Engineering Procedures Manual And Form Dry.pdf

ENGINEERING PROCEDURES MANUAL

Manual Number :DRY 01

TABLE OF CONTENT Chapter ToC RoR LEP Distribution

Chapter I

Chapter II

Chapter III

Chapter IV

Chapter V

Chapter VI

Chapter VII

Revision : ISSUE

Description Table of Content Record of Revision List of Effective Pages Distribution General Manual Case and Policy Distribution & Revision Reference Page Format Engineering Structural & Responsibility Engineering Chart Technical Services Division Staff Production Planning Control Staff Technical Publication Staff Material Planning Airworthiness Directives & Service Bulletins Background Purpose Responsibilities References Compliance AD or SB Maintenance Program Development Requirement Preparation of Aircraft Inspection and Maintenance Program Revision of Maintenance Program Computerization maintenance, component and inventory status maintenance record and control Introduction Responsibility Maintenance Record Filing Procedures Maintenance Record Preservation and Retrieval Requirements Record Keeping System Records Retention Computerized Maintenance, Component and Inventory Status Transfer Record Technical Publication General Responsibilities Technical Publication Control System Technical Publication Status Check Engineering Services General Responsibilities Date : May 10, 2019

ENGINEERING PROCEDURE MANUAL Page ii-iii iv v – vi vii 1-2 1 1 1 2 3-8 3 4 5 7 8 9-14 9 9 9 10 10 15-18 15 15 18 19-24 19 19 19 19 21 21 23 24 25-28 25 25 25 27 29-30 29 29 Halaman :

ii

TABLE OF CONTENT Chapter VII FORM DRY-100 DRY-101 DRY-102 DRY-103 DRY-104 DRY-105 DRY-106 DRY-107 DRY-108 DRY-109 DRY-110 DRY-111 DRY-112A DRY-112B DRY-113A DRY-113B DRY-114 DRY-115 DRY-117 DRY-119 DRY-120 DRY-121

Revision : ISSUE

Engineering Order Engineering Instruction Engineering Form List Manual Change Request Engineering Order Engineering Justification Engineering Instruction Job Card Work Report Daily Report Maintenance Discrepancies Report List Aircraft Monthly Report Technical Publication Status Report Inspection Sheet Task Card Weight and Balance C402B Weight and Balance BAe ATP Swing Compass Cessna 402 Swing Compass Cessna BAe ATP Aircraft Status Publication Transmittal Borescope Inspection Report Material Requesition Maintenance Log Book 402 Maintenance Log Book ATP

Date : May 10, 2019

ENGINEERING PROCEDURE MANUAL 29 29 1-2 1-3 1-3 1-2 1-2 1-2 1-2 1-2 1-2 1-2 1-2 1-2 1-4 1-4 1-4 1-4 1-2 1-2 1-2 1-2 1-3 1-3

Halaman :

iii

RECORD OF REVISON

No.

Revision No

Issued date

1

Issue

May 2019

ENGINEERING PROCEDURE MANUAL

Inserted By

2 3 4 5 6 7 8 9 10 11 12 13 14 15

Revision : ISSUE

Date : May 10, 2019

Halaman :

iv

DISTRIBUTION LIST

ENGINEERING PROCEDURE MANUAL

DISTRIBUTION LIST OF TRAINING PROCEDURE MANUAL NO 1 2 3 4 5 6 7 8 9 10

DISTRIBUTION MAINTENANCE MANAGER DGCA PRESIDENT DIRECTOR CHIEF INSPECTOR QUALITY, SAFETY AND SECURITY MANAGER

HARDCOPY NO. MASTER 01 02 03 04 05 06 07

Noted : 1. Distribution of each manual shall be registered in the Distribution List of each manual. The Engineering Procedures Manual shall be distributed to all personnel involved and responsible for Engineering Departmenty activities as the Controlled Copy. Other personnel may obtain copy of this Engineering Procedures Manual from Maintenance Manager but will not receive the revisions. “Uncontrolled Copy” stamp will be provided in the selected pages manual copy. 2. Softcopy will be uploaded on google drive with PDF format file, All technical personnel have been able to access this EPM, as is Controlled Copy Manual, if it has been downloaded it will be “uncontrolled copy”.

Revision : ISSUE

Date : May 10, 2019

Halaman :

vii

CHAPTER I GENERAL INFORMATION

ENGINEERING PROCEDURE MANUAL

1. MANUAL CASE AND POLICY The Engineering Procedure Manual (EPM) EPM is a detailed procedure for the implementation of tasks from engineering which is the technical sub division in charge, the engineering task include Implement the effectives Service Bulletin and Airworthiness Directives to the aircraft that operated by PT.DERAYA a. Develop Maintenance Program that is adopted from the manufacturing maintenance program. b. Record and control all maintenance activities, and input all record into a computerized system to maintain schedule of all maintenance activities. c. Keep all technical file, document and manual, controlling distribution all file, document and manual to other division and PT.DERAYA base. d. Issuing engineering orders if there is work to be done or can only be done by an approved maintenance organization e. Issuing engineering instruction if any service bulletin (SB) are issued by manufacture or airworthiness directives (AD) issued by local authority, analysis the method and requirement to implement SB or AD to the aircraft, Inform to technical manager and all sub ordinates if any defect and what should be done for next progress. 2. DISTRIBUTION AND REVISION Copies of this program are held by Maintenance Manager and Quality Assurance, to known and maintain all tasks are carried out as procedures that have been made and approved by Quality Assurance PT.DERAYA 3. REFERENCE 1. PT.DERAYA, COMPANY MAINTENANCE MANUAL 2. CASR, 135.380 Maintenance recording requirement 3. SI 8900-3.329 Maintenance Record System Evaluation

Revision : Issue

Date : May 10 , 2019

Halaman :

1

dari

30

CHAPTER I GENERAL INFORMATION

ENGINEERING PROCEDURE MANUAL

4. PAGE FORMAT COMPANY NAME/LOGO

MANUAL NAME

CHAPTER TITLE

CHAPTER I GENERAL INFORMATION

ENGINEERING PROCEDURE MANUAL

Revision identifier, on right side of the paragraph if any

Revision : ISSUED Revision Number

Revision : Issue

Date : April , 2019 Revision Date

Date : May 10 , 2019

Halaman :

2

dari

2

Page Number

Halaman :

2

dari

30

CHAPTER II : ENGINEERING STRUCTURE & RESPONSIBILITY

ENGINEERING PROCEDURE MANUAL

1. Engineering Chart MAINTENANCE MANAGER

3. 4.

TZ

CHIEF LINE MAINT

5.TECHNICAL SERVICES CHIEF

CHIEF WGS

C - LM

C - EP

C-WGS

6. 7.

CHIEF STORE C - STR

STAFF TECH PUBLICATION

STAFF – TECH PUB

STAFF PRODUCTION PLANING CONTROL STAFF – PPC

STAFF MATERIAL PLANING

7E

STAFF – MP

Note :

Revision : ISSUE

: subordinates : coordination

Date : may 10, 2019

Halaman :

3

dari

30

CHAPTER II : ENGINEERING STRUCTURE & RESPONSIBILITY

ENGINEERING PROCEDURE MANUAL

2. TECHNICAL SERVICES DIVISION Title : CHIEF TECHNICAL SERVICES Occupation Code : C – EP Responsible : MAINTENANCE MANAGER (TZ) A. Subordinates Staff Technical Publication Staff PPC Staff Material Planning B. Main Task The Chief Technical Division accountable to manage and to supervise of the production planning Control, technical publication and material planning activities in the company; in order to achieve the standardization of maintenance procedures and practices in accordance with the CASR and Company Maintenance Manual (CMM) rules, regulations and its standard practices. To analyze performance and improve maintenance procedures in coordination with Chief Inspector (QA). C. Job Description and Responsibility  Making work planning of aircraft maintenance support annually.  Making plan proposal of the technical material unit annually.  Coordinating completion of economic order quantity, re-order level and service level of the material.  To assist and conduct direct supervision to all personnel assigned in production planning and control.  To establish the company fleet maintenance planning and monitor its implementation.  Revising and evaluate MP, customize the aircraft maintenance program from manufacturer, and the latest regulations. Monitor all the updating and distribution of all manual, to the relevant sections and base operations area (outside base operation).

Revision : ISSUE

Date : may 10, 2019

Halaman :

4

dari

30

CHAPTER II : ENGINEERING STRUCTURE & RESPONSIBILITY

ENGINEERING PROCEDURE MANUAL

 To develop aircraft maintenance scheduling, power plant, and its component and continually generated adjustment due to change in actual aircraft utilization and unexpected maintenance.  To review and update the computer run status report and distribute them to related department and maintenance bases.  To request all pre-inspection projected items for maintenance prior schedule event.  To request items for modification or technical directive compliance prior to schedule event.  To coordinate with maintenance for manpower scheduling at out bases as required.  To prepare and distributed a report of aircraft daily status and monthly report must be ready every 5th day of current month.  To maintain complete technical record in a proper correlation, including the following : 

Aircraft, Engine, Propeller, Flight and Maintenance Log Book, and other related record



Inspection and repair records of aircraft, engine and component



Optional and mandatory modification records



Technical Directive Compliance records



Overhaul records



Release certificate



Accident / Incident records.

 Enforce

all

general

and

departmental

safety

rules

and

regulations.  Conduct the safety program as prescribe on CMM. 3. STAFF PRODUCTION, PLANING & CONTROL

Revision : ISSUE

Title

: STAFF PPC

Occupation Code

: STAFF – PPC

Responsible

: CHIEF TECHNICAL SERVICES (C – EP) Date : may 10, 2019

Halaman :

5

dari

30

CHAPTER II : ENGINEERING STRUCTURE & RESPONSIBILITY

ENGINEERING PROCEDURE MANUAL

A. Main Task The PPC staff accountable to manage and to supervise of the production planning Control activities in the company; in order to achieve the standardization of maintenance procedures and practices in accordance with the CASR and Company Maintenance Manual (CMM) and MP, regulations and its standard practices. B. Jobs Description and Responsibilities  Planning annual production activity for aircraft long term maintenance activity covering hangar space plan, shop and load plan, labor calculating plan, job time frame and task time plan.  Controlling availability of net work plan, and human resources and controlling aircraft inspection activity in line with Service Bulletin, Technical Instruction, and Modification Instruction.  Routine controlling of scheduling and routing of the fleet in line with flight net work and route structure.  Collecting production data by aircraft log books, engine log books, propeller log books and all aircraft document to improve quality and efficiency of product.  Issuing Aircraft status, DMIL, Major Component Report, Job Card, Task Card routinely.  Monitor the implementation of all work or inspections being or will be carried out by line maintenance, always communicate with line maintenance about the schedule, personal and administration of jobs.  Monitor implementation in Line Maintenance Inspection, Main base, or outside base station, monitoring the implementation of Job Cards that have been issued by PPC.

Revision : ISSUE

Date : may 10, 2019

Halaman :

6

dari

30

ENGINEERING PROCEDURE MANUAL

CHAPTER II : ENGINEERING STRUCTURE & RESPONSIBILITY 4. STAFF TECH. PUBLICATION Title

: STAFF TECHNICAL PUBLICATION

Occupation Code : STAFF – TECH.PUB Responsible

: CHIEF TECHNICAL SERVICES (C – EP)

A. Main Task The Technical Publication staff accountable to manage Technical Publication activities in the company; in order to achieve the standardization

of

maintenance

procedures

and

practices

in

accordance with the CASR and Company Maintenance Manual (CMM) rules, regulations and its standard practices. B. Jobs Description & Responsibilities  Reporting and controlling the budget of Engineering Section efficiently and effectively.  Maintaining a comprehensive administration system of incoming, keeping, maintenance, reproduction, distribution, service bulletin, service letter, airworthiness directive, etc.  Arranging the acquisition of manuals and technical literature in sufficient amount for all maintenance bases throughout all company operational regions.  Implement updating, revision and distribution of all aircraft manuals and company manuals to all departments / sections that need, including the main base and out base operations , make a listing of updates, revisions and distributions all manuals and is stored in the file, and report the update, revision and distribution to Chief Engineering and PPC.  Arranging publication and distribution of engineering information, instructions to related units.  Controls the aircraft manually updating all aircraft in the company, and always communicate with the vendor manually update the status of these manuals. Revision : ISSUE

Date : may 10, 2019

Halaman :

7

dari

30

ENGINEERING PROCEDURE MANUAL

CHAPTER II : ENGINEERING STRUCTURE & RESPONSIBILITY

 Monitor all technical manuals available in publications, and monitor all the manuals that exist in the area of operations, as well as constantly monitor the status updates manually, so that always controlled the same as in the main base.  Always communicate with aircraft factory operated by the company, in order to always updating the development of aircraft, both in terms of communication service bulletins, service letters, and other information issued by the factory. 5. STAFF MATERIAL PLANING Title

: STAFF MATPLAN

Occupation Code : STAFF – MP Responsible

: CHIEF TECHNICAL SERVICES (C – EP)

A. Main Task The material planning staff is accountable to manage material and part movement in the company; in order to achieve the standardization

of

maintenance

procedures

and

practices

in

accordance with the CASR and Company Maintenance Manual (CMM) rules, regulations and its standard practices. B. Jobs Description & Responsibilities  Planning and controlling major component staggering and replacing of component to achieve production hour oriented.  Controlling availability of material, spare part, and tools, component and engine replacement in line with Service Bulletin, Technical Instruction, and Modification Instruction.  To control the aircraft component due list, and make a report to technical manager with a limitation of minimum of 300 hrs/6 months before lead-time expires.  To coordinate with aircraft maintenance and logistic department to ensure continuous flow of required material to prevent work stoppage. Revision : ISSUE

Date : may 10, 2019

Halaman :

8

dari

30

CHAPTER III : AIRWORTHINESS DIRECTIVE AND SERVICE BULLETIN

ENGINEERING PROCEDURE MANUAL

1. BACKGROUND Airworthiness Directives (AD’s) are issued by the DGCA under the provisions of CASR Part 39 when an unsafe condition exists and that condition is likely to exist or to develop in other aircraft, aircraft engines or appliances of the same type design. AD’s mandate corrective measures that must be accomplished in a specified periods of time. These corrective measures may include one-time inspections, repetitive inspections at specific intervals, prescribed repair actions or modifications which may terminate special requirements of the A.D. To operate an aircraft, engine or appliance to which an A.D. applies, except in accordance with the requirements of the directive, is to be in “noncompliance” with the CASR’s. 2. PURPOSE The purpose of this procedures are to give the guidance for Technical services personnel of scheduling and controlling of applicable Airworthiness Directives or Service Bulletin task for each Aircraft operated by PT. DERAYA that shall be performed in the effort to maintain the continuing Airworthiness of each Aircraft. 3. RESPONSIBILITIES The technical services chief shall be responsible to set-up the maintenance task and scheduling the application of applicable AD or SB for each Aircraft operate by PT. DERAYA, Engineering PPC will coordinate with the Maintenance Manager in the scheduling of the AD accomplishments required. The Material personnel will prepare material if there are material requirements. The accomplishment of AD will be supplied/submit to DGCA by Chief Inspector. If an emergency AD is issued during other than normal working hours (i.e. nights, weekends or holidays) the DGCA will be notified by Engineering / PPC and supply them with a copy of the AD. They will contact the following people. Revision : ISSUE

Date : May 10 , 2019

Halaman :

9

dari

30

CHAPTER III : AIRWORTHINESS DIRECTIVE AND SERVICE BULLETIN

ENGINEERING PROCEDURE MANUAL

A. Maintenance Manager B. The Chief Inspector C. The personnel who directly responsible for the material & store. These individuals will take whatever action is required to facilitate the accomplishment of the Emergency AD. 4. REFERENCES The AD or SB task that applicable to each type of Aircraft operated by PT.DERAYA shall be set in accordance with: Airworthiness Directives issued by the DGCA or the Authority of country of the Manufacture, or Service Bulletin issued by the Manufacture 5. COMPLIANCE AD or SB Each aircraft will have an up-to-date Airworthiness Directive Compliance Record, which will be in a form or manner that contains all of the elements of AD/SB Compliance Form. The AD Compliance summary report may be used to record either compliance of the Aircraft AD/SB or the engine AD/SB. In addition, a record system will be utilized to track Airworthiness Directives, which have a time control or repetitive compliance requirement. a. The AD Compliance Record will be kept as part of the aircraft permanent records. b. The following steps shown below illustrate the routing and review process for all incoming Airworthiness directives.  The DGCA / FAA/ EASA issues the AD.  The Chief Inspector and the Engineering / PPC receive and review the incoming AD for applicability and urgency and then distribute it to the concerned section for further review and implementation.

Revision : ISSUE

Date : May 10 , 2019

Halaman :

10

dari

30

CHAPTER III : AIRWORTHINESS DIRECTIVE AND SERVICE BULLETIN

ENGINEERING PROCEDURE MANUAL

 Effected Department (Operations, Maintenance, etc.) will plan and route applicable AD(s) through the applicable section to obtain timely handling and accomplishment.  Completed AD(s) and associated, required paperwork are reviewed then verified by Chief Inspector for accuracy and completeness.  The completed of accomplishment AD report is forwarded to the Engineering Section where the data is transferred to the Airworthiness Directive Compliance Record  The completed AD is then filed in the aircraft records. c. AD or SB applicable to engines will be treated the same way as the Aircraft AD/SB and the necessary record(s) shall be entered in the engine logbook by Engineering Section. An AD or SB with a time control or repetitive compliance requirement will be tracked in the same manner as an aircraft AD. d. For AD or SB applicable the chief Engineering & PPC issued Engineering Instruction (EI), completed job card and work package include inspection sheet sent to Chief Line Maintenance to perform EI acknowledge by Maintenance Manager and Chief Inspector. e. Compliance of AD or SB will be recorded in the aircraft flight maintenance log and appropriate section of aircraft or engine log books. Technical record will enter all information regarding compliance of AD or SB into a computerized system which may be printed in a form of Airworthiness Directives Compliance Summary Report and ready available for inspection if SB or AD is repetitive.  For any defect found and still on limit given by manufacture Chief Engineering release EI to PPC to reschedule the maintenance Revision : ISSUE

Date : May 10 , 2019

Halaman :

11

dari

30

CHAPTER III : AIRWORTHINESS DIRECTIVE AND SERVICE BULLETIN

ENGINEERING PROCEDURE MANUAL

interval. And also sent the letter to the manufacture competed with A/C Serial Number, Time Since New, Cycle since New, and Date of work complishment  For any defect found and still on limit but need the preventive action Chief Engineering release EI to Chief Line Maintenance to take action of preventive action, Acknowledge by Maintenance Manager to scheduling repairman if any repair needed. And also sent the letter to the manufacture competed with A/C Serial Number, Time Since New, Cycle since New, and Date of work accomplishment  For any defect found and over the limit given by manufacture Chief Engineering follow the instruction state on SB or AD, if any replacement required, Chief Engineering send request the part and material needed to Material Planning Control to be forwarded to procurement department. The next step made a plan for replacement including prepare the material, man power, time frame for

scheduling

any

engineer

and

repairman.

After

the

accomplishment of replacement, Chief Engineering should sent the mail to the aircraft manufacture competed with A/C Serial Number, Time

Since

New,

Cycle

since

New,

and

Date

of

work

accomplishment. f. Instructions for filling out the Airworthiness Directive Compliance Record are as follows.  Enter Aircraft Registration.  Enter Aircraft Serial Number.  Enter Aircraft model.  Enter Aircraft manufacturer.  Enter AD Number. Revision : ISSUE

Date : May 10 , 2019

Halaman :

12

dari

30

CHAPTER III : AIRWORTHINESS DIRECTIVE AND SERVICE BULLETIN

ENGINEERING PROCEDURE MANUAL

 Enter repetitive interval (if not applicable, enter NA).  Enter date of current revision, if applicable  Enter date AD was accomplished.  Enter Aircraft hours when AD was accomplished.  Enter Aircraft cycles (landings) when AD was accomplished.  Enter date AD next due. (If not applicable, enter NA)  Enter aircraft hours AD next due. (if not applicable, enter NA)  Enter aircraft cycles (landings) AD next due. (If not applicable, enter NA)  Enter technical data used to comply with AD (i.e., SB number, manufacturer's maintenance manual reference) Enter initials of individual making entry.  Initials of individual making entry.

Revision : ISSUE

Date : May 10 , 2019

Halaman :

13

dari

30

CHAPTER III : AIRWORTHINESS DIRECTIVE AND SERVICE BULLETIN

ENGINEERING PROCEDURE MANUAL

-Intentionally Left Blank-

Revision : ISSUE

Date : May 10 , 2019

Halaman :

14

dari

30

ENGINEERING PROCEDURE MANUAL

CHAPTER IV : MAINTENANCE PROGRAM DEVELOPEMENT

1. REQUIREMENT Technical services chief will prepare aircraft inspection and maintenance program, in accordance with the following requirements: a. Aircraft inspection and maintenance program is complete, i.e. all inspection and maintenance related publications are incorporated. b. Aircraft inspection and maintenance program is up-to-date, the program is continuously reviewed and revised to incorporate the latest revision of aircraft maintenance manual, issue of airworthiness directive or any other approved technical data. c. Aircraft inspection and maintenance program can be implemented. 2. Preparation of Aircraft Inspection and Maintenance Program The initial step in preparing an aircraft inspection and maintenance program consists of collecting all relevant data, as listed in but not limited to the following: a. Maintenance manual (airframe, engine, propeller & component) b. Illustrated Part Catalogue (airframe, engine, propeller & component) c. Maintenance Program Document d. SB / SIL (airframe, engine, propeller & component) e. AD (airframe, engine, propeller & component). Before proceeding, it should be ensured that all relevant data is up-to-date for the latest revision status.

Revision : ISSUE

Date : May 10 , 2019

Halaman :

15

dari

30

CHAPTER IV : MAINTENANCE PROGRAM DEVELOPEMENT

ENGINEERING PROCEDURE MANUAL

The basis for the aircraft inspection and maintenance program should be the requirements prescribed in the maintenance manual of the airframe, engine, propeller and equipment manufacturer. If the airframe manufacturer recommendations differ from those of the manufacturer of the engine(s) or components, the recommendation of the airframe manufacturer shall prevail. Maintenance recommendations by service information such as service letters, service notices, service instruction etc. are not compulsory, however the Chief engineering & PPC shall review these publications and decide whether or not to include such recommendations in the aircraft maintenance program. Service information indicating a life limit (in hours, calendar time and number of cycle/landings between inspection, test and overhaul) is compulsory and shall be included in the aircraft maintenance program. The Company's Maintenance Program is a compilation of an individual maintenance and inspections.

The Maintenance Program consists of the

following elements:  The applicable of the company aircraft and the current revision of Inspection Program.  The company's aircraft Scheduled Maintenance and inspection Programs, Instructions and procedures for maintenance, preventive maintenance, and servicing (refer to CASR 121.133(b)).  The company’s aircraft Unscheduled Maintenance Program;  The company's aircraft inspection Programs for airframe and engine;  Time limitations (calendar time, operational hours, flight cycles)or standards for determining time limitations for overhauls, inspections, and

Revision : ISSUE

Date : May 10 , 2019

Halaman :

16

dari

30

CHAPTER IV : MAINTENANCE PROGRAM DEVELOPEMENT

ENGINEERING PROCEDURE MANUAL

checks of airframes, engines, propellers, appliances, and emergency equipment.  The company’s aircraft Required Inspection Items Program;  Aircraft Instrument and Avionic bench test interval.  Include the maintenance task and intervals that have been specified as mandatory in approval of the type design shall be identified as such.  Procedures for aircraft refueling, elimination of fuel contamination, fire protection (including electrostatic protection), and supervision and protection of passengers during refueling (refer to CASR 121.135(c)(9)(i) and 135.135(c)(9)(i))  Instructions and procedures for maintenance personnel to follow if confronted with errors or deficiencies in documented maintenance procedures (maintenance manual, work cards, etc.), especially while performing maintenance that requires immediate corrective action to ensure safe practices and Airworthy aircraft. The procedures must include instructions for documenting the error and ensuring the deviation or corrections are validated and acceptable to the DGCA.  Airworthiness inspections, including instructions covering procedures, standards, responsibilities, and authority of inspection personnel.  Method & procedures for maintaining the aircraft’s weight & center of gravity within approved limits (ref to CASR 121.135(c)(8), 121.135(d)(7), 135.135(c)(8) & 135.135(d)(7)). Chief Inspector ensures that maintenance; preventive maintenance, repairs and alterations are performed in accordance with the current Maintenance Program, DGCA regulations and the other PT. DERAYA Policies and

Revision : ISSUE

Date : May 10 , 2019

Halaman :

17

dari

30

CHAPTER IV : MAINTENANCE PROGRAM DEVELOPEMENT

ENGINEERING PROCEDURE MANUAL

Procedures Manual. Chief Inspector is responsible for the enforcement and monitoring of the accomplishment of the Maintenance Program. 3. Revision of Maintenance Program Revision of manufacturer’s technical publications or issuance of service information introducing or changing of life limits (in hours, calendar time and number of cycle/landings between inspection, test and overhaul) is compulsory, and therefore the aircraft maintenance program shall be revised accordingly.

Revision : ISSUE

Date : May 10 , 2019

Halaman :

18

dari

30

CHAPTER V : MAINTENANCE RECORD AND CONTROL, COMPUTERIZED MAINTENANCE COMPONENT AND INVENTORY STATUS

ENGINEERING PROCEDURE MANUAL

1. INTRODUCTION This chapter are describes an aircraft, aircraft engine, propeller, components and qualification personnel record system used by the PT. DERAYA The record system procedure and retention enable PT. DERAYA to achieve the maximum value and utilization of its aircraft by documenting proper parts installation a routine / non routine maintenance action. The standards for determining the time limitations of overhaul, inspection, and check of airframes, engines propeller and components including emergency equipment are documented in the maintenance program. 2. Responsibility The Chief Engineering and PPC is responsible for maintaining all maintenance record in the proper manner and in accordance with the requirement of CASR. PPC and technical publication responsible to keep all the records. 3. Maintenance Record Filing Procedures. a. All record of maintenance performance of each aircraft shall be filed in a folder. b. Each folder shall have clear identification showing the following:  The assigned number of the folder.  Description of the document filed.  The date of filing.  The retention time required c. Each folder shall have to be recorded in the file Log Book for easy to retrieve and control. 4. Maintenance Record Preservation and Retrieval Requirements Deraya maintain suitable system that provides for preservation and retrieval of information

Revision : ISSUE

Date : May 10, 2019

Halaman :

19

dari

30

CHAPTER V : MAINTENANCE RECORD AND CONTROL, COMPUTERIZED MAINTENANCE COMPONENT AND INVENTORY STATUS

ENGINEERING PROCEDURE MANUAL

The following records shall be kept for the specified periods a. All the records necessary to show that all requirements for the issuance of a maintenance release under CASR Part 135 have been met. b. A description of reference to data of the work performed. c. Records of all other maintenance work that Deraya done, identifying by name and number of the licensed engineer who performed or supervised the work, and the Inspector of that work. d. Records containing the following information:  The total time in service of the airframe.  The total time in service of each engine and propeller.  The current status of life-limited parts of each airframe, engine, propeller, and appliance.  The time since last overhaul of all items installed on the aircraft which are required to be overhauled on a specified time basis.  The identification of the current inspection status of the aircraft, including the time since last inspections required by the inspection program under which the aircraft and its appliance are maintained.  The current status of applicable Airworthiness Directives and Service Bulletins including the date and method of compliance, and if the Airworthiness Directives or Service Bulletin involves recurring action, the time and the date when the next action is required.  A list of current alterations to each Airframe, Engine, Propeller, and Appliance. Note: The “time” means calendar time, hours, or cycles as applicable. Revision : ISSUE

Date : May 10, 2019

Halaman :

20

dari

30

CHAPTER V : MAINTENANCE RECORD AND CONTROL, COMPUTERIZED MAINTENANCE COMPONENT AND INVENTORY STATUS

ENGINEERING PROCEDURE MANUAL

5. RECORD KEEPING SYSTEM A. The Record Keeping System assures that adequate and appropriate records are maintained for all work performed on PT. DERAYA aircraft. The retention of records enables the Company to maximize the value and legislation of its assets (aircraft, engines, propeller/rotor, components, appliances, etc.) by documenting proper parts installations, and routine and non-routine maintenance actions. B. The Record Keeping System classifies all records into four retention categories to improve storage and retrieval of data. These categories are: 1) Continuous - These records are continuously updated. Such record reflects to the current aircraft operations at any points in time. 2) Routine – These records may be discarded after 2 years. Except for minor check (before departure, transit check) and AML, CML station copy must be retaining for 24 (twenty four) hours. 3) Repetitive – These records must be retained for 2 (two) years after the item or group (inspection package) is accomplished again. 4) Permanent - This category includes permanent changes to the configuration of an airplane, engine, propeller/rotor, component and appliance. Such records are retained permanently. C. The Record Keeping System assures that records will be filed and stored in such a manner that the records will be readily accessible to authorized auditors and other personnel. The filling and storage system shall promote: ease of retrieval, accessibility, and adequate controls. Technical records which are maintained in the PT. DERAYAin the hard copy and/or soft copy will be secured with adequate security systems and continuous. 6. RECORDS RETENTION Company will retain the following records as follows: a. Aircraft Component Record Revision : ISSUE

Date : May 10, 2019

Halaman :

21

dari

30

ENGINEERING PROCEDURE MANUAL

CHAPTER V : MAINTENANCE RECORD AND CONTROL, COMPUTERIZED MAINTENANCE COMPONENT AND INVENTORY STATUS Item to be filled JOB INSTRUCTION 1. Transit/ Pre flight/ Daily Check sheet 2. Structural Sampling Inspection 3. Airworthiness Directive 4. Aircraft Log Book 5. Engine Log Book 6. Aircraft Maintenance Log 7. Weight and Balance Report 8. Compass Swing Report 9. Major Repair/ Alteration Report form DAAO 43337 10. Test Flight Report 11. Ferry Flight Report 12. Accident/Incident Report 13. Material Airworthiness Tag 14. Work Sheet AIRCRAFT INSPECTION STATUS 1. Time in service record 2. Time in service Last Inspection 3. Schedule Last Inspection 4. Non-Schedule Last Inspection

Routine

Repetitive Permanent

X X X X X X X X X X X X X X

X

X X X

X X X

b. Engine, Propeller/Rotor, Components record Item to be filled 1.

Routine

2.

Overhaul, Check & Hot Section Insp. Inspection record Time Since Last record

3.

Time Remaining to Next Overhaul

4.

Operating time limits record

X

5.

Accumulated hours and cycles record

X

6.

Component History record

X

7.

Strip Report

X

8.

Comp. Serviceable/Airworthiness Tag

X

Repetitive Permanent X X X

X

X X

Note :

Revision : ISSUE

Date : May 10, 2019

Halaman :

22

dari

30

CHAPTER V : MAINTENANCE RECORD AND CONTROL, COMPUTERIZED MAINTENANCE COMPONENT AND INVENTORY STATUS Routine Repetitive Permanent

ENGINEERING PROCEDURE MANUAL

: Time limited records which are maintained. : For work which repeated at specific intervals. : This category includes permanent changes to the configuration of an airplane, engine, propeller/rotor, component and appliance. Such records are retained permanently.

7. COMPUTERIZED MAINTENANCE, COMPONENT AND INVENTORY STATUS. To give the guidance to the Engineering and maintenance personnel of programming, scheduling and controlling of all maintenance of each aircraft operated by Deraya that shall be performed in the effort to maintain the continuing airworthiness of each aircraft. Technical Services chief is delegated by maintenance Manager shall be responsible to setup the Computerized Maintenance, Component and Inventory status. The maintenance and component status shall be used as a reference to setup the maintenance and component program. The computerized program shall be set-up in a manner that could be easily understand and perform by the assigned personnel for application. File and document record that need computerized, consist of: a. Component Status Report. b. Schedule Maintenance. c. Technical Directives Compliance Status Maintenance Status and Component Status shall be issued monthly and any time if required. The monthly report of maintenance and Component Status shall be distributed to: a. Technical Manager b. Chief Inspector QA c. Procurement & Purchasing Manager Revision : ISSUE

Date : May 10, 2019

Halaman :

23

dari

30

CHAPTER V : MAINTENANCE RECORD AND CONTROL, COMPUTERIZED MAINTENANCE COMPONENT AND INVENTORY STATUS

ENGINEERING PROCEDURE MANUAL

d. Finance Manager e. Chief Line Maintenance 8. TRANSFER RECORDS Should the ownership of the aircraft will be change to other party, all relevant original aircraft documents and records of installed components shall be transferred to the new owner at the time of transfer of title or de registration. Should the aircraft de-registration to a foreign country, an Export Certificate of Airworthiness issued by Indonesia DGCA is required. Transfer of maintenance records will take place in two cases: a. Purchase / lease in of an aircraft In the event of purchase / lease – in, assigned person will be checked and verified on behalf of Quality Department at either the aircraft owner’s location or other agreed place before the purchase / lease will take place. b. Sale / lease out of an aircraft. In the event of sale / lease-out, Technical Service will be prepare all relevant and verified by the Inspector before the sale / lease-out will take place. The Engineering / PPC Section are responsible for the coordination of the transfer.

Revision : ISSUE

Date : May 10, 2019

Halaman :

24

dari

30

ENGINEERING PROCEDURE MANUAL

CHAPTER VI : TECHNICAL PUBLICATION

1. GENERAL Technical publication in this context means all documents issued by the manufacturer of the aircraft, aircraft systems and aircraft components or by DGCA when related to technical affairs. For example, such documents are aircraft maintenance manual, flight manual, illustrated part catalogues, service bulletin, airworthiness directive, etc. It is PT. Deraya policy not to allow any person to perform maintenance, preventive maintenance and/or alterations on PT. Deraya aircraft and/or its component unless all required technical publication to support the work are available and up to date. In order to develop and maintain this situation, it must be ensured that the technical publication are at all times in good physical condition, up to date and available where and when they are required. 2. RESPONSIBILITIES a. Technical Services Chief is responsible for proper provision, control and distribution of all technical data required for company’s aircraft maintenance b. Maintenance manager is responsible to ensure that all data under his responsibility is properly maintained and utilized. All deficiencies must be reported to Technical Services & Quality Department. c. Chief Inspector is responsible to ensure that all works on company’s aircraft are performed in accordance with the approved technical data. 3. Technical Publication Control System. Due to the importance of any technical data, all incoming technical data require proper assessment. Many documents, such as revisions to existing documents may be distributed as required. It is important that the revisions

Revision : ISSUE

Date : May 10, 2019

Halaman :

25

dari

30

ENGINEERING PROCEDURE MANUAL

CHAPTER VI : TECHNICAL PUBLICATION

be received at the locations where they are required without delay in order to keep all documents current. Other

documents

requiring

further

action

and

evaluation

such

as

airworthiness directives, service bulletin, service letters, shall be immediately assessed by engineering section Procedures: a. Newly received documents will be registered and introduced into the document control system. A records file will be maintained to provide adequate control of the status of all documents within the organization. b. Valid issues of the applicable documents will be available at those places where work related to the contents of the publications is carried out. Engineering section distributes the documents to those places and transmittal sheet is attached to each document forwarded with Publication Transmittal form (Form DRY-115) c. The Technical transmittal form attached last updated document, the Superseded and/or cancelled documents shall be removed from places where they are in use or to which they were issued, the removed document must be sent back to technical publication. It is the responsibility of the lead engineer or the engineer in charge of each location to ensure that the documents are kept up to date. d. Revisions shall be recorded in the relevant document and on relevant records filling system. It is the responsibility of the engineer to record the revision he had incorporated into the manual. e. Upon completion of revising the publications the engineer will fill out the transmittal sheet, publication transmittals attached to the revision and sign it off to indicate that he had incorporated and recorded the revision into the affected publications. The lead engineer or the engineer in charge is responsible to return the completed transmittal sheet to the engineering section.

Revision : ISSUE

Date : May 10, 2019

Halaman :

26

dari

30

ENGINEERING PROCEDURE MANUAL

CHAPTER VI : TECHNICAL PUBLICATION

f. A periodic document revision status review will be carried out in order to check validity of all copies of documents within the organization. 4. Technical Publication Status Check All technical data kept in the technical library of PT. Deraya are maintained in an up to date status at all times. It is check for current status using information published by individual manufacturer. The information is published regularly and contain information regarding revision status of all technical issued by each manufacturer. It would be the responsibility of the chief engineering to ensure that all technical data kept in the technical library of the company are up to date where as the maintenance manager or lead engineer or engineer in charge is responsible to keep the technical data in his care in an up to date status at all time. Chief engineering will maintain a Publication Status Report FORM DRY-109 sample of such report, which contains records of technical data available at a location. The latest revision status of all technical data will be listed every any new updates of each manual

Revision : ISSUE

Date : May 10, 2019

Halaman :

27

dari

30

ENGINEERING PROCEDURE MANUAL

CHAPTER VI : TECHNICAL PUBLICATION

-Intentionally Left Blank-

Revision : ISSUE

Date : May 10, 2019

Halaman :

28

dari

30

ENGINEERING PROCEDURE MANUAL

CHAPTER VII : ENGINEERING SERVICES

1. GENERAL The function of the engineering section is to assist the maintenance by preparing the aircraft maintenance program, reviewing technical data received

from

manufacturer,

controlling

technical

data

required

for

maintenance of the aircraft. Gathering maintenance data, i.e. removal and installation of components, etc. for the purpose of component reliability analysis, based on the gathered data, if necessary, issue an engineering order or engineering instruction or engineering analysis. 2. RESPONSIBILITIES Technical services staff is responsible for proper execution of the company policy related to the operation of the engineering section 3. Engineering Order Engineering Order FORM DRY-101 is a document issued by engineering section in order to provide instruction to logistic department send the component (U/S component) to AMO holders for repair or alteration or inspection. Engineering order should be written compliance and instruction for repair or alteration or inspection of component (U/S component). 4. Engineering Instruction Engineering Instruction FORM DRY-103 is a document issued by engineering section in order to provide instruction to maintenance department compliance to a technical directive (AD or SB or SIL) to be embodied on company’s aircraft. Engineering instruction should be written in such a manner to be easily understood by the person performing the work and to provide detailed information and highlights of critical work stages. Revision : Issue

Date : May 10 , 2019

Halaman :

29

dari

30

CHAPTER VII : ENGINEERING SERVICES

ENGINEERING PROCEDURE MANUAL

Prior to issuance of an engineering instruction, technical directive received from manufacture (SB or SIL) or DGCA (AD) shall be evaluated by engineering section in order to determine its applicability on company’s aircraft. Should an engineering instruction be issued for the purpose of any major repair or alteration, all supporting documents shall be submitted to and be approved by DGCA in accordance with CASR part 43 appendix B.

Revision : Issue

Date : May 10 , 2019

Halaman :

30

dari

30

Engineering Procedure Manual

DRY-01 Form DRY-100

MANUAL CHANGE REQUEST Please change the Manual Last Revision by New Revision following: NO

DESCRIPTION

CHAPTER

PAGE

REASON

Requested by :

REFF.

REMARKS

Acknowledgement

Print Name & signature

Print Name & signature Form DRY-100 (May 2019)

Revision : Issue

Date May10, 2019

Page : 1 of 1

DRY-01 Form DRY-100 Name of Form Form Number Originator Purpose

Engineering Procedure Manual

MANUAL CHANGE REQUEST DRY-100 Engineering To Request a Revision of a manual to maintenance manager

Instruction for Use Name of Field

Information Required

Responsibility

NO

Listing number of part revision

Engineering

DESCRIPTION

Description of revision

Engineering

CHAPTER

Chapter will be revised

Engineering

PAGE

Page need to be revised

Engineering

REASON

Reason of revision

Engineering

REFF.

Reference for revision

Engineering

Requested by :

Person who request the revision

PIC

Acknowledgement

Quality control chief sign for acknowledgement of revison

QC

REMARKS

Revision : Issue

Date May10, 2019

Page : 1 of 1

Form DRY-101 ENGINEERING ORDER

PT. DERAYA ENGINEERING DEPARTEMEN JAKARTA

: : :

ATTENTION :

ENGINEERING ORDER

A.T.A. NO. DESCRIPTION MANUFACTURE MODEL / P/N. SERIAL NUMBER

NO. DATE PAGE

Engineering Procedure Manual

: : : :

REMARKS

LIST OF COMPONENTS / EQUIPMENT FITTED :

INSTRUCTION & REFERENCE

DISTRIBUTION : 1. Lembar ke-1 : ASLI 2. Lembar ke-2 : MAT.SUP.DEPT. 3. Lembar ke-3 : FILE

PREPARED BY :

CHECKED BY :

APPROVED BY :

FORM DRY-101(May 2019)

Revision : Issue

Date May10, 2019

Page : 1 of 1

Form DRY-101 ENGINEERING ORDER

Engineering Procedure Manual

ENGINEERING ORDER USING INSTRUCTION Name of Form Form Number Originator Purpose

Engineering Order DRY-101 Engineering This form is user for to provide instruction to logistic department send the component (U/S component) to AMO holder for repair or alteration or inspection.

Date

Instruction for Use Information Required Responsibility Fill with Engineering Order Serial Number that given by MPC ex : aaa/EOMPC/bb/cccc : aaa : 3 digit Serial Number Material Plaing bb : 2 digit of Month when the EO Made cccc : 4 Digit of year when the EO Made Material Plaing Date when the EO made

Page

Page of the EO

Attention

Which department is intended

ATA Number

JASC ATA for the component that would be sent to AMO

Description

Name of the component that would be sent to AMO

Manufacture

Manufacture name of the component that would be sent to AMO

Model P/N

Manufacture name of the component that would be sent to AMO

Serial Number

Serial Number of the component that would be sent to AMO

REMARKS

Records that are copied from rottable tags, the reason why the component are removed

Name of Field

No.

Revision : Issue

Date May10, 2019

Material Plaing Material Plaing Material Plaing

Material Plaing

Material Plaing

Material Plaing

Material Plaing

Material Plaing

Page : 1 of 2

ENGINEERING ORDER USING INSTRUCTION Material Plaing

LIST OF COMPONENTS / EQUIPMENT FITTED

All component or equipment that fitted on the component that would be sent to AMO as listing

INSTRUCTION & REFERENCE

An order to the procurement department about what must be done with the component

DISTRIBUTION :

Which department who will receipt the engineering order

PREPARED BY

sign who prepared EO

CHECKED BY

sign who checked EO

Chief Engineering

APPROVED BY

sign who approved EO

Technical Manager

Revision : Issue

Date May10, 2019

Material Plaing

Material Plaing

Material Plaing

Page : 2 of 2

Form DRY-102 ENGINEERING JUSTIFICATION

Engineering Procedure Manual

ENGINEERING JUSTIFICATION A/C. Type A/C. Reg P/N / Model S/N

: : : :

Subject

:

Provided By

:

EJ No. Date TBO TSN / CSN TSO / CSO

: : : : :

Engineering Dept.

A. Background / Reason

B. References

C. Consideration

D.

Conclusion

Title Signature

: : ________________________

Approved By

:

Quality Dept.

A. General Notice B. Technical Notice

Title Signature

: : _______________________

FORM DRY-102(May 2019)

Revision : Issue

Date May10, 2019

Page : 1 of 1

Engineering Procedure Manual

Form DRY-102 ENGINEERING JUSTIFICATION ENGINEERING JUSTIFICATION USING GUIDE Name of Form Form Number Originator

Engineering Justification DRY-102 Engineering To made the justification of any condition of an component or part on aircraft still worthy to be use with some consideration and analytical that must be tested and checked

Purpose

Instruction for Use Name of Field

Information Required

Responsibility

A/C. Type

Type of aircraft where the part or component is used

Engineering

A/C. Reg

Registration name of aircraft where the part or component is used

Engineering

Fill with Engineering Justification Serial EJ No.

Number that given by Engineering EJ/[Type

of

:

A/C]/[Month]/[serial

Engineering

number]/[Year] Date

Date when the EJ made

Engineering

P/N / Model

Part number or model of the intended part

Engineering

S/N

Serial number of the intended part

Engineering

TBO

TBO of the intended part

Engineering

TSN / CSN

TSN or CSN of the intended part (by hours or by Cycle)

Engineering

Revision : Issue

Date May10, 2019

Page : 1 of 2

Engineering Procedure Manual

Form DRY-102 ENGINEERING JUSTIFICATION ENGINEERING JUSTIFICATION USING GUIDE

Instruction for Use Name of Field

Information Required

Responsibility

TSO / CSO

TSO or CSO of the intended part (by hours or by Cycle)

Engineering

Subject

Name and description of intended part

Engineering

Background / Reason

The reason of the intended part still need to be installed on aircraft

Engineering

References

Document references the intended part still can be used

Engineering

Consideration

Job or inspection that need to make sure the intended part

Engineering

Conclusion

Describe the result the intended part still worthy to be used

Engineering

General Notice

Notice from quality assurance about intended part generally

Quality Assurance

Technical Notice

Notice from quality assurance about intended part technically

Quality Assurance

Revision : Issue

Date May10, 2019

Page : 2 of 2

Form DRY-103 ENGINEERING INSTRUCTION

ENGINEERING INSTRUCTION To

:

Subject

:

Applicability

:

Reference :  MFR  AD  MRB  SB Compliance

: …………………… : ……………………

Cc :

: : : : :

Prepared by :

Engineering

Revision : Issue

No. Date

Engineering Procedure Manual

Acknowledge by :

Chief Inspector FORM DRY-103(May 2019) Date May10, 2019

Approved by:

Maint Manager

Page : 1 of 1

Form DRY-103 ENGINEERING INSTRUCTION III.

Engineering Procedure Manual

ENGINEERING INSTRUCTION Name of Form Form Number Originator Purpose

Engineering Instruction DRY-103 Engineering To made the instruction for engineer or all of sub division of maintenance to provide a special job procedure one time or repetitive

Instruction for Use Name of Field

No. Date To Cc Subject Applicability Reference Compliance Prepared by Acknowledge by Approved by

Revision : Issue

Information Required Fill with Engineering Instruction Serial Number that given by Engineering : EI/[Type of A/C]/[Month]/[serial number]/[Year] Date when the EI made Designation to the division who will carried out EI All division and/or sub division that need to know EI to prepare requirement on the EI Title of EI Object suspected must be perform the EI Acuan pengerjaan atau sumber dari EI procedures for implementing EI Signed by Someone who prepared the EI Signed by Chief Inspector for knowing the Engineering would to release EI Signed by Maintenance Manager for approving EI that made by Engineering

Date May10, 2019

Responsibility

Engineering Engineering Engineering Engineering Engineering Engineering Engineering Engineering Engineering Chief Inspector Maintenance Manager

Page : 1 of 1

Form DRY-104 JOB CARD

JOB CARD

: ……………………. NO DATE : ……………………. : ……………………. TO

ENGINEERING & PPC DEPT

REFERENCE COMPLAINT

: :

A/C. TYPE PART NUMBER DESCRIPTION SERIAL NUMBER SUBJECT

: : : : :

A/C.REG. ATA

SIGN/LAME ENGINEER

SIGN/LAME INSPECTOR

SIGN

PPC. ATTENTION

: SEND BACK TO PPC WHEN CLOSED

Revision : Issue

Date May10, 2019

Engineering Procedure Manual

: PK:

DISTRIBUTION. 1. MAINTENANCE 2. MATERIAL PLANNING 3. STORE 4. FILE FORM DRY-104

Page : 1 of 1

Form DRY-104 JOB CARD

Engineering Procedure Manual

JOB CARD USING GUIDE Name of Form Form Number Originator Purpose

JOB CARD DRY-104 Engineering To made the instruction for engineer to provide maintenance Instruction for Use

Name of Field No. Date To REFERENCE COMPLIENCE A/C TYPE A/C REG PART NUMBER ATA DESCRIPTION SERIAL NUMBER SUBJECT SIGN SIGN/LAME ENGINEER SIGN/LAME INSPECTOR DISTRIBUTION

Revision : Issue

Information Required

Responsibility

Job Card Number Date JC release Designation to the division who will carried out JC

PPC PPC

Reference to work or sources from EI Task Must be complete to closing the JC the type of aircraft where the JC will work Registration Name of aircraft where the JC will Work Part number, where work will be Carried Out JASC ATA for part would to carried out maintenance progress Description of part where work will be carried out Serial number, where work will be Carried Out Kind of job that must be carried out PPC personel Sign who prepared

PPC PPC PPC PPC PPC

Sign by engineer who carried out the job card

PPC

Sign by inspector who checked the engineer work

PPC

Fill with department who will received the original or copy file of job card

PCC

Date May10, 2019

PPC

PPC PPC PPC PPC PPC

Page : 1 of 1

Engineering Procedure Manual

Form DRY-105 WORK REPORT

PT. DERAYA MAINTENANCE DEPT.

WORK REPORT

REFER TO JOB CARD NO

:

ENGINEER

:

NO

:

DATE

:

C.A No.

:

BOOK/AMM/IPC/MEL/AOM :

INSPECTOR

NAME / SIGN / STAMP

ENGINEER

NAME / SIGN / C.A.NO. FORM DRY-105(May 2019)

Revision : Issue

Date May10, 2019

Page : 1 of 1

Form DRY-105 WORK REPORT

Engineering Procedure Manual

V. WORK REPORT Name of Form Form Number Originator Purpose

Work Report DRY-105 Engineering to report on the results of the work that has been done based on the order State on the jobcard

Instruction for Use Name of Field No.

DATE REFER TO JOB CARD No. ENGINEER C.A No. BOOK/AMM/IPC/ME L/AOM INSPECTOR NAME / SIGN / STAMP ENGINEER NAME / SIGN / C.A. NO.

Revision : Issue

Information Required

Responsibility

Number of page work report

Engineer

Date the job has been carried out

Engineer

Number of JC that closed by Engineer

Engineer

Name of Engineer who carry out the JC

Engineer

Number of Company Authorization of the Engineer who carried out the JC

Engineer

Referances for carryout the JC

Engineer

Sign, Name, Stamp of inspector who checked the Engineer Work Report

Inspector

Sign, Name, C.A stamp of the engineer who carried out JC

Engineer

Date May10, 2019

Page : 1 of 1

Engineering Procedure Manual

Form DRY-106 DAILY REPORT

DAILY REPORT Date Place Aircraft Registration

Engineer Onboard

Daily Operation Aircraft Status

NO

DESCRIPTION

1.

Schedule Maintenance

2.

Un Schedule Maintenance

3.

Repetitive Trouble

4.

AD / SB Compliance

5.

RTA dan RTB report

6.

Delay Maintenance

7.

Defect finding Report

DESCREPANCIES

CORECTIVE ACTION

STATUS

Engineer Notice : Form DRY-106(May 2019) Prepare by,

Engineer in Charge Revision : Issue

Date May10, 2019

Page : 1 of 1

REMARKS

Form DRY-106 DAILY REPORT

Engineering Procedure Manual

DAILY REPORT USING GUIDE Name of Form

DAILY REPORT

Form Number

DRY-106

Originator

Engineering

Purpose

To report daily activity of an aircraft Instruction for Use

Name of Field

Information Required

Responsibility

Date

Date the daily report made

Engineer

Place

Base of the aircraft operation

Engineer

Aircraft Registration

Registration of aircraft

Engineer

Daily Operation

Type of aircraft operation

Engineer

Engineer Onboard

Name of engineer on board on the aircraft

Engineer

Engineer Notice

Notice from engineer about the aircraft

Engineer

Revision : Issue

Date May10, 2019

Page : 1 of 1

Engineering Procedure Manual

Form DRY-107 MAINTENANCE DISCREPANCIES REPORT LIST

MAINTENANCE DISCREPANCIES REPORT LIST A/C. TYPE : …………………………… …………………………… A/C. REG. : …………………………… ……………………………

A/C. TOTAL HRS

:

A/C. TOTAL LDG

:

ACTION NO

DATE

PART NAME

PART NUMBER

SERIAL NO.

TYPE OF DEFECT

REF. JC/TC NO.

RECTIFICATION

PERFORMED BY

FORM DRY-107 Revision : Issue

Date May10, 2019

Page : 1 of 1

INSPECTED BY

Form DRY-107 MAINTENANCE DISCREPANCIES REPORT LIST

Engineering Procedure Manual

MAINTENANCE DISCREPANCIES REPORT LIST USING GUIDE

Name of Form

MAINTENANCE DISCREPANCIES REPORT LIST

Form Number

DRY-107

Originator

Engineering

Purpose

To Collate and evaluate the maintenance discrepancies report from maintenance department Instruction for Use

Name of Field

Information Required

Responsibility

A/C Type

Type of aircraft

Engineering

A/C Reg

Registration Number of aircraft

Engineering

A/C Total HRS

Total operational hours since new

Engineering

A/C Total LDG

Total landing since new

Engineering

Date

Date of MDR

Engineering

Part Name

Name of affected part

Engineering

Part Number

Part Number of affected part

Engineering

Serial Number

Serial Number of affected part

Engineering

Type of Defect

Type of trouble affected

Engineering

Ref JC/TC no.

the number from JC / TC is being worked on when found trouble

Engineering

Rectification

Troubleshooting steps taken

Engineering

Performed By

Name of the engineer who perform the MDR

Engineering

Inspected By

Name of Inspector who checked the MDR

Engineering

Revision : Issue

Date May10, 2019

Page : 1 of 1

Engineering Procedure Manual

Form DRY-108 AIRCRAFT MONTHLY REPORT

No. …….. / IOM / DRY-PPC/……../………..

AIRCRAFT MONTHLY REPORT

( PERIOD : From No

N o

A/C. REG.

A/C. REG

DATE

A/C. TYPE

BASE

A/F. TSN

Component Replacement

A/F CSN

…………..... to …………., 200…..)

Production Hours

Production Landings

INSPECTION STATUS Last Insp Date Next Insp

NEXT MONTH COMPONENT REPLACEMENT PLAN Part Number Serial Number

PREPARED BY

CHECKED BY

PPC

PPC

A/C. Status

REMARK

Due Date

REMARK

DISTRIBUTE TO

FORM DRY-108

Revision : Issue

Date May10, 2019

Page : 1 of 1

Form DRY-108 AIRCRAFT MONTHLY REPORT

Engineering Procedure Manual

AIRCRAFT MONTHLY REPORT USING GUIDE Name of Form

Aircraft Monthly Report

Form Number

DRY-108

Originator

Engineering

Purpose

To inform all department, aircraft usage on 1 period, last and next inspection on A/C, and component replacement plan for next periode Instruction for Use

Name of Field A/C Reg.

Information Required Aircraft Registration

Responsibility Engineering

A/C Type

Aircraft Type

Engineering

BASE

Base operation of the aircraft

Engineering

A/C TSN A/C CSN Production Hours & Production Landing

Aircraft time since new Aircraft cycle since new

Engineering Engineering

Total aircraft Hours and Landing on one periode

Engineering

Inspection Status A/C Status Remark NEXT MONTH COMPONENT REPLACEMENT PLAN Date Prepared By Checked By Distribute To

Inspection carried out on aircraft on the period and next period Status of aircraft List of component will be replace on next period Date of AMR issued Sign of engineering person who prepare the AMR Sign of chief engineering List of department who will receive the AMR

Revision : Issue

Date May10, 2019

Engineering Engineering Engineering Engineering Engineering Engineering Engineering Engineering

Page : 1 of 1

Engineering Procedure Manual

Form DRY-109 TECHNICAL PUBLICATION LIST

TECHNICAL PUBLICATION LIST LOCATION Date

: :

No. 1 2 3 4 5 … …

Publication title

Revision Status

Prepared By

Date of Revision

Format

Acknowledge By

(Technical Publication)

(Chief Engineering)

Form Deraya No. DRY-109(May 2019)

Revision : Issue

Date May10, 2019

Page : 1 of 1

Form DRY-109 TECHNICAL PUBLICATION LIST

Engineering Procedure Manual

Name of Form

TECHNICAL PUBLICATION LIST

Form Number

DRY-109

Originator

Engineering

Purpose

To Give an information about all document and manual in a base and in the aircraft Instruction for Use

Name of Field

Information Required

Responsibility

Location

The location of manual

Technical Pub.

Date

Issued date of technical publication list revise every 6 month or any manual/document update

Technical Pub.

Publication Title

Name of Document or Manual

Technical Pub.

Revision Status

Last revision status

Technical Pub.

Date of Revision

Date of last revision of the manuals

Technical Pub.

Format

Kind of copy manual (Hard copy) or (soft Copy)

Technical Pub.

Prepared By

Sign of librarian who prepared Tech Pub. List

Technical Pub.

Acknowledge By

Sign of Chief Engineering who acknowledge the manual list on every base

Chief Engineering

Revision : Issue

Date May10, 2019

Page : 1 of 1

Engineering Procedure Manual

Form DRY-110 INSPECTION CHECK LIST [TYPE INSPECTION] INSPECTION LIST A/C REG.: No.

Date : DESCRIPTION

Revision : Issue

REFERENCE

Date May10, 2019

MECH

SIGN ENG

Page : 1 of 1

RII

Engineering Procedure Manual

Form DRY-110 INSPECTION CHECK LIST Name of Form

INSPECTION LIST

Form Number

DRY-110

Originator

ENGINEERING

Purpose

To display all inspection must be done on one of type inspection

Instruction for Use Name of Field

Information Required

Responsibility

[Type Inspection]

Kind of inspection list

Engineering

A/C REG.:

Reg Name of aircraft

Engineer

Date of Inspection

Engineer

Describe of inspection must be carried out

Engineering

Reference of Inspection

Engineering

Sign of mechanic, Engineer, and RI Inspector (if Required)

PiC

Date : DESCRIPTION REFERENCE SIGN

Revision : Issue

Date May10, 2019

Page : 1 of 1

Form DRY-111 TASK CARD

TASK CARD TYPE

REG

AREA/ZONE

REFERENCE

INTERVAL

Engineering Procedure Manual SKILL A/P AVIONIC OTHERS

ATA Task No

-

DESCRIPTION :

DEFECT :

M

MH

Actual M

Actual MH

MECHANIC

ENGINEER

ACTION TAKEN : RII SIGN

YES NO

PART REMOVED PN :

SN :

PARTS INSTALLED PN :

SN :

DATE A/C TSN A/C CSN

DRY FORM-111 (May 2019)

Revision : Issue

Date May10, 2019

Page : 1 of 1

Form DRY-111 TASK CARD

Engineering Procedure Manual

Name of Form

TASK CARD

Form Number

DRY-111

Originator

ENGINEERING

Purpose

To display all information of task, include job procedures

Instruction for Use Name of Field

Information Required

Responsibility

TYPE

Type of inspection

PPC

REG

Aircraft Registration

PPC

AREA/ZONE

Area/Zone of Aircraft

PPC

REFERENCE

Task References

PPC

Task Interval

PPC

ATA

ATA number of task

PPC

Task No

Number of task card

PPC

Task Description

PPC

INTERVAL

DESCRIPTION DEFECT

Finding defect of task fill if any finding

Engineer

ACTION TAKEN

Finding action taken

Engineer

PART REMOVED

Part number and Serial number removed

Engineer

PARTS INSTALLED

Part number and Serial number Installed

Engineer

M & MH Actual M & Actual MH

Man and Man Hours Required Actual Man and Man hours when the task perform

PPC Engineer

Mechanic Sign

Sign of mechanic who perform task

Mechanics

Engineer Sign

Sign of Engineer who perform task

Engineer

RII Sign Date

Sign of RII person if required

RI Inspector

Date when task perform

Engineer

A/C TSN

A/C TSN when task perform

Engineer

A/C CSN

A.C CSN when task perform

Engineer

Revision : Issue

Date May10, 2019

Page : 1 of 1

Engineering Procedure Manual

Form DRY-112A Weigh and Balance C402B Date Place Owner Expired date

: : : :

REACTION (Wheel, Jack Point) LEFT MAIN (lw) RIGHT MAIN (rw) SUB TOTAL(w) NOSE/TAIL (nw) TOTAL WEIGHT(W)

Revision : Issue

A/C. REG : A/C. S/N : A/C. Type : Weighing Type

SCALE READING (lbs)

Weight by : 1. 2. :

ITEM INCLUDED IN EMPTY WEIGHT : 1.Firex 2. First Aid Kit 3. Life Vest 4. Life Raft 5. Axe 6. ELT 7. Pilot & Copilot Seat 8. Double Sear (23.5kg) 9. Aircraft Document 10. Oxygen Bottle 11. 12.

Date May10, 2019

: : : : : : : : : :

Page : 1 of 3

Engineering Procedure Manual

Form DRY-112A Weigh and Balance C402B

Remark : 1.Aircraft weight at 2. Aircraft Fuel 3. Aircraft Hydraulic 4. Engine Oil

: Wheel Point : : :

Note : Basic Weight (s) include Unusable Fuel, Full hydraulic Fluid and Full Engine Oil. COLUMN I Item Weighed but not part of empty

Weight ( lbs )

Total

ARM ( inch )

Moment (lbs.inch )

COLUMN II Basic Items not included when weighed

Weight (lbs)

ARM ( inch )

Moment (lbs.inch )

Total

AIRCRAFT WEIGHED RECORD

=

−

× W

=

Note : D = CG Arm of Weighed N = Distance Between Reference Datum to the main wheel or wing jack point nw = Nose net Weight W = Total Weight L = Distance Between Nose & Wing jack point or Between Nose to Main Landing Gear

Revision : Issue

Date May10, 2019

Page : 2 of 3

Form DRY-112A Weigh and Balance C402B

No.

:

Date

:

Aircraft Registration

:

Aircraft Type

:

Aircraft Serial Number

:

Property of

:

Place Of Weighing

:

Reason Of Weighing

:

Weighing Equipments

:

PERFORMED BY

:

Engineering Procedure Manual

1.

Sign :

AMEL No. :

2.

Sign :

AMEL No. :

APPROVED BY : (Chief Inspector)

Sign :

RESULT WEIGHT : EMPTY WEIGHT ( BASIC ) EMPTY C.G FROM DATUM LINE

Revision : Issue

: lbs : Inch

Date May10, 2019

Page : 3 of 3

Form DRY-112A Weigh and Balance C402B

Engineering Procedure Manual

Name of Form

Weigh and Balance Cessna 402B

Form Number

DRY-112A

Originator

ENGINEERING

Purpose

To Calculate and inform the information of weigh and balance of the aircraft Instruction for Use Name of Field

Information Required

Responsibility

Date

Date when Reweighing performed

Engineer

Place

Location of reweighing

Engineer

Aircraft owner

Engineer

Expired date of weighing schedule

Engineer

Type of aircraft

Engineer

A/C SN

Serial number of aircraft

Engineer

A/C Reg

Registration code of the aircraft

Engineer

Type of weighing tool

Engineer

Person who perform reweighing

Engineer

Reading weigh on scale on every point

Engineer

List of item listed include as empty weight

Engineer

Item Weighed but not part of empty

Additional item not include at last reweighing

Engineer

Basic Items not included when weighed

List of basic item which not add on weighing

Engineer

Owner Expired date A/C Type

Weighing Type Weighing By Retraction & Scale Reading Item Included In Empty Weigh

No.

Number of reweighing

Engineering

Property of

Ownership of aircraft

Engineering

Reason of weighing

Engineering

Reason Of Weighing PERFORMED BY APPROVED BY EMPTY WEIGHT ( BASIC ) EMPTY C.G FROM DATUM LINE

Revision : Issue

Person who perform the reweighing Perform who approved reweiging

Engineer Engineer

Total empty weight

Engineering

Calculation C.G Result

Engineering

Date May10, 2019

Page : 4 of 3

Form DRY-112B Weigh and Balance BAe ATP Date Place Owner Expired date

: : : :

A/C. REG A/C. S/N A/C. Type Weight Type

: : : :

Engineering Procedure Manual

Weight by : 1. 2.

 Aircraft weighed at Landing Gear



Aircraft weighed at Jack Point

L = distance between nose to main wheel or Jack D = distance from C.G Datum point to AC CG M = distance from main wheel or jack to A/C CG N = distance CG datum point to main wheel

Revision : Issue

Date May10, 2019

Page : 1 of 3

Form DRY-112B Weigh and Balance BAe ATP

REACTION (Wheel, Jack Point)

SCALEREADING (Kg)

ITEM INCLUDED IN EMPTY WEIGHT : 1. Firex 2. First Aid Kit 3. Life Vest 4. Life Raft 5. Axe 6. ELT 7. Pilot & Copilot Seat 8. Double Sear (23.5kg) 9. Aircraft Document 10. Oxygen Bottle 11. 12.

LEFT MAIN (lw) RIGHT MAIN (rw) SUB TOTAL(w) NOSE/TAIL (nw) TOTAL WEIGHT(W)

Engineering Procedure Manual

: 3Ea : 1Ea : 4Ea : :1 : 1Ea : : 1Ea : 1 SET : 2Ea

Remark : 1.Aircraft weight at 2. Aircraft Fuel 3. Aircraft Hydraulic 4. Engine Oil

: : : :

Note : Basic Weight (s) include Unusable Fuel, Full hydraulic Fluid and Full Engine Oil. COLUMN I Item Weighed but not part of empty

Weight ( kg )

ARM ( inch )

Moment (kg.inch )

Total

COLUMN II Basic Items not included when weighed

Weight ( kg )

ARM ( inch )

Moment (kg.inch )

Total

AIRCRAFT WEIGHED RECORD

=

−

( )×( × = W+ ( = ( ) − ( ) = ____________

=

Note : distance between CG datum to Trim datum = 82.3

=

× (−82.3 + ) = 10000

Revision : Issue

)

)

= ____________

×( − 10000

Date May10, 2019

)

=

Page : 2 of 3

%

Form DRY-112B Weigh and Balance BAe ATP

No.

:

Date

:

Aircraft Registration

:

Aircraft Type

:

Aircraft Serial Number

:

Property of

: PT.DERAYA

Place Of Weighing

:

Reason Of Weighing

: PERIODIC

Weighing Equipments

:

PERFORMED BY

APPROVED BY

Engineering Procedure Manual

:1.

Sign :

AMEL No. :

2.

Sign :

AMEL No. :

:

Sign :

(Chief Inspector)

RESULT WEIGHT : EMPTY WEIGHT ( BASIC ) EMPTY C.G FROM DATUM LINE INDEX

: : :

Lbs Inch

FORM DRY-112 (May 2019)

Revision : Issue

Date May10, 2019

Page : 3 of 3

Form DRY-112B Weigh and Balance BAe ATP

Engineering Procedure Manual

Name of Form

Weigh and Balance Cessna ATP

Form Number

DRY-112A

Originator

ENGINEERING

Purpose

To Calculate and inform the information of weigh and balance of the aircraft Instruction for Use Name of Field

Information Required

Responsibility

Date

Date when Reweighing performed

Engineer

Place

Location of reweighing

Engineer

Aircraft owner

Engineer

Expired date of weighing schedule

Engineer

Type of aircraft

Engineer

A/C SN

Serial number of aircraft

Engineer

A/C Reg

Registration code of the aircraft

Engineer

Type of weighing tool

Engineer

Person who perform reweighing

Engineer

Reading weigh on scale on every point

Engineer

List of item listed include as empty weight

Engineer

Item Weighed but not part of empty

Additional item not include at last reweighing

Engineer

Basic Items not included when weighed

List of basic item which not add on weighing

Engineer

Owner Expired date A/C Type

Weighing Type Weighing By Retraction & Scale Reading Item Included In Empty Weigh

No.

Number of reweighing

Engineering

Property of

Ownership of aircraft

Engineering

Reason of weighing Person who perform the reweighing

Engineering Engineer

Reason Of Weighing PERFORMED BY APPROVED BY EMPTY WEIGHT ( BASIC ) EMPTY C.G FROM DATUM LINE

Revision : Issue

Perform who approved reweiging

Engineer

Total empty weight

Engineering

Calculation C.G Result

Engineering

Date May10, 2019

Page : 4 of 3

Form DRY-113A SWING COMPASS C402 DATE : PLACE : OWNER : Expired date: REF. N.000°

A/C. REG A/C. S/N A/C. TYPE Comp. Type COMPENSATING SWING ACTUAL AIRCRAFT HEAD(T) COMPASS (1) (2) 000°

Engineering Procedure Manual

: : : :

DEVIATION (D) (1-2)

Swing by : 1. 2. RESIDUAL SWING ACTUAL HEAD AIRCRAFT (M) STEERING (C) (3) (3+(1-2)) -1°

E.090° S.180°

090° 180°

089° 179°

W.270°

270° DEV. N − DEV. S Coeff. C = = 2 DEV. E − DEV. W coeff. B = = 2

269°

REF.

ACTUAL HEAD (T) (1) 000° 030° 060° 090° 120° 150° 180° 210° 240° 270° 300° 330°

− Coeff. C =……. 2 − = Coeff. B =……. 2 STANDBYCOMPASS AIRCRAFT DEVIATION ACTUAL HEAD COMPASS (D) (M) (2) (1-2) (3) -1° 029° 059° 089° 119° 149° 179° 219° 239° 269° 299° 329°

N 030 060 090 120 150 180 210 240 270 300 330 Note : 1. Radio / avionic master ON 2. Compass Swing Procedure refer to AC43.131B CHG 1. 3. Actual Head (M) is Magnetic = True Heading minus Variation (1E) for Indonesia Compass P/N :______________ Compass S/N :______________ Master Compass P/N : SCZ – 106 Master Compass S/N : 0618-150 Calibration Date : _________ Revision : Issue

=

AIRCRAFT STEERING (C) (3+(1-2))

I hereby certify that the aircraft PK- ............ has been maintained in accordance with…...... Approved Aircraft Inspection Program and met the requirements as set forth with the Indonesia Civil Aviation Safety Regulation and it is determined to be release to service.

AMEL Sign : 1. _____________AMEL No:_________ 2. _____________AMEL No:_________

Date May10, 2019

Page : 1 of 1

Form DRY-113A SWING COMPASS C402

Engineering Procedure Manual

Name of Form

Swing Compass C402B

Form Number

DRY-113A

Originator

ENGINEERING

Purpose

To Calculate and inform the information of Compass swing of the aircraft Instruction for Use Name of Field

Information Required

Date

Date when swing compass performed

Place

Location of swing compass

Owner Expired date A/C Type

Aircraft owner Expired date of swing compass schedule Type of aircraft

A/C SN

Serial number of aircraft

A/C Reg

Registration code of the aircraft

Comp Type

Type of Swing Compass tool

Swigged By

Person who perform reweighing

COMPENSATING SWING RESIDUAL SWING STANDBY COMPASS

Deviation check for aircraft compass swing Actual Heading and steering required Actual Heading, deviation and steering required for eat 30 degree

Compass P/N

Part Number of Swing Compass Tool

Compass S/N

Serial Number of Swing Compass Tool

Calibration Date AMEL Sign

Revision : Issue

Responsibility

Last tool calibration date Sign of engineer who perform swing compass

Date May10, 2019

Page : 1 of 1

Form DRY-113B SWING COMPASS BAE ATP DATE PLACE OWNER Expired date

: : : :

A/C. REG A/C. S/N A/C. TYPE Comp. Type

Engineering Procedure Manual

: : : :

ADJUSTED BY 1. 2.

CORRECTING SWING REFERENCE

ACTUAL COURSE

AIRCRAFT COMPASS

N.000°

000°

E.090°

090°

S.180°

180°

CO – EFFICIENTS DEVIATION " "=

NOT CORRECTED

CO – EFFICIENT “C” MAKE COMPASS READ W.270°

270°

-270 NOT CORRECTED

CO – EFFICIENT “B” MAKE COMPASS READ CHECK SWING

" "= " "= " "=

DEVIATION

DEV. N − DEV. S 2

DEV. E − DEV. W 2

FOR

NW.315°

315°

315

N.000°

000°

N

NE.045°

045°

45

E. 090°

090°

E

SE.135°

135°

135

S.180°

180°

S

SW.225°

225°

225

W.270°

270°

W

STR

" "= " "=

TOTAL DEV 8

NOT CORRECTED

TOTAL DEVIATION NOTE

ENGINE :

ON/OFF

RADIO : ON/OFF

APU : ON/OFF

ENGINEER

(

APPROVED BY

)

(

LIC. No.

Revision : Issue

) QA Inspector

Date May10, 2019

Page : 1 of 1

Form DRY-113B SWING COMPASS BAE ATP

Engineering Procedure Manual

Name of Form

Swing Compass BAe ATP

Form Number

DRY-113B

Originator

ENGINEERING

Purpose

To Calculate and inform the information of Compass swing of the aircraft Instruction for Use Name of Field

Information Required

Date

Date when swing compass performed

Place

Location of swing compass

Owner Expired date A/C Type

Aircraft owner Expired date of swing compass schedule Type of aircraft

A/C SN

Serial number of aircraft

A/C Reg

Registration code of the aircraft

Comp Type

Type of Swing Compass tool

Swigged By

Person who perform reweighing

Correcting Swing SWING

Deviation check for aircraft compass swing

Compass P/N

Part Number of Swing Compass Tool

Compass S/N

Serial Number of Swing Compass Tool

Calibration Date AMEL Sign

Revision : Issue

Responsibility

Last tool calibration date Sign of engineer who perform swing compass

Date May10, 2019

Page : 1 of 1

Form DRY-114 AIRCRAFT STATUS

Engineering Procedure Manual

PRODUCTION, PLANNING AND CONTROL ______________________________________________________________________

AIRCRAFT STATUS DATE : ………. / ………. / 200….

NO

A/C. REG

TYPE

BASE

STATUS

REMARK

1 2 3 4 5 6 7 8 9 NOTE :

DISTRIBUTION : DZ, TZ, CI, LZ, MAT.PLANNING, DFS, STORE

REPORTED BY : SIGN : NAME :

FORM DRY-114 Revision : Issue

Date May10, 2019

Page : 1 of 1

Form DRY-114 AIRCRAFT STATUS

Engineering Procedure Manual

Name of Form

AIRCRAFT STATUS

Form Number

DRY-114

Originator

ENGINEERING

Purpose

To Inform all aircraft status to other division

Instruction for Use Name of Field Date

Information Required

Responsibility

Date of aircraft status released

PPC

Number List List of aircraft registration

PPC

Type

List of aircraft type

PPC

Base

List of location of the aircraft

PPC

Status

Status information of an aircraft

PPC

Remark

Description of the aircraft status

PPC

Note

Note from planning sub division

PPC

Distribution

List of department who will received the aircraft status

PPC

Reported By

Person who report of all aircraft status

PPC

No A/C Reg

Revision : Issue

Date May10, 2019

PPC

Page : 1 of 1

Form DRY-115 PUBLICATION TRANSMITAL

Engineering Procedure Manual

PUBLICATION TRANSMITTAL Date To

: :

Attached, please find the following publication: No.

Title

Rev.

Date

Qty.

Remark

I acknowledge that item has received in good condition and work normally; understood and incorporated, sign off and return this transmittal sheet to Engineering Department as soon as possible. Sent by:

Received by:

(……………………………………) Date:

(………………………………….) Date:

Revision : Issue

Date May10, 2019

Page : 1 of 1

Form DRY-115 PUBLICATION TRANSMITAL

Name of Form Form Number Originator Purpose

Engineering Procedure Manual

Publication Transmittal DRY-115 Technical Publication To inform the list of manual that sending to operational base

Instruction for Use Name of Field Date

Information Required

Responsibility

Sending date of transmittal publication

Technical Publication

Destination of transmittal publication

Technical Publication

Title

Title of manual sent to operational base

Technical Publication

Rev.

Revision Number of manual

Technical Publication

Date

Revision Date of manual

Technical Publication

Qty.

Total Page of manuals

Technical Publication

Kind of manuals, and other description of manual

Technical Publication

To

Remark Sent by Received by

Revision : Issue

Sign of Technical Publication person who send the publication transmittal Sign of DERAYA’s person who receive the manuals when the manual received

Date May10, 2019

Technical Publication PiC

Page : 1 of 1

ENGINEERING PROCEDURE MANUAL

To Attention Date

DRY-01 FORM DRY-116

PT Deraya Graha Intrube 2, 1st Floor Jln. Cililitan Besar-Jakarta 13610 Telp.(021) 29373417-19 Fax. (021) 29373416 romadi@deraya .co.id

: : :

Internal Publication Receipt Confirmation If these documents have been received in good condition and or inserted in proper system please complete the section below and fax to or post \ e-mail to the following address : Technical publication Deraya E-mail Address Telp. Fax.

: : : : :

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

Signature Department Contact Date Address

: : : : :

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

Receipt publication : No

Document

Description

Rev

Qty

Remarks

1 2 3 4 5 6 7 8 9

ISSUED:

April 2019

REVISION No. : 00

Page : 1 of 1

ENGINEERING PROCEDURE MANUAL Name of Form Form Number Originator Purpose

DRY-01 FORM DRY-116

Internal Publication Receipt Confirmation DRY-116 Technical Publication To give the confirmation to technical publication

Instruction for Use Name of Field

Information Required

To

Department who will received the manual Person in charge from the department who will received the manuals Date the Internal Publication receipt confirmation send

Attention Date Technical publication Deraya E-mail Address Telp. Fax. Signature

Name of technical publication person who sent Internal Publication receipt confirmation Email of technical publication person who sent Internal Publication receipt confirmation Address of technical publication person who sent Internal Publication receipt confirmation Telp Number of technical publication person who sent Internal Publication receipt confirmation Fax Number of technical publication person who sent Internal Publication receipt confirmation

Responsibility Technical Publication Technical Publication Technical Publication Technical Publication Technical Publication Technical Publication Technical Publication Technical Publication

Sign of PiC who receive the manuals

Receiver

Department

Department of receiver

Receiver

Contact

Contact manual receiver

Receiver

Date manual received

Receiver

Address of receiver

Receiver

Document

Name of Document or manual

Technical Publication

Description

Description part of manuals

Technical Publication

Rev

Revision status of manuals

Technical Publication

Qty

Quantity of manual

Technical Publication

Date Address

Remarks

ISSUED:

Technical Publication

April 2019

REVISION No. : 00

Page : 1 of 1

Form DRY-117 BORESCOPE INSPECTION REPORT

Engineering Procedure Manual

BOROSCOPE INSPECTION REPORT Aircraft type Aircraft registration Engine S/N Engine Position Reason for BSI Date performed Reference

: : : : : : :

1. COMBUSTION CHAMBER LINER ASSEMBLY and SMALL EXIT DUCT [FIGURE] DESCRIPTION OF DAMAGED : 2. H.P VANE SEGMENT [FIGURE] DESCRIPTION OF DAMAGED : 3. HPT BLADES [FIGURE] DESCRIPTION OF DAMAGED : 4. H.P SHROUD SEGMENTS [FIGURE] DESCRIPTION OF DAMAGED : 5. LP IMPELER [FIGURE] DESCRIPTION OF DAMAGED : Performed by,

Revision : Issue

Inspector,

Date May10, 2019

Page : 1 of 2

Form DRY-120 MATERIAL REQUESITION

Engineering Procedure Manual

ENGINEERING DEPT.

To Copy No

: : Part Number

MATERIAL REQUESITION Description

A/C Stock Registration

Note :

Date Page Req.

: :

Remarks

Ref.

Prepared By :

( Material Planning )

Revision : Issue

Date May10, 2019

Page : 1 of 1

Form DRY-120 MATERIAL REQUESITION

Engineering Procedure Manual

Name of Form

MATERIAL REQUESITION

Form Number

DRY-120

Originator

ENGINEERING

Purpose

To Inform material requisition progress to department needed

Instruction for Use Name of Field

Information Required

Responsibility

To

Department who will received Department who will received the copied of material requisition form

PPC

Number of Material Request Release date of material requisition Page of material requisition

PPC PPC PPC

Part number of part

PPC

Name of part

PPC

Aircraft registration

PPC

Quantity available part on store

PPC

Request

Quantity Request part by engineer

PPC

Remarks

Description of availability

PPC

Reference

Reference part form IPC

PPC

Note from other department

PPC

Sign of PPC person who prepared the part requisition

PPC

Copy No Date Page Part Number Description A/C Stock

Note Prepared By

Revision : Issue

Date May10, 2019

PPC

Page : 1 of 1

PK -_____________ AIRCRAFT REG

FLIGHT & MAINTENANCE LOG CESSNA C402B

FLIGHT LOG FLT NO.

FROM

BLOCK TIME

TO

NO DATE

: …………………….. : ……………………..

PERFORMANCE LOG

FLIGHT TIME

ENG. CYCLE LDG

L/H

R/H

ENG NO.

RPM

MAP

FUEL FLOW

MAGNETTO DROP EGT/CHT

LH

RH

LH

OIL SYSTEM

RH

PRESSURE L R

TEMP L R

SAT/OAT (O C)

PRESS ALT (IN HG)

IAS (KNOT)

AMPERE METER

LH

RH LH RH AIRPLANE TOTAL HRS FORWARD TODAY TOTAL

TOTAL FUEL PLACE

Remaining LH RH

UPLIFT LH RH

: CAPT. : COPIL : F.A./FOO : ENGINEER DISTRIBUTION NO. 1 ORIGINAL (WHITE) NO. 2 COPY (RED) NO. 3 COPY (YELLOW) NO. 4 COPY (BLUE)

PRE-FLT / PDI Inspection Executed Name : …………………. Date Time Lic. No Sign

: ……………………. : …………………… : …………………… : …………………..

FORM DRY-122

ENGINE OIL L/H

HYD

No

Sign/Name

AIRPLANE TOTAL LDG

ENGINE I TOTAL HRS

ENGINE II TOTAL HRS

PROP. I TOTAL HRS

PROP. II TOTAL HRS

IDLE RPM ENG I

NEXT INSP

ENG II AT A/C HRS or CAL

DISCREPANCIES

RECTIFICATION

DESCRIPTION

DESCRIPTION

AMEL RELEASE RTS M.R

R/H

Lic no.: Sign :

Lic no.: Sign :

Lic no. : Sign :

Lic no.: Sign :

Lic no. : Sign :

Lic no.: Sign :

RII Stamp R.I.I (If Any)

Sign/Stamp

Sign/stamp

Sign/stamp

Lic no. : Sign : - ENGINEERING/PPC JKT - REMAIN IN BOOK - FLOPS JKT - BASE OPERATIONS

sign/stamp

MAINTENANCE RELEASE / MR With the following wording : I hereby certify that this Aircraft has been Maintened and Inspected in accordance with the requirement of the CASR applicable there to and is safe for flight. COMPONENT REPLACEMENT

DAILY INSPECTION Inspection Executed Name Date Time Lic No Sign

: …………………..... : …………………..... : ……………………. : .…………………… : …………………….

Lic no.:

CAPTAIN Name Date Lic. No Sign

SERIAL NO DESCRIPTION

: ………………… : ………………… : ………………… : …………………

Note : Flt log & Performance log filled by Pilot & others by Engineer Incharge

PART NO.

OFF

ON

CERTIFICATE OF RELEASE TO SERVICE : The work recorded above has been carried out in the CASR for the time being inforce and it that respect the aircraft/equipment is considered flt for release for service : A/C TSN : TTL LDG : Name : AMEL Lic : Date : Sign : Type Inspection :

Engineering Procedure Manual

Form DRY-122 FLIGHT MAINTENANCE LOG

Name of Form

AIRCRAFT FLIGHT AND MAINTENANCE LOG

Form Number

DRY-122

Originator

ENGINEERING

Purpose

To Record of aircraft movement and maintenance daily

Instruction for Use Name of Field

Information Required

Responsibility Maintenance Manager

No.

Number of AFML

Date

Date of AFML

Pilot

Number of flight per aircraft registration

Pilot

Departure location of the aircraft

Pilot

Arrival location of the aircraft

Pilot

Block Time

Time between start up the engine and shut down the engine

Pilot

Flight Time

Time between when the aircraft take off and touch down

Pilot

Count when the aircraft touch down on runway

Pilot

A period of an engine from engine start, take off, cruise, landing and shut down is one engine cycle

Pilot

Number of engine

Pilot

Total engine rotation per minute

Pilot

Flt. No. From To

LDG ENG. CYCLE ENG. No. RPM MAP Fuel Flow

Pilot Quantity of fuel flow

Pilot

EGT/CHT

Pilot

MAGNETTO DROP

Pilot

OIL SYSTEM

Pilot

SAT/OAT (O C) IAS (KNOT) PRESS ALT (IN HG)

Outside air temperature (OAT) or static air temperature (SAT) refers to the temperature of the air around an aircraft. State on SAT/OAT Indicator

Pilot

Indicated Air Speed, State on IAS Indicator

Pilot Pilot

AMPERE METER AIRPLANE TOTAL HRS AIRPLANE TOTAL LDG ENGINE I TOTAL HRS ENGINE II TOTAL HRS PROP. I TOTAL HRS PROP. II TOTAL HRS

Pilot Total hours of the aircraft accumulation from previous total hours and today flight hours Total landing of the aircraft is accumulation from previous total landing and today landing Total hours of the engine #1 is accumulation from previous total engine #1 hours and today flight hours Total hours of the engine #2 is accumulation from previous total engine #2 hours and today flight hours Total hours of the propeller #1 is accumulation from previous total propeller #1 hours and today flight hours Total hours of the propeller #2 is accumulation from previous total propeller #2 hours and today flight hours

IDLE RPM

Revision : Issue

Engineer Engineer Engineer Engineer Engineer Engineer Engineer

Date May10, 2019

Page 2 of 3

Engineering Procedure Manual

Form DRY-122 FLIGHT MAINTENANCE LOG

Instruction for Use Name of Field Next Inspection AT A/C HRS or CAL

Information Required

Responsibility

Detail due of the next routine inspection, with due date and hours

Engineer

PLACE

Engineer

FUEL

Engineer

ENGINE OIL

Engineer

HYD

Engineer

DISCREPANCIES

Discrepancies or a maintenance if any

Engineer

RECTIFICATION

Rectification of the discerpancies

Engineer

AMEL RELEASE RII Stamp

Sign of engineer who perform and/or release the trouble or inspection Sign and stamp of RII inspector who approve the inspection that perform by engineer

Engineer Engineer

CAPT.

Name of the pilot on board

Engineer

COPIL

Name of the copilot on board

Engineer

F.A./FOO

Name of F.A/FOO on board

Engineer

ENGINEER

Name of engineer on board

Engineer

DISTRIBUTION PRE-FLT / PDI Inspection Executed DAILY INSPECTION Inspection Executed COMPONENT REPLACEMENT CERTIFICATE OF RELEASE TO SERVICE

Revision : Issue

List of department that will receive the AFML Name, Date, time, Lic. No, & sign of the engineer who perform the preflight inspection Name, Date, time, Lic. No, & sign of the engineer who perform the Daily inspection Component that replace from the aircraft Sign of engineer who released the aircraft

Date May10, 2019

Engineer Engineer Engineer Engineer

Page 3 of 3

PK -_____________ AIRCRAFT REG

FLIGHT & MAINTENANCE LOG BAe ATP

FLIGHT LOG FLT NO.

FROM

BLOCK TIME

TO

NO DATE

: …………………….. : ……………………..

PERFORMANCE LOG

FLIGHT TIME

ENG. CYCLE LDG

L/H

R/H

ENG NO.

TORQUE PRESS. (%)

NP (RPM %)

NH (%)

NL (%)

ITT (O C)

FUEL FLOW (Kgs/HRS)

ENGINE I TOTAL HRS

ENGINE II TOTAL HRS

OIL TEMP (O C)

OIL PRESS (PSI)

SAT/OAT (O C)

IAS (KNOT)

PRESS. ALT (Feet)

AMPERE METER

LH

RH LH RH AIRPLANE TOTAL HRS FORWARD TODAY TOTAL

TOTAL FUEL PLACE

Remaining LH RH

UPLIFT LH RH

: CAPT. : COPIL : F.A./FOO : ENGINEER DISTRIBUTION NO. 1 ORIGINAL (WHITE) NO. 2 COPY (RED) NO. 3 COPY (YELLOW) NO. 4 COPY (BLUE)

PRE-FLT / PDI Inspection Executed Name : …………………. Date Time Lic. No Sign

: ……………………. : …………………… : …………………… : …………………..

FORM DRY-123

ENGINE OIL L/H

HYD

No

Sign/Name

AIRPLANE TOTAL LDG

PROP. I TOTAL HRS

PROP. II TOTAL HRS

START TEMP ENG I

NEXT INSP

ENG II AT A/C HRS or CAL

DISCREPANCIES

RECTIFICATION

DESCRIPTION

DESCRIPTION

AMEL RELEASE RTS M.R

R/H

Lic no.: Sign :

Lic no.: Sign :

Lic no. : Sign :

Lic no.: Sign :

Lic no. : Sign :

Lic no.: Sign :

Lic no. : Sign :

Lic no.:

RII Stamp R.I.I (If Any)

Sign/Stamp

Sign/stamp

Sign/stamp

- ENGINEERING/PPC JKT - REMAIN IN BOOK - FLOPS JKT - BASE OPERATIONS

sign/stamp

MAINTENANCE RELEASE / MR With the following wording : I hereby certify that this Aircraft has been Maintened and Inspected in accordance with the requirement of the CASR applicable there to and is safe for flight. COMPONENT REPLACEMENT

DAILY INSPECTION Inspection Executed Name Date Time Lic No Sign

: …………………..... : …………………..... : ……………………. : .…………………… : …………………….

CAPTAIN Name Date Lic. No Sign

SERIAL NO DESCRIPTION

: ………………… : ………………… : ………………… : …………………

Note : Flt log & Performance log filled by Pilot & others by Engineer Incharge

PART NO.

OFF

ON

CERTIFICATE OF RELEASE TO SERVICE : The work recorded above has been carried out in the CASR for the time being inforce and it that respect the aircraft/equipment is considered flt for release for service : A/C TSN : TTL LDG : Name : AMEL Lic : Date : Sign : Type Inspection :

Form DRY-123 FLIGHT MAINTENANCE LOG

Engineering Procedure Manual

Name of Form

AIRCRAFT FLIGHT AND MAINTENANCE LOG

Form Number

DRY-123

Originator

ENGINEERING

Purpose

To Record of aircraft movement and maintenance daily

Instruction for Use Name of Field

Information Required

Responsibility

No.

Number of AFML

Date

Date of AFML

Pilot

Number of flight per aircraft registration

Pilot

Departure location of the aircraft

Pilot

Arrival location of the aircraft

Pilot

Block Time

Time between start up the engine and shut down the engine

Pilot

Flight Time

Time between when the aircraft take off and touch down

Pilot

Count when the aircraft touch down on runway

Pilot

A period of an engine from engine start, take off, cruise, landing and shut down is one engine cycle

Pilot

Number of engine

Pilot

Flt. No. From To

LDG ENG. CYCLE ENG. No.

Maintenance Manager

Torque Pressure NP NH NL ITT FUEL FLOW

Quantity of fuel flow

OIL TIME OIL PRESS Outside air temperature (OAT) or static air temperature (SAT) refers to the temperature of the air around an aircraft. State on SAT/OAT Indicator

SAT/OAT IAS

Indicated Air Speed, State on IAS Indicator

PRESSURE ALTITUDE AMPERE METER AIRPLANE TOTAL HRS AIRPLANE TOTAL LDG ENGINE I TOTAL HRS ENGINE II TOTAL HRS PROP. I TOTAL HRS PROP. II TOTAL HRS

Total hours of the aircraft accumulation from previous total hours and today flight hours Total landing of the aircraft is accumulation from previous total landing and today landing Total hours of the engine #1 is accumulation from previous total engine #1 hours and today flight hours Total hours of the engine #2 is accumulation from previous total engine #2 hours and today flight hours Total hours of the propeller #1 is accumulation from previous total propeller #1 hours and today flight hours Total hours of the propeller #2 is accumulation from previous total propeller #2 hours and today flight hours

IDLE RPM

Engineer Engineer Engineer Engineer Engineer Engineer

Next Inspection AT A/C HRS or CAL

ISSUED:

Engineer

April 2019

Detail due of the next routine inspection, with due date and hours

REVISION No. : 00

Engineer

Page : 1 of 3

Instruction for Use Name of Field

Information Required

Responsibility

PLACE

Engineer

FUEL

Engineer

ENGINE OIL

Engineer

HYD

Engineer

DISCREPANCIES

Discrepancies or a maintenance if any

Engineer

RECTIFICATION

Rectification of the discerpancies

Engineer

AMEL RELEASE RII Stamp

Sign of engineer who perform and/or release the trouble or inspection Sign and stamp of RII inspector who approve the inspection that perform by engineer

Engineer Engineer

CAPT.

Name of the pilot on board

Engineer

COPIL

Name of the copilot on board

Engineer

F.A./FOO

Name of F.A/FOO on board

Engineer

ENGINEER

Name of engineer on board

Engineer

DISTRIBUTION PRE-FLT / PDI Inspection Executed DAILY INSPECTION Inspection Executed COMPONENT REPLACEMENT CERTIFICATE OF RELEASE TO SERVICE

Revision : Issue

List of department that will receive the AFML Name, Date, time, Lic. No, & sign of the engineer who perform the preflight inspection Name, Date, time, Lic. No, & sign of the engineer who perform the Daily inspection Component that replace from the aircraft Sign of engineer who released the aircraft

Date May10, 2019

Engineer Engineer Engineer Engineer

Page 3 of 3