AD 90-01-08

Active

Driveshaft Coupling

Key Information
90-01-08
Active
February 05, 1990
Not specified
89-ASW-10
39-6456
Applicability
["Aircraft"]
["Rotorcraft"]
MD Helicopters, Inc.
369 369A 369D 369E 369F 369FF 369H 369HE 369HM 369HS
Regulatory Text

90-01-08 MCDONNELL DOUGLAS HELICOPTER COMPANY (MDHC): Amendment 39-6456. Docket No. 89-ASW-10.

Applicability: Model 369 series helicopters (including Models YOH-6A and OH-6A) certificated in any category.

Compliance: Required as indicated, unless already accomplished.

To prevent possible failure of the engine-to-transmission driveshaft coupling, which could result in loss of control of the helicopter, accomplish the following:

(a) Within the next 25 hours' time in service or within 120 days after the effective date of the AD, whichever occurs first, inspect the couplings, MDHC Part Number (P/N) 369H5660, to determine serial numbers.

(b) Replace any couplings, P/N 369H5660, which have serial numbers in the range from 5200 through 5309, with airworthy parts.

(c) Record compliance with paragraph (a) of this AD in the AD compliance record and in the maintenance record of the helicopter log book. This record must include the serial numbers of any deficient couplings found during compliance with this AD.

NOTE: MDHC Service Information Notices HN-216, DN-157, EN-47, FN-35, dated April 5, 1989, pertain to this subject.

(d) In accordance with FAR Sections 21.197 and 21.199, flight is permitted to a base where the requirements of this AD may be accomplished.

(e) An alternate method of compliance or adjustment of the compliance time which provides an equivalent level of safety, may be used if approved by the Manager, Los Angeles Aircraft Certification Office, ANM-100L, FAA, 3229 East Spring Street, Long Beach, California 90806-2425.

NOTE: Unairworthy couplings removed from service and in spares inventory should be marked unairworthy. Unairworthy couplings should be purged from spares inventory in accordance with MDHC SIN HN-216, DN-157, EN-47, FN-35, dated April 5, 1989.

This amendment (39-6456, AD 90-01-08) becomes effective on February 5, 1990.

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References
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FAA Documents