Visually Examine the Pre-Cooler Duct of the Left C-Duct Fixed Structure without Component Removal [IAE]
TASK 78-32-49-200-015-A
Visually Examine the Pre-Cooler Duct of the Left C-Duct Fixed Structure without Component Removal
1. Reason for the Job
This task gives the procedure for a visual inspection of the Pre-Cooler Duct of the Left C-Duct fixed structure without component removal.
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 78-32-49-941-060-A ** ON A/C NOT FOR ALL
Subtask 78-32-49-210-061-A ** ON A/C NOT FOR ALL
Subtask 78-32-49-410-069-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 03:28:57 UTC
Visually Examine the Pre-Cooler Duct of the Left C-Duct Fixed Structure without Component Removal
1. Reason for the Job
This task gives the procedure for a visual inspection of the Pre-Cooler Duct of the Left C-Duct fixed structure without component removal.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 2M (6 FT) |
| No specific | AR | WARNING NOTICE(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| FOR [1000EM1] (ENGINE-1) | |
| 437AL, 438AR, 451AL, 452AR | |
| FOR [1000EM2] (ENGINE-2) | |
| 447AL, 448AR, 461AL, 462AR | |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 71-13-00-010-010-A | Opening of the Fan Cowls 437AL(447AL),438AR(448AR) |
| TASK 71-13-00-410-010-A | Closing of the Fan Cowls 437AL(447AL),438AR(448AR) |
| TASK 78-30-00-040-012-A | Deactivation of the Thrust Reverser Hydraulic Control Unit (HCU) for Ground Maintenance |
| TASK 78-30-00-440-012-A | Re-activation of the Thrust Reverser Hydraulic Control Unit (HCU) after Ground Maintenance |
| TASK 78-31-00-710-041-A | Operational Test of the Thrust Reverser System with the CFDS |
| TASK 78-31-00-710-041-A-02 | Operational test of the Thrust Reverser without the CFDS and Engine Running |
| TASK 78-32-00-010-010-A | Opening of the Thrust Reverser Halves |
| TASK 78-32-00-410-010-A | Closing of the Thrust Reverser Halves |
| SRM 543000 | |
Subtask 78-32-49-941-060-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(1) On the center pedestal, on the ENG panel 115VU:
(a) Put a WARNING NOTICE(S) in position to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
(b) Put a WARNING NOTICE(S) in position to tell persons not to energize the FADEC 1(2).
Subtask 78-32-49-010-069-A ** ON A/C NOT FOR ALL (1) On the center pedestal, on the ENG panel 115VU:
(a) Put a WARNING NOTICE(S) in position to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
(b) Put a WARNING NOTICE(S) in position to tell persons not to energize the FADEC 1(2).
B. Get Access
(1) Open the fan cowls (Ref. AMM TASK 71-13-00-010-010):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR.
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
(2) Put the ACCESS PLATFORM 2M (6 FT) in position.
Subtask 78-32-49-040-060-A ** ON A/C NOT FOR ALL (1) Open the fan cowls (Ref. AMM TASK 71-13-00-010-010):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR.
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
(2) Put the ACCESS PLATFORM 2M (6 FT) in position.
C. Deactivation of the Thrust Reverser
Subtask 78-32-49-010-070-A ** ON A/C NOT FOR ALL WARNING:
MAKE SURE THAT THE THRUST REVERSER HYDRAULIC CONTROL UNIT (HCU) IS DEACTIVATED BEFORE YOU DO WORK ON OR AROUND THE THRUST REVERSER. IF THE HCU IS NOT DEACTIVATED, THERE IS A RISK OF UNWANTED THRUST REVERSER OPERATION WHICH CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
(1) Do the deactivation of the thrust reverser Hydraulic Control Unit (HCU) (Ref. AMM TASK 78-30-00-040-012). D. Open the thrust reverser halves (Ref. AMM TASK 78-32-00-010-010):
(1) FOR [1000EM1] (ENGINE-1)
451AL 452AR.
(2) FOR [1000EM2] (ENGINE-2)
461AL 462AR.
4. Procedure(1) FOR [1000EM1] (ENGINE-1)
451AL 452AR.
(2) FOR [1000EM2] (ENGINE-2)
461AL 462AR.
Subtask 78-32-49-210-061-A ** ON A/C NOT FOR ALL
A. Inspection of the Pre-Cooler Duct Inlet
(1) Examine the pre-cooler duct inlet leading edge.
(a) Erosion damage on the highlight leading edge.
2 Larger than (1). (a). 1_ but less than 3.5 in. (89 mm) long and the number of damaged layers is less than or equal to 3 layers of laminated fabric SRM 543000.
1 Any size but no damage to laminate SRM 543000 SRM 543000.
5. Close-up(1) Examine the pre-cooler duct inlet leading edge.
(a) Erosion damage on the highlight leading edge.
NOTE: The highlight of the leading edge is comprised of 7 layers of laminated fabric. Each layer of fabric is approximately 0.014 in. (0.35 mm) thick.
1 Less than or equal to 0.5 in (12.7 mm) long and the number of damaged layers is less than or equal to 3 layers of laminated fabric or the remaining thickness of damage area is not less than 0.053 in. (1.35 mm) SRM 543000. 2 Larger than (1). (a). 1_ but less than 3.5 in. (89 mm) long and the number of damaged layers is less than or equal to 3 layers of laminated fabric SRM 543000.
NOTE: Erosion damage must be 1.5 in. (38 mm) away from the corner radius on either side (upper and lower) of the duct opening and must be within 1.5 in (38 mm) from leading edge highlight ridge mid point (forward and aft).
(b) Wear on ceramic coating. 1 Any size but no damage to laminate SRM 543000 SRM 543000.
Subtask 78-32-49-410-069-A ** ON A/C NOT FOR ALL
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the thrust reverser halves (Ref. AMM TASK 78-32-00-410-010):
(a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(b) FOR [1000EM2] (ENGINE-2)
461AL 462AR.
Subtask 78-32-49-440-060-A ** ON A/C NOT FOR ALL Subtask 78-32-49-410-070-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the thrust reverser halves (Ref. AMM TASK 78-32-00-410-010):
(a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(b) FOR [1000EM2] (ENGINE-2)
461AL 462AR.
C. Close Access
(1) Close the fan cowls (Ref. AMM TASK 71-13-00-410-010):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
(2) Remove the access platform(s).
(3) Remove the WARNING NOTICE(S).
Subtask 78-32-49-710-055-A ** ON A/C NOT FOR ALL (1) Close the fan cowls (Ref. AMM TASK 71-13-00-410-010):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
(2) Remove the access platform(s).
(3) Remove the WARNING NOTICE(S).
D. Operational Test
(1) Do an operational test of the thrust reverser system (Ref. AMM TASK 78-31-00-710-041).
(1) Do an operational test of the thrust reverser system (Ref. AMM TASK 78-31-00-710-041).
NOTE: As an alternative procedure, you can do the operational test without the CFDS (Ref. AMM TASK 78-31-00-710-041).
Pre-Cooler Duct Cross Section