1EFF : ALL 1 28-24-41Page 401 1 1 Aug 01/00 1 1 1CES 1 B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 28-10-00-910-001 Safety Procedures When You Do Work in a Fuel Tank 28-24-51-000-001 Removal of the LP Fuel Valve Actuator 28-25-00-650-001 Pressure Defuel 28-25-00-869-001 Fuel Transfer
R 57-41-37-000-003 Removal of the Access Panel 522AT(622AT) 28-24-41-991-001 Fig. 401
3. Job Set-up
__________
(Ref. Fig. 401/TASK 28-24-41-991-001)
Subtask 28-24-41-941-054
A. Safety Precautions
WARNING : OBEY THE SAFETY PROCEDURES WHEN YOU DO WORK IN A FUEL TANK.
_______
(1)
You must obey the fuel safety procedures (Ref. TASK 28-10-00-910-001) when you do work in a fuel tank.
(2)
Put the safety barriers in position.
Subtask 28-24-41-861-050
B. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
Subtask 28-24-41-650-052
C. Fuel Configuration
(1) Make sure that there is not more than approximately 3500 kg (7716.1770 lb) of fuel in the applicable tank. If necessary, move the fuel to the opposite tank (Ref. TASK 28-25-00-869-001) or defuel (Ref. TASK 28-25-00-650-001).
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LP Fuel Valve 12QM (13QM)
Figure 401/TASK 28-24-41-991-001
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1 1 Feb 01/98
1 1
1CES 1
Subtask 28-24-41-010-052
D. Get Access
(1)
Put the access platform in position below the applicable access panel 522AT(622AT).
(2)
Remove the access panel 522AT(622AT) (Ref. TASK 57-41-37-000-003).
Subtask 28-24-41-865-050
E. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU FUEL/L WING TK/PUMP2 SPLY 7QA N26 121VU FUEL/L WING TK/PUMP1 SPLY 1QA N23 121VU FUEL/R WING TK/PUMP2 SPLY 8QA Q26 121VU FUEL/R WING TK/PUMP1 SPLY 2QA Q23
FOR 12QM 49VU FUEL/LP VALVE/MOT1/ENG1 1QG A08 121VU FUEL/LP VALVE/MOT2/ENG1 3QG M25 FOR 13QM 49VU FUEL/LP VALVE/MOT1/ENG2 2QG A09
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
121VU FUEL/CTR TK/PUMP2 SPLY 30QA P26 121VU FUEL/CTR TK/PUMP1 SPLY 29QA P23
**ON A/C ALL
121VU FUEL/LP VALVE/MOT2/ENG2 4QG M26
Subtask 28-24-41-210-054
F. General Check
(1) On the fuel control panel, 40VU:
-make sure that the ON and OPEN legends on the crossfeed valve pushbutton switch are off.
Subtask 28-24-41-862-050
G. De-energize the Electrical Circuits
(1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
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4. Procedure
_________
(Ref. Fig. 401/TASK 28-24-41-991-001)
Subtask 28-24-41-020-052 R A. Removal of the LP Fuel Valve 12QM(13QM) R (1) Remove the LP fuel-valve actuator 9QG(10QG) (Ref. TASK 28-24-51-000-
001).
(2)
Put a cloth below the LP fuel valve (12).
(3)
Remove the screw (11) and the nut (9) then disconnect the end of the bonding strips (6) and (10).
(4)
Cut and discard the lockwire from the nuts (13) and (15).
(5)
Hold the connector (14) and release the nut (13) from the connector.
(6)
Slowly move the pipe assembly (1) away from the LP fuel valve (12) until fuel leakage occurs. Soak up all the fuel from the pipe with the cloth. When all the fuel has been removed, pull the pipe (1) as far as possible, away from the LP fuel valve (12).
(7)
Remove and discard the O-rings (2) and (3).
(8)
Seal the pipe (1) with a blanking cap.
(9)
Remove the bolts (5).
(10)
Remove the LP fuel valve (12) and discard the O-ring (7). Make sure that you soak up the fuel from the LP fuel valve with a cloth.
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