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AD 46-27-02 ACTIVE

Nose Wheel Brace Strut Collar
Key Information
AD Number 46-27-02 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) C54-DC C54A-DC C54B-DC C54D-DC C54E-DC C54G-DC DC-4
Regulatory Text

46-27-02 DOUGLAS: (Was Mandatory Note 4 of AD-762-7.) Applies to C-54 and DC-4 Aircraft. \n\n\tInspection to be accomplished immediately and at periods not to exceed 35 hours thereafter. \n\n\tNumerous reports have been received of cracks occurring in the nose wheel brace strut collar, P/N 5102824, in the region where the steering lugs meet the collar body. If cracks are found, repairs should be made as outlined in Douglas Service Bulletin C-54-209S (Supplement) dated May 31, 1946. After repairs have been accomplished, inspection must be continued at intervals not to exceed 35 hours. \n\n\tDouglas Service Bulletin C-54-209S (Supplement) dated August 12, 1946, contains the information which is included in the supplement dated May 31, 1946. In addition, the later supplement outlines a method for the installation of steel brace rods to the nose wheel brace strut collar. Although the addition of the steel brace rods is not mandatory, it is recommended by the Douglas Co. If the steelbrace rod installation has been incorporated in addition to the rework to the nose wheel brace strut collar which is required in the above paragraph, the 35-hour periodic inspections will not be required.