WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
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-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
No specific warning notices
No specific access platform 3 m (9 ft. 10 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft) No specific Torque Wrench : range 2.00 to 20.00 m.daN
(15.00 to 150.00 lbf.ft) 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 98D57004037000 1 EXTRACTOR FLAP SPIGOT B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116
Material No. 09-001 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)USA MIL-S-8802 TYPE I CLASS A
Material No. 09-018 FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00)USA AMS 3267/3 CORROSION INHIBITING LOW ADHESION SEALANT
Material No. 11-026 Material No. 19-003 (Ref. 20-31-00)GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)USA AMS 3819
Material No. 19-010 LINT-FREE COTTON CLOTH (Ref. 20-31-00)USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
2 cotter pin
R 2 cotter pin
2 cotter pin
R 2 cotter pin
5 cotter pins
R 5 cotter pins
5 cotter pins
R 5 cotter pins
16 cotter pins
R 16 cotter pins
16 cotter pins
R 16 cotter pins
23 cotter pin
R 23 cotter pin
24 cotter pin
24 cotter pin
R 24 cotter pin
27 cotter pin
R 27 cotter pin
28 cotter pin
57-51-05 75C-040 57-51-05 75D-04057-51-09 21 -060 57-51-09 21A-06057-51-05 75C-070 57-51-05 75D-07057-51-09 21 -090 57-51-09 21A-09057-51-05 75C-070 57-51-05 75D-07057-51-09 21 -090 57-51-09 21A-09057-51-33 22 -010 57-51-33 22A-01057-51-33 02B-01057-51-33 02C-010 57-51-33 02D-01057-51-33 22 -230 57-51-33 22A-23057-51-33 22 -230 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
cotter pin 57-51-33 22A-230
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)-
27-54-46-000-001 Removal of the Nos. 2, 3 and 4 Flap Carriages 27-54-46-400-001 Installation of the Nos 2, 3 and 4 Flap Carriages 27-54-49-400-002 Installation of the Flap Track 2 Actuator
6211CM(6261CM) 57-55-11-000-001 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-000-004 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-400-001 Installation of the Flap Track Fairings Nos. 2, 3 and
4 57-55-11-400-004 Installation of the Flap Track Fairings Nos. 2, 3 and 4
**ON A/C 301-399,
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