(11)
 Seal the mounting plate (8) with a blanking cap.

 (12)
 Remove the cloths and put them into an approved container.

 (13)
 If the LP fuel valve is to be replaced, remove the circlip (4) and the nut (13).

 1EFF : ALL 1 28-24-41Page 405 1 1 Aug 01/00 1 1 1CES 1 1EFF : ALL 1 28-24-41Page 406 1 1 May 01/03 1 1 1CES 1

 TASK 28-24-41-400-001
 Installation of the LP Fuel Valve 12QM(13QM)
 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING_______ NOTICES ARE IN POSITION.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING_______ GEAR.
 1. Reason for the Job__________________ 
R R  Self Explanatory
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R  No specific  safety barriers
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R  Material No. 01-001 Material No. 04-012 Material No. 11-026 Material No. 19-003 Material No. 19-010  USA ASTM-D-1655-93 (JET A-1) FUEL, TURBO (Ref. 20-31-00)USA VV-P-236 PURE MINERALVASELINE OR PETRO- LATUM (Ref. 20-31-00) GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)USA AMS 3819 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 O-ring 28-21-05 25 -080 3 O-ring 28-21-05 25 -070 7 O-ring 28-24-05 01A-120
R 7 O-ring  28-24-05 01B-120
 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
12-11-28-650-003  Pressure Refuel with Automatic Control
 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)-
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 28-24-00-710-002 Operational Test of the ENG 1(2) LP Fuel Valve 12QM
 (13QM)
 28-24-51-400-001 Installation of the LP Fuel Valve Actuator
 28-25-00-650-001 Pressure Defuel
 28-25-00-869-001 Fuel Transfer
 57-41-37-000-003 Removal of the Access Panel 522AT(622AT)
 57-41-37-400-003 Installation of the Access Panel 522AT(622AT)
 28-24-41-991-001 Fig. 401

 3. Job Set-up
__________
 Subtask 28-24-41-941-055
 A. Safety Precautions
 (1)
 You must obey the fuel safety procedures (Ref. TASK 28-10-00-910-001) when you do work in a fuel tank.

 (2)
 Make sure that the safety barriers are in position.

 1EFF : ALL 1 28-24-41Page 407 1 1 May 01/04 1 1 1CES 1 Subtask 28-24-41-860-050

 B. Aircraft Maintenance 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).

 (2)
 Make sure that the aircraft electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).

 (3)
 Make sure that the access platform is below the applicable access panel 522AT(622AT).

 (4)
 Make sure that the access panel 522AT(622AT) has been removed (Ref. TASK 57-41-37-000-003).

 Subtask 28-24-41-865-054
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FUEL/LP VALVE/MOT1/ENG2 2QG A09 49VU FUEL/LP VALVE/MOT1/ENG1 1QG A08

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 121VU FUEL/CTR TK/PUMP2 SPLY 30QA P26
　
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