Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
(Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
Material No. 19-004
WHITE TALCUM POWDER (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R 140 seal 57-41-37 02E-260 R 140 seal 57-41-37 02L-260 R 140 seal 57-41-37 02M-260
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
SRM 514211
SRM 514411
SRM 574118
SRM 574126
57-41-37-991-008 Fig. 801
57-41-37-991-009 Fig. 802
57-41-37-991-013 Fig. 803
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
57-41-37-991-016 Fig. 804
**ON A/C 301-399,
57-41-37-991-016-A Fig. 804A R **ON A/C 106-149, 157-199, 209-299, 301-399, 401-499,
57-41-37-991-017 Fig. 805
**ON A/C ALL
57-41-37-991-014 Fig. 806
3. Job Set-up
__________
Subtask 57-41-37-941-054
A. Job Set-up
(1)
Put warning notices in position to tell persons not to operate the slat and the pneumatic systems.
(2)
Put the access platform in position below the applicable pressure-relief panels: For the LH wing
-
below the panels 521AB and 521CB
For the RH wing
-
below the panels 621AB and 621CB.
(1)
Remove the bolts (10).
(2)
Carefully remove the pressure-relief panel 521AB(621AB) (9).
(3)
Remove the bolts (28).
(4)
Carefully remove the pressure-relief panel 521CB(621CB) (30).
(5)
When you remove the pressure-relief panel (30), a part of the landings (20) and (22) will fall. Make a note of the related position of these landings and keep them for later assembly.
Subtask 57-41-37-865-059
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
4. Procedure_________
(Ref. Fig. 801/TASK 57-41-37-991-008, 802/TASK 57-41-37-991-009, 803/TASK 57-41-37-991-013)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 804/TASK 57-41-37-991-016)
**ON A/C 301-399,
(Ref. Fig. 804A/TASK 57-41-37-991-016-A)
R **ON A/C 106-149, 157-199, 209-299, 301-399, 401-499,
(Ref. Fig. 805/TASK 57-41-37-991-017)
**ON A/C 001-049, 051-099, 101-105, 151-156, 201-208,
Subtask 57-41-37-350-052
R R A. Repair of the Leading Edge Pressure-Relief Panel 521CB(621CB) After it has Operated
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.
NOTE : The two parts of the landing (25) are connected by lanyards.
____
(6)
Remove the nuts (21) and the bolts (35) (Ref. SRM 514211).
(7)
Remove the part of the landing (20) that is attached to the aircraft structure.
(8)
Remove the nuts (26) and the bolts (27) (Ref. SRM 514211).
(9)
Remove the landing (25).
(10)
Remove the nuts (23) and the bolts (24) (Ref. SRM 514211).
(11)
Remove the part of the landing (22) that is attached to the aircraft structure.
(12)
Remove and discard the rivets (29) (Ref. SRM 514211).
(13)
Remove and discard the forward angle (31).
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