- Models
- 707-100 Long Body, 707-100B Long Body, 707-100B Short Body
- Data sheet
- TCDS4A21
- Product
- Aircraft · Large airplane
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 19 KB | f4a4115b…2f6b419 | FAA DRS (API key needed) |
On this page
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 TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.