AD 88-25-08

Active

Engine Cooling System

Key Information
88-25-08
Active
January 03, 1989
November 22, 1988
Unknown
39-6087
Applicability
["Aircraft"]
["Small Airplane"]
Piper Aircraft Inc.
PA-46-310P
Regulatory Text

88-25-08 PIPER: Amendment 39-6087. Applies to Model PA-46-310P (all serial numbers) airplanes certificated in any category.

Compliance: Required within the next 50 hours time-in-service after the effective date of this AD, unless already accomplished.

To prevent possible catastrophic engine failure accomplish the following:

(a) Modify the engine cooling system in accordance with Piper Service Bulletin 892, dated August 24, 1988.

(b) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished.

(c) An equivalent means of compliance with this AD, if used, must be approved by the Manager, Atlanta Aircraft Certification Office, ACE-115A, Federal Aviation Administration, 1669 Phoenix Parkway, Suite 210C, Atlanta, Georgia 30349.

This amendment (39-6087, AD 88-25-08) becomes effective on January 3, 1989.

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References
This information is not available.
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Issuing Office
["AIR-720: Operational Safety Branch"]
FAA Documents