- Effective
- November 14, 1974
- Model
- TFE731-2
- Data sheet
- TCDSE6WE
- Registered aircraft
- 1,026 matched by model
- Product
- Engine
- Amendment
- 39-2008
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 | 22 KB | 4abdfb22…c873ee0 | FAA DRS (API key needed) |
On this page
The airworthiness directive
74-23-05 AIRESEARCH MANUFACTURING COMPANY OF ARIZONA: Amendment 39-2008. Applies to AiResearch Model TFE731-2-2B and -2-1C engines installed in, but not limited to, AMD Falcon DA-10 and Lear-Gates Models 35 and 36 aircraft certificated in all categories.
(A) Upon receipt of this telegram, except as authorized in (C) below, P/N 3070851-2, -4, -5, and -6 fuel pumps with less than 25 hours total time in service must be replaced before exceeding 25 hours total time in service. Fuel pumps with more than 25 hours total time in service must be replaced before further flight.
(B) The maximum service life of P/N 3070851-2, -4, -5, and -6 fuel pumps is 25 hours total time in service since new or overhaul.
(C) AiResearch Service Bulletin TFE731-73-3005, dated July 10, 1974, provides instructions for inspecting and re-identifying P/N 3070851-5 and -6 fuel pumps which have been determined to conform to the -7 and -8 configuration.
(D) P/N 3070851-7 and -8 fuel pumps are not subject to the service life limit prescribed in (A) above and may be installed in accordance with AiResearch Service Bulletin TFE731-73-3005, dated July 10, 1974, or later FAA-approved revisions.
(E) Equivalent procedures may be approved by the Chief, Aircraft Engineering Division, FAA Western Region, upon submission of adequate substantiation data.
(F) Aircraft may be flown to a base for performance of maintenance required by the AD per FAR's 21.197 and 21.199.
This supersedes telegram dated June 4, 1974 and AD 74-13-08.
This amendment becomes effective November 14, 1974, for all persons except those to whom it was made effective immediately by telegram dated June 4, 1974.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 1,026
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1966 | 2 |
|---|---|
| 1967 | 3 |
| 1969 | 2 |
| 1972 | 1 |
| 1974 | 11 |
| 1975 | 10 |
| 1976 | 18 |
| 1977 | 21 |
| 1978 | 10 |
| 1979 | 13 |
| 1980 | 35 |
| 1981 | 49 |
| 1982 | 45 |
| 1983 | 24 |
| 1984 | 43 |
| 1985 | 26 |
| 1986 | 23 |
| 1987 | 27 |
| 1988 | 28 |
| 1989 | 17 |
| 1990 | 19 |
| 1991 | 16 |
| 1992 | 20 |
| 1993 | 26 |
| 1994 | 22 |
| 1995 | 24 |
| 1996 | 26 |
| 1997 | 23 |
| 1998 | 28 |
| 1999 | 39 |
| 2000 | 38 |
| 2001 | 57 |
| 2002 | 51 |
| 2003 | 20 |
| 2004 | 44 |
| 2005 | 25 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2011 | 1 |
135 with no year recorded