AD 43-12-01

Active

Elevator Hinge Brackets

Key Information
43-12-01
Active
Not specified
Not specified
Unknown
N/A
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
DC3A-S1C3G DC3A-S1CG DC3A-S4C4G DC3A-SC3G DC3A-SCG
Regulatory Text

43-12-01 DOUGLAS: (Was Service Note 4 of AD-669-3.) Applies to DC3A aircraft. \n\n\tAt each periodic inspection, check the elevator hinge brackets and if cracks are present the brackets should be replaced. Due to the possibility of vibration causing fatigue failures, continuous operation of the airplanes in the range of engine speeds between 1,300 and 1,600 r.p.m. should be avoided. A minimum engine speed of 1,700 r.p.m. during cruising flight is recommended. \n\n\t(Douglas Service Letter dated January 15, 1943, covers this same subject.)

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