86-24-01: T/R Assembly
FAA order 86-24-01 is an airworthiness directive in force since December 15, 1986. The FAA's subject line: T/R Assembly. It names Bell 206 JetRanger and LongRanger: about 1,453 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
- Bell Helicopter Textron Canada Limited
- Models
- 206A, 206B, 206L
- On this site
- Bell 206 JetRanger and LongRanger 1,453 registered
Dates and paperwork
- In force since
- December 15, 1986
- Docket
- Unknown
- Status
- Current
- The FAA's document
- Read the order on the FAA's site
The order itself the regulatory text, as published
Show the full text (1,219 characters)
86-24-01 BELL HELICOPTER TEXTRON, INC.: Amendment 39-5468. Applies to Model 206A, 206B, and 206L helicopters certificated in any category equipped with T/R yoke Part Number (P/N) 206-011-819-101 in combination with T/R crosshead P/N 206-010-741-001 or -003.
Compliance is required as indicated unless already accomplished.
To prevent failure of the T/R pitch links, accomplish the following:
(a) Within the next 25 hours' time in service, inspect T/R assembly and determine if T/R yoke P/N 206-011-819-101 is installed in combination with T/R crosshead P/N 206-010-741- 001 or -003. If this T/R yoke and crosshead combination is installed, either:
(1) Remove T/R yoke P/N 206-011-819-101 and replace it with T/R yoke P/N 206-011-811-009; or
(2) Remove T/R crosshead P/N 206-010-741-001 or -003 and replace it with T/R crosshead P/N 206-011-855-001 or 206-011-857-001.
(b) Alternative inspections, modification, or other actions which provide an equivalent level of safety may be used when approved by the Manager, Helicopter Certification Branch, Southwest Region, Federal Aviation Administration, P.O. Box 1689, Fort Worth, Texas 76101.
This amendment becomes effective December 15, 1986.
Related safety bulletins advice on the same designs, not orders
2019-12-05SW-19-18 · Fuselage Cracks
2019-04-04SW-19-05 · Tail Rotor Drive System, Spline Damage
2017-11-02SW-18-02 · Loss of Hardware Tail Rotor Drive Shaft Couplings
2015-08-13SW-15-20 · Air Conditioning System Wiring
2012-10-03SW-12-45 · Garmin Model 400W/500W Series GPS-WAAS Navigation System
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/86-24-01.json · aircraft systems.
