AD 89-24-03

Airworthiness directive · Turbocharger Inlet Assembly · Continental Motors TSIO-520-UB

Effective
June 18, 1990
Model
TSIO-520-UB
Data sheet
TCDSE8CE
Registered aircraft
4,140 matched by model
Product
Engine
Amendment
39-6386
Docket
89-ANE-19

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.

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The airworthiness directive

89-24-03 TELEDYNE CONTINENTAL MOTORS (TCM): Amendment 39-6386. Correction issued on May 8, 1990. Docket No. 89-ANE-19. Applicability: TCM Model TSIO-520-UB engines, serial numbers 515000 thru 515999 and 527000 thru 527070, and to all remanufactured and overhauled engines of this model, regardless of serial number, which are equipped with part number (P/N) 642668 turbocharger inlet assembly. Compliance: Required at the next 100 hour inspection or annual inspection, or within 100 flight hours, whichever occurs first after the effective date of this AD, and thereafter at intervals not to exceed 100 flight hours. To prevent possible cracking of the turbocharger inlet assembly which could result in engine compartment fire, accomplish the following: (a) Visually inspect turbocharger inlet assembly P/N 642668 for cracks especially in the weld joints just above the turbine inlet temperature boss. If a crack is found, replace P/N 642668 with P/N 646795 turbocharger inlet assembly, prior to further flight. (b) Make appropriate log book entry showing compliance with this AD. NOTES: (1) Beechcraft Aircraft Corporation Service Communique No. 70, dated October 28, 1983, refers to this subject. NOTES: (2) When determining the P/N assembly installed in order to comply with this AD, a distinguishing feature of the P/N 646795 turbocharger inlet assembly is 2 ribs (approximately 0.25 inches in height, 0.1 inches in width, and 2.1 inches in length) on the top of the turbocharger mating flange. NOTES: (3) If P/N 642668 is not installed, no action is required. (c) Aircraft may be ferried in accordance with the provisions of FAR 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,Atlanta Aircraft Certification Office, Federal Aviation Administration, 1669 Phoenix Parkway, Suite 210C, Atlanta, Georgia 30349. This amendment 39-6386 (AD 89-24-03) became effective on December 4, 1989. This correction becomes effective on June 18, 1990.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 4,140

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Cessna3,180 aircraft
  • Beech690 aircraft
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By year built
19182003
Registered aircraft by year built: 3,685 aircraft
19181
19471
19482
19491
19551
19561
19571
19622
19631
19642
19657
196614
196715
196813
196926
197016
197127
197297
1973141
1974137
1975172
1976233
1977282
1978476
1979572
1980416
1981351
1982160
198370
1984123
198587
198656
198726
198822
19894
19909
19919
19928
199312
199410
19957
19965
19977
199812
199915
200012
200118
20023
20032

455 with no year recorded

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