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80-17-09: Main Rotor Straps

FAA order 80-17-09 is an airworthiness directive in force since September 15, 1980. The FAA's subject line: Main Rotor Straps. It names Bell 204, Bell 205, Bell 212, Bell 214, Bell UH-1 Huey (Iroquois): about 559 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
Bell Helicopter Textron, Inc.; California Department of Forestry; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; Rotorcraft Development Corporation; San Joaquin Helicopters; International Helicopters, Inc.; US Helicopter, Inc.; Richards Heavylift Helo, Inc.
Models
204B, 205A-1, 212, 214B, 214B-1, UH-1F, UH-1B, UH-1E, UH-1F, UH-1H, UH-1L, UH-1P, UH-1B, UH-1B, UH-1A, UH-1B, UH-1E, UH-1H, UH-1L
On this site
Bell 204 7 registered
Bell 205 58 registered
Bell 212 59 registered
Bell 214 31 registered
Bell UH-1 Huey (Iroquois) 404 registered

Dates and paperwork

In force since
September 15, 1980
Docket
Unknown
Replaced by
2002-22-14
Status
Historical
The FAA's document
Read the order on the FAA's site

The order itself the regulatory text, as published

Show the full text (1,397 characters)
80-17-09 BELL: Amendment 39-3876. Applies to Models 204B, 205A-1, 212, 214B, and 214B-1 helicopters and military UH-1 series helicopters certified in all categories. Compliance required as indicated for helicopters equipped with main rotor straps, P/N 204-012-122-1, -5, or 214-010-179-1. To preclude possible separation of a main rotor blade tension-torsion strap and loss of a main rotor blade, accomplish the following: a. Within the next 100 hours' time in service after the effective date of this airworthiness directive (AD), remove and replace main rotor straps having: (1) 1,100 or more hours of total time in service on the effective date of this AD, or (2) 24 or more months elapsed calendar time in service as of the effective date of this AD, whichever comes first. b. Remove and replace main rotor straps having less than 1,100 hours' total time in service or having less than 24 months elapsed time in service on the effective date of this AD:(1) Prior to attaining 1,200 hours' total time in service, or (2) Prior to exceeding 24 months elapsed time in service, whichever comes first. c. The helicopter may be flown in accordance with FAR's 21.197 and 21.199 to a base where this AD may be accomplished. (Bell Helicopter Textron Alert Service Bulletin No. 212-80-17 pertains to this subject.) This amendment becomes effective September 15, 1980.

Related safety bulletins advice on the same designs, not orders

2019-02-19SW-18-29R1 · Rotorcraft Tail Boom, Attach Structure Failure
2018-10-01SW-18-29 · Rotorcraft Tail Boom, Attach Structure Failure
2012-07-30SW-12-38 · Emergency Push Out Window Retention
2008-08-27SW-08-42 · Emergency Float with Liferaft Kits (kits)
2007-05-02SW-07-33 · Quick connect fittings

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/80-17-09.json · aircraft systems.