(6)
Remove the Hi-Lock rivets (Ref. ASRM 51-42-11-001) and the plate (9).
(7)
Remove the hinge arm fitting (10).
1EFF : ALL 1 55-36-41Page 410 1 1 Feb 01/02R 1 1 1CES 1
TASK 55-36-41-400-001
Installation of the Hinge Arm Fittings No. 1 thru No. 7
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.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
CAUTION : DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF
_______ CARBONFIBER REINFORCED PLASTIC.
NOTE : The installation procedures are given for the hinge arm fitting No. 1;
____ the installation procedures for the hinge arm fittings No. 2 thru No.5 are almost the same.
1. Reason for the Job
__________________
Self Explanatory
1EFF : ALL 1 55-36-41Page 411 1 1 Feb 01/02R 1 1 1CES 1
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific nonmetallic scraper
No specific warning notices
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) No specific Torque Wrench : range 2.00 to 20.00 m.daN
(15.00 to 150.00 lbf.ft) SL90-313-5625 2 TOOL - INSTALLATION, TAB WASHERS STA-LOK NSA5454 SL90-313-7500 1 TOOL - INSTALLATION, TAB WASHERS STA-LOK NSA5454 SL90-322-5625 2 WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 SL90-374-7500 1 WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004 USA MIL-PRF-23827 TYPE I
SYNTH.ESTER BASED GREASE HIGH PRESSURE
(Ref. 20-31-00)
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
(Ref. 20-31-00)
R Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00) Material No. 16-003 F ASNB70720 COATING (OBSOLETE USE 16-021) (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
bushes 27-21-04 15A-040
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
27-21-00-720-002 Functional Test of the Rudder Mechanical Control 27-21-41-200-001 Inspection/Check of the Rudder 27-21-41-400-001 Installation of the Rudder 29-10-00-864-001 Depressurize the Green Hydraulic System 29-10-00-864-002 Depressurize the Yellow Hydraulic System 29-10-00-864-003 Depressurize the Blue Hydraulic System 53-55-12-000-001 Removal of the Rudder Fairings 325AL and 325AR 53-55-12-400-001 Installation of the Rudder Fairings 325AL and 325AR 55-33-13-000-001 Removal of the Trailing Edge Access-Panels 325EL,
325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
55-33-13-400-001 Installation of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
R 55-34-11-400-001 Installation of the Vertical Stabilizer Tip 55-36-48-400-001 Installation of the Rudder Support Strut 55-42-13-400-001 Installation of the Access Panel 326CT at the Rudder
Attach Fitting No. 7
ASRM 51-42-11-001
ASRM 55-36-42-201
55-36-41-991-001 Fig. 401
55-36-41-991-002 Fig. 402
55-36-41-991-003 Fig. 403
3. Job Set-up
__________
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM STABILIZERS 安定面(99)
