国内精品♨️_崩380级突破_.手.动.输.入.网.址.联.系.客.服.人.员.lanan_shell
-the clearance between the wing-skin and the edges of the panels. The clearance must be not less than 0.5 mm (0.0196 in.). Subtask 57-41-37-390-050 B. Seal Installation (Ref. Fig. 805/TASK 57-41-37-991-017)
NOTE : The procedure that follows can be done at the subsequent servicing ____ interval.
NOTE : Seal only the clearance between the trailing edge of the ____ pressure-relief panels and the wing skin.
(1) Fully degrease the area to be filled with a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026).
(2) Apply masking tape around the edges of the area to be filled.
(3) Use a spatula or extrusion gun to insert SEALANTS (Material No. 09-002B) or SEALANTS (Material No. 09-016) into the applicable prepared area.
(4) Use a non-metallic scraper to remove unwanted sealant before it cures.
(5) Let the sealant cure (refer to the manufacturers instructions).
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(6) Make sure the surface of the seal is flush with the surfaces of the applicable pressure-relief panel (9) and/or (30) and the wing skin.
(7) Remove the masking tape from the area around the seal.
(8) Remove the applicable bolts (10) and/or (28).
(9) Remove the applicable pressure-relief panel (9) and/or (30). Use a suction cup if necessary.
(10) Examine the seal to make sure that:
- there is a full strip of sealant along the trailing edge of the panel opening
- there are no bubbles or spaces in the sealant
-no parts of the seal are loose.
(11) If the sealant does not make a full strip, or there are bubbles or spaces, or the seal is loose:
(a) Use a non-metallic scraper to remove the seal.
(b) Do again steps (1) thru (11).
(12) Apply talcum powder MISCELLANEOUS (Material No. 19-004) to the mating surface of the seal.
(13) Install the applicable pressure-relief panel (9) and/or (30) with the applicable bolts (10) and/or (28).
**ON A/C ALL 5. Close-up ________ Subtask 57-41-37-865-058 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV. Subtask 57-41-37-942-053 B. Removal of Equipment (1) Remove the access platform(s).
(2) Remove the warning notice(s).
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(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
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TASK 57-41-37-350-002
Repair to the Leading Edge Pressure-Relief Panel 521CB(621CB) After it has Operated 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. 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 cutting tool No specific extrusion gun No specific lint-free cloth No specific masking tape No specific non metallic scraper No specific non-metallic scraper No specific spatula No specific suction cup No specific warning notices No specific access platform 2.5 m (8 ft. 2 in.) 1EFF : ALL 1 57-41-37Page 829 1 1 May 01/04R 1 1 1CES 1
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------- Material No. 05-064 GB ABP1-4053 RELEASE AGENT (Ref. 20-31-00) Material No. 09-001 USA MIL-S-8802 TYPE I CLASS A FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00) Material No. 09-002B F ASNA 0163 FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00)
