ACARS with dual ARINC 758 CMU provisions

Level 0A data link with single ARINC 724B, ACARS MU provisions, and dual ARINC 758 CMU provisions

CMU

ACARS

Left tray ARINC 758

Left tray ARINC 758

Right tray ARINC 724B

Right tray ARINC 758

APM ARINC 716 VHF wiring 429 bus

ARINC 758 CMU wiring

1 VHF

429 bus

ARINC 724B ACARS wiring

ARINC 716 VHF wiring

ARINC 724B ACARS wiring

429 bus

429 bus

3 VDRs

ARINC 758 CMU wiring

ARINC 758 CMU wiring

ARINC 758 CMU wiring

Other airplane systems

Other airplane systems

VDL mode 2 / AOA data link with dual ARINC 758 CMU provisions

CMU

Left tray ARINC 758

Right tray ARINC 758

APM

429 bus

429 bus

3 VDRs ARINC 758 CMU wiring

ARINC 758 CMU wiring

Other airplane systems

797-FD-0037C 1-19-02-whp/DD

Options 5 —Communications 767-200/767-300 - VDL Mode 2/AOA Architecture Data Link Air

Ground VDL mode

Interface systems: • FMC • ACMS • Printer

CMU

VDL ground network

Airline operational control (AOC)

ACARS ground network

ATC

VDR

ACARS • VDL mode 2/AOA data link interface with VDL mode 2/AOA ground stations and conventional ACARS ground stations

797-FD-0038C 1-19-02-whp/DD

Options 6 —Avionics 767-200ER/-300ER Feature Data Loader Printer ACMS - Expanded Engine Parameter Recording MIDU (Multipurpose Interactive Display Unit) Engine out Takeoff Thrust Operation

Basic Airborne Data Loader None Basic Parameters None Five Minutes

Option Portable Data Loader Connector ARINC 744 PrinterARINC 740 Printer Basic and Expanded Parameters Provided Ten Minutes

ECS Temperature Indications

Celsius

Fahrenheit

Instrumentation Display Units

English units

Metric units

Navigation Systems Feature Metric Altimeters

Standby Attitude Indicator Weather Radar System EGPWS Peaks & Obstacles

Basic None

Backcourse Switch Included Single System Inhibited

Option Two Metric Altimeters with Digital Display One Metric Altimeter with Analog DisplayTwo Metric Altimeters with Digital Display and One Metric Altimeter with Analog Display Backcourse Switch Deactivated Dual System Single System with Auto-Tilt Dual System with Auto-Tilt Enabled

EGPWS Altitude Callout Volume

Standard Volume

Low Volume

EGPWS "Smart 500" foot Callout

Inhibited

Enabled

EGPWS Altitude Callouts

Inhibited

Many options available

797-FD-0216C 2-25-2-whp

Options 6 —Navigation Systems 767-200ER/-300ER Peaks and Obstacles • Option provides for the display of man-made obstacles on the EHSI when an obstacle is contained in the Enhanced Ground Proximity Warning Computer (EGPWC) terrain database and a conflict is identified. Aural and visual caution and warning alerts are provided.

8.8 NM

TRK

194

18

“CAUTION CAUTION OBSTACLE CAUTION OBSTACLE OBSTACLE”

1717.1Z 21

15

Speaker Speaker

M

24

10

Amber for caution Red for warning

OBSTACLE

TERR

797-FD-0029 2-26-2-WHP/CF

Options 6 —Navigation Systems 767-200ER/-300ER EGPWS Peaks and Obstacles Peaks Display

8.8 NM

TRK

194 M

18

•

Provides a “look down” to the highest terrain ahead of the airplane

•

Displays terrain

•

Displays terrain altitudes

•

Blends with normal terrain colors when flying near terrain altitude

•

Peaks display when more than 2,000 feet above terrain

1717.1Z

24

10

Height of surrounding terrain

Peaks and obstacles is an optional feature of the EGPWS

21

15

Highest peak

•

TERR 144 050

797-FD-0030 2-26-2-whp/CF

Options 7 —Crew Accommodations 767-200ER/-300ER

Flight Deck Accommodations Feature Captain's and First Officer's Seats First Observer's Seat Second Observer's Seat Sun Visors

Basic Manually Operated Seats Wall Mounted None Standard Sun Visors

Option Power Operated Seats Track Mounted Provided Roller Sunshades and improved Sun Visors

Portable Breathing Equipment

None

Provided

Flight Deck Flashlights

None

One Flashlight with ShieldTwo Flashlights Two Flashlights with Shield

Emergency Evacuation Signal System

None

Provided

797-FD-0217C 2-26-2-whp

Options 7 —Crew Accomodations 767-200ER/-300ER • Powered IPECO Captain’s and First Officer’s seats • Second Observer’s station (not available on 767 Freighter) • Track-mounted First Observer’s seat (basic on 767 Freighter)

First Officer’s tiller wheel

• Flashlights • Protective breathing equipment • Emergency evacuation signal system • First Officer’s nose wheel steering tiller (not available on 767 Freighter)

Second Observer’s seat • Two headphone jacks • Oxygen mask • Life vest • Audio selector panel (optional)

797-FD-0177C 2-26-2-whp

Options 8 —Airframe Systems 767-200ER/-300ER

Feature

Basic

Option

Bulk Cargo Heating and Ventilation

None

Provided

Catalytic Converters for Ozone Control

None

Provided

APU - Additional Starting Capability

None

Provided

Duct Leak Detection System

Single Loop System

APU Fire Extinguisher Bottle

Single Standard APU Bottle

Dual Loop System (PW & GE engines only) Single APU Bottle, common with Engine fire bottlesDual Standard APU BottlesDual APU Bottles, common with Engine fire bottles

Ice Detection

None

Advisory Ice DetectionAutomatic Anti-Ice System

APU Hour Meter

None

Provided on Flight Deck Provided in E/E Bay

APU Cycle Meter

None

Provided on Flight Deck Provided in E/E Bay

797-FD-0218C 2-25-2-whp

Acronyms and Abbreviations ACARS ACMS ADC ADF ADL AFDS A/G ALTN AOA A/P APU ASP ATC AUX BFE BITE CONF CRT DME EADI ECS E/E EEC EFIS EGPWS EGT EHSI EICAS ELEC ENG EXCD EPCS EPR ER ETOPS FADEC FCC F/D FMC FPR GA GMT GPS GS HDG HMG HYD

– Aircraft communications addressing and reporting system – Airplane condition monitoring system – Air data computer – Automatic direction finder – Airborne data loader – Autopilot/flight director system – Air-ground – Alternate – Angle of attack – Autopilot – Auxiliary power unit – Audio selector panel – Air traffic control – Auxiliary – Buyer-furnished equipment – Built-in test equipment – Configuration – Cathode ray tube – Distance measuring equipment – Electronic attitude director indicator – Environmental control system – Electrical/electronic – Electronic engine control – Electronic flight instrument system – Enhanced ground proximity warning system – Exhaust gas temperature – Electronic horizontal situation indicator – Engine indication and crew alerting system – Electrical – Engine exceedance – Electronic propulsion control system – Engine pressure ratio – Extended range – Extended-range twin-engine operations – Full-authority digital engine control – Flight control computer – Flight director – Flight management computer – Flight plan request – Go-around – Greenwich mean time – Global positioning system – Ground speed – Heading – Hydraulic motor generator – Hydraulics

IAS ILS IRS LAT/LON LNAV LRC LRU MASI MCDP MCDU MCP MMR MSG OVRD PA PERF PLI PWS QAR RA RAT RDMI RTO RVR SAT SATCOM SEL SELCAL SID STAR STBY TAI TAS TAT TCAS TMC TMSP TO TRK VHF VNAV VOR VSI WEU WPT WXR

– Indicated airspeed – Instrument landing system – Inertial reference system – Latitude/longitude – Lateral navigation – Long-range cruise – Line replaceable unit – Mach/airspeed indicator – Maintenance control and display panel – Multifunction control display unit – Mode control panel – Multi-mode receiver – Message – Override – Passenger address – Performance – Pitch limit indicator – Predictive windshear system – Quick access recorder – Resolution advisory (or radio altimeter) – Ram air turbine – Radio distance magnetic indicator – Refused takeoff – Runway visual range – Static air temperature – Satellite communications – Standby engine indicator – Selective calling – Standard instrument departure – Standard terminal arrival route – Standby – Thermal anti-ice – True airspeed – Total air temperature – Traffic alert and collision avoidance system – Thrust management computer – Thrust mode select panel – Takeoff – Track – Very high frequency – Vertical navigation – Very high frequency omni range – Vertical speed indicator – Warning electronics unit – Waypoint – Weather radar 797-FD-0178C 1-19-2-whp/CF