# AD 66-16-02: Engine Mounting Fuselage Frame

- Type: Airworthiness directive
- Status: Current
- Products: Airbus BAC 1-11 200 Series
- Effective: July 31, 1966
- Superseded by: Nothing supersedes this AD
- Product type: Aircraft, Large airplane
- Amendment: 39-254
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B27016C40D28C8A78625699F005E8205.0001
- DRS record last changed: May 30, 2024
- Page: https://openairdocs.org/ad/66-16-02

## The airworthiness directive

66-16-02 BRITISH AIRCRAFT CORPORATION: Amdt. 39-254 Federal Register July 1, 1966. Applies to Model BAC 1-11 200 Series Airplanes.

Compliance required before the accumulation of 3,000 hours' time in service for airplanes with less than 2,900 hours' time in service on the effective date of this AD and within the next 100 hours' time in service after the effective date of this AD for airplanes with 2,900 or more hours' time in service on the effective date of this AD unless already accomplished.

To prevent chafing of the fuselage frame forward flange by the aft end of the headliner, rework the headliner, P/N AB77 A1605, and inspect the flange of fuselage frame, P/N AB29 A501, and rework as necessary in accordance with British Aircraft Corporation (BAC) One- Eleven Alert Service Bulletin 53-A-PM 2107, dated February 1, 1966, or later ARB-approved issue.

This directive effective July 31, 1966.

## Affected data sheets (1) (OpenAirDocs)

The type certificate data sheets whose models the AD names.

- [TCDS A5EU](https://openairdocs.org/tcds/A5EU): Airbus SAS; names 1 of 2 models: BAC 1-11 200 Series

## Registered aircraft it may apply to (OpenAirDocs)

No registered aircraft matched the models it names.

Its text cites no advisory circulars or STCs.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.