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AD 83-22-04 ACTIVE

Injector Fuel Diaphragm Stem
Key Information
AD Number 83-22-04 Status Active
Effective Date November 04, 1983 Issue Date Not specified
Docket Number Unknown Amendment 39-4748
Product Type ["Engine"] Product Subtype Not specified
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) Lycoming Engines
Model(s) 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
Regulatory Text

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.