Removal of the Fuel Quantity Probes of the ACT (AFT Cargo Compartment)
TASK 28-42-24-000-003-A
Removal of the Fuel Quantity Probes of the ACT (AFT Cargo Compartment)
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 28-42-24-860-055-B ** ON A/C NOT FOR ALL
Subtask 28-42-24-020-052-B ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:18:08 UTC
Removal of the Fuel Quantity Probes of the ACT (AFT Cargo Compartment)
WARNING:
BE CAREFUL NOT TO GET AIRCRAFT FUEL IN YOUR MOUTH OR IN YOUR EYES.
IF YOU GET FUEL ON YOUR SKIN OR ON YOUR CLOTHES, FLUSH IT IMMEDIATELY WITH WATER.
IF NECESSARY, GET MEDICAL HELP.
AIRCRAFT FUEL IS POISONOUS.
WARNING:
DO NOT GET YOUR CLOTHES SOAKED WITH FUEL.
WARNING:
MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT AVAILABLE.
WARNING:
OBEY THE FUEL SAFETY PROCEDURES.
ZONE: 130
ZONE: 150
ZONE: 160
FIN: 69QT ** ON A/C NOT FOR ALL
FIN: 70QT ** ON A/C NOT FOR ALL
FIN: 71QT ** ON A/C NOT FOR ALL
FIN: 72QT ** ON A/C NOT FOR ALL
1. Reason for the JobZONE: 150
ZONE: 160
FIN: 69QT ** ON A/C NOT FOR ALL
FIN: 70QT ** ON A/C NOT FOR ALL
FIN: 71QT ** ON A/C NOT FOR ALL
FIN: 72QT ** ON A/C NOT FOR ALL
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | CAP - BLANKING |
| No specific | AR | PLUG - BLANKING |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | AR | WARNING NOTICE(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 130 | FWD CARGO COMPT AFT BULKHEAD OF AVNCS COMPT TO FWD PRESSURE BULKHEAD OF WING CENTER BOX |
| 150 | AFT CARGO COMPARTMENT FWD PRESS BULKHEAD TO AFT BULKHEAD OF AFT CARGO COMPARTMENT |
| 160 | BULK CARGO COMPARTMENT AFT BULKHEAD OF AFT CARGO COMPARTMENT TO AFT BULKHEAD OF BULK CARGO COMPARTMENT |
| FOR [69QT] (PROBE-FQI NO 1, ACT1) | |
| 151AY, 251BG, 251CG, 251DG, 251TG | |
| FOR [70QT] (PROBE-FQI NO 2, ACT1) | |
| 151AY, 251TG, 252BG, 252CG, 252DG | |
| FOR [71QT] (PROBE-FQI NO.1, ACT 2) | |
| 151AC, 251AF, 251BF, 251CF, 251DF, 251EG | |
| FOR [72QT] (PROBE-FQI NO.2, ACT 2) | |
| 151AC, 251AF, 252BF, 252CF, 252EF, 252EG | |
| 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 28-00-00-910-001-A | Fuel Safety Procedures |
| 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 28-28-00-00 | ADDITIONAL CENTER TANK TRANSFER SYSTEM - DESCRIPTION AND OPERATION |
| FOR [69QT] (PROBE-FQI NO 1, ACT1) | |
| TASK 25-28-41-000-001-A | Removal of the Textile Floor Covering |
| TASK 25-55-11-000-002-A | Removal of the Ceiling Panels in the Aft Cargo-Compartment - FR47/FR59 |
| TASK 53-00-00-000-801-A-01 | Removal of the Floor Panels in the Cabin from FR12 to FR70 (Alternative Removal Procedure - Dry Sealing Concept) |
| FOR [70QT] (PROBE-FQI NO 2, ACT1) | |
| TASK 25-28-41-000-001-A | Removal of the Textile Floor Covering |
| TASK 25-55-11-000-002-A | Removal of the Ceiling Panels in the Aft Cargo-Compartment - FR47/FR59 |
| TASK 53-00-00-000-801-A-01 | Removal of the Floor Panels in the Cabin from FR12 to FR70 (Alternative Removal Procedure - Dry Sealing Concept) |
| FOR [71QT] (PROBE-FQI NO.1, ACT 2) | |
| TASK 25-28-41-000-001-A | Removal of the Textile Floor Covering |
| TASK 25-55-11-000-002-A | Removal of the Ceiling Panels in the Aft Cargo-Compartment - FR47/FR59 |
| TASK 53-00-00-000-801-A-01 | Removal of the Floor Panels in the Cabin from FR12 to FR70 (Alternative Removal Procedure - Dry Sealing Concept) |
| FOR [72QT] (PROBE-FQI NO.2, ACT 2) | |
| TASK 25-28-41-000-001-A | Removal of the Textile Floor Covering |
| TASK 25-55-11-000-002-A | Removal of the Ceiling Panels in the Aft Cargo-Compartment - FR47/FR59 |
| TASK 53-00-00-000-801-A-01 | Removal of the Floor Panels in the Cabin from FR12 to FR70 (Alternative Removal Procedure - Dry Sealing Concept) |
Subtask 28-42-24-860-055-B ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Obey the fuel safety procedures (Ref. AMM TASK 28-00-00-910-001).
(2) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(3) Defuel the applicable Additional Center Tank (ACT) (Ref. AMM TASK 28-25-00-650-001).
(4) Drain the remaining fuel from the ACT (Ref. AMM TASK 28-25-00-650-003).
(5) Put the WARNING NOTICE(S) on the panels that follow, to tell persons not to operate the fuel system:
- Refuel/Defuel panels 800VU and 801VU
- Fuel control panel 40VU
- ACT control panel 28VU.
Subtask 28-42-24-865-062-A ** ON A/C NOT FOR ALL (1) Obey the fuel safety procedures (Ref. AMM TASK 28-00-00-910-001).
(2) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(3) Defuel the applicable Additional Center Tank (ACT) (Ref. AMM TASK 28-25-00-650-001).
(4) Drain the remaining fuel from the ACT (Ref. AMM TASK 28-25-00-650-003).
(5) Put the WARNING NOTICE(S) on the panels that follow, to tell persons not to operate the fuel system:
- Refuel/Defuel panels 800VU and 801VU
- Fuel control panel 40VU
- ACT control panel 28VU.
B. Open, safety and tag this(these) circuit breaker(s):
Subtask 28-42-24-010-053-C ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | FUEL/ACT AIR SOV/MAN/SPLY | 64QH | J20 |
| 121VU | FUEL/ACT AIR SOV/AUTO/SPLY | 63QH | J19 |
| 121VU | FUEL/ACT XFR VLV/MOT2 | 66QH | J18 |
| 121VU | FUEL/ACT XFR VLV/MOT1 | 65QH | J17 |
| 121VU | FUEL/INLET VLV MOT2 AUTO SP AFT 2 | 44QH2 | K16 |
| 121VU | FUEL/INLET VLV MOT2 AUTO SP AFT 1 | 44QH1 | K15 |
| 121VU | FUEL/INLET VLV/MOT1/AFT 2 | 84QH | L29 |
| 121VU | FUEL/INLET VLV/MOT1/MAN SPLY/AFT 1 | 46QH | L28 |
| 121VU | FUEL/HI/LVL/SPLY | 1QJ | L24 |
| 121VU | FUEL/RFL/DFL/SPLY | 2QU | L23 |
| 121VU | FUEL/RFL/DFL/XFR/DEFUEL/VALVE | 1QU | L22 |
| 121VU | FUEL/ACT VENT VLV/MAN/SPLY | 62QH | L21 |
| 121VU | FUEL/ACT VENT VLV/AUTO/SPLY | 61QH | L20 |
| 121VU | FUEL/INLET VLV MAN CTL SPLY AFT 2 | 81QH | L16 |
| 121VU | FUEL/INLET VLV MAN CTL SPLY AFT 1 | 45QH | L15 |
| 121VU | FUEL/ACT/FUEL PUMP/SPLY | 25QH | Q29 |
C. Get Access
(1) For the location of the ACT AFT1 and ACT AFT2 refer to Para. Component Location (Ref. AMM D/O 28-28-00-00).
(2) FOR [69QT] (PROBE-FQI NO 1, ACT1)
(a) Remove the sufficient carpet from the passenger compartment floor to get access to cabin floor panels 251TG, 251BG, 251CG and 251DG (Ref. AMM TASK 25-28-41-000-001).
(b) Remove cabin floor panels 251TG, 251BG, 251CG and 251DG (Ref. AMM TASK 53-00-00-000-801).
(c) Remove cargo-compartment ceiling panel 151AY (Ref. AMM TASK 25-55-11-000-002).
(3) FOR [70QT] (PROBE-FQI NO 2, ACT1)
(a) Remove the sufficient carpet from the passenger compartment floor to get access to cabin floor panels 252DG, 252CG, 252BG and 251TG (Ref. AMM TASK 25-28-41-000-001).
(b) Remove cabin floor panels 252DG, 252CG, 252BG and 251TG (Ref. AMM TASK 53-00-00-000-801).
(c) Remove cargo-compartment ceiling panel 151AY (Ref. AMM TASK 25-55-11-000-002).
(4) FOR [71QT] (PROBE-FQI NO.1, ACT 2)
(a) Remove the sufficient carpet from the passenger compartment floor to get access to cabin floor panels 251AF, 251BF, 251CF, 251DF and 251EG (Ref. AMM TASK 25-28-41-000-001).
(b) Remove cabin floor panels 251AF, 251BF, 251CF, 251DF and 251EG (Ref. AMM TASK 53-00-00-000-801).
(c) Remove cargo-compartment ceiling panel 151AC (Ref. AMM TASK 25-55-11-000-002).
(5) FOR [72QT] (PROBE-FQI NO.2, ACT 2)
(a) Remove the sufficient carpet from the passenger compartment floor to get access to cabin floor panels 252EG, 252EF, 252CF, 252BF and 251AF (Ref. AMM TASK 25-28-41-000-001).
(b) Remove cabin floor panels 252EG, 252EF, 252CF, 252BF and 251AF (Ref. AMM TASK 53-00-00-000-801).
(c) Remove cargo-compartment ceiling panel 151AC (Ref. AMM TASK 25-55-11-000-002).
4. Procedure(1) For the location of the ACT AFT1 and ACT AFT2 refer to Para. Component Location (Ref. AMM D/O 28-28-00-00).
(2) FOR [69QT] (PROBE-FQI NO 1, ACT1)
(a) Remove the sufficient carpet from the passenger compartment floor to get access to cabin floor panels 251TG, 251BG, 251CG and 251DG (Ref. AMM TASK 25-28-41-000-001).
(b) Remove cabin floor panels 251TG, 251BG, 251CG and 251DG (Ref. AMM TASK 53-00-00-000-801).
(c) Remove cargo-compartment ceiling panel 151AY (Ref. AMM TASK 25-55-11-000-002).
(3) FOR [70QT] (PROBE-FQI NO 2, ACT1)
(a) Remove the sufficient carpet from the passenger compartment floor to get access to cabin floor panels 252DG, 252CG, 252BG and 251TG (Ref. AMM TASK 25-28-41-000-001).
(b) Remove cabin floor panels 252DG, 252CG, 252BG and 251TG (Ref. AMM TASK 53-00-00-000-801).
(c) Remove cargo-compartment ceiling panel 151AY (Ref. AMM TASK 25-55-11-000-002).
(4) FOR [71QT] (PROBE-FQI NO.1, ACT 2)
(a) Remove the sufficient carpet from the passenger compartment floor to get access to cabin floor panels 251AF, 251BF, 251CF, 251DF and 251EG (Ref. AMM TASK 25-28-41-000-001).
(b) Remove cabin floor panels 251AF, 251BF, 251CF, 251DF and 251EG (Ref. AMM TASK 53-00-00-000-801).
(c) Remove cargo-compartment ceiling panel 151AC (Ref. AMM TASK 25-55-11-000-002).
(5) FOR [72QT] (PROBE-FQI NO.2, ACT 2)
(a) Remove the sufficient carpet from the passenger compartment floor to get access to cabin floor panels 252EG, 252EF, 252CF, 252BF and 251AF (Ref. AMM TASK 25-28-41-000-001).
(b) Remove cabin floor panels 252EG, 252EF, 252CF, 252BF and 251AF (Ref. AMM TASK 53-00-00-000-801).
(c) Remove cargo-compartment ceiling panel 151AC (Ref. AMM TASK 25-55-11-000-002).
Subtask 28-42-24-020-052-B ** ON A/C NOT FOR ALL
A. Removal of the Fuel Quantity Indicator (FQI) Probe
(b) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
(2) Remove the bolts (3), the washer (4) and the bonding strap (5) from the flange (8) of the FQI probe (9).
(3) Remove and discard the sealing rings (12).
(4) Safety the bonding strap (5) to the ACT structure.
(5) Carefully remove the FQI probe (9) from the funnel (10) of the ACT base plate (11).
(6) Remove and discard the O-rings (6) and (7).
(7) Put the PLUG-BLANKING in each disconnected line end.
NOTE: The subsequent procedure is the same for each tank. Therefore only one is given.
(1) Disconnect the electrical connections: CAUTION:
MAKE SURE THAT THE ELECTRICAL CONNECTOR(S) IS(ARE) DISCONNECTED BEFORE YOU DISCONNECT THE BONDING STRAP(S).
CAUTION:
MAKE SURE THAT THE ELECTRICAL CONNECTORS ARE CLEAN BEFORE YOU DISCONNECT OR CONNECT THEM. CONTAMINATION ON THE ELECTRICAL CONNECTORS CAN CAUSE DAMAGE TO EQUIPMENT.
(a) Disconnect the electrical connector (1) from the receptacle (2). (b) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
(2) Remove the bolts (3), the washer (4) and the bonding strap (5) from the flange (8) of the FQI probe (9).
(3) Remove and discard the sealing rings (12).
(4) Safety the bonding strap (5) to the ACT structure.
(5) Carefully remove the FQI probe (9) from the funnel (10) of the ACT base plate (11).
(6) Remove and discard the O-rings (6) and (7).
(7) Put the PLUG-BLANKING in each disconnected line end.
Fuel Quantity Probe of the ACT (AFT Cargo Compartment)