AD 80-03-06

final rule

GENERAL ELECTRIC Model CF6-6 Series Engines

AD Number
80-03-06
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine General Electric Company CF6-6D GENERAL ELECTRIC Model CF6-6 Series Engines
engine General Electric Company CF6-6D1 GENERAL ELECTRIC Model CF6-6 Series Engines
engine General Electric Company CF6-6D1A GENERAL ELECTRIC Model CF6-6 Series Engines
engine General Electric Company CF6-6K GENERAL ELECTRIC Model CF6-6 Series Engines
engine General Electric Company CF6-6K2 GENERAL ELECTRIC Model CF6-6 Series Engines

Unsafe Condition

Stage 2 HPT disks may fail due to fatigue.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Remove Stage 2 HPT disks from service based on their cycle counts. Disks with over 8400 cycles at AD effective date must be removed within 100 cycles. Disks with under 8400 cycles must be removed before reaching 8500 cycles. Specific disks (P/N 9137M15P02, serial numbers MP036073, MP030786, MP030797, MP035005, RPO24722) must be removed before 8800 cycles. Additional cycles may be approved individually by FAA.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Effective February 8, 1980

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

General Electric CF6-6 series engines with Stage 2 HPT disks, Part Numbers 9083M48P01, 9084M52P02, 9084M52P05, 9137M15P01, and 9137M15P02

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Stage 2 HPT Disks

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_80-03-06.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
80-03-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
GENERAL ELECTRIC Model CF6-6 Series Engines
Subject:
Stage 2 HPT Disks
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/08/1980
Make:
General Electric Company
Model:
CF6-6D | CF6-6D1 | CF6-6D1A | CF6-6K | CF6-6K2
Product Type:
Engine
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 80-03-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3683

AD NUMBER:   80-03-06

SUBJECT HEADING:   GENERAL ELECTRIC Model CF6-6 Series Engines

ACTION:  

SUMMARY:  

DATES:   Effective February 8, 1980.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
80-03-06 GENERAL ELECTRIC: Amendment 39-3683. Applies to General Electric CF6-6 series engines, Stage 2 HPT disks, Part Numbers 9083M48P01, 9084M52P02, 9084M52P05, 9137M15P01, and 9137M15P02. Compliance is required as indicated. To preclude disk failure due to fatigue, these disks are to be removed from service as follows:

(a) All disks, except those noted in (c) below, which have more than 8400 cycles on the effective date of this AD are to be removed from service within 100 cycles.

(b) All disks, except those noted in (c) below, which have less than 8400 cycles are to be removed before they accrue 8500 cycles.

(c) Those disks, P/N 9137M15P02, with Serial Numbers MP036073, MP030786, MP030797, MP035005, and RPO24722 because of their refurbishment schedule shall be removed from service before they accrue 8800 cycles.

(d) Other disks than those identified in (c) above may be allowed additional cycles on an individual basis when approved by the Chief, Engineering and Manufacturing Branch, FAA, Great Lakes Region.

CF6-6 Service Bulletin 72-761 dated November 28, 1979 also applies to this subject.

This amendment becomes effective on February 8, 1980.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_80-03-06.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
80-03-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
GENERAL ELECTRIC Model CF6-6 Series Engines
Subject:
Stage 2 HPT Disks
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/08/1980
Make:
General Electric Company
Model:
CF6-6D | CF6-6D1 | CF6-6D1A | CF6-6K | CF6-6K2
Product Type:
Engine
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 80-03-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3683

AD NUMBER:   80-03-06

SUBJECT HEADING:   GENERAL ELECTRIC Model CF6-6 Series Engines

ACTION:  

SUMMARY:  

DATES:   Effective February 8, 1980.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
80-03-06 GENERAL ELECTRIC: Amendment 39-3683. Applies to General Electric CF6-6 series engines, Stage 2 HPT disks, Part Numbers 9083M48P01, 9084M52P02, 9084M52P05, 9137M15P01, and 9137M15P02. Compliance is required as indicated. To preclude disk failure due to fatigue, these disks are to be removed from service as follows:

(a) All disks, except those noted in (c) below, which have more than 8400 cycles on the effective date of this AD are to be removed from service within 100 cycles.

(b) All disks, except those noted in (c) below, which have less than 8400 cycles are to be removed before they accrue 8500 cycles.

(c) Those disks, P/N 9137M15P02, with Serial Numbers MP036073, MP030786, MP030797, MP035005, and RPO24722 because of their refurbishment schedule shall be removed from service before they accrue 8800 cycles.

(d) Other disks than those identified in (c) above may be allowed additional cycles on an individual basis when approved by the Chief, Engineering and Manufacturing Branch, FAA, Great Lakes Region.

CF6-6 Service Bulletin 72-761 dated November 28, 1979 also applies to this subject.

This amendment becomes effective on February 8, 1980.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.