82-15-01 R1: Main Transmission
FAA order 82-15-01 R1 is an airworthiness directive in force since October 4, 1982. The FAA's subject line: Main Transmission. It names Hughes 269 300 series helicopters, Schweizer 269 300 series helicopters: about 419 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
- Schweizer Aircraft Corporation
- Models
- 269A, 269A-1, 269B, 269C
- On this site
- Hughes 269 300 series helicopters 207 registered
Schweizer 269 300 series helicopters 212 registered
Dates and paperwork
- In force since
- October 4, 1982
- 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 (2,110 characters)
82-15-01 R1 HUGHES HELICOPTERS: Amendment 39-4414 as amended by Amendment 39-4463. Applies to Model 269A (all S/N's), TH-55A (all S/N's converted to civil use), 269A-1 (all S/N's), 269B (all S/N's), and 269C (S/N's 0001 through 1074) helicopters equipped with main transmission assemblies P/N 269A5175-7, -9, -11, -13, -15, and -17, except those transmissions with the letter "W" on the transmission nameplate below and adjacent to the transmission serial number. Applies to helicopters certificated in all categories.
Compliance is required as indicated unless already accomplished.
To prevent failure of the main transmission, accomplish the following:
(a) Within 50 hours' additional time in service after the effective date of this AD, disassemble the transmission and inspect the ring gear/carrier interface and attachment bolts for possible fretting or cracking, and rework in accordance with Service Information Notice N-181, paragraphs a. through j., or later FAA approvedequivalent. All parts that cannot be reworked within the criteria of Service Information Notice N-181 are considered unairworthy and must be replaced with like serviceable parts.
NOTE: Those portions of Service Information Notice N-181 which address disposition of parts which exceed the prescribed inspection and rework criteria are not applicable.
(b) Reassemble the transmission in accordance with Service Information Notice N- 181, paragraphs k. through o., or FAA approved equivalent.
(c) Special flight permits may be issued in accordance with Sections 21.197 and 21.199 of the Federal Aviation Regulations to operate aircraft to a base for the accomplishment of inspections or modifications required by this AD.
(d) Alternative inspections, modifications, or other actions which provide an equivalent level of safety may be used when approved by the Chief, Aircraft Certification Field Office, FAA Northwest Mountain Region, 15000 Aviation Boulevard, Room 5W26, Hawthorne, California.
Amendment 39-4414 became effective July 12, 1982.
This Amendment 39-4463 becomes effective October 4, 1982.
Related safety bulletins advice on the same designs, not orders
2009-07-28SW-09-44 · Cabin door
2005-12-15NE-06-03R1 ·
2005-10-18NE-06-03 ·
2004-10-21NE-05-05 ·
2003-11-07SW-04-13 ·
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 6, 2026. Connections as data: /graph/directive/82-15-01 R1.json · aircraft systems.
