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2009-12-01: Main rotor blade box beam clip (clip)

FAA order 2009-12-01 is an airworthiness directive in force since June 29, 2009. The FAA's subject line: Main rotor blade box beam clip (clip). It names Bell-Carson 47, Bell 47: about 482 aircraft on the U.S. register today across them, 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
Scotts-Bell 47 Inc
Models
47, 47B, 47B3, 47D, 47D1, 47E, 47G, 47G-2, 47G-2A, 47G-2A-1, 47G-3, 47G-3B, 47G-3B-1, 47G-3B-2, 47G-3B-2A, 47G-4, 47G-4A, 47G-5, 47G-5A, 47H-1, 47J, 47J-2, 47J-2A, 47K
On this site
Bell-Carson 47 5 registered
Bell 47 477 registered

Dates and paperwork

In force since
June 29, 2009
Published
June 12, 2009 (signed May 19, 2009)
Docket
FAA-2009-0484
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 the specified Bell Helicopter Textron, Inc. (Bell) helicopters. This action requires visually inspecting each main rotor blade box beam clip (clip) for correct installation. This amendment is prompted by a report of a main rotor blade with an incorrectly installed clip. The actions specified in this AD are intended to prevent a main rotor blade spar crack as a result of an incorrectly installed clip, loss of a main rotor blade, and subsequent loss of control of the helicopter.

The order itself the regulatory text, as published

Show the full text (3,143 characters)
2009-12-01 Bell Helicopter Textron, Inc.: Amendment 39-15924. Docket No. FAA-2009-15924; Directorate Identifier 2008-SW-44-AD. \n\n\tApplicability: Model 47, 47B, 47B3, 47D, 47D1, 47E, 47G, 47G-2, 47G-2A, 47G-2A-1, 47G-3, 47G-3B, 47G-3B-1, 47G-3B-2, 47G-3B-2A, 47G- 4, 47G-4A, 47G-5, 47G-5A, 47H-1, 47J, 47J-2, 47J-2A, and 47K helicopters with a main rotor blade, installed, with a part number (P/N) and serial number (S/N), listed as follows, certificated in any category: \n\n\nMain rotor blade, P/N\nWith a S/N of\n047-110-250-021\nA-303, A-304, A-312, or A-316\n047-110-250-023\nA-298, A-301, or A-305\n\n\n\tCompliance: Required as indicated, unless done previously. \n\tTo prevent a main rotor blade spar crack as a result of an incorrectly installed main rotor blade box beam clip (clip), loss of a main rotor blade, and subsequent loss of control of the helicopter, do the following: \n\t(a) Within 10 hours time-in-service (TIS), visually inspect the entire length of each upper and lower clip of each main rotor blade from the main rotor blade tip to the root by following Part II of the Accomplishment Instructions, paragraphs 1. through 8., of Bell Helicopter Textron, Inc. Alert Service Bulletin No. 47-08-25, dated May 26, 2008 (ASB) and referring to the depictions in Figures 1 and 2 of the ASB and Figure 1 of this AD for correct installation. \n\n\tNote: Figure 3 of the ASB depicts a clip installed incorrectly. \n\n\n\n\n\t(b) Before further flight, if you find a main rotor blade with an incorrectly installed clip, replace that unairworthy main rotor blade with an airworthy main rotor blade that has a clip that is installed correctly. \n\t(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 Manager, Rotorcraft Certification Office, FAA, ATTN: Michael Kohner, Aviation Safety Engineer, Rotorcraft Directorate, Fort Worth, Texas 76193-0170, telephone (817) 222-5170, fax (817) 222-5783.(d) Special flight permits may be issued under 14 CFR 21.197 and 21.199 to operate the helicopter to a location where the requirements of this AD can be done provided the onetime ferry flight does not exceed 5 hours TIS. \n\t(e) The visual inspection shall be done by following the specified portions of Bell Helicopter Textron, Inc., Alert Service Bulletin No. 47-08-25, dated May 26, 2008. The Director of the Federal Register approved this incorporation by reference in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Bell Helicopter Textron, Inc., P.O. Box 482, Fort Worth, TX 76101, telephone (817) 280-3391, fax (817) 280-6466, or at http://www.bellcustomer.com/files/. 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. \n\t(f) This amendment becomes effective on June 29, 2009.

Related safety bulletins advice on the same designs, not orders

2001-02-09SW-01-13 ·

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/2009-12-01.json · aircraft systems.