AD 47-02-04

Active

Engine Primer Solenoid

Key Information
47-02-04
Active
Not specified
Not specified
Unknown
N/A
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
C54-DC C54A-DC C54B-DC C54D-DC C54E-DC C54G-DC DC-4
Regulatory Text

47-02-04 DOUGLAS: (Was Mandatory Note 12 AD-762-7.) Applies to C-54 and DC-4 Aircraft.\n \n\tTo be accomplished not later than March 15, 1947. \n\n\tRelocate engine primer solenoid to prevent fuel leaking into firewall junction box. This change shall be accomplished in accordance with item 25 of Douglas Service Bulletin C-54-266, dated May 17, 1946, or part 2A, item 4; and part 2C, item 12 of Douglas Service Bulletin DC-4 No. 66, dated June 18, 1947. \n\n\tRevised May 24, 1948.

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