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AD 46-43-02 ACTIVE

Rudder Pedal Slide Tube Support
Key Information
AD Number 46-43-02 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) DC3-G102 DC3-G102A DC3-G103A DC3-G202A DC3A-S1C3G DC3A-S1CG DC3A-S4C4G DC3A-SC3G DC3A-SCG DC3C-R-1830-90C DC3C-S1C3G DC3C-S4C4G DC3C-SC3G DC3D-R-1830-90C
Regulatory Text

46-43-02 DOUGLAS: (Was Mandatory Note 12 of AD-618-3 and Mandatory Note 13 of AD-669-3.) Applies Only to DC3 Series Aircraft Having the No. 4118923 Magnesium Alloy Casting Rudder Pedal Slide Tube Support. \n\n\tTo be accomplished not later than January 1, 1947. \n\n\tInstall a third AN 3-21 bolt in the existing hold between the two holes now having AN 3-21 bolts in the attachment of the Rudder Pedal Slide Tube Support No. 4118923 and -1, to its Pedal Assembly (5118929, 5118931, and 5118928). If necessary, to correct misalignment among the three holes, it is permissible to use 24ST or 4130 bushing with 1/32-inch wall thickness. This additional bolt is necessary to insure the 100% margin of safety required on the magnesium casting. \n\n\t(Douglas Service Bulletin C-47-101 covers this same subject.)