AD 72-16-03

Airworthiness directive · Turbine Discs · General Electric CF6-6D and CF6-6D1

Effective
August 8, 1972
Models
CF6-6D, CF6-6D1
Data sheet
TCDSE23EA
Registered aircraft
11 matched by model
Product
Engine
Amendment
39-1495

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

On this page

The airworthiness directive

72-16-03 GENERAL ELECTRIC: Amendment 39-1495. Applies to Models CF6-6D and CF6-6D1 turbofan engines.

Compliance required as indicated.

To prevent cracking and possible failure of stage 2 high pressure turbine discs, unless already accomplished, remove from service stage 2 high pressure turbine discs Part No. 9687M40P03, P04, P05, or P06 prior to reaching a life limit of 2100 cycles.

For the purposes of this AD, the definition of cycles is that appearing in the CF6 Shop Manual GEK 9266 Section 72-00-00 Inspection page 301.

(General Electric Alert Service Bulletin CF6 72-320 pertains to this subject.)

This amendment is effective August 8, 1972.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 11

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Boeing6 aircraft
  • Mcdonnell Douglas3 aircraft
  • Airbus Industrie2 aircraft
By year built
19711999
Registered aircraft by year built: 11 aircraft
19711
19721
19931
19952
19984
19992

By model

Aircraft