(c)
Hold the access panel (15) and remove the hinge attach screws (11).
(d)
Remove the access panel (15).
(2) For access panels 325EL, 325ER and 325DR: NOTE : The removal procedure for one access panel is given; the
____ procedures for all access panels are almost the same.
(a)
Release the studs (16).
(b)
Hold the access panel and release the studs (17).
(c)
Remove the access panel.
Vertical Stabilizer-Trailing Edge
Figure 401/TASK 55-33-13-991-001
1EFF : ALL 1 55-33-13 Page 404
1 1 Feb 01/98
1 1
1CES 1
TASK 55-33-13-400-001
Installation of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
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.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific nonmetallic scraper.
No specific warning notice R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-013 D TV-53-3507/73 RELEASE AGENT (OBSOLETE USE 05-013A) (Ref. 20-31-00)
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
(Ref. 20-31-00)
Material No. 09-018 USA AMS 3267/3
CORROSION INHIBITING LOW ADHESION SEALANT
(Ref. 20-31-00)
-------------------------------------------------------------------------------
REFERENCE ------------------ DESIGNATION-------------------------------------------------------------
Material No. 11-008
(USE 11-008A) (Ref. 20-31-00)
C. Expendable Parts
---------FIG.ITEM --------- -------------------------------------------------|DESIGNATION ------------------------------------------------- ---------------------|IPC-CSN---------------------
12 cotter pin 55-33-04 02 -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)-
29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
55-33-13-410-002 Closing/Installation of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
55-33-13-991-001 Fig. 401
3. Job Set-up__________
Subtask 55-33-13-860-052
A. Aircraft Maintenance Configuration
(1)
Make sure that the warning notice is in position in the cockpit to tell persons not to operate the flight controls.
(2)
Make sure that the Green, Blue and Yellow hydraulic system is depressurized(Ref. TASK 29-00-00-864-001).
(3)
Make sure that the access platform is in position.
(4)
Make sure that the rudder pedals are in the neutral position.
1EFF : ALL 1 55-33-13Page 406 1 1 Nov 01/03R 1 1 1CES 1
Subtask 55-33-13-865-052
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
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(91)
