Operational Test of the APU Fuel-Pump System on Ground to Purge the Fuel Line
TASK 28-22-00-710-001-A
Operational Test of the APU Fuel-Pump System on Ground to Purge the Fuel Line
Self Explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 28-22-00-860-052-A
Subtask 28-22-00-710-050-A
Subtask 28-22-00-860-053-A
[Rev.10 from 2021]
2026.04.01 04:21:35 UTC
Operational Test of the APU Fuel-Pump System on Ground to Purge the Fuel Line
WARNING:
OBEY THE FUEL SAFETY PROCEDURES.
1. Reason for the JobSelf Explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 3M (10 FT) |
| No specific | AR | CONTAINER 5 L (1.32 USGAL) |
| 98A28007570000 | 1 | ADAPTER - VENT AND DRAIN VALVE, APU |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 315AL, 316AR |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| TASK 24-41-00-862-002-A-01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| TASK 24-41-00-862-002-A-02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
| TASK 52-41-00-010-001-A | Open the APU Doors for Access |
| TASK 52-41-00-410-001-A | Close the APU Doors after Access |
Subtask 28-22-00-860-052-A
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) On the APU section of the overhead panel 25VU, make sure that the APU MASTER SW is in the off position (the ON legend is off).
(3) On the FUEL overhead panel 40VU, make sure that all L TK PUMPS and R TK PUMPS pushbutton switches are released (the OFF legends are on).
Subtask 28-22-00-865-050-A (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) On the APU section of the overhead panel 25VU, make sure that the APU MASTER SW is in the off position (the ON legend is off).
(3) On the FUEL overhead panel 40VU, make sure that all L TK PUMPS and R TK PUMPS pushbutton switches are released (the OFF legends are on).
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 28-22-00-010-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | APU/FUEL/BLOW OFF/PUMP | 2QC | B14 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | APU/FUEL/BLOW OFF/CTL | 1QC | K39 |
| ** ON A/C ALL | |||
| 121VU | APU/APU/CTL | 2KD | L42 |
| 121VU | APU/ECB/SPLY | 1KD | L41 |
| 121VU | APU/FUEL/LP VALVE/CTL | 1QF | M40 |
| 121VU | APU/FUEL/LP VALVE/SPLY | 2QF | M39 |
| 121VU | APU/FUEL/PUMP/CTL | 3QC | M38 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | APU/FUEL/BLOW OFF/CTL | 1QC | P38 |
C. Get Access
(2) Open the APU access doors 315AL 316AR (Ref. AMM TASK 52-41-00-010-001).
(3) Remove the blanking plug from the APU fuel vent and drain valve and install the 98A28007570000 ADAPTER - VENT AND DRAIN VALVE, APU.
(4) Put a CONTAINER 5 L (1.32 USGAL) below the APU fuel vent and drain valve to collect the fuel.
(5) Make sure that the outlet from the drain mast at FR47 has no blockage.
4. ProcedureWARNING:
LOCK THE MECHANISM OF THE ACCESS DOOR 316AR WITH THE PIP PIN WHEN YOU OPEN THE ACCESS DOOR. THIS WILL PREVENT INJURY.
(1) Put the ACCESS PLATFORM 3M (10 FT) in position below the APU compartment. (2) Open the APU access doors 315AL 316AR (Ref. AMM TASK 52-41-00-010-001).
(3) Remove the blanking plug from the APU fuel vent and drain valve and install the 98A28007570000 ADAPTER - VENT AND DRAIN VALVE, APU.
(4) Put a CONTAINER 5 L (1.32 USGAL) below the APU fuel vent and drain valve to collect the fuel.
(5) Make sure that the outlet from the drain mast at FR47 has no blockage.
Subtask 28-22-00-710-050-A
A. Do this test.
5. Close-up| ACTION | RESULT |
|---|---|
1.On the front firewall FR80 in the APU compartment:
| At the APU fuel vent and drain valve:
|
2.On the front firewall FR80 in the APU compartment:
| At the APU fuel vent and drain valve:
|
Subtask 28-22-00-860-053-A
A. Put the aircraft back to its initial configuration.
(1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(2) Put the system back to the serviceable condition.
Subtask 28-22-00-410-050-A (1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(2) Put the system back to the serviceable condition.
B. Close Access
(1) Remove the 98A28007570000 ADAPTER - VENT AND DRAIN VALVE, APU and replace the blanking plug and tighten.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Close the APU access doors 315AL 316AR (Ref. AMM TASK 52-41-00-410-001).
(4) Remove the access platform(s).
(1) Remove the 98A28007570000 ADAPTER - VENT AND DRAIN VALVE, APU and replace the blanking plug and tighten.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Close the APU access doors 315AL 316AR (Ref. AMM TASK 52-41-00-410-001).
(4) Remove the access platform(s).