Detailed Visual Inspection of the Ramp Fairing [CFMI]

TASK 78-32-42-210-040-A
Detailed Visual Inspection of the Ramp Fairing

FIN: 1000EM1 ** ON A/C NOT FOR ALL
FIN: 1000EM2 ** ON A/C NOT FOR ALL

1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	AR	ACCESS PLATFORM 1M(3 FT)
No specific	AR	WARNING NOTICE(S)
HIX3005	1	SAFETY SLEEVE - PIVOTING DOOR ACTUATOR

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.CP2517)	aerodynamic tape

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
437AL, 438AR, 451AL, 452AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR, 461AL, 462AR

D. Referenced Information

REFERENCE	DESIGNATION
TASK 71-13-00-010-040-A	Opening of the Fan Cowl Doors
TASK 71-13-00-410-040-A	Closing of the Fan Cowl Doors
TASK 78-30-00-081-041-A	Make the Thrust Reverser Serviceable after Maintenance
TASK 78-30-00-481-041-A	Make the Thrust Reverser Unserviceable for Maintenance
TASK 78-32-41-080-040-A	Removal of the Safety Sleeve from Blocker Door Actuator
TASK 78-32-41-480-040-A	Installation of the Safety Sleeve on Blocker Door Actuator
TASK 78-32-41-860-040-A	Manual Deployment of the Blocker Door
TASK 78-32-41-860-041-A	Manual Stowing of the Blocker Door
TASK 78-32-42-000-040-A	Removal of the Ramp Fairing
TASK 78-32-42-400-040-A	Installation of the Ramp Fairing
TASK 78-36-00-010-040-A	Opening of the Thrust Reverser Doors
TASK 78-36-00-410-040-A	Closing of the Thrust Reverser Doors
Ramp Fairing

3. Job Set-up
Subtask 78-32-42-941-056-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) 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) to tell persons not to energize the FADEC 1(2).

Subtask 78-32-42-010-067-A ** ON A/C NOT FOR ALL

B. Get Access
(1) Open the fan cowl doors: (Ref. AMM TASK 71-13-00-010-040)
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(2) Put the ACCESS PLATFORM 1M(3 FT) in position.

Subtask 78-32-42-040-060-A ** ON A/C NOT FOR ALL

C. Make the thrust reverser unserviceable (Ref. AMM TASK 78-30-00-481-041).

Subtask 78-32-42-860-056-A ** ON A/C NOT FOR ALL

D. Manually bring the blocker door to deploy position (Ref. AMM TASK 78-32-41-860-040).

Subtask 78-32-42-480-053-A ** ON A/C NOT FOR ALL

E. Install the HIX3005 SAFETY SLEEVE - PIVOTING DOOR ACTUATOR on the blocker door actuator (Ref. AMM TASK 78-32-41-480-040).

Subtask 78-32-42-010-068-A ** ON A/C NOT FOR ALL

F. Open the thrust reverser cowl doors: (Ref. AMM TASK 78-36-00-010-040)
(1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(2) FOR [1000EM2] (ENGINE-2)
461AL 462AR

4. Procedure
Subtask 78-32-42-210-053-A ** ON A/C NOT FOR ALL

A. Do a visual inspection of the ramp fairing as follows :

INSPECT/CHECK	MAXIMUM SERVICEABLE LIMITS	REMARKS
1.Inspect the ramp fairing for :
A.Damage	No damage allowed	If you find some damage, replace the defective part (Ref. AMM TASK 78-32-42-000-040) and (Ref. AMM TASK 78-32-42-400-040).
B.Crack	1 in. (25.4 mm) maximum length in any direction	Protect damage area from entrance of moisture by application of appropriate sealing tape
	7.4 in. (187.96 mm) minimum separation between other cracks, holes and delaminations	Monitor at 750 Flight Hours / 750 Flight Cycles / 4 calendar months (whichever the earliest)
	Five cracks maximum per ramp fairing	If the crack is not allowable, replace the ramp fairing (Ref. AMM TASK 78-32-42-000-040) and (Ref. AMM TASK 78-32-42-400-040).
C.Hole	1 in. (25.4 mm) maximum diameter	Protect damage area from entrance of moisture by application of appropriate sealing tape
	7.4 in. (187.96 mm) minimum separation between other holes, cracks and delaminations	Monitor at 750 Flight Hours / 750 Flight Cycles / 4 calendar months (whichever the earliest)
	Five holes maximum per ramp fairing	If the hole is not allowable, replace the ramp fairing (Ref. AMM TASK 78-32-42-000-040) and (Ref. AMM TASK 78-32-42-400-040).
D.Delamination	1.5 in. (38.1 mm) maximum length	Monitor at 750 Flight Hours / 750 Flight Cycles / 4 calendar months (whichever the earliest)
	7.4 in. (187.96 mm) minimum separation between other delaminations, holes and cracks	It is recommended that all delaminations be repaired no later than 7500 Flight Hours / 5000 Flight Cycles / 24 calendar months (whichever the earliest)
	Five delaminations maximum per ramp fairing	If the delamination is not allowable, replace the ramp fairing (Ref. AMM TASK 78-32-42-000-040) and (Ref. AMM TASK 78-32-42-400-040).
E.Abrasion	No carbon fiber damage allowed	Seal surface damage with aerodynamic tape (Material No.CP2517) (paint and surface resin only). Replace tape if peeled
		If there is carbon fiber damage, replace the ramp fairing (Ref. AMM TASK 78-32-42-000-040) and (Ref. AMM TASK 78-32-42-400-040).
F.Gouge, nick and scratch	0.008 in. (0.20 mm) maximum depth over 8 in. (203.2 mm) length	Monitor at 750 Flight Hours / 750 Flight Cycles / 4 calendar months (whichever the earliest)
		If the defect is not allowable, replace the ramp fairing (Ref. AMM TASK 78-32-42-000-040) and (Ref. AMM TASK 78-32-42-400-040).
2.Inspect the related hardware of the ramp fairing for:
A.Damage	No damage allowed	If you find some damage, replace the defective part (Ref. AMM TASK 78-32-42-000-040) and (Ref. AMM TASK 78-32-42-400-040).

5. Close-up
Subtask 78-32-42-410-065-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 cowl doors without making thrust reverser serviceable: (Ref. AMM TASK 78-36-00-410-040)
(a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(b) FOR [1000EM2] (ENGINE-2)
461AL 462AR

Subtask 78-32-42-080-053-A ** ON A/C NOT FOR ALL

B. Remove the safety sleeve (HIX 3005) from the blocker door actuator (Ref. AMM TASK 78-32-41-080-040).

Subtask 78-32-42-860-057-A ** ON A/C NOT FOR ALL

C. Bring the blocker doors.

CAUTION: BLOCKER DOOR LATCH MUST BE OPENED WHEN YOU CLOSE THE BLOCKER DOOR OR DAMAGE CAN OCCUR.

(1) Manually bring the blocker doors to stow position (Ref. AMM TASK 78-32-41-860-041).

Subtask 78-32-42-440-057-A ** ON A/C NOT FOR ALL

D. Make the thrust reverser serviceable (Ref. AMM TASK 78-30-00-081-041).

Subtask 78-32-42-410-066-A ** ON A/C NOT FOR ALL

E. Close Access
(1) Close the fan cowl doors: (Ref. AMM TASK 71-13-00-410-040)
(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).

[Rev.10 from 2021] 2026.04.02 06:38:11 UTC