Installation of the Aircraft Protection Equipment

TASK 10-11-00-555-013-A
Installation of the Aircraft Protection Equipment

WARNING: DO NOT APPLY ADHESIVE TAPE ON THE PROBES, DUCTS, SENSORS (STATIC, PITOT, TAT, AOA). USE ONLY THE SPECIFIED TOOLS FOR THE PROTECTION OF THE AIRCRAFT. THE SPECIFIED TOOLS:

GIVE THE CORRECT PROTECTION TO THE AIRCRAFT EQUIPMENT,
ARE EASY TO SEE FROM THE GROUND,
ARE EASY TO REMOVE.

IF YOU USE TAPE, THERE IS A RISK THAT SOME TAPE, OR ADHESIVE FROM THE TAPE, WILL STAY ON THE PROBES, DUCTS OR SENSORS. THIS CAN CAUSE INCORRECT INDICATIONS ON THE RELATED COCKPIT INSTRUMENTS.

WARNING: BE CAREFUL WHEN YOU DO WORK ON THE PROBES ON THE GROUND. THE PROBES CAN STAY HOT FOR A LONG TIME AND WILL BURN YOU.

WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AFTER SHUTDOWN. THE ENGINE CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.

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
No specific	AR	WARNING NOTICE(S)
636-0001-4GSE	2	COVER-AIR INTAKE
636-1100-4GSE	2	INLET COWL LIP COVER
636-3000-11GSE	2	TR C DUCT COVER
636-4000-23GSE	2	EXHAUST COVER
98A10001005000	3	COVER-PITOT PROBE
98A10001013000	2	COVER-TOTAL TEMP SENSOR
98A10001500000	3	COVER-SLIP ON,ANGLE OF ATTACK SENSOR
98D10003000000	2	COVER-INLET COWL ENGINE
98D10003001000	2	COVER-INLET COWL ENGINE
98D10003002000	2	COVER - INLET COWL ENGINE
98D10007512000	1	COVER-EXHAUST DUCT,APU
98D10007513000	1	COVER-OILCOOLER OUTLET,APU
98D10103500001	2	COVER-STATIC PROBE
98D10103501000	2	COVER - ICE DETECTION PROBE
HIX6002	2	HALF PLUG, RIGHT-THRUST REVERSER
HIX6003	2	HALF PLUG, LEFT-THRUST REVERSER
IAE1N20008	2	COVER-COMMON NOZZLE
IAE1N20400	2	COVER-INLET COWL
RSE1114	2	COVER BLANKING ENGINE AIR INTAKE
RSE1132	2	COVER - COMMON NOZZLE
RSE1244	2	COVER - INLET COWL ENGINE

B. Referenced Information

REFERENCE	DESIGNATION
Protective Equipment ** ON A/C NOT FOR ALL
Protective Equipment ** ON A/C NOT FOR ALL
Protective Equipment ** ON A/C NOT FOR ALL
Protective Equipment ** ON A/C NOT FOR ALL
Protective Equipment ** ON A/C NOT FOR ALL
Protective Equipment ** ON A/C NOT FOR ALL
Half Plug ** ON A/C NOT FOR ALL
Protective Equipment

3. Job Set-up
Subtask 10-11-00-941-056-A

A. Safety Precautions
(1) On panel 115VU:

Make sure that the ENG/MODE selector switch is in the NORM position.
Make sure that the ENG/MASTER 1(2) control lever is in the OFF position.

(2) On panel 25VU:

Make sure that the PROBE/WINDOW HEAT pushbutton switch is released (the ON legend is off).

(3) In the cockpit, put the WARNING NOTICE(S) in position:

To tell persons that the protection covers/devices on the probes are installed.
On the CAPT side stick to tell the crew that the protection covers/devices are installed and not to operate the systems.

(4) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position near the aircraft.

4. Procedure
Subtask 10-11-00-555-069-A ** ON A/C NOT FOR ALL

A. Installation of the Protection Devices on the Fuselage

Protective Equipment ** ON A/C NOT FOR ALL

WARNING: MAKE SURE THAT THE PROBES, THE ENGINE AND THE APU ARE COOL BEFORE INSTALLATION OF THE PROTECTIVE DEVICES. IF THE PROBES ARE HOT, THERE IS A RISK OF INJURY AND THE PROTECTIVE DEVICES CAN MELT.

(1) Protection of the 2 total temperature sensors

Put the 98A10001013000 COVER-TOTAL TEMP SENSOR in position.

(2) Protection of the 3 pitot probes

Put the 98A10001005000 COVER-PITOT PROBE in position.

(3) Protection of the 3 angle-of-attack sensors

Put the 98A10001500000 COVER-SLIP ON,ANGLE OF ATTACK SENSOR in position.

(4) Protection of the 6 static probes

Put the 98D10103500001 COVER-STATIC PROBE in position.

(5) Protection of the 2 ice detection probes

Put the 98D10103501000 COVER - ICE DETECTION PROBE in position.

Subtask 10-11-00-555-069-B ** ON A/C NOT FOR ALL

A. Installation of the Protection Devices on the Fuselage

Protective Equipment ** ON A/C NOT FOR ALL

(1) Protection of the 2 total temperature sensors

Put the 98A10001013000 COVER-TOTAL TEMP SENSOR in position.

(2) Protection of the 3 pitot probes

Put the 98A10001005000 COVER-PITOT PROBE in position.

(3) Protection of the 3 angle-of-attack sensors

Put the 98A10001500000 COVER-SLIP ON,ANGLE OF ATTACK SENSOR in position.

(4) Protection of the 6 static probes

Put the 98D10103500001 COVER-STATIC PROBE in position.

Subtask 10-11-00-555-069-D ** ON A/C NOT FOR ALL

A. Installation of the Protection Devices on the Fuselage

Protective Equipment ** ON A/C NOT FOR ALL

(1) Protection of the 2 total temperature sensors

Put the 98A10001013000 COVER-TOTAL TEMP SENSOR in position.

(2) Protection of the 3 pitot probes

Put the 98A10001005000 COVER-PITOT PROBE in position.

(3) Protection of the 3 angle-of-attack sensors

Put the 98A10001500000 COVER-SLIP ON,ANGLE OF ATTACK SENSOR in position.

(4) Protection of the 6 static probes

Put the 98D10103500001 COVER-STATIC PROBE in position.

(5) Protection of the 2 ice detection probes

Put the 98D10103501000 COVER - ICE DETECTION PROBE in position.

Subtask 10-11-00-555-070-B ** ON A/C NOT FOR ALL

B. Installation of the Protection Devices on the Engines

Protective Equipment ** ON A/C NOT FOR ALL

(1) Protection of the engine air intakes

Put the IAE1N20400 COVER-INLET COWL or 98D10003001000 COVER-INLET COWL ENGINE in position.

(2) Protection of the engine exhaust nozzles

Put the IAE1N20008 COVER-COMMON NOZZLE in position.

Subtask 10-11-00-555-070-C ** ON A/C NOT FOR ALL

B. Installation of the Protection Devices on the Engines

Protective Equipment ** ON A/C NOT FOR ALL

Half Plug ** ON A/C NOT FOR ALL

(1) Protection of the engine air intakes

Put the RSE1114 COVER BLANKING ENGINE AIR INTAKE or 98D10003000000 COVER-INLET COWL ENGINE in position.

(2) Protection of the engine exhaust nozzles

Put the RSE1132 COVER - COMMON NOZZLE in position.

(3) Protection of the thrust reverser openings

Put the HIX6002 HALF PLUG, RIGHT-THRUST REVERSER and HIX6003 HALF PLUG, LEFT-THRUST REVERSER in position.

Subtask 10-11-00-555-070-D ** ON A/C NOT FOR ALL

B. Installation of the Protection Devices on the Engines

Protective Equipment ** ON A/C NOT FOR ALL

Half Plug ** ON A/C NOT FOR ALL

(1) Protection of the engine air intakes

Put the RSE1244 COVER - INLET COWL ENGINE or 98D10003002000 COVER - INLET COWL ENGINE in position.

(2) Protection of the engine exhaust nozzles

Put the RSE1132 COVER - COMMON NOZZLE in position.

(3) Protection of the thrust reverser openings

Put the HIX6002 HALF PLUG, RIGHT-THRUST REVERSER and HIX6003 HALF PLUG, LEFT-THRUST REVERSER in position.

Subtask 10-11-00-555-070-E ** ON A/C NOT FOR ALL

B. Installation of the Protection Devices on the Engines

(1) Protection of the engine air intakes

Put the 636-1100-4GSE INLET COWL LIP COVER in position.

(2) Protection of the engine exhaust nozzles

Put the 636-4000-23GSE EXHAUST COVER in position.

(3) Protection of the thrust reverser opening

Put the 636-3000-11GSE TR C DUCT COVER in position.

Subtask 10-11-00-555-070-I ** ON A/C NOT FOR ALL

B. Installation of the Protection Devices on the Engines

(1) Protection of the engine air intakes

Put the 636-0001-4GSE COVER-AIR INTAKE in position.

(2) Protection of the engine exhaust nozzles

Put the 636-4000-23GSE EXHAUST COVER in position.

(3) Protection of the thrust reverser opening

Put the 636-3000-11GSE TR C DUCT COVER in position.

Subtask 10-11-00-555-071-A

C. Installation of the Protection Devices on the APU Area

Protective Equipment

(1) Protection of the APU exhaust duct

Put the 98D10007512000 COVER-EXHAUST DUCT,APU in position.

(2) Protection of the outlet duct of the APU oil cooler

Put the 98D10007513000 COVER-OILCOOLER OUTLET,APU in position.

5. Close-up
Subtask 10-11-00-942-058-A

A. Close-up
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
(2) Make sure that the WARNING NOTICE(S) are installed on the CAPT side stick to tell the crew that the protection covers/devices are installed.

[Rev.10 from 2021] 2026.04.01 03:55:35 UTC