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83-22-04: Injector Fuel Diaphragm Stem

FAA order 83-22-04 is an airworthiness directive in force since November 4, 1983. The FAA's subject line: Injector Fuel Diaphragm Stem. It names the Lycoming AEIO-540-L1B5D, Lycoming IO-540-AA1A5, Lycoming IO-540-G1B5, Lycoming IO-540-G1C5, Lycoming IO-540-G1D5, Lycoming IO-540-K1A5, Lycoming IO-540-K1A5D, Lycoming IO-540-K1B5, Lycoming IO-540-K1C5, Lycoming IO-540-K1F5, Lycoming IO-540-K1G5, Lycoming IO-540-K1G5D, Lycoming IO-540-K1J5, Lycoming IO-540-M1B5D, Lycoming IO-540-S1A5, Lycoming IO-540 series, Lycoming LTIO-540-F2BD, Lycoming LTIO-540-J2BD, Lycoming TIGO-541-E1A, Lycoming TIO-540-F2BD, Lycoming TIO-540-J2BD, Lycoming TIO-540-S1AD, Lycoming TIO-540 series, Lycoming TIO-540-U2A, Lycoming TIO-540-V2AD, Lycoming TIO-541-E1C4, Lycoming TIO-541 series engines: about 9,902 aircraft on the U.S. register today across them, 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
AEIO-540-L1B5D, IO-540-AA1A5, IO-540-G1B5, IO-540-G1C5, IO-540-G1D5, IO-540-K1A5, IO-540-K1A5D, IO-540-K1B5, IO-540-K1C5, IO-540-K1D5, IO-540-K1F5, IO-540-K1F5D, IO-540-K1G5, IO-540-K1G5D, IO-540-K1J5, IO-540-K1J5D, IO-540-M1B5D, IO-540-S1A5, LTIO-540-F2BD, LTIO-540-J2BD, LTIO-540-N2BD, LTIO-540-U2A, LTIO-540-V2AD, TIGO-541-E1A, TIO-540-F2BD, TIO-540-J2BD, TIO-540-N2BD, TIO-540-S1AD, TIO-540-U2A, TIO-540-V2AD, TIO-541-E1A4, TIO-541-E1B4, TIO-541-E1C4
Engine series
Lycoming AEIO-540-L1B5D 41 aircraft
Lycoming IO-540-AA1A5 8 aircraft
Lycoming IO-540-G1B5 3 aircraft
Lycoming IO-540-G1C5 3 aircraft
Lycoming IO-540-G1D5 26 aircraft
Lycoming IO-540-K1A5 44 aircraft
Lycoming IO-540-K1A5D 3 aircraft
Lycoming IO-540-K1B5 18 aircraft
Lycoming IO-540-K1C5 1 aircraft
Lycoming IO-540-K1F5 2 aircraft
Lycoming IO-540-K1G5 48 aircraft
Lycoming IO-540-K1G5D 52 aircraft
Lycoming IO-540-K1J5 10 aircraft
Lycoming IO-540-M1B5D 2 aircraft
Lycoming IO-540-S1A5 10 aircraft
Lycoming IO-540 series 4,222 aircraft
Lycoming LTIO-540-F2BD 1 aircraft
Lycoming LTIO-540-J2BD 5 aircraft
Lycoming TIGO-541-E1A 1 aircraft
Lycoming TIO-540-F2BD 4 aircraft
Lycoming TIO-540-J2BD 24 aircraft
Lycoming TIO-540-S1AD 13 aircraft
Lycoming TIO-540 series 5,074 aircraft
Lycoming TIO-540-U2A 3 aircraft
Lycoming TIO-540-V2AD 2 aircraft
Lycoming TIO-541-E1C4 9 aircraft
Lycoming TIO-541 series 273 aircraft

Dates and paperwork

In force since
November 4, 1983
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 (2,435 characters)
83-22-04 AVCO LYCOMING: Amendment 39-4748. Applies to all Avco Lycoming IO-540-G1B5, -G1C5, -G1D5, -K1A5, -K1A5D, -K1B5, -K1C5, -K1D5, -K1F5, -K1F5D, -K1G5, -K1G5D, -K1J5, -K1J5D, - M1B5D, -S1A5, -AA1A5: AEIO-540-L1B5D; TIO-540-F2BD, -J2BD, -N2BD, -S1AD, -U2A, -V2AD; LTIO-540-F2BD, -J2BD, -N2BD, S1AD -U2A, -V2AD; LTI-540-F2BD, -J2BD, -N2BD, -U2A, -V2AD; TIO-541-E1A4, -E1B4, -E1C4; TIGO-541-E1A, series engines equipped with Bendix Models RSA-10DB1, RSA-10DB2, RSA-10ED1, and RSA-10ED2 fuel injectors as identified in Bendix Service Bulletin RS-88, including Supplement 1, Section 1.A. (1), (2) and (3). Compliance required within the next 50 hours in service after the effective date of this AD, unless previously accomplished. To prevent engine failure due to fatigue failure of the injector fuel diaphragm stem, replace P/N 2539806 fuel diaphragm assembly with P/N 2541803 and perform flow calibration and nameplate reidentification in accordance with Section 2 Accomplishment Instructions of Bendix Energy Controls Division Service Bulletin RS-85, or FAA approved equivalent. An equivalent method of compliance with this AD, may be used if approved by the Manager, New York Aircraft Certification Office, FAA, New England Region. Upon submission of substantiation data by an owner or operator through an FAA maintenance inspector, the Manager, New York Aircraft Certification Office, may adjust the compliance time specified in this AD. In accordance with FAR 21.197 and 21.199, the aircraft may be flown to a location where the alterations required by this AD can be performed. AVCO Lycoming S/B No. 467, Bendix Energy Control Service Bulletin Nos. RS-85 including Supplement No. 1, Revised August 10, 1983, and RS-88 including Supplement No. 1, Revised August 10, 1983, identified and described in this directive are incorporated herein and made by reference a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents may obtain copies upon request to Bendix Energy Controls Division, 717 North Bendix Drive, South Bend, Indiana 46620. These documents may also be examined at the Office of Regional Counsel, FAA New England Regional Office, 12 New England Executive Park, Burlington, Massachusetts 01803. A historical file on this AD is maintained at the New England Regional Office. This amendment becomes effective on November 4, 1983.

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/83-22-04.json · aircraft systems.