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88-21-05: Exhaust Systems (STC SA980NM)

FAA order 88-21-05 is an airworthiness directive in force since November 6, 1988. The FAA's subject line: Exhaust Systems (STC SA980NM). It names Piper PA-60 Aerostar: about 57 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Aerostar Aircraft Corporation
Models
PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P), PA-60-700P (Aerostar 700P)
On this site
Piper PA-60 Aerostar 57 registered

Dates and paperwork

In force since
November 6, 1988
Docket
Unknown
Status
Current
The FAA's document
Read the order on the FAA's site

The order itself the regulatory text, as published

Show the full text (1,934 characters)
88-21-05 PIPER: Amendment 39-6039. Applies to PA-60 series (all serial numbers) airplanes certificated in any category modified per Machen, Inc., Supplemental Type Certification (STC) No. SA980NM. NOTE: STC No. SA980NM pertains to installation of AVCO Lycoming Model TIO-and LTIO-540-J2BD engines. Compliance: Required as indicated, unless previously accomplished. To prevent a possible inflight engine fire, accomplish the following: (a) Within the next 50 hours time-in-service, after the effective date of this AD, and thereafter at every 100 hours time-in-service, inspect, and replace, as necessary, the exhaust systems on both engines in accordance with Machen, Inc. Service Bulletin (SB) No. 66- 018, dated June 5, 1987. (b) The repetitive inspections specified in paragraph (a) are no longer required when the exhaust system has been modified in accordance with Machen, Inc. SB 66-019, dated January 8, 1988. (c) Within the next 50 hours time-in-service, after the effective date of this AD, and thereafter at every 100 hours time-in-service, inspect, and replace as necessary the oil lines on both engines in accordance with Machen, Inc. SB 66-018, dated June 5, 1987. (d) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished. (e) An equivalent means of compliance with this AD may be used if approved by the Manager, Modification Branch, ANM-190S, FAA, Northwest Mountain Region, 17900 Pacific Highway South, C-68966, Seattle, Washington 98168. All persons affected by this directive may obtain copies of the documents referred to herein upon request to Machen, Inc., South 3608 Davison Boulevard, Spokane, Washington 99204 or may examine these documents at the Office of the Assistant Chief Counsel, Room 1558, FAA, 601 East 12th Street, Kansas City, Missouri 64106. This amendment, 39-6039, becomes effective on November 6, 1988.

Related safety bulletins advice on the same designs, not orders

2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
2003-09-18CE-03-55 ·

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 6, 2026. Connections as data: /graph/directive/88-21-05.json · aircraft systems.