AD 48-41-01

Active

Wing Bulkhead Flanges and Stringers

Key Information
48-41-01
Active
Not specified
Not specified
Unknown
N/A
Applicability
["Aircraft"]
["Large Airplane"]
Kelowna Flightcraft R & D Ltd.
240 Series
Regulatory Text

48-41-01 CONVAIR: Applies to All Model 240 Aircraft.

Compliance required as indicated.

I. Inspect wing bulkhead flanges and stringers at their intersections in the fuel tank area for cracks and repair as necessary at each No. 2 inspection (or equivalent periodic inspection approximating 100 hours) until permanent repairs and rework are accomplished.

II. Complete rework in accordance with CVAC Service Bulletin No. 240-166A dated September 27, 1948, or equivalent should be accomplished not later than the next engine change.

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