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2010-23-24: Gear

FAA order 2010-23-24 is an airworthiness directive in force since December 22, 2010. The FAA's subject line: Gear. It names Sikorsky S-70: about 29 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
Sikorsky Aircraft Corporation
Models
S-70A, S-70C
On this site
Sikorsky S-70 29 registered

Dates and paperwork

In force since
December 22, 2010
Published
November 17, 2010 (signed November 1, 2010)
Docket
FAA-2010-0490
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 Sikorsky Model S-70A and S-70C helicopters. This AD requires an ultrasonic test (UT) inspection of the tail gearbox output bevel gear (gear) for a crack. If you find a crack, replacing the gear with an airworthy gear is required before further flight. This AD is prompted by three gear cracking incidents, one of which resulted in the tail rotor separating from the helicopter. The actions specified by this AD are intended to detect a crack in the gear to prevent a tail rotor separating, loss of tail rotor control, and subsequent loss of control of the helicopter.

The order itself the regulatory text, as published

Show the full text (2,516 characters)
2010-23-24 Sikorsky Aircraft Corp.: Amendment 39-16514; Docket No. FAA-2010-0490; Directorate Identifier 2010-SW-037-AD. Applicability: Model S-70A and S-70C helicopters with a tail gearbox output bevel gear (gear), part number 70358-06620, certificated in any category. Compliance: Required as indicated. To prevent a tail rotor separating, loss of tail rotor control, and subsequent loss of control of the helicopter, do the following: (a) Within 500 hours time-in-service (TIS), unless accomplished previously, and thereafter at intervals not to exceed 500 hours TIS, remove the tail rotor servo control and pitch beam shaft, and using a Level II Ultrasonic Testing Technician or equivalent, ultransonic inspect the gear for a crack. Ultrasonic inspect the gear by following paragraphs A.(5)a. through A(5)n. of Special Service Instructions No. 70-121A, Revision A, dated May 21, 2009. If you find a crack, before further flight, replace the gear with an airworthy gear.(b) 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, Boston Aircraft Certification Office, FAA, Attn: Michael Schwetz, Aviation Safety Engineer, Boston Aircraft Certification Office, 12 New England Executive Park, Burlington, MA 01803, telephone (781) 238-7761, fax (781) 238-7170, for information about previously approved alternative methods of compliance. (c) The Joint Aircraft System/Component (JASC) Code is 6520: Tail rotor gearbox. (d) The inspections shall be done in accordance with the specified portions of Sikorsky Special Service Instructions No. 70- 121A, Revision A, dated May 21, 2009. 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 Sikorsky Aircraft Corporation, Attn: Manager, Commercial Technical Support, mailstop s581a, 6900 Main Street, Stratford, CT, telephone (203) 383-4866, e-mail address tsslibrary@sikorsky.com, or at http:/ /www.sikorsky.com. 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. (e) This amendment becomes effective on December 22, 2010.

Related safety bulletins advice on the same designs, not orders

2006-04-04SW-06-36 ·
2004-08-04SW-04-75 ·

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 7, 2026. Connections as data: /graph/directive/2010-23-24.json · aircraft systems.