General Information¶
Preamble¶
This Maintenance Program is a part of, and shall be used in conjunction with the approved General Maintenance Manual. The program specifies the detail of maintenance and inspection, schedule and unscheduled, to be performed on the certain aircraft.
The detail in this maintenance program is established from the related maintenance manuals, publication and regulation to be used as a reference document for the company maintenance personnel. Therefore, it may be alerted, revised and/or completely change upon requirement specified by manufacturer, Airworthiness Authority or the company.
However, the approval from Civil Aviation Authority of Thailand (CAAT) Thailand is needed for all cases. The program holder is required to maintain this maintenance program in an up to date condition by insertion of the revision page or section upon receive of the revision.
Signed: ......................................................
Date: ....................................................
Name: Teerapong Prajittanon
Title: Director of Maintenance (Acting) On behalf of AC Aviation Company Co., Ltd.
Aircraft General¶
The Hawker Beechcraft 850XP is a company aircraft manufactured by Hawker Beechcraft Corporation (BHC), Wichita, Kansas, USA.
It is under Type Certificate (TC) No. A3EU. The general information of this aircraft is as follow.
Aircraft model | HAWKER 850XP | |
---|---|---|
Manufacture date | March 2007 | |
Serial No. | 258830 | |
Registration No. | HS-PEK | |
Engine Manufacture and Model | Honeywell TFE731-5BR Turbofan Engine | |
APU Manufacture and Model | Honeywell GTCP36-150(W) Gas Turbine Engine |
Revision¶
In order to keep the program update, any change required by the manufacturer, FAA, DCA and/or he company pertaining to this program will be revised as applicable. The revision may be made on the effected page, partial of section or section depends on particular circumstances.
Besides, one or more section may be deleted and/or supplemented upon changing of the company aircraft fleet.
To revise or supplement this program, the List of Effective Pages issued with each revision and/or supplement will be changed and each page to be revised and/or supplemented will be changed, inserted, deleted and/or supplemented as specified in the list. The Record of Revision should then be entered by the person performing the revision and/or supplement.
Record of Revision¶
Upon receiving of revision and/or supplement, change, insert, delete and/or supplement the revision pages in the program and enter the revision number, revision date, insertion date and initial of person incorporating the revision and/or supplement in the appropriate block.
Revision No. | Revision Date | Insertion page | IML CD rev. Reference | Remark |
---|---|---|---|---|
Original | 10 Febuary 2014 | -none- | -none- | -none |
1 | 23 August 2016 | Change all pages template format. p. 51/p. 175/p. 299 | 74 IML June 2016 | Transmittal Rev. 31 March 2016 |
List of Effective Pages¶
Section | ||
---|---|---|
Section 1 General Information | ||
1.1 Preamble | 3 | 1 |
1.2 Aircraft General | 4 | 1 |
1.3 Revision | 5 | 1 |
1.4 Record of Revision | 6 | 1 |
1.5 List of Effective Page | 7-8 | 1 |
1.6 List of Program Holder | 9 | 1 |
Section 2 Introduction | ||
2.1 Introduction | 10-25 | 1 |
2.2 Introduction appendix | 26-31 | |
2.3 ATA Task code | 32-74 | 1 |
Section 3 Part of Inspection | ||
3.1 Part 1 Minor Inspection | 75 | 1 |
3.1.1 Preflight Inspection | 76-88 | 1 |
3.1.2 Post flight Inspection | 89-98 | 1 |
3.1.3 TFE731-5BR-1H Inspection | 99-100 | 1 |
3.1.4 APU Inspection | 101-102 | 1 |
3.1.5 200 Hrs. Lubrication | 103 | 1 |
3.1.6 400 Hrs. Lubrication | 104 | 1 |
3.1.7 400 Hrs. Detailed walk-around Inspection | 105-116 | 1 |
3.2 Part 2 Routine Inspection | ||
3.2.1 Inspection B | 118-138 | 1 |
3.2.2 Inspection C | 139-158 | 1 |
3.2.3 Inspection D | 159-172 | 1 |
3.2.4 Inspection E | 173-185 | 1 |
3.2.5 Inspection F | 186-198 | 1 |
3.2.6 Inspection G | 199-2-4 | 1 |
3.3 Part 3 Structural Inspection | 205-227 | 1 |
3.4 Part 4 Out of Phase Inspection | 228-236 | 1 |
3.5 Part 5 Special Incident Inspection | 237 | 1 |
3.5.1 Inspection after Overweight or Heavy Landing | 238-241 | 1 |
3.5.2 Inspection after flight in Heavy Turbulence | 242-243 | 1 |
3.5.3 Inspection after Lightning Strike | 244-245 | 1 |
3.5.4 Inspection after Misuse of Reverse Thrust | 246 | 1 |
3.5.5 Inspection after Landing Gear Vibration | 247-252 | 1 |
3.5.6 Inspection Cold Soak below -40 Deg. C | 253 | 1 |
3.5.7 Inspection After landing or Aborted Takeoff in Deep. | 254 | 1 |
3.5.8 Inspection After an Emergency Stop. | 255 | 1 |
3.5.9 Inspection After Abnormal APU Conditions. | 256 | 1 |
3.5.10 Inspection After Flap over Speed. | 257 | 1 |
3.6 Part 6 Panel Location Charts | 258-267 | 1 |
3.7 Part 7 Lubrication | 268-291 | 1 |
3.8 Part 8 Component requirements. | 292-299 | 1 |
3.9 Part 9 Supplemental Type Certificate | 300-304 | 1 |
3.10 Part 10 Mandatory Life Limitations | 305-325 | 1 |
3.10.1 Mandatory Life Limitation Appendix | 326 | 1 |
List of Program Holders¶
The following is the list of the ACA Maintenance Program holders who responsible to revise and/or supplement the revision and/or supplement of the program when the need is apparent.
No. | Holder |
---|---|
PEK-MP-001 | Aircraft Maintenance Engineering Manager |
PEK-MP-002 | Quality Control Manager |
PEK-MP-003 | Director of Operation |
PEK-MP-004 | Department of Civil Aviation (DCA) |
PEK-MP-005 | Civil Aviation Authority of Thailand (CAAT) |