Removal of the Aircraft Protection Equipment
TASK 10-11-00-555-014-A
Removal of the Aircraft Protection Equipment
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 10-11-00-941-057-A
Subtask 10-11-00-555-075-A ** ON A/C NOT FOR ALL
Subtask 10-11-00-942-059-A
[Rev.10 from 2021]
2026.03.31 22:53:17 UTC
Removal of the Aircraft Protection Equipment
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE |
| REFERENCE | DESIGNATION |
|---|---|
Subtask 10-11-00-941-057-A
A. Safety Precautions
(1) Make sure that the aircraft electrical circuits are de-energized.
(2) Make sure that the ENG/MODE selector switch is in the NORM position.
(3) Make sure that the ENG/MASTER 1(2) control switch is in the OFF position.
(4) Make sure that the WARNING NOTICE(S) is(are) in position in the cockpit to tell persons not to operate the systems while you remove the protective devices from the aircraft.
(5) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position near the aircraft.
4. Procedure(1) Make sure that the aircraft electrical circuits are de-energized.
(2) Make sure that the ENG/MODE selector switch is in the NORM position.
(3) Make sure that the ENG/MASTER 1(2) control switch is in the OFF position.
(4) Make sure that the WARNING NOTICE(S) is(are) in position in the cockpit to tell persons not to operate the systems while you remove the protective devices from the aircraft.
(5) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position near the aircraft.
Subtask 10-11-00-555-075-A ** ON A/C NOT FOR ALL
A. Removal of the Protection Devices from the Fuselage
(1) Protection of the 2 total temperature sensors
Subtask 10-11-00-555-075-B ** ON A/C NOT FOR ALL (1) Protection of the 2 total temperature sensors
- Remove the 98A10001013000 COVER-TOTAL TEMP SENSOR.
- Remove the 98A10001005000 COVER-PITOT PROBE.
- Remove the 98A10001500000 COVER-SLIP ON,ANGLE OF ATTACK SENSOR.
- Remove the 98D10103500001 COVER-STATIC PROBE.
- Remove the 98D10103501000 COVER - ICE DETECTION PROBE.
A. Removal of the Protection Devices from the Fuselage
(1) Protection of the 2 total temperature sensors
Subtask 10-11-00-555-075-D ** ON A/C NOT FOR ALL (1) Protection of the 2 total temperature sensors
- Remove the 98A10001013000 COVER-TOTAL TEMP SENSOR.
- Remove the 98A10001005000 COVER-PITOT PROBE.
- Remove the 98A10001500000 COVER-SLIP ON,ANGLE OF ATTACK SENSOR.
- Remove the 98D10103500001 COVER-STATIC PROBE.
A. Removal of the Protection Devices from the Fuselage
(1) Protection of the 2 total temperature sensors
Subtask 10-11-00-555-076-B ** ON A/C NOT FOR ALL (1) Protection of the 2 total temperature sensors
- Remove the 98A10001013000 COVER-TOTAL TEMP SENSOR.
- Remove the 98A10001005000 COVER-PITOT PROBE.
- Remove the 98A10001500000 COVER-SLIP ON,ANGLE OF ATTACK SENSOR.
- Remove the 98D10103500001 COVER-STATIC PROBE.
- Remove the 98D10103501000 COVER - ICE DETECTION PROBE.
B. Removal of the Protection Devices from the Engines
(1) Protection of the engine air intakes
Subtask 10-11-00-555-076-C ** ON A/C NOT FOR ALL (1) Protection of the engine air intakes
- Remove the IAE1N20400 COVER-INLET COWL or 98D10003001000 COVER-INLET COWL ENGINE.
- Remove the IAE1N20008 COVER-COMMON NOZZLE.
B. Removal of the Protection Devices from the Engines
(1) Protection of the engine air intakes
Subtask 10-11-00-555-076-D ** ON A/C NOT FOR ALL (1) Protection of the engine air intakes
- Remove the RSE1114 COVER BLANKING ENGINE AIR INTAKE or 98D10003000000 COVER-INLET COWL ENGINE.
- Remove the RSE1132 COVER - COMMON NOZZLE.
B. Removal of the Protection Devices from the Engines
(1) Protection of the engine air intakes
Subtask 10-11-00-555-076-E ** ON A/C NOT FOR ALL (1) Protection of the engine air intakes
- Remove the RSE1244 COVER - INLET COWL ENGINE or 98D10003002000 COVER - INLET COWL ENGINE.
- Remove the RSE1132 COVER - COMMON NOZZLE.
B. Removal of the Protection Devices from the Engines
(1) Protection of the engine air intakes
Subtask 10-11-00-555-076-H ** ON A/C NOT FOR ALL (1) Protection of the engine air intakes
- Remove the 636-1100-4GSE INLET COWL LIP COVER.
- Remove the 636-4000-23GSE EXHAUST COVER.
- Remove the 636-3000-11GSE TR C DUCT COVER.
B. Removal of the Protection Devices from the Engines
(1) Protection of the engine air intakes
Subtask 10-11-00-555-077-A (1) Protection of the engine air intakes
- Remove the 636-0001-4GSE COVER-AIR INTAKE.
- Remove the 636-4000-23GSE EXHAUST COVER.
- Remove the 636-3000-11GSE TR C DUCT COVER.
C. Removal of the Protection Devices from the APU Area
(1) Protection of the APU exhaust duct
5. Close-up(1) Protection of the APU exhaust duct
- Remove the 98D10007512000 COVER-EXHAUST DUCT,APU.
- Remove the 98D10007513000 COVER-OILCOOLER OUTLET,APU.
Subtask 10-11-00-942-059-A
A. Close-up
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
(2) Remove the WARNING NOTICE(S) from the CAPT side stick and the cockpit.
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
(2) Remove the WARNING NOTICE(S) from the CAPT side stick and the cockpit.
Protective Equipment