AD 70-23-01

Active

Gear Side Strut Spindle Nut

Key Information
70-23-01
Active
November 06, 1970
Not specified
Unknown
39-1103
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
747-100 Series
Regulatory Text

70-23-01\tBOEING: Amdt. 39-1103. Applies to Boeing Model 747-100 Series airplanes certificated in all categories. \n\tCompliance required within the next 200 hours' time in service after the effective date of this ad, unless already accomplished. \n\tTo prevent failures of the spindle nut, accomplish the following: \n\tReplace the wing gear upper side strut spindle nut in accordance with Boeing Service Bulletin 32-2055 dated October 2, 1970, or later FAA approved revision, or an equivalent method approved by the Chief, Aircraft Engineering Division, FAA Western Region. \n\tThe amendment becomes effective November 6, 1970.

AD Assistant

Get AI-powered answers about this AD, check applicability, and find compliance steps.

Sign Up to Unlock
References
This information is not available.
--- - Part 39
FAA Documents