ALERT OPERATOR TRANSMISSION - ALERT OPERATOR TRANSMISSION

SUBJECT: A330 - ATA52 - INSPECTION OF AFT CARGO COMPARTMENT DOOR AT 

FRAME 60 AND FRAME 60A

OUR REF: AOT A330-A52L001-12 dated 3 Dec 2012

1. AIRCRAFT AFFECTED

All A330-200/300 aircraft up to MSN 0162 except those that have SB 52-3044 incorporated.

2. REFERENCED DOCUMENTATION

Ref.1: SRM 52-31-00 PB 001 Fig.3 Sheet 1 Item 100

Ref.2: SRM 52-31-00 PB 001 Fig.3 Sheet 1 Item 105

Ref.3: AOT A330-52A3085 - Inspection of forward cargo compartment door

Ref.4: SRM 52-32-00 PB 001 Fig.3 Sheet 1 Item 100

Ref.5: SRM 52-32-00 PB 001 Fig.3 Sheet 1 Item 105

Ref.6: AOT A330-52A3084 - Inspection of aft cargo compartment door

Ref.7: IPC 52-32-11- COVER-ACCESS, HANDLE Zone(s): 822 - Access Panels 822DR and 

822CR

Ref.8: TFU 52.32.00.003 - Aft cargo door cracked frame

3. REASON

3.1 FACTS

One operator has recently reported a case of A330 forward cargo door with two adjacent 

frame forks found cracked. Frame 20B (Ref.1) was found cracked through, frame 21 (Ref.2) 

was found cracked half through. At time of findings the aircraft had accumulated around 

21000 FC.

This A/C has been regularly inspected as per AOT Ref.3 inspection. However, during AOT 

Ref.3 accomplishment, the forward cargo door handle access panels 821CR and 821DR 

(Ref.7) were not removed, thus cracks at these two frames location might have remained 

undetected.

Note: A330/A340 forward cargo door Frame 20B between beam 3 and beam 4 is inspected 

according to ALI Task 523106-01-1 (for A/C pre-mod 50528 and A/C pre-mod 51038) with a 

first inspection at 10600FC and repetitive inspections every 2600 FC.

3.2 CONSEQUENCES
In case of one cracked or ruptured forward or aft cargo door frame, the loads will be 

transferred to the remaining structural elements. This second load path is able to sustain the 

loads for a limited number of flight cycles.

A Safety Assessment has shown that rupture of two vertical frames represents an unsafe 

condition due to the loss of the structural integrity of the cargo door.

As a consequence of the above and based on this new event on forward cargo door, it is 

necessary to launch an in-service action for both forward and aft cargo doors to ensure that 

structure behind handle access panels has been properly inspected. 

3.3 AIM

The aim of this AOT is to provide instructions for a repetitive inspection of the aft cargo door 

frames Fr60 (Ref.4) and Fr60A (Ref.5) for cracks and for sheared, loose or missing rivets.

4. ACTION REQUIRED

4.1 PLANNING

Perform the inspection described in paragraph 4.3 before the accumulation of 15800 FC after 

the first flight or within 100 FC from AOT issue date whichever occurs later. Afterwards, 

inspection described in paragraph 4.3 has to be repeated every 400FC.

4.2 MANPOWER

0.5 man-hours per aircraft are estimated for the inspection accomplishment.

4.3 DESCRIPTION

Before inspecting, close and lock the forward cargo door. 

Perform a detailed visual inspection of outer skin rivets at frame fork end Fr60 and Fr60A for 

loose, sheared or missing rivets (Refer to appendix 01)

Remove handle access panels 822CR and 822DR Ref. 7 (Refer to appendix 02).

Perform a detailed visual inspection of the whole Fr60 and Fr60A forks for cracks and for 

loose, sheared or missing rivets at frame web and flanges (Refer to appendix 03). 

In case of crack findings or rivets found sheared, loose or missing, the aft cargo door has to be 

repaired before next flight. Contact Airbus for repair instructions.
In case of nil finding repeat this inspection every 400 FC as well as the inspection as per AOT 

Ref.6 which remains applicable.

4.4 MATERIAL

AIRBUS MATERIAL, LOGISTICS AND SUPPLIERS 

WEG BEIM JAEGER 150

D-22335 HAMBURG

GERMANY

FAX: + 49 40 5076 4012

INTERNET: HTTP://SPARES.AIRBUS.COM

5. TERMINATING ACTION

A repetitive inspection service bulletin for the aft cargo door is under preparation and will 

supersede and cancel this AOT as well as AOT Ref. 6 and mandatory ISB 52-3043 "AFT 

CARGO COMPARTMENT DOOR - INSPECT STRUCTURE FOR CRACKS". It is 

anticipated that this inspection service bulletin will be mandatory.

TFU Ref.8 will keep operators informed about the forthcoming terminating action.

6. AOT APPROVAL

The technical content of this document is approved under the authority of DOA nr. 

EASA.21J.031.

It is anticipated that this AOT will be rendered mandatory by an EASA AD.

7. REPORTING/ACKNOWLEDGEMENT

Operators are requested to acknowledge receipt of this AOT within 48 hours after receipt to:

Cecile BORDES, SEES

E-mail: cecile.bordes@airbus.com

Fax number: +33+ (0)5 61.93.36.14

Question about this AOT and inspection results with or without findings are to be sent to 

AIRBUS CUSTOMER SERVICES ENGINEERING as soon as possible, after the AOT 

application, to the attention of:

Celine GALLET, SEES3

Phone number: +33+ (0)5 61.18.87.45
Fax number: +33+ (0)5 61.93.36.14

E-mail: celine.gallet@airbus.com

Best Regards,

Jean-Luc MOUYSSET Philippe GOURDON

VICE PRESIDENT ENGINEERING SUPPORT VICE PRESIDENT A330/A340 

PROGRAMME

CUSTOMER SERVICES CUSTOMER SERVICES