Removal of the Right Thrust Reverser Half - Eng. No. 2 [IAE]

TASK 78-32-04-000-010-A
Removal of the Right Thrust Reverser Half - Eng. No. 2

WARNING: DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH.

WARNING: BE CAREFUL DURING THE REMOVAL OR INSTALLATION OF THE THRUST REVERSER HALF. IT WEIGHS 567lb (257kg). IF IT FALLS, IT CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.

CAUTION: YOU MUST NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT- FREE CLOTH. THE HYDRAULIC FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND SOME PARTS.

CAUTION: DO NOT REMOVE/INSTALL THE THRUST REVERSER HALF IF THE WING LEADING EDGE SLATS ARE EXTENDED. THIS WILL CAUSE DAMAGE TO THE THRUST REVERSER, THE WING LEADING EDGE SLATS AND THE WING.

CAUTION: DO NOT USE THE TRANSLATING HOISTING POINT TO REMOVE THE THRUST REVERSER COWL.

CAUTION: WHEN YOU REMOVE/INSTALL THE THRUST REVERSER, BE CAREFUL NOT TO CAUSE DAMAGE TO THE PRESSURE BULKHEAD AND CROSSOVER BEAM TANGS.

CAUTION: THIS PART IS A REMOVABLE STRUCTURAL COMPONENT (RSC), WHICH CAN BE MOVED BETWEEN AIRCRAFT. THUS IT CAN HAVE DIFFERENT OPERATION CONDITIONS AND A DIFFERENT LIFE RECORD (FLIGHT HOURS/FLIGHT CYCLES/CALENDAR) FROM THE AIRCRAFT IT IS INSTALLED ON OR REMOVED FROM. THE OPERATOR IS RESPONSIBLE FOR THE SPECIFIC TRACKING AND CONTINUED AIRWORTHINESS OF REMOVABLE STRUCTURAL COMPONENTS. INCORRECT MAINTENANCE OF THESE COMPONENTS CAN CAUSE A RISK FOR THE FLIGHT SAFETY.

FIN: 3410KM2 ** ON A/C NOT FOR ALL

1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Referenced Information

REFERENCE	DESIGNATION
TASK 78-32-03-000-010-A	Removal of the Right Thrust Reverser Half - Eng No. 1

3. Job Set-up
Subtask 78-32-04-869-050-A ** ON A/C NOT FOR ALL

A. Not Applicable

4. Procedure
Subtask 78-32-04-020-050-A ** ON A/C NOT FOR ALL

A. Removal of the right thrust reverser half (Eng. No. 2) is identical to (Ref. AMM TASK 78-32-03-000-010).

[Rev.10 from 2021] 2026.04.01 03:28:10 UTC