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97-12-02: Link Assembly

FAA order 97-12-02 is an airworthiness directive in force since December 2, 1997. The FAA's subject line: Link Assembly. It names Md Helicopters Inc MD 900: about 11 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: other and general.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
MD Helicopters, Inc.
Models
MD900
On this site
Md Helicopters Inc MD 900 11 registered

Dates and paperwork

In force since
December 2, 1997
Published
November 17, 1997
Docket
97-SW-17-AD
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

This amendment supersedes an existing priority letter airworthiness directive (AD), applicable to McDonnell Douglas Helicopter Systems (MDHS) Model MD900 helicopters, which prohibits flight or ground operations of helicopters with a certain adjustable collective drive link assembly (link assembly) installed. This amendment requires installation of a redesigned airworthy link assembly after which further operations are permitted. This amendment is prompted by recent incidents in which the link assembly failed during flight. The actions specified by this AD are intended to prevent failure of the link assembly, which could result in loss of control of the helicopter.

The order itself the regulatory text, as published

Show the full text (2,217 characters)
97-12-02 MCDONNELL DOUGLAS HELICOPTER SYSTEMS: Amendment 39-10206. Docket No. 97-SW-17-AD. Applicability: Model MD900 helicopters, with adjustable collective drive link assembly (link assembly), part number (P/N) 900C2010233-103 or -105, installed, certificated in any category. NOTE 1: This AD applies to each helicopter identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For helicopters that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must use the authority provided in paragraph (b) to request approval from the FAA. This approval may address either no action, if the current configuration eliminates the unsafe condition, or different actions necessary to address the unsafe condition described in this AD. Such a request should include an assessment of the effect of thechanged configuration on the unsafe condition addressed by this AD. In no case does the presence of any modification, alteration, or repair remove any helicopter from the applicability of this AD. Compliance: Required as indicated, unless accomplished previously. To prevent failure of the link assembly, which could result in loss of control of the helicopter, accomplish the following: (a) Before further flight, remove the link assembly, P/N 900C2010233-103 or -105, and replace with link assembly, P/N 900C2010233-107. (b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Los Angeles Aircraft Certification Office. Operators shall submit their requests through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Los Angeles Aircraft Certification Office. NOTE 2: Information concerning the existence of approvedalternative methods of compliance with this AD, if any, may be obtained from the Los Angeles Aircraft Certification Office. (c) Special flight permits will not be issued. (d) This amendment becomes effective on December 2, 1997.

Related safety bulletins advice on the same designs, not orders

2007-11-14SW-08-05 · MD900 Main Rotor Blade Retention Bolt Check

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 6, 2026. Connections as data: /graph/directive/97-12-02.json · aircraft systems.