AD 87-15-06

Airworthiness directive · Tail Boom Assembly · Bell Helicopter Textron, A Division of Textron Canada 222B and 222U

Effective
August 7, 1987
Models
222B, 222U
Data sheet
TCDSH9SW
Registered aircraft
5 matched by model
Product
Aircraft · Rotorcraft
Amendment
39-5644

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

87-15-06 BELL HELICOPTER TEXTRON, INC. (BHTI): Amendment 39-5644. Applies to BHTI Model 222B and 222U helicopters that have tail boom assembly, P/N 222-035- 150-103 or -107, installed.

To prevent failure of the tailboom, accomplish the following:

(a) Within the next 25 hours time in service and thereafter at intervals not to exceed 25 hours time in service, inspect the tailboom in accordance with Part I of BHTI Alert Service Bulletin Number 222-85-28 for the Model 222B and Number 222U-85-3 for the Model 222U.

(b) If any crack is identified during the inspection required in paragraph (a) above, Part II (Repair) or Part III (Modification) of Alert Service Bulletin Number 222-85-28 for the Model 222B or Number 222U-85-3 for the Model 222U must be accomplished before further flight.

(c) Upon completion of Part II (Repair) or Part III (Modification) of Alert Service Bulletin Number 222-85-28 for the Model 222B or Number 222U-85-3 for the Model 222U, the inspectionsrequired by paragraph (a) of this AD are no longer necessary.

(d) This AD does not apply if Part II (Repair) or Part III (Modification) of Alert Service Bulletin Number 222-85-28 for the Model 222B or 222U-85-3 for the Model 222U has been previously accomplished.

(e) Any alternate method of compliance with this AD which provides an equivalent level of safety must be approved by the Manager, Helicopter Certification Branch, Federal Aviation Administration, 4400 Blue Mound Road, Fort Worth, Texas 76101.

(f) In accordance with Sections 21.197 and 21.199, flight is permitted to a base where the inspection required by this AD may be accomplished.

The procedure shall be done in accordance with Bell Helicopter Textron, Inc., Alert Service Bulletin No. 222-85-28 or 222U-85-3, both dated March 21, 1985.

This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a)(1). Copies may be obtained from Bell HelicopterTextron, Inc., P.O. Box 482, Fort Worth, Texas 76101. Copies may be inspected at the Office of the Regional Counsel, FAA, Southwest Region, 4400 Blue Mound Road, Fort Worth, Texas, or at the Office of the Federal Register, 1100 L Street, N.W., Room 8401, Washington, D.C.

This amendment, 39-5644, becomes effective August 7, 1987.

Affected TCDS · 1

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

Registered aircraft · 5

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
  • Bell5 aircraft
By year built
19841987
Registered aircraft by year built: 3 aircraft
19842
19871

2 with no year recorded

By model

Aircraft