# Proposed AD FAA-2011-0037: Airbus Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes)

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2011-10-10
- Products: Airbus
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: February 7, 2011, 76 FR 6581
- Comments due: March 24, 2011
- Became: [AD 2011-10-10](https://openairdocs.org/ad/2011-10-10)
- Docket: FAA-2011-0037 (https://www.regulations.gov/docket/FAA-2011-0037, where comments are filed)
- Project: 2010-NM-273-AD
- FR document: 2011-2612
- Official PDF: https://openairdocs.org/files/sha256/49/ed/49edf22c18b9e3aa34ab2c58828b0e8e77eb30fe6b87a38c23f3bf189d502651 (from https://www.govinfo.gov/content/pkg/FR-2011-02-07/pdf/2011-2612.pdf)
- Federal Register: https://www.federalregister.gov/documents/2011/02/07/2011-2612/airworthiness-directives-airbus-model-a300-b4-600-b4-600r-and-f4-600r-series-airplanes-and-model
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6EE6A9E7B1FB0EB48625783000528207.0001
- Page: https://openairdocs.org/proposed/FAA-2011-0037

## Summary

We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

[T]he FAA has published SFAR 88 (Special Federal Aviation Regulation 88).

In their letters referenced 04/00/02/07/01-L296, dated March 4th, 2002, and 04/00/02/07/03-L024, dated February 3rd, 2003, the JAA [Joint Aviation Authorities] recommended the application of a similar regulation to the National Aviation Authorities (NAA).

Under this regulation, all holders of type certificates for passenger transport aircraft * * * are required to conduct a design review against explosion risks.

During improvement of the protection of fuel pump wiring against short-circuit by accomplishment of Airbus Service Bulletin (SB) A300-24-6094, astudy led by the manufacturer concluded that the harness, installed through the wing panel needed to be protected to prevent possible damage in case of chafing which could potentially lead to short-circuit [and intermittent function or loss of the inner tank fuel pump. Loss of both inner tank fuel pumps could result in inability to use the remaining fuel supply in the inner tank. A short-circuit could also result in an ignition source in a flammable leakage zone]. * * * * *

The proposed AD would require actions that are intended to address the unsafe condition described in the MCAI.

## Notices in this docket

- Feb 7, 2011: Notice of proposed rulemaking (NPRM). (first notice), FR document 2011-2612, comments due Mar 24, 2011 (https://www.federalregister.gov/documents/2011/02/07/2011-2612/airworthiness-directives-airbus-model-a300-b4-600-b4-600r-and-f4-600r-series-airplanes-and-model)

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