is turned and pushed into the canister during the fuel pump installation procedure.
R (18) Remove the EXTRACTOR TOOL from the fuel pump (2).
R (19) Remove and discard the O-rings (1), (11) and (10) from the fuel pump (2).
R (20) Examine the fuel pump (2) and the adjacent aircraft structure for signs of fuel leakage.
R (21) If fuel leakage is found, examine the applicable landing light assembly for fuel contamination (Ref. TASK 33-42-11-000-001).
Installation of the Fuel Pumps 21QA(26QA) and 25QA(22QA)
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE LANDING GEAR ARE CLEAR.
_______
CAUTION : WHEN YOU REPLACE THE FUEL PUMP(S) 21QA(26QA) OR 25QA(22QA), EXAMINE
_______ THE APPLICABLE LANDING LIGHT ASSEMBLY FOR SIGNS OF FUEL CONTAMINATION. IF YOU FIND FUEL CONTAMINATION, EXAMINE THE ITEMS THAT FOLLOW FOR SIGNS OF FUEL LEAKAGE:
-
THE FUEL PUMP(S) 21QA(26QA) OR 25QA(22QA)
-
THE WATER DRAIN VALVE 25QM(26QM) DIRECTLY FORWARD OF THE LANDING
LIGHT ASSEMBLY.
REFER TO AMM 28-11-00-06 FOR LEAKAGE LIMITS AND REPAIR AS NECESSARY.
IF YOU DO NOT REPAIR THE LEAK, NO PERSONS MUST OPERATE THE APPLICABLE
LANDING LIGHT UNTIL:
-
THE LEAK IS REPAIRED
-
THE LANDING LIGHT ASSEMBLY IS REPLACED.
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 access platform 2.8 m (9 ft. 2 in.)
No specific Torque Wrench : range 0.00 to 1.20 m.daN
(0.00 to 9.00 lbf.ft)
R 558-1-05903 1 EXTRACTOR - FUEL PUMP 558-1-05903-002 1 EXTRACTOR TOOL
1EFF : ALL 1 28-21-51Page 410 1 1 Aug 01/05 1 1 1CES 1 B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 01-001 USA ASTM-D-1655-93 (JET A-1) FUEL, TURBO (Ref. 20-31-00) Material No. 04-012 USA VV-P-236 PURE MINERALVASELINE OR PETRO- LATUM (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. 19-010 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ---------------------------------------- |IPC-CSN------------------------------
1 O-ring 28-21-51 01 -010
9 O-ring 28-21-51 01 -100
9 O-ring 28-21-51 01 -100A
10 O-ring 28-21-51 01 -020
10 O-ring 28-21-51 01 -020A
11 O-ring 28-21-51 01 -020
11 O-ring 28-21-51 01 -020A
D. Referenced Information
------------------REFERENCE -------------------------------DESIGNATION ------------------------------
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