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AD 70-23-01 ACTIVE

Gear Side Strut Spindle Nut
Key Information
AD Number 70-23-01 Status Active
Effective Date November 06, 1970 Issue Date Not specified
Docket Number Unknown Amendment 39-1103
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) 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.