Installation of the Jet Pump Fuel Control Valve

TASK 28-26-43-400-001-A
Installation of the Jet Pump Fuel Control Valve

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.

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. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.

FIN: 153QM ** ON A/C NOT FOR ALL
FIN: 154QM ** ON A/C NOT FOR ALL

1. Reason for the Job
Self Explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	AR	ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
No specific	AR	CAP - BLANKING
No specific	AR	SAFETY BARRIER(S)
No specific	AR	WARNING NOTICE(S)
No specific	Torque wrench: range to between 0.8 and 0.7 m.daN (70.80 and 61.95 lbf.in )
No specific	Torque wrench: range to between 1.06 and 0.82 m.daN (93.81 and 72.57 lbf.in )
98D28004088000	1	FUEL PUMP ELBOW

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.01ABA1)	Turbine Fuel-- Kerosene -
(Material No.03FAB1)	Mineral Oil base Grease-- Vaseline or Petrolatum -
(Material No.06ABB1)	Polysulfide Sealant-Fuel Tank Fillet -
(Material No.08BAA9)	Non Aqueous Cleaner-General - -
(Material No.14SBA1)	Textile-Lint free Cotton -

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
FOR [153QM] (FUEL CONTROL VALVE-JET PUMP, L WING TK)
195BB
147AZ
FOR [154QM] (FUEL CONTROL VALVE-JET PUMP, R WING TK)
148AZ, 196BB

D. Expendable Parts

FIG.ITEM	DESIGNATION	IPC-CSN
19	O-RING	AIPC 28-26-05-04-040
2	O-RING	AIPC 28-26-05-05-160
5	O-RING	AIPC 28-26-05-06-070
19	O-RING	AIPC 28-26-85-04-030
5	O-RING	AIPC 28-26-85-06-100

E. Referenced Information

REFERENCE	DESIGNATION
TASK 12-11-28-650-003-A	Pressure Refuel with Automatic Control
TASK 20-28-00-912-802-A	Electrical Bonding - General Maintenance Procedure
TASK 28-10-00-910-001-A	Safety Procedures When You Do Work in a Fuel Tank
TASK 28-10-00-910-002-A	Access to the Fuel Tanks and the Work Areas
TASK 28-25-00-650-001-A	Pressure Defuel
TASK 28-25-00-650-003-A	To Drain Remaining Fuel from the Wing Tanks and the Center Tank
TASK 28-25-00-650-003-A-01	To Drain Remaining Fuel from the Wing Tanks and the Center Tank
TASK 28-25-00-869-001-A	Fuel Transfer
TASK 28-26-00-710-001-A	Operational Test of the Main Transfer System
TASK 28-26-51-000-001-A	Removal of the Fuel Control-Valve Actuator
TASK 28-26-51-400-001-A	Installation of the Fuel Control-Valve Actuator
TASK 32-12-00-010-001-A	Open the Main Gear Doors for Access
TASK 32-12-00-410-001-A	Close the Main Gear Doors after Access
TASK 53-35-13-400-002-A	Installation of the Quick-Release Access Panels on the Belly Fairing Structure
TASK 57-17-11-000-001-A	Removal of Access Cover 147AZ(148AZ)
TASK 57-17-11-000-001-B	Removal of Access Cover 148AZ or/and the ACT-Equipment Support Door
TASK 57-17-11-400-001-A	Installation of Access Cover 147AZ(148AZ)
TASK 57-17-11-400-001-B	Installation of Access Cover 148AZ or/and the ACT-Equipment Support-Door
Jet Pump Fuel Control Valve 153 QM (154 QM)

3. Job Set-up
Subtask 28-26-43-941-053-A ** ON A/C NOT FOR ALL

A. Safety Precautions

WARNING: BEFORE YOU DO WORK IN OR NEAR A FUEL TANK, MAKE SURE THAT YOU OBEY ALL THE SAFETY PROCEDURES. THIS WILL PREVENT INJURY TO PERSONS AND/OR DAMAGE TO THE AIRCRAFT.

(1) You must obey the fuel safety procedures (Ref. AMM TASK 28-10-00-910-001) when you do work in a fuel tank.
(2) Make sure that the SAFETY BARRIER(S) are in position.
(3) Make sure that the WARNING NOTICE(S) to tell persons not to operate the MLG doors is in position.

Subtask 28-26-43-860-050-A ** ON A/C NOT FOR ALL

B. Aircraft Maintenance Configuration
(1) Make sure that the center tank and the applicable wing tank are defueled (Ref. AMM TASK 28-25-00-650-001).
(2) Make sure that the remaining fuel has been drained from the applicable wing tank and the center tank (Ref. AMM TASK 28-25-00-650-003).
(3) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is below the applicable access panel 147AZ (148AZ).
(4) Make sure that the applicable MLG door is open (Ref. AMM TASK 32-12-00-010-001).
(5) Make sure that the 460005835 SLEEVE - GROUND LOCK is installed on the applicable MLG door actuating cylinder.
(6) Make sure that the applicable access doors on the access panels 195AB (196AB) are open.
(7) Make sure that the applicable access panel 147AZ (148AZ) is removed (Ref. AMM TASK 28-10-00-910-002), (Ref. AMM TASK 57-17-11-000-001).
(8) Make sure that the actuator (9) is removed (Ref. AMM TASK 28-26-51-000-001).

Subtask 28-26-43-860-050-B ** ON A/C NOT FOR ALL

B. Aircraft Maintenance Configuration
(1) Make sure that the center tank and the applicable wing tank are defueled (Ref. AMM TASK 28-25-00-650-001).
(2) Make sure that the remaining fuel has been drained from the applicable wing tank and the center tank (Ref. AMM TASK 28-25-00-650-003).
(3) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is below the ACT-Equipment Support Door or the access panel 148AZ.
(4) Make sure that the applicable MLG door is open (Ref. AMM TASK 32-12-00-010-001).
(5) Make sure that the 460005835 SLEEVE - GROUND LOCK is installed on the applicable MLG door actuating cylinder.
(6) Make sure that the applicable access doors on the access panels 195AB (196AB) are open.
(7) Make sure that the ACT-Equipment Support Door or access panel 148AZ is removed (Ref. AMM TASK 28-10-00-910-002), (Ref. AMM TASK 57-17-11-000-001).
(8) Make sure that the actuator (9) is removed (Ref. AMM TASK 28-26-51-000-001).

Subtask 28-26-43-865-051-A ** ON A/C NOT FOR ALL

C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
121VU	FUEL/CTR TK/AUTO/CTL	3QL	R27
121VU	FUEL/CTR TK/L&R XFR/CTL & IND	2QL	R26
121VU	FUEL/CTR TK/L&R XFR/CTL & IND	1QL	R25

4. Procedure
Subtask 28-26-43-420-050-A ** ON A/C NOT FOR ALL

A. Preparation for Installation
(1) Clean the component interfaces and the adjacent areas with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
(4) If necessary, install the nut (18) on the valve (21) and install the retaining ring (17).
(5) Lubricate the new AIPC 28-26-05-06-070 O-RING (5) or AIPC 28-26-85-06-100 O-RING (5) with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
(6) Install the new O-ring (5) on the valve (21).
(7) Lubricate the new AIPC 28-26-05-04-040 O-RING (19) or AIPC 28-26-85-04-030 O-RING (19) with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
(8) Install the O-ring (19) on the valve (21).

Subtask 28-26-43-420-051-A ** ON A/C NOT FOR ALL

B. Installation of the Jet Pump Fuel Control Valve 153QM (154QM)
(1) Remove the blanking caps from the pipes (1) and (16) and from the valve (21).
(2) Lubricate the new AIPC 28-26-05-05-160 O-RING (2) with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
(3) Install the new O-ring (23) in the flange of the pipe (1).
(4) Install the valve (21) on the bottom skin (6).
(5) Install the pipe (1) on the valve (21) with the bolts (24) and the nuts (22).
(6) Install the pipe (16) on the valve (21) and fully tighten the nut (18).
(7) Connect the bonding lead (3) to the valve (21) with the bolt (2) and the nut (4) (Ref. AMM TASK 20-28-00-912-802).
(8) Connect the bonding lead (13) and the bonding lead (14) to the valve (21) with the bolt (20) and the nut (15) (Ref. AMM TASK 20-28-00-912-802).
(9) Apply Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the flange of the drive sub-assembly (7).
(10) Install the drive sub-assembly (7) with the nuts (8).
(11) Connect the bonding lead (11) with the bolt (12) and the nut (10) (Ref. AMM TASK 20-28-00-912-802).
(12) Install the actuator (9) (Ref. AMM TASK 28-26-51-400-001).

Subtask 28-26-43-420-051-B ** ON A/C NOT FOR ALL

B. Installation of Jet-Pump Fuel Control-Valve 153QM (154QM)
(1) Remove the CAP - BLANKING from the pipes (1) and (16) and the valve (21).
(2) Lubricate a new AIPC 28-26-05-05-160 O-RING (2) with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
(3) Install the new O-ring (23) in the flange of the pipe (1).
(4) Install the valve (21) on the bottom skin (6).
(5) Install the pipe (1) on the valve (21) with the bolts (24) and the nuts (22).
(6) TORQUE the bolts (24) to between 1.06 and 0.82 m.daN (93.81 and 72.57 lbf.in )

with a 98D28004088000 FUEL PUMP ELBOW.
(7) If removed, install the retaining ring (17) and the nut (18).
(8) Install the pipe (16) on the valve (21) and fully tighten the nut (18).
(9) Connect the bonding lead (3) to the valve (21) with the bolt (2) and the nut (4) (Ref. AMM TASK 20-28-00-912-802).
(10) Tighten the nut (4).
(11) Connect the bonding leads (13) and (14) to the valve (21) with the bolt (20) and the nut (15) (Ref. AMM TASK 20-28-00-912-802).
(12) Tighten the nut (15).
(13) Apply Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the flange of the drive sub-assembly (7).
(14) Install the drive sub-assembly (7) with the nuts (8).
(15) TORQUE the nuts (8) to between 0.8 and 0.7 m.daN (70.80 and 61.95 lbf.in )

.
(16) Connect the bonding lead (11) with the bolt (12) and the nut (10) (Ref. AMM TASK 20-28-00-912-802).
(17) Tighten the nut (10).
(18) Install the actuator (9) on the drive sub-assembly (7) (Ref. AMM TASK 28-26-51-400-001).

Subtask 28-26-43-410-050-A ** ON A/C NOT FOR ALL

C. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable access panel (Ref. AMM TASK 57-17-11-400-001):
(a) FOR [153QM] (FUEL CONTROL VALVE-JET PUMP, L WING TK)
install 147AZ
(b) FOR [154QM] (FUEL CONTROL VALVE-JET PUMP, R WING TK)
install 148AZ.
(3) Close the applicable access door on the access panel 195AB(196AB) (Ref. AMM TASK 53-35-13-400-002):
(a) FOR [153QM] (FUEL CONTROL VALVE-JET PUMP, L WING TK)
close 195BB
(b) FOR [154QM] (FUEL CONTROL VALVE-JET PUMP, R WING TK)
close 196BB.
(4) Remove the access platform(s).
(5) Close the applicable MLG door (Ref. AMM TASK 32-12-00-410-001).

Subtask 28-26-43-410-050-B ** ON A/C NOT FOR ALL

C. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable access panel (Ref. AMM TASK 57-17-11-400-001):
(a) FOR [153QM] (FUEL CONTROL VALVE-JET PUMP, L WING TK)
install the ACT-Equipment Suport Door
(b) FOR [154QM] (FUEL CONTROL VALVE-JET PUMP, R WING TK)
install 148AZ.
(3) Close the applicable access door on the access panel 195AB(196AB) (Ref. AMM TASK 53-35-13-400-002):
(a) FOR [153QM] (FUEL CONTROL VALVE-JET PUMP, L WING TK)
close 195BB
(b) FOR [154QM] (FUEL CONTROL VALVE-JET PUMP, R WING TK)
close 196BB.
(4) Remove the access platform(s).
(5) Close the applicable MLG door (Ref. AMM TASK 32-12-00-410-001).

Subtask 28-26-43-865-052-A ** ON A/C NOT FOR ALL

D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
121VU	FUEL/CTR TK/AUTO/CTL	3QL	R27
121VU	FUEL/CTR TK/L&R XFR/CTL & IND	2QL	R26
121VU	FUEL/CTR TK/L&R XFR/CTL & IND	1QL	R25

Subtask 28-26-43-710-050-A ** ON A/C NOT FOR ALL

E. Test
(1) Do a test of the main transfer system (Ref. AMM TASK 28-26-00-710-001).

5. Close-up
Subtask 28-26-43-650-051-A ** ON A/C NOT FOR ALL

A. Fuel Configuration
(1) Refuel, defuel or transfer fuel as necessary (Ref. AMM TASK 12-11-28-650-003), (Ref. AMM TASK 28-25-00-650-001) or (Ref. AMM TASK 28-25-00-869-001).

Subtask 28-26-43-942-050-A ** ON A/C NOT FOR ALL

B. Removal of Equipment
(1) Remove the safety barriers.
(2) Remove the WARNING NOTICE(S).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.

[Rev.10 from 2021] 2026.04.02 06:17:45 UTC