80-23-02: Turbine Power Conversions
FAA order 80-23-02 is an airworthiness directive in force since November 20, 1980. The FAA's subject line: Turbine Power Conversions. It names Bell-Carson 47, Bell 47, Hiller UH-12: about 700 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: engine.
What it applies to as the FAA lists it
- Kind of product
- Appliance
- Makes
- Hiller Aviation; Scotts-Bell 47 Inc; Siam Hiller Holdings, Inc.; Soloy Conversions, Ltd.
- Models
- UH-12D, 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, UH-12E, Turbine Power Conversions
- On this site
- Bell-Carson 47 5 registered
Bell 47 478 registered
Hiller UH-12 217 registered
Dates and paperwork
- In force since
- November 20, 1980
- 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 (1,688 characters)
80-23-02 SOLOY CONVERSIONS, LTD: Amendment 39-3971. Applies to Hiller UH-12D, UH-12E (including 4 place) and Bell 47G series helicopters certificated in all categories which have been converted to turbine power under Soloy Conversions, Ltd. Supplemental Type Certificates SH177WE, SH178WE and SH657NW respectively.
Compliance required within 25 hours time-in-service or 30 days, whichever occurs first after the effective date of this AD.
To prevent failure of Soloy transmission oil lubrication jets which may result in complete transmission failure and possible loss of the aircraft:
1. Inspect all Soloy transmission oil lubrication jets in accordance with the following Soloy Service Bulletins:
a. Soloy/Hiller UH-12D and UH-12E (including 4 place): 14-560 dated October 20, 1980, or later FAA Approved revisions.
b. Soloy/Bell 47G series: 14-660 dated October 20, 1980, or later FAA Approved revisions.
2. Replace defective jets before further flight.
Equivalent methods of compliance may be used when approved by the Chief, Seattle Aircraft Certification Area Office, FAA Northwest Region.
The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1).
All persons affected by this directive who have not already received these documents from the manufacturer, may obtain copies upon request to Soloy Conversions, Ltd., Post Office Box 60, Chehalis, Washington 98532. These documents may also be examined at FAA Northwest Region, 9010 East Marginal Way South, Seattle, Washington 98108.
This amendment becomes effective November 20, 1980.
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 November 2, 2026. Connections as data: /graph/directive/80-23-02.json · aircraft systems.
