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2004-13-26: Main rotor blade (blade) grips

FAA order 2004-13-26 is an airworthiness directive in force since July 22, 2004. The FAA's subject line: Main rotor blade (blade) grips. It names Kaman Aerospace Corp K-1200: about 17 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: rotorcraft systems.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Kaman Aerospace Corporation
Models
K-1200
On this site
Kaman Aerospace Corp K-1200 17 registered

Dates and paperwork

In force since
July 22, 2004
Published
July 7, 2004 (signed June 24, 2004)
Docket
2003-SW-46-AD
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

This amendment adopts a new airworthiness directive (AD) for Kaman Aerospace Corporation (Kaman) Model K-1200 helicopters. This action requires certain initial and repetitive visual inspections of the main rotor blade (blade) grips for a crack. If a crack is found, this AD requires replacing the blade grip before further flight. This amendment is prompted by an accident involving the loss of all blades because of a crack in a blade grip on the upper surface around the bolthole. The actions specified in this AD are intended to prevent failure of a blade grip, loss of a blade, and subsequent loss of control of the helicopter.

The order itself the regulatory text, as published

Show the full text (2,647 characters)
2004-13-26 Kaman Aerospace Corporation: Amendment 39-13708. Docket No. 2003-SW-46-AD. Applicability: Model K-1200 helicopters, certificated in any category. Compliance: Required as indicated. To prevent failure of a blade grip, blade contact with the opposite rotor mast, blade failure, and loss of control of the helicopter, accomplish the following: (a) Before further flight, unless accomplished previously, remove the paint topcoat and primer from each blade grip; and using a light and 10x power or higher magnifying glass, visually inspect each blade grip in accordance with the Accomplishment Instructions, paragraph 1. and 2.a., of Kaman Aerospace Corporation Service Bulletin No. 109, dated October 31, 2003 (SB). Note: Do not damage or remove the sealant around the blade grip bolt heads and nuts. (1) If a crack is detected, remove the grip and replace it with an airworthy grip. (2) If no crack is detected, cover the exposed area with corrosion preventative compound. (b) Before the first flight of each day, remove corrosion preventative compound from each blade grip using acetone. Using a light and 10x power or higher magnifying glass, visually inspect each blade grip for a crack in the area depicted in Figure 1 of the SB. (1) If a crack is detected, remove the grip and replace it with an airworthy grip. (2) If no crack is detected, cover the exposed area with corrosive preventative compound. (c) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19. Contact the Safety Management Group, Rotorcraft Directorate, FAA, for information about previously approved alternative methods of compliance. (d) Special flight permits will not be issued. (e) The inspections shall be done in accordance with Kaman Aerospace Corporation Service Bulletin No. 109, dated October 31, 2003. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Kaman Aerospace Corporation, P.O. Box 2, Old Windsor Rd., Bloomfield, CT 06002-0002, telephone (888) 626-KMAX (5629), fax (880) 243-7047. Copies may be inspected at the FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html . (f) This amendment becomes effective on July 22, 2004.

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 October 5, 2026. Connections as data: /graph/directive/2004-13-26.json · aircraft systems.