AD 59-10-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 707-100 Long Body | BOEING Model 707-100 Series Airplanes |
| aircraft | The Boeing Company | 707-100B Long Body | BOEING Model 707-100 Series Airplanes |
| aircraft | The Boeing Company | 707-100B Short Body | BOEING Model 707-100 Series Airplanes |
Unsafe Condition
The absence of suitable plates on the cabin sidewalls near fuselage Station 196.5 could result in insufficient clearance between the left outboard and right outboard rudder pedals and the cabin sidewall structures during rudder pedal travel.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
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 plates of 0.032 gauge aluminum alloy or 0.062 thick Royalite material on the cabin sidewalls near fuselage Station 196.5 to ensure positive clearance for rudder pedals throughout their full travel.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
May 30, 1959
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 707-100 Series Airplanes with registration numbers N707PA through N712PA, N70773, N7501A through 7510A, and N732TW through N736TW.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.