Embraer 175
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E-JETS FAMILY – EMBRAER 175
E-JETS FAMILY
170
175
SPECIFICATIONS WEIGHTS Maximum Takeoff Weight
STD & LR Versions STD
82,673 lb
37,500 kg
LR
85,517 lb
38,790 kg
Maximum Landing Weight
74,957 lb
Maximum Zero Fuel Weight Basic Operation Weight
AR Version 89,000 lb
40,370 kg
34,000 kg
75,178 lb
34,100 kg
69,887 lb
31,700 kg
70,548 lb
32,000 kg
47,664 lb
21,620 kg
47,708 lb
21,640 kg
Maximum Payload
22,223 lb
10,080 kg
22,840 lb
10,360 kg
Maximum Fuel*
20,580 lb
9,335 kg
20,580 lb
9,335 kg
*Fuel Density: 0.803 kg/l (6.70lb/gal)
PERFORMANCE (AR Version) Maximum Operating Speed
M 0.82
M 0.82
Time to Climb to FL 350, TOW for 500 nm
18 min
18 min
Takeoff Field Length, ISA, SL MTOW
7,362 ft
2,244 m
Takeoff Field Length, ISA, SL TOW to 500 nm
4,137 ft
1,261 m
Landing Field Length, ISA, SL MLW
4,278 ft
1,304 ft
2,000 nm
3,706 km
Range 78 PAX @ 220 lb (100 kg), LRC
VIEWS
31 ft 11 in (9.73 m)
103 ft 11 in (31.68 m)
31 ft 11 in (9.73 m)
103 ft 11 in (31.68 m)
31 ft 11 in (9.73 m)
EXTERNAL DIMENSIONS Wingspan
32 ft 10 in (10.00 m)
85 ft 4 in
26.00 m
Length Overall
103 ft 11 in
31.68 m
Height Overall
31 ft 11 in
9.73 m
Horizontal Stabilizer Span
32 ft 10 in
10.00 m
Fuselage Width
9 ft 11 in
3.01 m
Fuselage Height
11 ft 0 in
3.35 m
69 ft 7 in
21.20 m
Cabin Width (at armrest)
9 ft 0 in
2.74 m
Cabin Height
6 ft 7 in
2.00 m
Aisle Width
19.75 in
0.50 m
Seat Width
18.25 in
0.46 m
103 ft 11 in (31.68 m)
32 ft 10 in (10.00 m)
85 ft 4 in (26.00 m)
32 ft 10 in (10.00 m)
INTERNAL DIMENSIONS Cabin Length (excluding cockpit)
85 ft 4 in (26.00 m)
85 ft 4 in (26.00 m)
June 2007
EMBRAER 175
190
195
E-JETS FAMILY – EMBRAER 175
A NEW CABIN CONCEPT
PERFORMANCE
A double-bubble fuselage design means passengers enjoy an extraordinary amount of personal space. The widest seat and the widest aisle in the category add to passenger comfort. Four-abreast seating eliminates the undesirable middle seat, easing access and making boarding and deplaning smoother and faster.
Short field capability, superior hot and high performance, and 2,000 nm range combine to deliver maximum operational versatility. PAYLOAD
(kg) 12,000
AR
10,000
LR 88 PAX @ 100 kg
8,000
Carry-on Bag Size 24 x 16 x 10 in 61 x 40 x 25 cm
30.80 in 0.78 m
EMBRAER 175 INTERIOR LAYOUTS SINGLE CLASS 78 seats at 32” pitch
20,000
78 PAX @ 100 kg
15,000
4,000
Pilot workload is reduced and aircraft performance is optimized with integrated flight control systems guided by fly-by-wire technology. FBW and 100% cockpit commonality minimize crew transition costs between any aircraft in the E-Jets family.
25,000
STD
6,000
FLY- BY- WIRE (FBW)
(lb) 30,000
10,000
2,000
5,000 0
0 0
500
1,000 1,500 2,000 2,500 3,000 RANGE (nm)
FADEC-controlled diagnostics, fully
SINGLE CLASS 86 seats at 31” pitch 11 ft 0 in 3.35 m
4 ft 9 in 1.44 m
39˚
COCKPIT
ENGINE
6 ft 7 in 2.00 m
18.25 in 0.46 m
ASSUMPTIONS Typical Mission Reserves - Cruise at M 0.78 - Passengers @ 100 kg (220 lb) each
interchangeable right and left engines,
ECONOMICS
environmental enhancements, and 30-
The cost-effective use of the latest technologies makes the EMBRAER 175 the most efficient aircraft available in the 78 to 88 seat segment. The best structural efficiency, excellent fuel burn, and outstanding aircraft maintainability characteristics provide significant cost advantages to airlines.
minute LRU replacement efficiency make General Electric’s CF34-8E the most comprehensive, value-added propulsion system in the industry. Engine Characteristics GE CF34-8E
HIGH CAPACITY 88 seats 30” pitch 3 ft 1 in 0.94 m
19.75 in 0.50 m
9 ft 0 in 2.74 m 9 ft 11 in 3.01 m
DUAL CLASS 78 seats (6F/72Y) at 38”/31” pitch
Sea Level Flat Rating 86F/30C APR Thrust - Installed
14,200 lb
NTO Thrust - Installed
13,800 lb
Length
121.2 in / 307.8 cm
Weight - Dry Engine
2,627 lb / 1,192 kg
Maximum Diameter
53.4 in / 136 cm
03. Cursor Control Device (CCD)
Thrust-to-Weight Ratio
5.41
04. EICAS
Control
05. Integrated
Fan Bypass Ratio
5:1
Electronic
Display Unit (MCDU)
Noise
Stage III and IV Compliant
Standby System 12. Engine Panel (IESS) 13. Ram Air Turbine
01. Audio Control Panel 02. Speed Brake
09. Primary Flight Display (PFD) 10. Multi-Function Display (MFD)
BREAK-EVEN*
58%
11. Multi-Function
06. Lights Panel
14. Flap
07. Guidance Panel
15. Thrust Lever
PROFIT
08. Landing Gear
Based on Total Operation Costs; 500 sm sector
*
E-JETS FAMILY
170
175
SPECIFICATIONS WEIGHTS Maximum Takeoff Weight
STD & LR Versions STD
82,673 lb
37,500 kg
LR
85,517 lb
38,790 kg
Maximum Landing Weight
74,957 lb
Maximum Zero Fuel Weight Basic Operation Weight
AR Version 89,000 lb
40,370 kg
34,000 kg
75,178 lb
34,100 kg
69,887 lb
31,700 kg
70,548 lb
32,000 kg
47,664 lb
21,620 kg
47,708 lb
21,640 kg
Maximum Payload
22,223 lb
10,080 kg
22,840 lb
10,360 kg
Maximum Fuel*
20,580 lb
9,335 kg
20,580 lb
9,335 kg
*Fuel Density: 0.803 kg/l (6.70lb/gal)
PERFORMANCE (AR Version) Maximum Operating Speed
M 0.82
M 0.82
Time to Climb to FL 350, TOW for 500 nm
18 min
18 min
Takeoff Field Length, ISA, SL MTOW
7,362 ft
2,244 m
Takeoff Field Length, ISA, SL TOW to 500 nm
4,137 ft
1,261 m
Landing Field Length, ISA, SL MLW
4,278 ft
1,304 ft
2,000 nm
3,706 km
Range 78 PAX @ 220 lb (100 kg), LRC
VIEWS
31 ft 11 in (9.73 m)
103 ft 11 in (31.68 m)
31 ft 11 in (9.73 m)
103 ft 11 in (31.68 m)
31 ft 11 in (9.73 m)
EXTERNAL DIMENSIONS Wingspan
32 ft 10 in (10.00 m)
85 ft 4 in
26.00 m
Length Overall
103 ft 11 in
31.68 m
Height Overall
31 ft 11 in
9.73 m
Horizontal Stabilizer Span
32 ft 10 in
10.00 m
Fuselage Width
9 ft 11 in
3.01 m
Fuselage Height
11 ft 0 in
3.35 m
69 ft 7 in
21.20 m
Cabin Width (at armrest)
9 ft 0 in
2.74 m
Cabin Height
6 ft 7 in
2.00 m
Aisle Width
19.75 in
0.50 m
Seat Width
18.25 in
0.46 m
103 ft 11 in (31.68 m)
32 ft 10 in (10.00 m)
85 ft 4 in (26.00 m)
32 ft 10 in (10.00 m)
INTERNAL DIMENSIONS Cabin Length (excluding cockpit)
85 ft 4 in (26.00 m)
85 ft 4 in (26.00 m)
June 2007
EMBRAER 175
190
195
E-JETS FAMILY – EMBRAER 175
A NEW CABIN CONCEPT
PERFORMANCE
A double-bubble fuselage design means passengers enjoy an extraordinary amount of personal space. The widest seat and the widest aisle in the category add to passenger comfort. Four-abreast seating eliminates the undesirable middle seat, easing access and making boarding and deplaning smoother and faster.
Short field capability, superior hot and high performance, and 2,000 nm range combine to deliver maximum operational versatility. PAYLOAD
(kg) 12,000
AR
10,000
LR 88 PAX @ 100 kg
8,000
Carry-on Bag Size 24 x 16 x 10 in 61 x 40 x 25 cm
30.80 in 0.78 m
EMBRAER 175 INTERIOR LAYOUTS SINGLE CLASS 78 seats at 32” pitch
20,000
78 PAX @ 100 kg
15,000
4,000
Pilot workload is reduced and aircraft performance is optimized with integrated flight control systems guided by fly-by-wire technology. FBW and 100% cockpit commonality minimize crew transition costs between any aircraft in the E-Jets family.
25,000
STD
6,000
FLY- BY- WIRE (FBW)
(lb) 30,000
10,000
2,000
5,000 0
0 0
500
1,000 1,500 2,000 2,500 3,000 RANGE (nm)
FADEC-controlled diagnostics, fully
SINGLE CLASS 86 seats at 31” pitch 11 ft 0 in 3.35 m
4 ft 9 in 1.44 m
39˚
COCKPIT
ENGINE
6 ft 7 in 2.00 m
18.25 in 0.46 m
ASSUMPTIONS Typical Mission Reserves - Cruise at M 0.78 - Passengers @ 100 kg (220 lb) each
interchangeable right and left engines,
ECONOMICS
environmental enhancements, and 30-
The cost-effective use of the latest technologies makes the EMBRAER 175 the most efficient aircraft available in the 78 to 88 seat segment. The best structural efficiency, excellent fuel burn, and outstanding aircraft maintainability characteristics provide significant cost advantages to airlines.
minute LRU replacement efficiency make General Electric’s CF34-8E the most comprehensive, value-added propulsion system in the industry. Engine Characteristics GE CF34-8E
HIGH CAPACITY 88 seats 30” pitch 3 ft 1 in 0.94 m
19.75 in 0.50 m
9 ft 0 in 2.74 m 9 ft 11 in 3.01 m
DUAL CLASS 78 seats (6F/72Y) at 38”/31” pitch
Sea Level Flat Rating 86F/30C APR Thrust - Installed
14,200 lb
NTO Thrust - Installed
13,800 lb
Length
121.2 in / 307.8 cm
Weight - Dry Engine
2,627 lb / 1,192 kg
Maximum Diameter
53.4 in / 136 cm
03. Cursor Control Device (CCD)
Thrust-to-Weight Ratio
5.41
04. EICAS
Control
05. Integrated
Fan Bypass Ratio
5:1
Electronic
Display Unit (MCDU)
Noise
Stage III and IV Compliant
Standby System 12. Engine Panel (IESS) 13. Ram Air Turbine
01. Audio Control Panel 02. Speed Brake
09. Primary Flight Display (PFD) 10. Multi-Function Display (MFD)
BREAK-EVEN*
58%
11. Multi-Function
06. Lights Panel
14. Flap
07. Guidance Panel
15. Thrust Lever
PROFIT
08. Landing Gear
Based on Total Operation Costs; 500 sm sector
*
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