89-15-10: Nozzle Vent Manifold
FAA order 89-15-10 is an airworthiness directive in force since November 30, 1989. The FAA's subject line: Nozzle Vent Manifold. It names the Lycoming TIO-540-AE2A engine: about 488 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
- Engine
- Makes
- Lycoming Engines
- Models
- TIO-540-AE2A
- Engine series
- Lycoming TIO-540-AE2A 488 aircraft
Dates and paperwork
- In force since
- November 30, 1989
- 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 (2,182 characters)
89-15-10 TEXTRON LYCOMING: Amendment 39-6377. Final copy of Priority Letter AD.
Applicability: Model TIO-540-AE2A engines (with serial numbers up to and including L9064-61A) installed in Piper PA-46-350P airplanes certified in any category.
Compliance: Required within 5 hours in service after the effective date of this AD unless already accomplished.
To prevent engine roughness and loss of engine power, accomplish the following:
(a) Perform a fuel leak check at the upper deck left nozzle vent manifold or at the fuel pump vent hose check valve in accordance with Appendix I and Appendix II of this AD. Observe if any fuel emerges at the disconnected line with the aircraft emergency boost pump operating. If fuel is observed, the engine pump diaphragm is considered defective. Prior to further flight, replace pump with a new or serviceable pump and repeat the above leak check.
(b) Remove tee fitting P/N AN-825-4 from the engine fuel pump vent and install restrictor typetee fitting P/N 02A21171 (Piper P/N 766-224) in accordance with Appendix I and Appendix II of this AD.
(c) Aircraft may be ferried in accordance with the provisions of FAR's 21.197 and 21.199 to a base where the AD can be accomplished.
(d) Upon submission of substantiating data by an owner or operator through an FAA Airworthiness Inspector, an alternate method of compliance with the requirements of this AD or adjustments to the compliance schedule specified in this AD may be approved by the Manager, New York Aircraft Certification Office, Engine and Propeller Directorate, Aircraft Certification Service, Federal Aviation Administration, Room 202, 181 South Franklin Avenue, Valley Stream, New York 11581.
This amendment (39-6377, AD 89-15-10) becomes effective on November 30, 1989, as to all persons except those persons to whom it was made immediately effective by priority letter AD No. 89-15-10, issued on July 26, 1989, which contained this amendment.
APPENDIX I
NOTE: TEXTRON Lycoming Service Bulletin No. 487, dated July 7, 1989, pertain to these inspections.
APPENDIX II
NOTE: PIPER Service Bulletin No. 915, dated July 8, 1989, pertain to these inspections.
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 October 30, 2026. Connections as data: /graph/directive/89-15-10.json · aircraft systems.
