AD 59-10-01

Active

Cabin Sidewalls

Key Information
59-10-01
Active
Not specified
Not specified
Unknown
N/A
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
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.)

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References
This information is not available.
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FAA Documents