67-01-02: Rotor Discs
FAA order 67-01-02 is an airworthiness directive in force since August 24, 1976. The FAA's subject line: Rotor Discs. It names the General Electric CT58-140-1, General Electric CT58-140-2, General Electric CT58 series, General Electric T58 series engines: about 83 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
- Engine
- Makes
- General Electric Company
- Models
- CT58-100-1, T58-GE-5, T58-GE-1, CT58-100-2, CT58-110-1, CT58-110-2, CT58-140-1, CT58-140-2
- Engine series
- General Electric CT58-140-1 20 aircraft
General Electric CT58-140-2 33 aircraft
General Electric CT58 series 13 aircraft
General Electric T58 series 17 aircraft
Dates and paperwork
- In force since
- August 24, 1976
- Published
- August 12, 1976 (signed August 2, 1976)
- 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 (1,173 characters)
67-01-02 GENERAL ELECTRIC: Amendment 39-332 as amended by Amendment 39-536 and Amendment 39-1085 is further amended by Amendment 39-2688. Applies to Model CT58-100-1, CT58-100-2, CT58-110-1, CT58-110-2, CT58-140-1, CT58-140-2, T58-GE-1 and T58-GE-5 Engines.
Compliance required as indicated.
To ensure adequate life limit margin for first stage compressor rotor discs, remove from service G.E. P/N's 37D400218P101, 37D400218P101 CEB #148, 37D400218P102, 37D400359P101, 37D400359P102, 3920T11P01, 3920T11P02, 5013T06P01, 5001T20P01, and 5001T20P02 as follows:
(a) Discs with more than 9,700 cycles on October 15, 1970, prior to the accumulation of 200 additional cycles.
(b) Discs with 9,700 cycles or less on October 15, 1970, before 9,900 cycles.
For the purposes of this AD a cycle is considered as any engine operating sequence involving engine start, at least one acceleration to a power required for take off, and shutdown.
Amendment 39-332 became effective December 29, 1966.
Amendment 39-536 became effective January 9, 1968.
Amendment 39-1085 became effective October 15, 1970.
This amendment 39-2688 becomes effective August 24, 1976.
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/67-01-02.json · aircraft systems.