# AD 69-11-07: Fuselage Center Section

- Type: Airworthiness directive
- Status: Current
- Products: Slingsby Type T.53.B.
- Effective: June 2, 1969
- Superseded by: Nothing supersedes this AD
- Product type: Aircraft, Glider
- Amendment: 39-771
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AC31AD4E9647EB4B86256A560052F5D2.0001
- DRS record last changed: May 30, 2024
- Page: https://openairdocs.org/ad/69-11-07

## The airworthiness directive

69-11-07 SLINGSBY: Amdt. 39-771. Applies to all Slingsby Model T.53.B Gliders.

Before further flight after the effective date of this AD, modify the fuselage center section structure in accordance with Slingsby Technical Instruction No. 39, dated March 1969, or later ARB-approved issue or FAA-approved equivalent.

This amendment becomes effective June 2, 1969.

## Affected data sheets (1) (OpenAirDocs)

The type certificate data sheets whose models the AD names.

- [TCDS G17EU](https://openairdocs.org/tcds/G17EU): Slingsby Aircraft Co Ltd.; names 1 of 1 models: Type T.53.B.

## Registered aircraft it may apply to (OpenAirDocs)

No registered aircraft matched the models it names.

Its text cites no advisory circulars or STCs.

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