# AD 59-10-01: Cabin Sidewalls

- Type: Airworthiness directive
- Status: Current
- Products: Boeing 707-100 Long Body, 707-100B Long Body and 707-100B Short Body
- Superseded by: Nothing supersedes this AD
- Product type: Aircraft, Large airplane
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/94D4117EEA090E368625682A0065DC0B.0001
- DRS record last changed: May 30, 2024
- Page: https://openairdocs.org/ad/59-10-01

## The airworthiness directive

59-10-01 BOEING: Applies to Boeing Model 707-100 Series Airplanes Registration Number N707PA Through N712PA, N70773, N7501A Through 7510A, N732TW Through N736TW. Compliance required by May 30, 1959. Remove lining trim strip 65-1910-10 and lining panels 65-1910-3 and -4 from left-hand and right-hand cabin sidewall panel installations. Install suitable plate of 0.032 gage aluminum alloy or 0.062 thick Royalite material on the left-hand and right-hand cabin sidewalls in vicinity of fuselage Station 196.5 such that left outboard and right outboard rudder pedals will have positive clearance throughout the full range of rudder pedal travel. (Boeing Service Bulletin NO. 298 Revision R-1 covers this subject.)

## Affected data sheets (1) (OpenAirDocs)

The type certificate data sheets whose models the AD names.

- [TCDS 4A21](https://openairdocs.org/tcds/4A21): The Boeing Company; names 3 of 4 models: 707-100B Short Body, 707-100 Long Body, 707-100B Long Body

## 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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