General Visual Inspection of Fuselage Skin and Door Frame around Forward Passenger/Crew Door, between FR12 and FR24 and between Upper and Lateral ...

TASK 53-11-00-210-820-A
General Visual Inspection of Fuselage Skin and Door Frame around Forward Passenger/Crew Door, between FR12 and FR24 and between Upper and Lateral ...

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.

ZONE: 120
ZONE: 210
ZONE: 220
ZONE: 230

1. Reason for the Job
Refer to the MPD TASK: 531106-01
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND DOOR FRAME AROUND FORWARD PASSENGER/CREW DOOR, BETWEEN FR 12 AND FR 24 AND BETWEEN UPPER AND LATERAL STRINGERS, EXCEPT SCUFF PLATE AREA, EXTERNAL SURFACE, LH/RH

NOTE: The effectivity of this task is "ALL". To know if this task is applicable to your aircraft, refer to the MPD task applicability and the weight variant data given in the SRM introduction.

2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	AR	ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.08BAA9)	Non Aqueous Cleaner-General - -
(Material No.14SBA1)	Textile-Lint free Cotton -

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
120	AVIONICS COMPARTMENT
210	CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD
220	FWD CAB UTILITY AREAS
230	FWD PASSENGER COMPARTMENT

D. Referenced Information

REFERENCE	DESIGNATION
SRM 511100	(for corrective action)
SRM 512200	(for corrective action)
External Surface of the Fuselage Skin and the Door Frame around the Forward Passenger/Crew Door

3. Job Set-up
Subtask 53-11-00-010-121-A

A. Get Access
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position in front of the inspection area.

Subtask 53-11-00-110-140-A

B. Preparation of Inspection Area
(1) Make sure that the inspection area is sufficiently clean to do a satisfactory inspection of the area.
(2) If it is not sufficiently clean, clean the inspection area with Non Aqueous Cleaner-General - - (Material No.08BAA9) and Textile-Lint free Cotton - (Material No.14SBA1) .

4. Procedure
Subtask 53-11-00-210-098-A

A. Inspection

External Surface of the Fuselage Skin and the Door Frame around the Forward Passenger/Crew Door

(1) Do a general visual inspection of the external surface of the fuselage skin and the door frame around the forward passenger/crew door. Do this inspection on the left and right sides. This inspection includes the area between FR12 and FR24 and between the upper and the lateral stringers. This inspection does not include the scuff plate area.
(2) Make sure that there is no:
(a) Corrosion damage:

If you find corrosion damage, refer to Structural Repair Manual SRM 512200 for types of corrosion, inspection, removal and corrosion protection.

(b) Other damage (scratches, cracks, gouges, dents, creases):

If you find this type of damage, refer to Structural Repair Manual SRM 511100 for damage classification and corrective action.

5. Close-up
Subtask 53-11-00-410-121-A

A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the access platform(s).

[Rev.10 from 2021] 2026.04.02 06:28:46 UTC