AD 80-02-15

Superseded

Elevator Butt Rib Cracks

Key Information
80-02-15
Superseded
January 29, 1980
Not specified
Unknown
39-3676
Applicability
["Aircraft"]
["Small Airplane"]
Piper Aircraft, Inc., The New
PA-31P PA-31T PA-31T1
Regulatory Text

80-02-15 PIPER: Amendment 39-3676. Applies to Model PA-31P, Serial Nos. 31P-1 thru 31P-7730012, Model PA-31T, Serial Nos. 31T-7400002 thru 31T-7920075 and Model PA- 31T1, Serial Nos. 31T-7804001 thru 31T-7904036 and 31T-7904038 thru 31T-79O4044 certificated in all categories except aircraft incorporating Piper Kit No. 763 943.

To prevent possible hazards in flight associated with cracks in the elevator butt ribs and adjoining area accomplish the following:

a. Within the next 100 hours in service from the effective date of this AD or upon the attainment of 400 hours in service, whichever is later, inspect and alter the elevators in accordance with Piper Kit No. 763 943 or equivalent.

b. Equivalent inspections or alterations must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

c. Upon submission of substantiating data by an owner or operator through an FAA Maintenance Inspector, the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region may adjust the inspection intervals specified in this AD.

(Piper Service Bulletin No. 658 dated July 31, 1979, refers to this subject.)

This amendment is effective January 29, 1980.

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Related ADs
2001-06-01 Replaced by the above
References
This information is not available.
--- - Part 39
FAA Documents