Inspection after a Tail Runway Impact

TASK 05-51-21-200-001-A
Inspection after a Tail Runway Impact

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 4M (13 FT)-ADJUSTABLE

B. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
312AR, 314AR, 315AL, 316AR

C. Referenced Information

REFERENCE	DESIGNATION
TASK 49-16-00-200-002-A	Detailed Inspection of APU Air Intake, Diffuser Elbow, Seals and Felt Metal
TASK 49-16-00-210-002-A	Detailed Inspection of APU Air Intake, Diffuser Elbow, Seals and Felt Metal (APS 3200)
Tailcone Equipment (L Side)
APU Installation (R side)

3. Job Set-up
Subtask 05-51-21-010-050-A

A. Get Access
(1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position.
(2) Open the access doors 312AR 314AR 315AL 316AR.

4. Procedure
Subtask 05-51-21-210-051-A

A. Inspection of the Tail Area

Tailcone Equipment (L Side)

APU Installation (R side)

NOTE: You must do this inspection if:

the tail hits the runway during the take-off,
the tail hits the runway during the landing.

NOTE: All inspections are visual unless the text gives other instructions.

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Fuselage
A.	Examine the skin panels, the splices and the rivets for distortion, cracks, pulled or torn fasteners and damaged paintwork. If you find damage:	X
	(1) Internally examine the frames, the cleats and the stringers for distortion, cracks, pulled and torn fasteners.		X
	(2) Internally examine the lower part of the pressure bulkhead FR70, on the forward and the aft face, in the area below the passenger-compartment floor level, between the L STGR28 and R STGR28, the pressure dome, the frame segment and the vertical cross beam at the aircraft center line for: - distortion, cracks and dents.		X
2.	APU Air Intake and Tail Cone Attachment Fittings
A.	Examine the APU diverter, intake flap, intake nose and drain mast for distortion, cracks, pulled or torn fasteners and damaged paintwork -for APU GTCP 36-300: (Ref. AMM D/O 49-16-00-21) -for APU APS 3200: (Ref. AMM TASK 49-16-00-210-002) -for APU 131-9(A): (Ref. AMM TASK 49-16-00-200-002) If you find damage:	X
	(1) Internally examine the diverter system, the ball bearing control and the flap actuator for distortion. Make sure that they are correctly attached.		X

5. Close-up
Subtask 05-51-21-410-050-A

A. Close Access
(1) CLOSE THE ACCESS DOORS 312AR 314AR 315AL 316AR.

Subtask 05-51-21-942-050-A

B. Put the aircraft back to the serviceable condition.
(1) Remove the access platform(s).
(2) Remove the ground support and maintenance equipment, the special and standard tools and all other items.

[Rev.10 from 2021] 2026.03.31 22:51:35 UTC