AD 47-33-02

Active

Cowl Flap Hydraulic Lines

Key Information
47-33-02
Active
Not specified
Not specified
Unknown
N/A
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
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

47-33-02\tDOUGLAS: (Was Mandatory Note 14 of AD-618-3, Supplement 2; and Mandatory Note 15 of AD-669-3, Supplement 2.) Applies to All DC3 Series Aircraft. \n\nTo be accomplished not later than the first engine change after September 1, 1947, but in any event not later than December 1, 1947. \n\nIn order to preclude cowl flap hydraulic line failures and possible subsequent fires, replace grommets and lines forward of the firewall with AN 833-4 elbows and AN 924-4 nuts, or equivalent, and new fire resistant flexible hose assemblies of proper length.

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References
This information is not available.
--- - Part 39
FAA Documents