57-41-37-991-014 Fig. 806
57-41-37-991-011 Fig. 808
3. Job Set-up
__________
Subtask 57-41-37-941-056
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 panel 522AB(622AB).
Subtask 57-41-37-865-063
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. 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 ALL
(Ref. Fig. 806/TASK 57-41-37-991-014, 808/TASK 57-41-37-991-011)
Leading Edge Pressure-Relief Panel 522AB(622AB) - Location and Detail Figure 808/TASK 57-41-37-991-011
1EFF : ALL 1 57-41-37Page 868 1 1 May 01/05R 1 1 1CES 1
R **ON A/C 001-049, 051-099, 101-105, 151-156, 201-208,
Subtask 57-41-37-350-054 R A. Repair of the Leading Edge Pressure-Relief Panel 522AB(622AB) After it R 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.
(1)
Remove the bolts (80).
(2)
Carefully remove the pressure-relief panel 522AB(622AB) (79).
(3)
When you remove the pressure-relief panel (79), a part of the landing
(73) will fall. Make a note of the position of this and keep it landing for later assembly.
NOTE : The two parts of the landings (71), (77) and (88) are
____
connected with lanyards.
(4)
Remove the nuts (70) and the bolts (87) (Ref. SRM 514211).
(5)
Remove the landing (88).
(6)
Remove the nuts (72) and the bolts (85) (Ref. SRM 514211).
(7)
Remove the landing (71).
(8)
Remove the nuts (76) and the bolts (75) (Ref. SRM 514211).
(9)
Remove the landing (77).
(10)
Remove bolts (74) and (84) (Ref. SRM 514211).
(11)
Remove the landing (73).
(12)
Remove and discard the rivets (78) (Ref. SRM 514211).
R 1EFF : 001-049, 051-099, 101-105, 151-156, 1 57-41-37Page 869 1201-208, 1May 01/05 1 1 1CES 1
(13)
Remove and discard the forward angle (82).
(14)
Remove and discard the rivets (83) (Ref. SRM 514211).
(15)
Remove and discard the forward angle (86).
(16)
Clean these items with a lint-free cloth made moist with CLEANING AGENTS (Material No. 11-026):
-
the forward sub-spar (81)
-
the landings (71), (73), (77) and (88)
-
the landing (71), (73), (77) and (88) interfaces and the adjacent areas.
(17)
Examine the two parts of the landings (71), (73), (77) and (88) for damage, discard those that are damaged.
(18)
Assemble the landings (71), (73), (77) and (88) as follows:
(a)
Put the two parts of the applicable landing together.
(b)
Install the spacers (122) and the washers (121).
(c)
Install the shear rivets (120) (Ref. SRM 514211).
(d)
Make sure that the two parts of the landings can move on the spacers (122).
(19)
Examine the pressure-relief panel (79) for damage. Discard it if it is damaged.
(20)
Put the new plate nuts (130) and the new spacers (131) in position on the new forward angle (82) (Ref. SRM 574118).
(21)
Install the rivets (132) (Ref. SRM 514211).
(22)
Apply SEALANTS (Material No. 09-001) to the mating faces of the forward angle (82) and the forward sub-spar (81).
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