AD 74-26-05

Active

Fuel Control Units

Key Information
74-26-05
Active
January 02, 1975
Not specified
Unknown
39-2046
Applicability
["Engine"]
Not specified
Pratt & Whitney Canada Corp.
JT15D-1 JT15D-4
Regulatory Text

74-26-05 PRATT & WHITNEY AIRCRAFT and UNITED AIRCRAFT OF CANADA, LIMITED: Amendment 39-2046. Applies to all Pratt & Whitney Aircraft and United Aircraft of Canada Limited JT15D-1 and JT15D-4 turbofan engines containing fuel control P/Ns 3022332 and 3023349.

Compliance required within the next 25 hours time in service after the effective date of this AD unless already accomplished.

To prevent fuel leaks, inspect fuel control units for possible interference between the fuel outlet housing and the fuel control main body by placing a .003 inch feeler gage between the mating faces of the fuel outlet housing (P/N 3240082) and the fuel control main body (P/N 3240451). If the feeler gage can be inserted between the mating faces, replace fuel control with dimensionally correct fuel control prior to next flight.

United Aircraft of Canada Limited's Special Instruction No. 3-74, dated September 20, 1974, pertains to this subject.

This amendment becomes effective January 2,1975.

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