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FAA
Federal Aviation Administration Department of Transportation
Aviation Safety
AIRWORTHINESS DIRECTIVE
Generated by Aircraft-logs.com — March 21, 2026

AD 59-10-01 ACTIVE

Cabin Sidewalls
Key Information
AD Number 59-10-01 Status Active
Effective Date Not specified Issue Date Not specified
Docket Number Unknown Amendment N/A
Product Type ["Aircraft"] Product Subtype ["Large Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) The Boeing Company
Model(s) 707-100 Long Body 707-100B Long Body 707-100B Short Body
Regulatory Text

59-10-01\tBOEING: Applies to Boeing Model 707-100 Series Airplanes Registration Number N707PA Through N712PA, N70773, N7501A Through 7510A, N732TW Through N736TW. \n\tCompliance required by May 30, 1959. \n\tRemove 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. \n\t(Boeing Service Bulletin NO. 298 Revision R-1 covers this subject.)

AD 59-10-01 — Cabin Sidewalls
Printed from Aircraft-logs.com — 03/21/2026