AD 90-25-17

Airworthiness directive · Oil Cooler Inlet · SOCATA TB 10, TB 20, TB 21 and 1 more

Effective
January 3, 1991
Models
TB 10, TB 20, TB 21, TB9
Data sheet
TCDSA51EU
Registered aircraft
304 matched by model
Product
Aircraft · Small airplane
Amendment
39-6807

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

90-25-17 SOCATA GROUPE AEROSPATIALE: Amendment 39-6807. Docket No. 90-CE-45-AD.

Applicability: Models TB9, TB10, TB20, and TB21 airplanes (all serial numbers), certificated in any category.

Compliance: Required within the next 25 hours time-in-service after the effective date of this AD, unless already accomplished.

To prevent possible uncontrolled release of flammable fluids into the engine compartment and engine malfunction because of loss of oil, accomplish the following:

(a) Visually inspect the mounting bases of the oil cooler inlet and outlet elbows and the sponsons located near the outlet fittings for cracks or distortions.

(1) If no cracks or distortions are found, return the airplane to service.

(2) If cracks or distortions are found, prior to further flight remove the damaged cooler and install a new engine oil cooler as specified below in accordance with SOCATA Groupe AEROSPATIALE TB Aircraft Mandatory Service Bulletin No. 50/1, undated:Model Oil Cooler Part Number TB9-TB10 Z00.12258.64 TB20 Z00.12258.513 TB21 Z00.12258.518

(b) Airplanes may be flown in accordance with FAR 21.197 and 21.199 to a location where the AD can be accomplished.

(c) An alternate method of compliance or adjustment to the compliance time that provides an equivalent level of safety may be approved by the Manager, Brussels Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Office, c/o American Embassy, 15 Rue de la Loi, B-1040, Brussels, Belgium.

NOTE 1: The request should be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Brussels Aircraft Certification Staff.

NOTE 2: All persons affected by this directive may obtain copies of the document referred to herein upon request to SOCATA Groupe AEROSPATIALE, Socata Product Support, Aeroport Tarbes-Ossun-Lourdes, B P 930, 65009 Tarbes Cedex, France; Telephone 62.41.74.26; Facsimile62.41.74.32; or the Product Support Manager, U.S.; AEROSPATIALE, 2701 Forum Drive, Grand Prairie, Texas 75053; Telephone (214) 641-3614; Facsimile (214) 641-3527; or may examine these documents at the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106.

This amendment (39-6807, AD 90-25-17) becomes effective on January 3, 1991.

Affected TCDS · 1

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

Registered aircraft · 304

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
  • Socata303 aircraft
  • Socata Group Aerospatiale1 aircraft
By year built
19792005
Registered aircraft by year built: 159 aircraft
19791
19832
198411
198511
198614
19875
19881
198913
199010
19918
19921
19931
19946
19954
19963
19972
199810
199911
200014
200113
20028
20038
20052

145 with no year recorded

By model

Aircraft

See all 304 aircraft