CES TASK 49-16-51-400-001
Installation of the Air-Intake FLap Actuator (4015KM) (GTCP 36-300)
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific access platform 2.5 m (8 ft. 2 in.)
No specific Torque Wrench : range 0.00 to 1.20 m.daN
(0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific lockwire-corrosion resistant steel 0,8 mm Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
Material No. 07-001 ELECTRICAL BONDING COATING (BLUE COLOR) (Ref. 20-31-00)
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B CORROSION INHIBITING FILLET CONSISTENCY (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
1 cotter pin 49-16-04 03 -070 12 bellows 49-16-04 03 -080 17 cotter pin 49-16-04 03 -070 D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
49-16-43-400-001 Installation of the Air Intake Flap (GTCP 36-300) 49-16-51-820-001 Adjustment of the Air-Intake Flap Actuator (4015KM) (GTCP 36-300) 49-16-51-991-001 Fig. 201
3. Job Set-up
__________
Subtask 49-16-51-860-051
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position below the APU compartment.
(2)
Make sure that the maintenance door 314AR is open.
(3)
Make sure that the catwalk panel is not installed on the service panel.
Subtask 49-16-51-865-062
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41
4. Procedure
_________
(Ref. Fig. 201/TASK 49-16-51-991-001)
Subtask 49-16-51-210-055
A. Preparation for Installation
(1)
Make an inspection of the bellows (12) for cracks and damage. If necessary, replace the bellows as follows:
(a)
Remove the screws (14), the washers (13), the ring (9) and the bellows (12).
(b)
Install the new bellows (12), the ring (9), the washers (13) and the screws (14).
(2)
Make an inspection of the air intake flap and the structure fittings for cracks and corrosion. Replace the fittings if necessary.
(3)
Close and open the air intake flap manually and examine the adjustment. Adjust the air intake flap if necessary (Ref. TASK 49-16-43-400-001).
(4)
Protective Treatment
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(a) Apply the SPECIAL MATERIALS (Material No. 05-002) to all the mating surfaces. Do not apply the putty to any part of the bonding jumper (21) or it's mating surface.
Subtask 49-16-51-420-050
B. Installation of the Air Intake Actuator (4015KM)
(1)
Hold the air intake flap in the top position.
(2)
Make sure that the new air-intake flap actuator (4015KM) (6) is in the flap open position (retracted).
NOTE : Turn the manual override device on the air-intake flap
____ actuator with a torque wrench until the actuator rod is in the retracted position (which agrees with the open position of the air intake flap). For the 43-1-1100 Amendment 1 actuator a torque up to 0.3 m.daN (26.54 lbf.in) is permitted. For the 106-1-1100-02 actuator, a torque up to 0.4 m.daN
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM 機(jī)載輔助動力 AIRBORNE AUXILIARY POWER3(44)
