Inspection of the Tank Venting System
TASK 28-12-00-200-001-A
Inspection of the Tank Venting System
To make sure that the tank venting system is serviceable and is not blocked.
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 28-12-00-941-050-A ** ON A/C NOT FOR ALL
Subtask 28-12-00-210-050-B ** ON A/C NOT FOR ALL
Subtask 28-12-00-410-050-B ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 07:02:01 UTC
Inspection of the Tank Venting System
WARNING:
OBEY THE FUEL SAFETY PROCEDURES.
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.
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:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
1. Reason for the Job- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
To make sure that the tank venting system is serviceable and is not blocked.
NOTE: For the New Engine Option (NEO) aircraft with an Additional Center Tank (ACT) installed in the forward cargo compartment, the term ACT FWD can also be described as ACT 4.1.
2. Job Set-up InformationA. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | WARNING NOTICE(S) |
| 98D57004014000 | 2 | HOOK-COVER (RIB2-SURGE DOORS) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 130 | FWD CARGO COMPT AFT BULKHEAD OF AVNCS COMPT TO FWD PRESSURE BULKHEAD OF WING CENTER BOX |
| 140 | CENTER WING |
| 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 |
| 500 | LEFT WING |
| 600 | RIGHT WING |
| 540BZ, 640BZ | |
| 147AZ | |
| 826 | |
| 148AZ |
| 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 28-00-00-910-001-A | Fuel Safety Procedures |
| 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 28-10-00-910-003-A | Safety Procedures When You Do Work in a Dry Fuel Tank |
| TASK 28-11-27-000-001-A | Removal of the Additional Center Tank (ACT) |
| TASK 28-11-27-000-002-A | Removal of Additional Center Tank No.1 (ACT AFT1) |
| TASK 28-11-27-000-003-A | Removal of the Additional Center Tank No.2 (ACT AFT2) |
| TASK 28-11-27-400-001-A | Installation of the Additional Center Tank (ACT) |
| TASK 28-11-27-400-002-A | Installation of Additional Center Tank No.1 (ACT AFT1) |
| TASK 28-11-27-400-003-A | Installation of the Additional Center Tank No.2 (ACT AFT2) |
| TASK 28-11-37-000-001-A | Removal of the Inner Manhole-Cover ACT |
| TASK 28-11-37-000-004-A | Removal of the Outer Manhole-Cover ACT |
| TASK 28-11-37-400-001-A | Installation of the Inner Manhole-Cover ACT |
| TASK 28-11-37-400-004-A | Installation of the Outer Manhole Cover ACT |
| TASK 28-12-41-200-001-A | Inspection of the Overpressure Protector |
| TASK 28-12-41-200-002-A | Inspection of the Overpressure Protector |
| TASK 28-12-41-200-003-A | Inspection of the Overpressure Protector |
| TASK 28-12-46-200-001-A | Inspection of the Wing-Tank Overpressure Protector Outlet |
| TASK 28-12-47-000-001-A | Removal of the NACA Vent Intake |
| TASK 28-12-47-200-001-A | Visual Check of NACA Intake for Signs of Blockage |
| TASK 28-12-47-400-001-A | Installation of the NACA Vent Intake |
| 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 28-25-00-650-005-A | To Drain the Remaining Fuel from the Additional Center Tank (ACT) |
| TASK 28-25-00-869-001-A | Fuel Transfer |
| 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 |
| TASK 57-27-11-000-001-A | Removal of the Access Panel |
| TASK 57-27-11-000-002-A | Removal of the Access Panel |
| TASK 57-27-11-400-001-A | Installation of the Access Panel |
| TASK 57-27-11-400-002-A | Installation of the Access Panel |
| TASK 57-27-12-000-002-A | Removal of the Rib 2 Access Panel 540AZ(640AZ) or 540BZ(640BZ) |
| TASK 57-27-12-400-002-A | Installation of the Rib 2 Access Panel 540AZ (640AZ) or 540BZ (640BZ) |
Subtask 28-12-00-941-050-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(1) Obey the safety procedures (Ref. AMM TASK 28-00-00-910-001), (Ref. AMM TASK 28-10-00-910-001) and (Ref. AMM TASK 28-10-00-910-003).
(2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(3) On fuel control panel 40VU and refuel/defuel control panel 800VU:
(a) Put a WARNING NOTICE(S) in position to tell persons not to operate the refuel/defuel system.
(4) In the cockpit, put the WARNING NOTICE(S) in position to tell persons not to operate the flight controls.
Subtask 28-12-00-941-050-B ** ON A/C NOT FOR ALL (1) Obey the safety procedures (Ref. AMM TASK 28-00-00-910-001), (Ref. AMM TASK 28-10-00-910-001) and (Ref. AMM TASK 28-10-00-910-003).
(2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(3) On fuel control panel 40VU and refuel/defuel control panel 800VU:
(a) Put a WARNING NOTICE(S) in position to tell persons not to operate the refuel/defuel system.
(4) In the cockpit, put the WARNING NOTICE(S) in position to tell persons not to operate the flight controls.
A. Safety Precautions
(1) Obey the safety procedures (Ref. AMM TASK 28-00-00-910-001), (Ref. AMM TASK 28-10-00-910-001) and (Ref. AMM TASK 28-10-00-910-003).
(2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(3) On fuel control panel 40VU, Additional Center Tank (ACT) fuel control-panel 28VU and refuel/defuel control panels 800VU and 801VU:
(a) Put a WARNING NOTICE(S) in position to tell persons not to operate the refuel/defuel system.
(4) In the cockpit, put the WARNING NOTICE(S) in position to tell persons not to operate the flight controls.
Subtask 28-12-00-650-050-A ** ON A/C NOT FOR ALL (1) Obey the safety procedures (Ref. AMM TASK 28-00-00-910-001), (Ref. AMM TASK 28-10-00-910-001) and (Ref. AMM TASK 28-10-00-910-003).
(2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(3) On fuel control panel 40VU, Additional Center Tank (ACT) fuel control-panel 28VU and refuel/defuel control panels 800VU and 801VU:
(a) Put a WARNING NOTICE(S) in position to tell persons not to operate the refuel/defuel system.
(4) In the cockpit, put the WARNING NOTICE(S) in position to tell persons not to operate the flight controls.
B. Fuel Configuration
(1) Defuel the applicable fuel tank(s) (Ref. AMM TASK 28-25-00-650-001).
(2) Drain the remaining fuel from the applicable fuel tank(s) (Ref. AMM TASK 28-25-00-650-003).
Subtask 28-12-00-650-050-B ** ON A/C NOT FOR ALL (1) Defuel the applicable fuel tank(s) (Ref. AMM TASK 28-25-00-650-001).
(2) Drain the remaining fuel from the applicable fuel tank(s) (Ref. AMM TASK 28-25-00-650-003).
B. Fuel Configuration
(1) Defuel the applicable fuel tank(s) (Ref. AMM TASK 28-25-00-650-001).
(2) Drain the remaining fuel from the applicable fuel tank(s), (Ref. AMM TASK 28-25-00-650-003) and (Ref. AMM TASK 28-25-00-650-005).
Subtask 28-12-00-010-050-B ** ON A/C NOT FOR ALL (1) Defuel the applicable fuel tank(s) (Ref. AMM TASK 28-25-00-650-001).
(2) Drain the remaining fuel from the applicable fuel tank(s), (Ref. AMM TASK 28-25-00-650-003) and (Ref. AMM TASK 28-25-00-650-005).
C. Get Access
(1) Remove all of the access panels (Ref. AMM TASK 57-27-11-000-001) (Ref. AMM TASK 57-27-11-000-002).
(2) Safety open the applicable spring-loaded surge-door 540BZ 640BZ with the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS).
(3) Remove the NACA vent intake (Ref. AMM TASK 28-12-47-000-001).
(4) Remove the access panels 147AZ 148AZ (Ref. AMM TASK 57-17-11-000-001).
Subtask 28-12-00-010-050-D ** ON A/C NOT FOR ALL (1) Remove all of the access panels (Ref. AMM TASK 57-27-11-000-001) (Ref. AMM TASK 57-27-11-000-002).
(2) Safety open the applicable spring-loaded surge-door 540BZ 640BZ with the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS).
(3) Remove the NACA vent intake (Ref. AMM TASK 28-12-47-000-001).
(4) Remove the access panels 147AZ 148AZ (Ref. AMM TASK 57-17-11-000-001).
C. Get Access
(1) Remove all of the access panels (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 57-27-11-000-002).
(2) Safety open the applicable spring-loaded surge-door 540BZ 640BZ with the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS).
(3) Remove the NACA vent intake (Ref. AMM TASK 28-12-47-000-001).
(4) Remove the access panel 148AZ and the ACT-Equipment Support Door (Ref. AMM TASK 57-17-11-000-001).
(5) Open the aft cargo door 826 to get access to the ACT.
(6) Remove the manhole cover of the ACT (Ref. AMM TASK 28-11-37-000-001).
Subtask 28-12-00-010-050-J ** ON A/C NOT FOR ALL (1) Remove all of the access panels (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 57-27-11-000-002).
(2) Safety open the applicable spring-loaded surge-door 540BZ 640BZ with the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS).
(3) Remove the NACA vent intake (Ref. AMM TASK 28-12-47-000-001).
(4) Remove the access panel 148AZ and the ACT-Equipment Support Door (Ref. AMM TASK 57-17-11-000-001).
(5) Open the aft cargo door 826 to get access to the ACT.
(6) Remove the manhole cover of the ACT (Ref. AMM TASK 28-11-37-000-001).
C. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable wing.
(2) Remove all the access panels (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 57-27-11-000-002).
(3) Remove the applicable RIB2 access panels that follow:
(5) Remove the applicable access cover 147AZ ( 148AZ) (Ref. AMM TASK 57-17-11-000-001).
Subtask 28-12-00-010-050-M ** ON A/C NOT FOR ALL (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable wing.
(2) Remove all the access panels (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 57-27-11-000-002).
(3) Remove the applicable RIB2 access panels that follow:
- For the left wing, remove 540BZ (Ref. AMM TASK 57-27-12-000-002)
- For the right wing, remove 640BZ (Ref. AMM TASK 57-27-12-000-002).
(5) Remove the applicable access cover 147AZ ( 148AZ) (Ref. AMM TASK 57-17-11-000-001).
C. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable wing.
(2) Remove all the access panels (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 57-27-11-000-002).
(3) Remove the applicable RIB2 access panels that follow:
(5) Remove access cover 148AZ and the ACT-equipment support door (Ref. AMM TASK 57-17-11-000-001).
(6) Remove the applicable ACT(s):
Subtask 28-12-00-010-050-N ** ON A/C NOT FOR ALL (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable wing.
(2) Remove all the access panels (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 57-27-11-000-002).
(3) Remove the applicable RIB2 access panels that follow:
- For the left wing, remove 540BZ (Ref. AMM TASK 57-27-12-000-002)
- For the right wing, remove 640BZ (Ref. AMM TASK 57-27-12-000-002).
(5) Remove access cover 148AZ and the ACT-equipment support door (Ref. AMM TASK 57-17-11-000-001).
(6) Remove the applicable ACT(s):
NOTE: It is recommended that you remove the ACT from the aircraft to do a visual inspection of the equipment from the inner side of the ACT.
- If installed, remove ACT AFT1 (Ref. AMM TASK 28-11-27-000-002)
- If installed, remove ACT AFT2 (Ref. AMM TASK 28-11-27-000-003)
- If installed, remove ACT FWD (Ref. AMM D/O 28-11-27-00).
C. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable wing.
(2) Remove all the access panels (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 57-27-11-000-002).
(3) Remove the applicable RIB2 access panels that follow:
(5) Remove access cover 148AZ and the ACT-equipment support door (Ref. AMM TASK 57-17-11-000-001).
(6) Remove the applicable ACT(s):
Subtask 28-12-00-010-063-A ** ON A/C NOT FOR ALL (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable wing.
(2) Remove all the access panels (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 57-27-11-000-002).
(3) Remove the applicable RIB2 access panels that follow:
- For the left wing, remove 540BZ (Ref. AMM TASK 57-27-12-000-002)
- For the right wing, remove 640BZ (Ref. AMM TASK 57-27-12-000-002).
(5) Remove access cover 148AZ and the ACT-equipment support door (Ref. AMM TASK 57-17-11-000-001).
(6) Remove the applicable ACT(s):
NOTE: It is recommended that you remove the ACT from the aircraft to do a visual inspection of the equipment from the inner side of the ACT.
- If installed, remove ACT AFT2 (Ref. AMM TASK 28-11-27-000-003)
- If installed, remove ACT AFT1 (Ref. AMM TASK 28-11-27-000-002).
D. Get Access
(1) Remove all of the access panels (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 57-27-11-000-002).
(2) Safety open the applicable spring-loaded surge-door 540BZ 640BZ with the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS).
(3) Remove the NACA vent intake (Ref. AMM TASK 28-12-47-000-001).
(4) Remove access panel 148AZ and the ACT-equipment support door (Ref. AMM TASK 57-17-11-000-001).
(5) Open the aft cargo door 826 to get access to the ACT(s).
(6) If ACT1 is installed:
(a) For access to the ACT components, remove the ACT manhole cover (Ref. AMM TASK 28-11-37-000-001).
(7) If ACT2 is installed:
(a) For access to the ACT components:
1 Remove ACT2 to give access to the manhole cover on the rear wall of ACT1 and ACT2 (Ref. AMM TASK 28-11-27-000-001).
2 Remove the manhole covers of ACT1 and ACT2 (Ref. AMM TASK 28-11-37-000-001), (Ref. AMM TASK 28-10-00-910-002).
4. Procedure(1) Remove all of the access panels (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 57-27-11-000-002).
(2) Safety open the applicable spring-loaded surge-door 540BZ 640BZ with the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS).
(3) Remove the NACA vent intake (Ref. AMM TASK 28-12-47-000-001).
(4) Remove access panel 148AZ and the ACT-equipment support door (Ref. AMM TASK 57-17-11-000-001).
(5) Open the aft cargo door 826 to get access to the ACT(s).
(6) If ACT1 is installed:
(a) For access to the ACT components, remove the ACT manhole cover (Ref. AMM TASK 28-11-37-000-001).
(7) If ACT2 is installed:
(a) For access to the ACT components:
1 Remove ACT2 to give access to the manhole cover on the rear wall of ACT1 and ACT2 (Ref. AMM TASK 28-11-27-000-001).
2 Remove the manhole covers of ACT1 and ACT2 (Ref. AMM TASK 28-11-37-000-001), (Ref. AMM TASK 28-10-00-910-002).
Subtask 28-12-00-210-050-B ** ON A/C NOT FOR ALL
A. Inspection of the Tank Venting System
Tank Venting System ** ON A/C NOT FOR ALL
Tank Venting System ** ON A/C NOT FOR ALL
Refuel Spill Pipe - Location and Detail ** ON A/C NOT FOR ALL
Tank Venting System ** ON A/C NOT FOR ALL
(1) Do a visual inspection of the open end of the center-tank vent-pipe at the aircraft centerline. The pipe must not be blocked.
(2) Do a visual inspection of the open end of the wing-tank vent-inlet-duct located outboard of STA700/RIB2. The pipe must not be blocked.
(3) Do a visual inspection of the open end of the wing-tank vent-duct and the center-tank vent-pipe. They are installed outboard of STA11664/RIB22. They must not be blocked.
(4) Do a visual inspection of:
(9) Do a visual inspection of the vent float valves:
(13) Do a visual inspection of the NACA vent intake (Ref. AMM TASK 28-12-47-200-001).
Subtask 28-12-00-210-050-C ** ON A/C NOT FOR ALL
Tank Venting System ** ON A/C NOT FOR ALL
Tank Venting System ** ON A/C NOT FOR ALL
Refuel Spill Pipe - Location and Detail ** ON A/C NOT FOR ALL
Tank Venting System ** ON A/C NOT FOR ALL (2) Do a visual inspection of the open end of the wing-tank vent-inlet-duct located outboard of STA700/RIB2. The pipe must not be blocked.
(3) Do a visual inspection of the open end of the wing-tank vent-duct and the center-tank vent-pipe. They are installed outboard of STA11664/RIB22. They must not be blocked.
(4) Do a visual inspection of:
- The complete wing-tank vent-duct and the wing-tank vent-inlet-duct
- The complete center-tank vent-pipe.
There must be no: - Large dents
- Cracks
- Distortion
- Corrosion.
Make sure that the ducts and the pipe are correctly sealed along their length.
- Large dents
- Cracks
- Distortion
- Corrosion.
- Large dents
- Cracks
- Distortion
- Corrosion.
- One installed in the center-tank vent-pipe inboard of STA0/RIB1
- One installed in the wing-tank vent-inlet-duct outboard of STA700/RIB2
- One installed in the vent pipe outboard of STA 8268/RIB15
- One installed at the end of the wing-tank vent-duct inboard of STA700/RIB2
- One installed in the spill pipe outboard of STA 8268/RIB15.
Make sure that the valves: - Are not blocked
- Will open and close correctly
- Are attached correctly
- Are not damaged
- Are not corroded
- Are closed.
Make sure that the front edge of the check valve is horizontal.
(9) Do a visual inspection of the vent float valves:
- One installed outboard of STA8268/RIB15
- One installed inboard of STA8268/RIB15.
Make sure that: - The valve will operate correctly
- The valve plate will operate correctly
- The valve closes correctly
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
- Damage
- Blockage
- Large dents
- Cracks
- Distortion
- Corrosion.
- Damage
- Blockage
- Large dents
- Cracks
- Distortion
- Corrosion.
(13) Do a visual inspection of the NACA vent intake (Ref. AMM TASK 28-12-47-200-001).
A. Inspection of the Tank Venting System
(1) Make a visual inspection of the open end of the center-tank vent-pipe at the aircraft centerline. The pipe must not be blocked.
(2) Make a visual inspection of the open end of the wing-tank vent-inlet-duct located outboard of RIB2. The pipe must not be blocked.
(3) Make a visual inspection of the open end of the wing-tank vent-duct and the center-tank vent-pipe. They are installed outboard of RIB22. They must not be blocked.
(4) Make a visual inspection of:
(8) Make a visual inspection of the vent float valves 212QM(213QM). The float vent valves are installed inboard of RIB22.
Make sure that:
Make sure that:
(11) Make a visual inspection of the NACA vent intake (Ref. AMM TASK 28-12-47-200-001).
Subtask 28-12-00-210-050-D ** ON A/C NOT FOR ALL (1) Make a visual inspection of the open end of the center-tank vent-pipe at the aircraft centerline. The pipe must not be blocked.
(2) Make a visual inspection of the open end of the wing-tank vent-inlet-duct located outboard of RIB2. The pipe must not be blocked.
(3) Make a visual inspection of the open end of the wing-tank vent-duct and the center-tank vent-pipe. They are installed outboard of RIB22. They must not be blocked.
(4) Make a visual inspection of:
- The complete wing-tank vent-duct and the wing-tank vent-inlet-duct
- The complete center-tank vent-pipe.
There must be no: - Large dents
- Cracks
- Distortion
- Corrosion.
Make sure that the ducts and the pipe are correctly sealed along their length.
- Large dents
- Cracks
- Distortion
- Corrosion.
- One installed in the center-tank vent-pipe inboard of RIB1
- One installed in the wing-tank vent-inlet-duct outboard of RIB2
- One installed at the end of the wing-tank vent-duct inboard of RIB2.
Make sure that the valves: - Are not blocked
- Will open and close correctly
- Are attached correctly
- Are not damaged
- Are not corroded
- Are closed.
Make sure that the front edge of the check valve is horizontal.
(8) Make a visual inspection of the vent float valves 212QM(213QM). The float vent valves are installed inboard of RIB22.
Make sure that:
- The valve will operate correctly
- The valve plate will operate correctly
- The valve closes correctly
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
Make sure that:
- The valve will operate correctly
- The valve flap will operate correctly
- The valve closes correctly
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
(11) Make a visual inspection of the NACA vent intake (Ref. AMM TASK 28-12-47-200-001).
A. Inspection of the Tank Venting System
(1) Make a visual inspection of the open end of the center-tank vent-pipe at the aircraft centerline. The pipe must not be blocked.
(2) Make a visual inspection of the open end of the wing-tank vent-inlet-duct located outboard of RIB2. The pipe must not be blocked.
(3) Make a visual inspection of the open end of the wing-tank vent-duct and the center-tank vent-pipe. They are installed outboard of RIB22. They must not be blocked.
(4) Make a visual inspection of the open end of the ACT vent pipe. The ACT vent pipe is in the center tank. The pipe must not be blocked.
(5) Make a visual inspection of the open end of the ACT vent pipe. The ACT vent pipe is in the ACT. The pipe must not be blocked.
(6) Make a visual inspection of:
(7) Make a visual inspection of the surge-tank vent-duct outboard of RIB23. There must be no:
(10) Make a visual inspection of the overpressure protector 170QM1 in the ACT.
Make sure that:
Make sure that:
Make sure that:
(14) Make a visual inspection of the NACA vent intake (Ref. AMM TASK 28-12-47-200-001).
(15) Make a visual inspection of the inward pressure relief valve 172QM1.
Make sure that:
Make sure that:
Subtask 28-12-00-210-050-J ** ON A/C NOT FOR ALL (1) Make a visual inspection of the open end of the center-tank vent-pipe at the aircraft centerline. The pipe must not be blocked.
(2) Make a visual inspection of the open end of the wing-tank vent-inlet-duct located outboard of RIB2. The pipe must not be blocked.
(3) Make a visual inspection of the open end of the wing-tank vent-duct and the center-tank vent-pipe. They are installed outboard of RIB22. They must not be blocked.
(4) Make a visual inspection of the open end of the ACT vent pipe. The ACT vent pipe is in the center tank. The pipe must not be blocked.
(5) Make a visual inspection of the open end of the ACT vent pipe. The ACT vent pipe is in the ACT. The pipe must not be blocked.
(6) Make a visual inspection of:
- The complete wing-tank vent-duct and the wing-tank vent-inlet-duct
- The complete center-tank vent-pipe.
There must be no: - Large dents
- Cracks
- Distortion
- Corrosion.
(7) Make a visual inspection of the surge-tank vent-duct outboard of RIB23. There must be no:
- Large dents
- Cracks
- Distortion
- Corrosion.
- One installed in the center-tank vent-pipe inboard of RIB1
- One installed in the wing-tank vent-inlet-duct outboard of RIB2
- One installed at the end of the wing-tank vent-duct inboard of RIB2
- One installed at the end of the ACT vent pipe in the ACT.
Make sure that the valves: - Are not blocked
- Will open and close correctly
- Are attached correctly
- Are not damaged
- Are not corroded
- Are closed.
Make sure that the front edge of the check valve is horizontal.
(10) Make a visual inspection of the overpressure protector 170QM1 in the ACT.
Make sure that:
- The burst disc is not broken.
There must be no: - Large dents
- Cracks
- Distortion
- Corrosion.
Make sure that:
- The valve will operate correctly
- The valve plate will operate correctly
- The valve closes correctly
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
Make sure that:
- The valve will operate correctly
- The valve flap will operate correctly
- The valve closes correctly
- There is no corrosion
- There are no cracks
- There are no large dents
- there is no distortion.
(14) Make a visual inspection of the NACA vent intake (Ref. AMM TASK 28-12-47-200-001).
(15) Make a visual inspection of the inward pressure relief valve 172QM1.
Make sure that:
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
Make sure that:
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
A. Inspection of the Tank Venting System
(1) Make a visual inspection of the open end of the center-tank vent-pipe at the aircraft centerline. The pipe must not be blocked.
(2) Make a visual inspection of the open end of the wing-tank vent-inlet-duct installed outboard of RIB2. The pipe must not be blocked.
(3) Make a visual inspection of the open end of the wing-tank vent-duct and the center-tank vent-pipe. They are installed outboard of RIB22. They must not be blocked.
(4) Make a visual inspection of the open end of the ACT vent pipe. The ACT vent pipe is in the center tank. The pipe must not be blocked.
(5) Make a visual inspection of the open end of each ACT vent pipe. There is an ACT vent pipe in each installed ACT. The pipes must not be blocked.
(6) Make a visual inspection of:
(a) The wing-tank vent-duct and the wing-tank vent-inlet-duct.
(b) The center-tank vent-pipe.
(c) Make sure that:
(a) Make sure that:
(a) One installed in the center-tank vent-pipe inboard of RIB1.
(b) One installed in the center-tank vent-pipe before the ACT vent valve 234QM.
(c) One installed in the wing-tank vent-inlet-duct outboard of RIB2.
(d) One installed at the end of the wing-tank vent-duct inboard of RIB2.
(e) One installed at the end of each ACT vent pipe in each installed ACT.
(f) Make sure that the valves:
(9) Make a visual inspection of the overpressure protectors 46QM (47QM) (Ref. AMM TASK 28-12-41-200-003), 96QM (Ref. AMM TASK 28-12-41-200-002) and the overpressure protector outlets (Ref. AMM TASK 28-12-46-200-001).
(10) Make a visual inspection of the overpressure protectors 256QM, 257QM and 258QM (if the ACT FWD is installed).
(11) Make a visual inspection of the vent float valves 212QM (213QM), installed inboard of RIB22:
(a) Make sure that:
(a) Make sure that:
(14) Make a visual inspection of the NACA vent intake (Ref. AMM TASK 28-12-47-200-001).
(15) If the ACT AFT1 is installed, make a visual inspection of the inward pressure relief valve 229QM1:
(a) Make sure that:
(a) Make sure that:
(a) Make sure that:
(a) Make sure that:
Subtask 28-12-00-210-050-K ** ON A/C NOT FOR ALL (1) Make a visual inspection of the open end of the center-tank vent-pipe at the aircraft centerline. The pipe must not be blocked.
(2) Make a visual inspection of the open end of the wing-tank vent-inlet-duct installed outboard of RIB2. The pipe must not be blocked.
(3) Make a visual inspection of the open end of the wing-tank vent-duct and the center-tank vent-pipe. They are installed outboard of RIB22. They must not be blocked.
(4) Make a visual inspection of the open end of the ACT vent pipe. The ACT vent pipe is in the center tank. The pipe must not be blocked.
(5) Make a visual inspection of the open end of each ACT vent pipe. There is an ACT vent pipe in each installed ACT. The pipes must not be blocked.
(6) Make a visual inspection of:
(a) The wing-tank vent-duct and the wing-tank vent-inlet-duct.
(b) The center-tank vent-pipe.
(c) Make sure that:
- There are no large dents
- There are no cracks
- There is no distortion
- There is no corrosion
- The ducts and the pipe are correctly sealed along their length.
(a) Make sure that:
- There are no large dents
- There are no cracks
- There is no distortion
- There is no corrosion.
(a) One installed in the center-tank vent-pipe inboard of RIB1.
(b) One installed in the center-tank vent-pipe before the ACT vent valve 234QM.
(c) One installed in the wing-tank vent-inlet-duct outboard of RIB2.
(d) One installed at the end of the wing-tank vent-duct inboard of RIB2.
(e) One installed at the end of each ACT vent pipe in each installed ACT.
(f) Make sure that the valves:
- Are not blocked
- Will open and close correctly
- Are attached correctly
- Are not damaged
- Are not corroded
- Are closed.
(9) Make a visual inspection of the overpressure protectors 46QM (47QM) (Ref. AMM TASK 28-12-41-200-003), 96QM (Ref. AMM TASK 28-12-41-200-002) and the overpressure protector outlets (Ref. AMM TASK 28-12-46-200-001).
(10) Make a visual inspection of the overpressure protectors 256QM, 257QM and 258QM (if the ACT FWD is installed).
(11) Make a visual inspection of the vent float valves 212QM (213QM), installed inboard of RIB22:
(a) Make sure that:
- The valve will operate correctly
- The valve plate will operate correctly
- The valve closes correctly
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
(a) Make sure that:
- The valve will operate correctly
- The valve flap will operate correctly
- The valve closes correctly
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
(14) Make a visual inspection of the NACA vent intake (Ref. AMM TASK 28-12-47-200-001).
(15) If the ACT AFT1 is installed, make a visual inspection of the inward pressure relief valve 229QM1:
(a) Make sure that:
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
(a) Make sure that:
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
(a) Make sure that:
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
(a) Make sure that:
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
A. Inspection of the Tank Venting System
(1) Do a visual inspection of the open end of the center-tank vent-pipe at the aircraft centerline. The pipe must not be blocked.
(2) Do a visual inspection of the open end of the wing-tank vent-inlet-duct located outboard of STA700/RIB2. The pipe must not be blocked.
(3) Do a visual inspection of the open end of the wing-tank vent-duct and the center-tank vent-pipe. They are installed outboard of STA11664/RIB22. They must not be blocked.
(4) Do a visual inspection of:
(9) Do a visual inspection of the vent float valves:
(13) Do a visual inspection of the NACA vent intake (Ref. AMM TASK 28-12-47-200-001).
Subtask 28-12-00-210-050-M ** ON A/C NOT FOR ALL (1) Do a visual inspection of the open end of the center-tank vent-pipe at the aircraft centerline. The pipe must not be blocked.
(2) Do a visual inspection of the open end of the wing-tank vent-inlet-duct located outboard of STA700/RIB2. The pipe must not be blocked.
(3) Do a visual inspection of the open end of the wing-tank vent-duct and the center-tank vent-pipe. They are installed outboard of STA11664/RIB22. They must not be blocked.
(4) Do a visual inspection of:
- The complete wing-tank vent-duct and the wing-tank vent-inlet-duct
- The complete center-tank vent-pipe.
There must be no: - Large dents
- Cracks
- Distortion
- Corrosion.
Make sure that the ducts and the pipe are correctly sealed along their length.
- Large dents
- Cracks
- Distortion
- Corrosion.
- Large dents
- Cracks
- Distortion
- Corrosion.
- One installed in the center-tank vent-pipe inboard of STA0/RIB1
- One installed in the wing-tank vent-inlet-duct outboard of STA700/RIB2
- One installed in the vent pipe outboard of STA 8268/RIB15
- One installed at the end of the wing-tank vent-duct inboard of STA700/RIB2
- One installed in the spill pipe outboard of STA 8268/RIB15.
Make sure that the valves: - Are not blocked
- Will open and close correctly
- Are attached correctly
- Are not damaged
- Have no sign of corrosion
- Are closed.
Make sure that the front edge of the check valve is horizontal.
(9) Do a visual inspection of the vent float valves:
- One installed inboard of STA8268/RIB15.
Make sure that: - The valve will operate correctly
- The valve plate will operate correctly
- The valve closes correctly
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
- Damage
- Blockage
- Large dents
- Cracks
- Distortion
- Corrosion.
- Damage
- Blockage
- Large dents
- Cracks
- Distortion
- Corrosion.
(13) Do a visual inspection of the NACA vent intake (Ref. AMM TASK 28-12-47-200-001).
A. Inspection of the Tank Venting System
(1) Make a visual inspection of the open end of the center-tank vent pipe at the aircraft centerline. The pipe must not be blocked.
(2) Make a visual inspection of the open end of the wing-tank vent inlet-duct installed outboard of RIB2. The pipe must not be blocked.
(3) Make a visual inspection of the open end of the wing-tank vent duct and the center-tank vent pipe. They are installed outboard of RIB22. They must not be blocked.
(4) Make a visual inspection of the open end of the ACT vent pipe. The ACT vent pipe is in the center tank. The pipe must not be blocked.
(5) Make a visual inspection of the open end of each ACT vent pipe. There is an ACT vent pipe in each installed ACT. The pipes must not be blocked.
(6) Make a visual inspection of:
(a) The wing-tank vent duct and the wing-tank vent inlet-duct.
(b) The center-tank vent pipe.
(c) Make sure that:
(a) Make sure that:
(a) One installed in the center-tank vent pipe inboard of RIB1.
(b) One installed in the center-tank vent pipe before the ACT vent valve 234QM.
(c) One installed in the wing-tank vent inlet-duct outboard of RIB2.
(d) One installed at the end of the wing-tank vent duct inboard of RIB2.
(e) One installed at the end of each ACT vent pipe in each installed ACT.
(f) Make sure that the valves:
(9) Make a visual inspection of the overpressure protectors 46QM (47QM) (Ref. AMM TASK 28-12-41-200-003), 96QM (Ref. AMM TASK 28-12-41-200-002) and the overpressure protector outlets (Ref. AMM TASK 28-12-46-200-001).
(10) Make a visual inspection of the overpressure protector 256QM.
(11) Make a visual inspection of the vent float valves 212QM (213QM), installed inboard of RIB22:
(a) Make sure that:
(a) Make sure that:
(14) Make a visual inspection of the NACA vent intake (Ref. AMM TASK 28-12-47-200-001).
(15) If ACT AFT1 is installed, make a visual inspection of inward pressure-relief-valve 229QM1:
(a) Make sure that:
(a) Make sure that:
(a) Make sure that:
Subtask 28-12-00-210-060-A ** ON A/C NOT FOR ALL (1) Make a visual inspection of the open end of the center-tank vent pipe at the aircraft centerline. The pipe must not be blocked.
(2) Make a visual inspection of the open end of the wing-tank vent inlet-duct installed outboard of RIB2. The pipe must not be blocked.
(3) Make a visual inspection of the open end of the wing-tank vent duct and the center-tank vent pipe. They are installed outboard of RIB22. They must not be blocked.
(4) Make a visual inspection of the open end of the ACT vent pipe. The ACT vent pipe is in the center tank. The pipe must not be blocked.
(5) Make a visual inspection of the open end of each ACT vent pipe. There is an ACT vent pipe in each installed ACT. The pipes must not be blocked.
(6) Make a visual inspection of:
(a) The wing-tank vent duct and the wing-tank vent inlet-duct.
(b) The center-tank vent pipe.
(c) Make sure that:
- There are no large dents
- There are no cracks
- There is no distortion
- There is no corrosion
- The ducts and the pipe are correctly sealed along their length.
(a) Make sure that:
- There are no large dents
- There are no cracks
- There is no distortion
- There is no corrosion.
(a) One installed in the center-tank vent pipe inboard of RIB1.
(b) One installed in the center-tank vent pipe before the ACT vent valve 234QM.
(c) One installed in the wing-tank vent inlet-duct outboard of RIB2.
(d) One installed at the end of the wing-tank vent duct inboard of RIB2.
(e) One installed at the end of each ACT vent pipe in each installed ACT.
(f) Make sure that the valves:
- Are not blocked
- Will open and close correctly
- Are attached correctly
- Are not damaged
- Are not corroded
- Are closed.
(9) Make a visual inspection of the overpressure protectors 46QM (47QM) (Ref. AMM TASK 28-12-41-200-003), 96QM (Ref. AMM TASK 28-12-41-200-002) and the overpressure protector outlets (Ref. AMM TASK 28-12-46-200-001).
(10) Make a visual inspection of the overpressure protector 256QM.
(11) Make a visual inspection of the vent float valves 212QM (213QM), installed inboard of RIB22:
(a) Make sure that:
- The valve will operate correctly
- The valve plate will operate correctly
- The valve closes correctly
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
(a) Make sure that:
- The valve will operate correctly
- The valve flap will operate correctly
- The valve closes correctly
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
(14) Make a visual inspection of the NACA vent intake (Ref. AMM TASK 28-12-47-200-001).
(15) If ACT AFT1 is installed, make a visual inspection of inward pressure-relief-valve 229QM1:
(a) Make sure that:
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
(a) Make sure that:
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
(a) Make sure that:
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
B. Inspection of the Tank Venting System
(1) Make a visual inspection of the open end of the center-tank vent-pipe at the aircraft centerline. The pipe must not be blocked.
(2) Make a visual inspection of the open end of the wing-tank vent-inlet-duct installed outboard of RIB2. The pipe must not be blocked.
(3) Make a visual inspection of the open end of the wing-tank vent-duct and the center-tank vent-pipe. They are installed outboard of RIB22. They must not be blocked.
(4) Make a visual inspection of the open end of the ACT vent pipe. The ACT vent pipe is in the center tank. The pipe must not be blocked.
(5) Make a visual inspection of the open end of each ACT vent pipe. There is an ACT vent pipe in each installed ACT. The pipes must not be blocked.
(6) Make a visual inspection of:
(a) The complete wing-tank vent-duct and the wing-tank vent-inlet-duct.
(b) The complete center-tank vent-pipe.
(c) Make sure that:
(a) Make sure that:
(a) One installed in the center-tank vent-pipe inboard of RIB1.
(b) One installed in the wing-tank vent-inlet-duct outboard of RIB2.
(c) One installed at the end of the wing-tank vent-duct inboard of RIB2.
(d) One installed at the end of each ACT vent pipe in each installed ACT.
(e) Make sure that the valves:
(9) Make a visual inspection of the overpressure protectors 46QM(47QM) (Ref. AMM TASK 28-12-41-200-003), 96QM (Ref. AMM TASK 28-12-41-200-002) and the overpressure protector outlets (Ref. AMM TASK 28-12-46-200-001).
(10) Make a visual inspection of the vent float valves 212QM(213QM), installed inboard of RIB22:
(a) Make sure that:
(a) Make sure that:
(a) Make sure that:
(a) Make sure that:
(15) Make a visual inspection of the NACA vent intake (Ref. AMM TASK 28-12-47-200-001).
(16) If the ACT1 is installed, make a visual inspection of the inward pressure relief valve 172QM1:
(a) Make sure that:
(a) Make sure that:
(a) Make sure that:
5. Close-up(1) Make a visual inspection of the open end of the center-tank vent-pipe at the aircraft centerline. The pipe must not be blocked.
(2) Make a visual inspection of the open end of the wing-tank vent-inlet-duct installed outboard of RIB2. The pipe must not be blocked.
(3) Make a visual inspection of the open end of the wing-tank vent-duct and the center-tank vent-pipe. They are installed outboard of RIB22. They must not be blocked.
(4) Make a visual inspection of the open end of the ACT vent pipe. The ACT vent pipe is in the center tank. The pipe must not be blocked.
(5) Make a visual inspection of the open end of each ACT vent pipe. There is an ACT vent pipe in each installed ACT. The pipes must not be blocked.
(6) Make a visual inspection of:
(a) The complete wing-tank vent-duct and the wing-tank vent-inlet-duct.
(b) The complete center-tank vent-pipe.
(c) Make sure that:
- There are no large dents
- There are no cracks
- There is no distortion
- There is no corrosion
- The ducts and the pipe are correctly sealed along their length.
(a) Make sure that:
- There are no large dents
- There are no cracks
- There is no distortion
- There is no corrosion.
(a) One installed in the center-tank vent-pipe inboard of RIB1.
(b) One installed in the wing-tank vent-inlet-duct outboard of RIB2.
(c) One installed at the end of the wing-tank vent-duct inboard of RIB2.
(d) One installed at the end of each ACT vent pipe in each installed ACT.
(e) Make sure that the valves:
- Are not blocked
- Will open and close correctly
- Are attached correctly
- Are not damaged
- Are not corroded
- Are closed.
(9) Make a visual inspection of the overpressure protectors 46QM(47QM) (Ref. AMM TASK 28-12-41-200-003), 96QM (Ref. AMM TASK 28-12-41-200-002) and the overpressure protector outlets (Ref. AMM TASK 28-12-46-200-001).
(10) Make a visual inspection of the vent float valves 212QM(213QM), installed inboard of RIB22:
(a) Make sure that:
- The valve will operate correctly
- The valve plate will operate correctly
- The valve closes correctly
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
(a) Make sure that:
- The valve will operate correctly
- The valve flap will operate correctly
- The valve closes correctly
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
(a) Make sure that:
- The burst disc is not broken
- There are no large dents
- There are no cracks
- There is no distortion
- There is no corrosion.
(a) Make sure that:
- The burst disc is not broken
- There are no large dents
- There are no cracks
- There is no distortion
- There is no corrosion.
(15) Make a visual inspection of the NACA vent intake (Ref. AMM TASK 28-12-47-200-001).
(16) If the ACT1 is installed, make a visual inspection of the inward pressure relief valve 172QM1:
(a) Make sure that:
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
(a) Make sure that:
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
(a) Make sure that:
- There is no corrosion
- There are no cracks
- There are no large dents
- There is no distortion.
Subtask 28-12-00-410-050-B ** ON A/C NOT FOR ALL
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS) and carefully close the surge door:
(3) Install the NACA vent intake (Ref. AMM TASK 28-12-47-400-001).
(4) Install all of the access panels (Ref. AMM TASK 57-27-11-400-001), (Ref. AMM TASK 57-27-11-400-002).
(5) Install the access panels 147AZ 148AZ, (Ref. AMM TASK 57-17-11-400-001).
Subtask 28-12-00-410-050-D ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS) and carefully close the surge door:
(3) Install the NACA vent intake (Ref. AMM TASK 28-12-47-400-001).
(4) Install all of the access panels (Ref. AMM TASK 57-27-11-400-001), (Ref. AMM TASK 57-27-11-400-002).
(5) Install the access panels 147AZ 148AZ, (Ref. AMM TASK 57-17-11-400-001).
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the manhole cover of the ACT (Ref. AMM TASK 28-11-37-400-001).
(3) Install the NACA vent intake (Ref. AMM TASK 28-12-47-400-001).
(4) Remove the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS) and carefully close the surge door:
(5) Install all of the access panels (Ref. AMM TASK 57-27-11-400-001), (Ref. AMM TASK 57-27-11-400-002) and (Ref. AMM TASK 28-11-37-400-001).
(6) Install the access panel 148AZ and the ACT-Equipment Support Door (Ref. AMM TASK 57-17-11-400-001).
Subtask 28-12-00-410-050-J ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the manhole cover of the ACT (Ref. AMM TASK 28-11-37-400-001).
(3) Install the NACA vent intake (Ref. AMM TASK 28-12-47-400-001).
(4) Remove the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS) and carefully close the surge door:
(5) Install all of the access panels (Ref. AMM TASK 57-27-11-400-001), (Ref. AMM TASK 57-27-11-400-002) and (Ref. AMM TASK 28-11-37-400-001).
(6) Install the access panel 148AZ and the ACT-Equipment Support Door (Ref. AMM TASK 57-17-11-400-001).
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable access cover 147AZ ( 148AZ) (Ref. AMM TASK 57-17-11-400-001).
(3) Install the NACA vent intake (Ref. AMM TASK 28-12-47-400-001).
(4) Install the applicable RIB2 access panels that follow:
Subtask 28-12-00-410-050-N ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable access cover 147AZ ( 148AZ) (Ref. AMM TASK 57-17-11-400-001).
(3) Install the NACA vent intake (Ref. AMM TASK 28-12-47-400-001).
(4) Install the applicable RIB2 access panels that follow:
- For the left wing, install 540BZ (Ref. AMM TASK 57-27-12-400-002)
- For the right wing, install 640BZ (Ref. AMM TASK 57-27-12-400-002).
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the manhole covers of the applicable ACT(s) (Ref. AMM TASK 28-11-37-400-001) and (Ref. AMM TASK 28-11-37-400-004).
(3) Install the applicable ACT(s):
(5) Install the NACA vent intake (Ref. AMM TASK 28-12-47-400-001).
(6) Install the applicable RIB2 access panels that follow:
Subtask 28-12-00-410-050-O ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the manhole covers of the applicable ACT(s) (Ref. AMM TASK 28-11-37-400-001) and (Ref. AMM TASK 28-11-37-400-004).
(3) Install the applicable ACT(s):
- If removed, install ACT AFT1 (Ref. AMM TASK 28-11-27-400-002)
- If removed, install ACT AFT2 (Ref. AMM TASK 28-11-27-400-003)
- If removed, install ACT FWD (Ref. AMM D/O 28-11-27-40).
(5) Install the NACA vent intake (Ref. AMM TASK 28-12-47-400-001).
(6) Install the applicable RIB2 access panels that follow:
- For the left wing, install 540BZ (Ref. AMM TASK 57-27-12-400-002)
- For the right wing, install 640BZ (Ref. AMM TASK 57-27-12-400-002).
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the manhole covers of the applicable ACT(s) (Ref. AMM TASK 28-11-37-400-001) and (Ref. AMM TASK 28-11-37-400-004).
(3) Install the applicable ACT(s):
(5) Install the NACA vent intake (Ref. AMM TASK 28-12-47-400-001).
(6) Install the applicable RIB2 access panels that follow:
Subtask 28-12-00-410-061-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the manhole covers of the applicable ACT(s) (Ref. AMM TASK 28-11-37-400-001) and (Ref. AMM TASK 28-11-37-400-004).
(3) Install the applicable ACT(s):
- If removed, install ACT AFT1 (Ref. AMM TASK 28-11-27-400-002)
- If removed, install ACT AFT2 (Ref. AMM TASK 28-11-27-400-003).
(5) Install the NACA vent intake (Ref. AMM TASK 28-12-47-400-001).
(6) Install the applicable RIB2 access panels that follow:
- For the left wing, install 540BZ (Ref. AMM TASK 57-27-12-400-002)
- For the right wing, install 640BZ (Ref. AMM TASK 57-27-12-400-002).
B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) If ACT1 is installed:
(a) Install the manhole covers of ACT1 (Ref. AMM TASK 28-11-37-400-001).
(3) If ACT2 is installed:
(a) Install the manhole covers of ACT1 and ACT2 (Ref. AMM TASK 28-11-37-400-001).
(b) Install ACT2 (Ref. AMM TASK 28-11-27-400-001).
(4) Close aft cargo-compartment door 826.
(5) Install the NACA vent intake (Ref. AMM TASK 28-12-47-400-001).
(6) Remove the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS) and carefully close the surge door:
(7) Install all the access panels (Ref. AMM TASK 57-27-11-400-001), (Ref. AMM TASK 57-27-11-400-002) and (Ref. AMM TASK 28-11-37-400-001).
(8) Install access panel 148AZ and the ACT-equipment support door (Ref. AMM TASK 57-17-11-400-001).
Subtask 28-12-00-650-051-A (1) Make sure that the work area is clean and clear of tools and other items.
(2) If ACT1 is installed:
(a) Install the manhole covers of ACT1 (Ref. AMM TASK 28-11-37-400-001).
(3) If ACT2 is installed:
(a) Install the manhole covers of ACT1 and ACT2 (Ref. AMM TASK 28-11-37-400-001).
(b) Install ACT2 (Ref. AMM TASK 28-11-27-400-001).
(4) Close aft cargo-compartment door 826.
(5) Install the NACA vent intake (Ref. AMM TASK 28-12-47-400-001).
(6) Remove the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS) and carefully close the surge door:
(7) Install all the access panels (Ref. AMM TASK 57-27-11-400-001), (Ref. AMM TASK 57-27-11-400-002) and (Ref. AMM TASK 28-11-37-400-001).
(8) Install access panel 148AZ and the ACT-equipment support door (Ref. AMM TASK 57-17-11-400-001).
C. 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 28-12-00-942-051-A (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).
D. Removal of the Equipment
(1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Remove the access platform(s).
(4) Remove the WARNING NOTICE(S).
(5) Remove the SAFETY BARRIERS.
(1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Remove the access platform(s).
(4) Remove the WARNING NOTICE(S).
(5) Remove the SAFETY BARRIERS.