- Effective
- September 26, 1979
- Models
- AEIO-320-D1B, AEIO-320-E1A, AEIO-320-E1B, AEIO-320-E2A, AEIO-320-E2B, AEIO-360-A1A and 212 more
- Registered aircraft
- 23,938 matched by model
- Product
- Engine
- Amendment
- 39-3570
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 29 KB | 03c44937…9338afa | FAA DRS (API key needed) |
On this page
The airworthiness directive
79-04-05 AVCO LYCOMING: Amendment 39-3418 as amended by Amendment 39-3570. Applies to all fuel injected Lycoming series engines equipped with the following Bendix Injector Models and Parts List Numbers:
Model Parts List and Issue Serial Numbers RSA-5AB1 2524254-4 2524712-1 63758 thru 65862 63503 thru 66027 RSA-5AD1 2524054-4 62999 thru 66249
2524147-6 65988 thru 65997
2524171-4 64961 thru 65060
2524213-4 61032 thru 66290
2524291-4 63678 thru 65867
2524297-3 64428 thru 64432
2524307-3 64828 thru 66854
2524335-3 65721 thru 66920
2524359-3 62401 thru 65412
2524450-2 61392 thru 65987
2524550-1 64635 thru 65887
2524673-1 63643 thru 64265
2524682-1 65071 thru 65499
2524723-1 61928 thru 65231
2524469(B) 64915 thru 65338 RSA-10AD1 2524163-7 63742 thru 65720
2524175-3 63399 thru 66941
and to all Lycoming fuel injected engines irrespective of parts list number or serial number whose Bendix Injector Models RSA-5AD1, RSA-5AB1, and RSA-10AD1 have been overhauled by a Bendix Authorized Warrant Repair Station or by AVCO Lycoming between April 1, 1977, and August 14, 1978, and to all Lycoming fuel injected engines irrespective of parts list number or serial number, whose Bendix Models RSA-5AB1, RSA- 5AD1, and RSA-10AD1 fuel injectors have been overhauled after March 31, 1977, by repair stations other than the above in which the fuel diaphragm has been replaced with a new P/N 2529471 diaphragm assembly.
Compliance required within the next 10 hours in service after the effective date of this AD, unless previously accomplished.
To prevent an in-flight power loss due to the separation of the P/N 2529192 regulator diaphragm stem assembly, the P/N 2529471 regulator diaphragm assembly must be removed, inspected, and replaced if necessary, in accordance with the Accomplishment Instructions listed in Bendix Energy Controls Division Service Bulletin No. RS-57 Rev. 1 or FAAapproved equivalent.
Equivalent methods of compliance must be approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Eastern Region. Upon submission of substantiating data by an owner or operator through an FAA Maintenance Inspector, the Chief, Engineering and Manufacturing Branch, FAA Eastern Region may adjust the compliance time specified in this AD.
NOTE: AVCO Lycoming Service Bulletin No. 433A also pertains to this subject.
Amendment 39-3418 was effective February 26, 1979.
This Amendment 39-3570 is effective September 26, 1979.
Affected TCDS · 15
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 23,938
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1929 | 1 |
|---|---|
| 1930 | 1 |
| 1937 | 1 |
| 1939 | 1 |
| 1940 | 1 |
| 1941 | 1 |
| 1943 | 1 |
| 1946 | 9 |
| 1947 | 6 |
| 1948 | 8 |
| 1949 | 2 |
| 1950 | 7 |
| 1951 | 7 |
| 1952 | 1 |
| 1953 | 5 |
| 1954 | 4 |
| 1955 | 2 |
| 1956 | 7 |
| 1957 | 4 |
| 1958 | 6 |
| 1959 | 7 |
| 1960 | 23 |
| 1961 | 38 |
| 1962 | 53 |
| 1963 | 180 |
| 1964 | 449 |
| 1965 | 531 |
| 1966 | 781 |
| 1967 | 783 |
| 1968 | 593 |
| 1969 | 718 |
| 1970 | 273 |
| 1971 | 384 |
| 1972 | 502 |
| 1973 | 662 |
| 1974 | 643 |
| 1975 | 707 |
| 1976 | 955 |
| 1977 | 1,004 |
| 1978 | 1,058 |
| 1979 | 611 |
| 1980 | 373 |
| 1981 | 386 |
| 1982 | 226 |
| 1983 | 146 |
| 1984 | 148 |
| 1985 | 81 |
| 1986 | 62 |
| 1987 | 73 |
| 1988 | 78 |
| 1989 | 125 |
| 1990 | 115 |
| 1991 | 121 |
| 1992 | 135 |
| 1993 | 154 |
| 1994 | 127 |
| 1995 | 175 |
| 1996 | 169 |
| 1997 | 280 |
| 1998 | 575 |
| 1999 | 631 |
| 2000 | 628 |
| 2001 | 471 |
| 2002 | 339 |
| 2003 | 441 |
| 2004 | 601 |
| 2005 | 625 |
| 2006 | 242 |
| 2007 | 162 |
| 2008 | 148 |
| 2009 | 113 |
| 2010 | 118 |
| 2011 | 102 |
| 2012 | 109 |
| 2013 | 81 |
| 2014 | 94 |
| 2015 | 72 |
| 2016 | 84 |
| 2017 | 99 |
| 2018 | 122 |
| 2019 | 150 |
| 2020 | 160 |
| 2021 | 149 |
| 2022 | 199 |
| 2023 | 215 |
| 2024 | 207 |
| 2025 | 227 |
| 2026 | 125 |
2,645 with no year recorded
By model
See all 136 modelsAircraft
NTSB investigations that cite this AD · 1
Their narratives or probable cause name AD 79-04-05, often to say whether the aircraft complied with it.