Deactivation of the HP Air-Ground Connector Door
TASK 47-20-00-040-002-A
Deactivation of the HP Air-Ground Connector Door
CDL 52-20
Access Door to HP Air Ground Connector 191 DB
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 47-20-00-860-054-A ** ON A/C NOT FOR ALL
Subtask 47-20-00-020-051-A ** ON A/C NOT FOR ALL
Subtask 47-20-00-410-052-A ** ON A/C NOT FOR ALL Subtask 47-20-00-865-055-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:26:18 UTC
Deactivation of the HP Air-Ground Connector Door
WARNING:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING:
YOU MUST PUT ON AND ATTACH A SAFETY HARNESS BEFORE YOU START WORK:
- ON THE THS OR IN THE REAR FUSELAGE
- ON TOP OF THE WINGS OR PYLONS.
Task Summary
1. Reason for the Job| Access | Test | Specific Tools | Mhr | E/T | Nb Men |
|---|---|---|---|---|---|
| NO | NO | NO | 0.7 | 0.7 | 1 |
CDL 52-20
Access Door to HP Air Ground Connector 191 DB
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 2M (6 FT) |
| No specific | 1 | LIGHT SOURCE - WHITE |
| No specific | 1 | MIRROR - INSPECTION |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| 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 52-42-16-000-001-A | Removal of the HP Air-Ground Connector Door |
| TASK 53-35-13-000-002-A | Removal of the Quick-Release Access Panels from the Belly Fairing Structure |
| TASK 53-35-13-400-002-A | Installation of the Quick-Release Access Panels on the Belly Fairing Structure |
Subtask 47-20-00-860-054-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002)
Subtask 47-20-00-865-054-A ** ON A/C NOT FOR ALL Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002)
B. Open, safety and tag this(these) circuit breaker(s):
Subtask 47-20-00-010-052-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | IGGS/CTRL | 7YA | N28 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | IGGS/CTRL | 7YA | P28 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | CSAS / CTRL | 1HW | U17 |
C. Get Access
(1) Put an ACCESS PLATFORM 2M (6 FT) in position at zone 191.
(2) Remove the HP Air-Ground Connector Door (191DB) (Ref. AMM TASK 52-42-16-000-001)
(3) Remove the access panel 191BB (Ref. AMM TASK 53-35-13-000-002)
4. Procedure(1) Put an ACCESS PLATFORM 2M (6 FT) in position at zone 191.
(2) Remove the HP Air-Ground Connector Door (191DB) (Ref. AMM TASK 52-42-16-000-001)
(3) Remove the access panel 191BB (Ref. AMM TASK 53-35-13-000-002)
Subtask 47-20-00-020-051-A ** ON A/C NOT FOR ALL
A. Deactivation of the HP Air-Ground Connector Door (191DB)
(2) Loosen the screw of the clamp (2).
(3) Remove the bellow (3) and the clamp (2) from the pipe assy CPL (pipe) (1).
Subtask 47-20-00-210-051-A ** ON A/C NOT FOR ALL WARNING:
DO NOT GO INTO THE WORK AREA UNTIL A MINIMUM OF 5 MINUTES AFTER YOU REMOVE THE ACCESS PANEL. LET AIR FLOW THROUGH THE WORK AREA. AIR FROM THIS SYSTEM HAS A LOW OXYGEN CONTENT AND CAN CAUSE INJURY OR DEATH.
(1) Record the position of the clamp (2) on the bellow OEA outlet (bellow) (3). (2) Loosen the screw of the clamp (2).
(3) Remove the bellow (3) and the clamp (2) from the pipe assy CPL (pipe) (1).
B. General Visual Inspection
(1) If the HP Air-Ground Connector Door (191DB) fell during a flight, examine
(3) Make an entry in the log book to record that
5. Close-up(1) If the HP Air-Ground Connector Door (191DB) fell during a flight, examine
- the pipe (1) area
and - the assembly of the HP Air-Ground Connector Door (191DB) to the access panel 191BB,
for damage on the structure, equipments and electrical harnesses.
NOTE: Use a MIRROR - INSPECTION and a LIGHT SOURCE - WHITE if necessary.
(2) Make sure that the work area is clean and clear of tools and other items.(3) Make an entry in the log book to record that
- the bellow (3) is removed,
and - the HP Air-Ground Connector Door (191DB) is deactivated.
Subtask 47-20-00-410-052-A ** ON A/C NOT FOR ALL Subtask 47-20-00-865-055-A ** ON A/C NOT FOR ALL
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 47-20-00-860-055-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | IGGS/CTRL | 7YA | N28 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | IGGS/CTRL | 7YA | P28 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | CSAS / CTRL | 1HW | U17 |
C. Put the aircraft back to its initial configuration.
(1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
(2) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(3) Remove the WARNING NOTICE(S).
(1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
(2) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(3) Remove the WARNING NOTICE(S).
Bellow OEA Outlet