Removal of the MLG Free-Fall Extension Cables
TASK 32-33-16-000-002-A
Removal of the MLG Free-Fall Extension Cables
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 32-33-16-941-051-A
Subtask 32-33-16-020-051-A
[Rev.10 from 2021]
2026.04.01 00:46:42 UTC
Removal of the MLG Free-Fall Extension Cables
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.
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | SAFETY BARRIER(S) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | 1 | WARNING NOTICE(S) |
| No specific | 2 | WEDGE - NON METALLIC |
| 98A27801001000 | 1 | RIGGING PIN |
| 98DNSA20208060 | 1 | RIGGING PIN |
| 98DNSA20208150 | 1 | RIGGING PIN |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 822, 824, 825 |
| REFERENCE | DESIGNATION |
|---|---|
| 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 25-54-12-000-001-A | Removal of the Forward Cargo-Compartment Partition |
| TASK 25-54-12-000-002-A | Removal of the Ceiling Panels in the Forward Cargo Compartment |
| TASK 32-00-00-481-001-A | Installation of the Safety Devices on the Landing Gears |
| TASK 32-00-00-481-002-A | Installation of the Safety Devices on the Landing Gear Doors |
| TASK 32-00-00-860-001-A | Flight Configuration Precautions with Electrical Power |
| TASK 32-00-00-860-001-A-01 | Flight Configuration Precautions without Electrical Power |
| TASK 32-12-00-010-001-A | Open the Main Gear Doors for Access |
| TASK 52-30-00-860-001-A | Open the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump |
| TASK 52-41-00-010-002-A | Open the Avionics Compartment Doors for Access |
| TASK 53-12-11-000-001-A | Removal of the Cockpit Floor Panels from FR1 thru FR12 |
| TASK 53-12-12-000-001-A | Removal of the Cabin Floor Panels from FR12 thru FR24 |
| TASK 53-32-12-000-002-A | Removal of the Cabin Floor Panels |
| TASK 06-41-53-00 | FUSELAGE-DESCRIPTION AND OPERATION |
Subtask 32-33-16-941-051-A
A. Safety Precautions
(1) Put the SAFETY BARRIER(S) in position.
(2) Make sure that the ground safety locks are on the landing gear (Ref. AMM TASK 32-00-00-481-001).
(3) On panel 400VU:
(5) Install a WEDGE - NON METALLIC on each side of the GRAVITY GEAR EXTN handle to lock the handle in position.
Subtask 32-33-16-010-053-A (1) Put the SAFETY BARRIER(S) in position.
(2) Make sure that the ground safety locks are on the landing gear (Ref. AMM TASK 32-00-00-481-001).
(3) On panel 400VU:
- make sure that the landing-gear control-lever is in the DOWN position
- put a WARNING NOTICE(S) in position to tell persons not to operate the landing gear.
(5) Install a WEDGE - NON METALLIC on each side of the GRAVITY GEAR EXTN handle to lock the handle in position.
B. Get Access
(1) Open the MLG doors for access (Ref. AMM TASK 32-12-00-010-001).
(2) Make sure that the safety devices are installed on each MLG door (Ref. AMM TASK 32-00-00-481-002).
(3) Open avionics compartment doors 822 and 824 for access (Ref. AMM TASK 52-41-00-010-002).
(4) Open forward cargo-compartment door 825 (Ref. AMM TASK 52-30-00-860-001).
(5) Remove the access panels that follow:
For location of the access panels, (Ref. AMM D/O 06-41-53-00).
(a) In zones 131 and 132:
1 Remove the applicable ceiling panels in the forward cargo compartment between FR25 and FR34 (Ref. AMM TASK 25-54-12-000-002).
2 Remove the forward cargo-compartment partition at FR34 (Ref. AMM TASK 25-54-12-000-001).
(b) In zone 212:
1 Remove the applicable cockpit floor panels between FR8 and FR12 (Ref. AMM TASK 53-12-11-000-001).
(c) In zones 222 and 232:
1 Remove the applicable cabin floor panels between FR12 and FR24 (Ref. AMM TASK 53-12-12-000-001).
(d) In zones 241 and 242:
1 Remove the applicable cabin floor panels between FR35 and FR47 (Ref. AMM TASK 53-32-12-000-002).
Subtask 32-33-16-869-054-A (1) Open the MLG doors for access (Ref. AMM TASK 32-12-00-010-001).
(2) Make sure that the safety devices are installed on each MLG door (Ref. AMM TASK 32-00-00-481-002).
(3) Open avionics compartment doors 822 and 824 for access (Ref. AMM TASK 52-41-00-010-002).
(4) Open forward cargo-compartment door 825 (Ref. AMM TASK 52-30-00-860-001).
(5) Remove the access panels that follow:
For location of the access panels, (Ref. AMM D/O 06-41-53-00).
(a) In zones 131 and 132:
1 Remove the applicable ceiling panels in the forward cargo compartment between FR25 and FR34 (Ref. AMM TASK 25-54-12-000-002).
2 Remove the forward cargo-compartment partition at FR34 (Ref. AMM TASK 25-54-12-000-001).
(b) In zone 212:
1 Remove the applicable cockpit floor panels between FR8 and FR12 (Ref. AMM TASK 53-12-11-000-001).
(c) In zones 222 and 232:
1 Remove the applicable cabin floor panels between FR12 and FR24 (Ref. AMM TASK 53-12-12-000-001).
(d) In zones 241 and 242:
1 Remove the applicable cabin floor panels between FR35 and FR47 (Ref. AMM TASK 53-32-12-000-002).
C. Flight Configuration Precautions
(1) If the electrical power is not necessary for other maintenance tasks, de-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002). Then, it is not necessary to operate the LGCIU circuit breakers.
(2) If the electrical power is necessary, do the precautions for flight configuration (Ref. AMM TASK 32-00-00-860-001) before you open the LGCIU circuit breakers.
Subtask 32-33-16-865-053-A (1) If the electrical power is not necessary for other maintenance tasks, de-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002). Then, it is not necessary to operate the LGCIU circuit breakers.
(2) If the electrical power is necessary, do the precautions for flight configuration (Ref. AMM TASK 32-00-00-860-001) before you open the LGCIU circuit breakers.
D. Open, safety and tag this(these) circuit breaker(s):
Subtask 32-33-16-480-051-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | L/G/LGCIU/SYS1/NORM | 1GA | C09 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R33 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R32 |
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/LGCIU/SYS2 | 2GA | Q35 |
| 121VU | HYDRAULIC/LGCIU/SYS1/GRND SPLY | 52GA | Q34 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R32 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R31 |
E. Installation of the Rigging Pins
(1) For the cables (13), (15), (25) and (27):
Location of the Rigging Pins ** ON A/C NOT FOR ALL
Location of the Rigging Pins ** ON A/C NOT FOR ALL
Free-Fall Extension Cables - MLG (FR7 to FR41) ** ON A/C NOT FOR ALL
Free-Fall Extension Cables - MLG (FR 7 to FR 41) ** ON A/C NOT FOR ALL
Location of the Rigging Pins ** ON A/C NOT FOR ALL
Location of the Rigging Pins ** ON A/C NOT FOR ALL
4. Procedure(1) For the cables (13), (15), (25) and (27):
Location of the Rigging Pins ** ON A/C NOT FOR ALL
Location of the Rigging Pins ** ON A/C NOT FOR ALL
Free-Fall Extension Cables - MLG (FR7 to FR41) ** ON A/C NOT FOR ALL
Free-Fall Extension Cables - MLG (FR 7 to FR 41) ** ON A/C NOT FOR ALL - put a 98A27801001000 RIGGING PIN in the position Pin 1
- put a 98DNSA20208150 RIGGING PIN in the position Pin 2.
Location of the Rigging Pins ** ON A/C NOT FOR ALL
Location of the Rigging Pins ** ON A/C NOT FOR ALL - put a 98DNSA20208150 RIGGING PIN in the position Pin 2
- put a 98DNSA20208060 RIGGING PIN in the applicable position Pin 3.
Subtask 32-33-16-020-051-A
A. Removal of the MLG Free-Fall Extension Cables (13) and/or (15)
Free-Fall Extension Cables - MLG (FR7 to FR41) ** ON A/C NOT FOR ALL
Free-Fall Extension Cables - MLG (FR 7 to FR 41) ** ON A/C NOT FOR ALL
(1) Remove these items as necessary, the:
(3) Remove the locking clips (24) from the turnbuckles (23).
(4) Loosen the turnbuckles (23) for the cables (13) and (15) until the tension in the cables is released.
(5) On the cable(s) to be removed, continue to loosen the turnbuckle(s) (23) until the cable(s) is/are disconnected.
(6) Temporarily attach the cable(s) (25) and/or (27) to the structure.
(7) Remove the cotter pin(s) (14) for the cable(s) (13) and/or (15).
(8) Release the cable(s) (13) and/or (15) from the pulley (16) and remove it/them from the aircraft.
Subtask 32-33-16-020-052-A
Free-Fall Extension Cables - MLG (FR7 to FR41) ** ON A/C NOT FOR ALL
Free-Fall Extension Cables - MLG (FR 7 to FR 41) ** ON A/C NOT FOR ALL - cotter pins (8) and (11)
- washers (9) and (12)
- tubes (7) and (10).
(3) Remove the locking clips (24) from the turnbuckles (23).
(4) Loosen the turnbuckles (23) for the cables (13) and (15) until the tension in the cables is released.
(5) On the cable(s) to be removed, continue to loosen the turnbuckle(s) (23) until the cable(s) is/are disconnected.
(6) Temporarily attach the cable(s) (25) and/or (27) to the structure.
(7) Remove the cotter pin(s) (14) for the cable(s) (13) and/or (15).
(8) Release the cable(s) (13) and/or (15) from the pulley (16) and remove it/them from the aircraft.
B. Removal of the MLG Free-Fall Extension Cables (25) and/or (27)
Free-Fall Extension Cables - MLG (FR7 to FR41) ** ON A/C NOT FOR ALL
Free-Fall Extension Cables - MLG (FR 7 to FR 41) ** ON A/C NOT FOR ALL
(1) Remove the applicable cable-guard items, the:
(3) Remove the cable-guide locking-devices (21) and the fairleads (22) for the related cable.
(4) For the cable (27) remove these items at the bracket (2) on FR 12, the:
(6) Loosen the turnbuckles (23) for the cables (25) and (27) until the tension in the cables is released.
(7) On the cable(s) to be removed, continue to loosen the turnbuckle(s) (23) until the cable(s) is/are disconnected.
(8) Temporarily attach the cable(s) (13) and/or (15) to the structure.
(9) Release the cable(s) (25) and/or (27) from the pulley (26) and remove it/them from the aircraft.
Subtask 32-33-16-020-053-A
Free-Fall Extension Cables - MLG (FR7 to FR41) ** ON A/C NOT FOR ALL
Free-Fall Extension Cables - MLG (FR 7 to FR 41) ** ON A/C NOT FOR ALL - nuts (20)
- bolts (18)
- spacers (19).
(3) Remove the cable-guide locking-devices (21) and the fairleads (22) for the related cable.
(4) For the cable (27) remove these items at the bracket (2) on FR 12, the:
- cotter pin (4)
- nut (5)
- washer (6)
- bolt (1)
- spacer (3).
(6) Loosen the turnbuckles (23) for the cables (25) and (27) until the tension in the cables is released.
(7) On the cable(s) to be removed, continue to loosen the turnbuckle(s) (23) until the cable(s) is/are disconnected.
(8) Temporarily attach the cable(s) (13) and/or (15) to the structure.
(9) Release the cable(s) (25) and/or (27) from the pulley (26) and remove it/them from the aircraft.
C. Removal of the MLG Free-Fall Extension Cables (37) and/or (38)
(2) Remove these items from the applicable cable-pressure-seal(s):
(5) Loosen the turnbuckles (41) for the cables (37) and (38) until the tension in the cables is released.
(6) On the cable(s) to be removed, continue to loosen the turnbuckle(s) (41) until the cable(s) is/are disconnected.
(7) Temporarily attach the cable(s) (39) and/or (40) to the structure.
(8) Release the cable(s) (37) and/or (38) from the pulley (65).
(9) Remove the cable(s), the pressure-seal-flanges (58) and (60) and the sleeve (63).
Subtask 32-33-16-020-054-A WARNING:
USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
(1) At the cable pressure seals, remove and discard the locking wire for the bolts (62). (2) Remove these items from the applicable cable-pressure-seal(s):
- the retaining ring (64)
- the bolts (62)
- the washers (61)
- the swivel cable-guides (59).
- the cotter pins (54) and (55)
- the washers (53) and (56)
- the tubes (52) and (57)
- the nut (66), the washer (67) and the guide bolt (68).
(5) Loosen the turnbuckles (41) for the cables (37) and (38) until the tension in the cables is released.
(6) On the cable(s) to be removed, continue to loosen the turnbuckle(s) (41) until the cable(s) is/are disconnected.
(7) Temporarily attach the cable(s) (39) and/or (40) to the structure.
(8) Release the cable(s) (37) and/or (38) from the pulley (65).
(9) Remove the cable(s), the pressure-seal-flanges (58) and (60) and the sleeve (63).
D. Removal of the MLG Free-Fall Extension Cables (39) and/or (40)
(a) Remove and discard the locking wire for the nuts (87).
(b) Remove and discard the cotter pins (77), (80).
(c) Remove these items:
(3) Remove the locking clips (42).
(4) Loosen the turnbuckles (41) for the cables (39) and (40) until the tension in the cables is released.
(5) On the cable(s) to be removed, continue to loosen the turnbuckle(s) (41) until the cable(s) is/are disconnected.
(6) Temporarily attach the cable(s) (37) and/or (38) to the structure.
(7) Release the cable(s) (39) and/or (40) from the pulley (83) and remove it/them from the aircraft.
WARNING:
USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
(1) At the cable pulley assemblies: (a) Remove and discard the locking wire for the nuts (87).
(b) Remove and discard the cotter pins (77), (80).
(c) Remove these items:
- the washers (76), (79) and the tubes (75), (78)
- the nuts (87) and the washers (86)
- the cable guard assembly (85)
- the pins (84).
(3) Remove the locking clips (42).
(4) Loosen the turnbuckles (41) for the cables (39) and (40) until the tension in the cables is released.
(5) On the cable(s) to be removed, continue to loosen the turnbuckle(s) (41) until the cable(s) is/are disconnected.
(6) Temporarily attach the cable(s) (37) and/or (38) to the structure.
(7) Release the cable(s) (39) and/or (40) from the pulley (83) and remove it/them from the aircraft.