AD 74-25-01

final rule

GENERAL ELECTRIC COMPANY Model CT58-140 Engine

AD Number
74-25-01
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

Applicability

TypeManufacturerModelDetails
engine General Electric Company CT58-140-1 GENERAL ELECTRIC COMPANY Model CT58-140 Engine
engine General Electric Company CT58-140-2 GENERAL ELECTRIC COMPANY Model CT58-140 Engine

Unsafe Condition

Failure of the fuel filter to flow divider hose P/N 3007T22P02 (VIN SR 9844CC6-00910) due to specific serial numbers and dates (November 72, December 72, December 73 with specified serial numbers).

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

Required Actions

Remove hoses with specified serial numbers and dates, replace with new hoses P/N 3007T22P02 (VIN SR 9844CC6-00910) or P/N 3007T22P02 (VIN 95387).

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

Compliance Time

within the next fifteen (15) days time in service after the effective date of this AD

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

Affected Aircraft

General Electric Company CT58-140 engine fuel system hose P/N 3007T22P02 (VIN SR 9844CC6-00910) with serial numbers and dates specified in the AD.

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

Federal Register Abstract

Fuel System Hose

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_74-25-01.html
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AD Number:
74-25-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
GENERAL ELECTRIC COMPANY Model CT58-140 Engine
Subject:
Fuel System Hose
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/10/1974
Make:
General Electric Company
Model:
CT58-140-1 | CT58-140-2
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Superseded AD: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Superseded By: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: 74-25-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2009

AD NUMBER:   74-25-01

SUBJECT HEADING:   GENERAL ELECTRIC COMPANY Model CT58-140 Engine

ACTION:  

SUMMARY:  

DATES:   Effective December 10, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   74-25-01 GENERAL ELECTRIC COMPANY: Amendment 39-2009. Applies to General Electric Company CT58-140 engine fuel system hose, P/N 3007T22P02 (VIN SR 9844CC6-00910).

Compliance required unless already accomplished, within the next fifteen (15) days time in service after the effective date of this AD.

To prevent possible failure of the fuel filter to flow divider hose, remove hose P/N 3007T22P02 (VIN SR 9844CC6-00910) with identification bands bearing date and/or serial number as follows:

November 72 or December 72 (3 parts total), and hoses dated December 73 having Serial Numbers 1507, 1508, 1509, 1510, 1512, 1514, 1516, 1517, 1519, 1520, 1522, and 1525 (12 parts total).

Replace hoses removed with new hose, P/N 3007T22P02 (VIN SR 9844CC6-00910) or P/N 3007T22P02 (VIN 95387), which are hoses other than those of serial nubmer and/or date identified for removal above.

Upon request of the operator, an FAA Maintenance Inspector, subject to prior approval of the Chief, Engineering and Manufacturing Branch, FAA, New England Region, may adjust the inspection interval specified in this AD to permit compliance at an established inspection period of the operator if the request contains substantiating data to justify the increase for that operator.

NOTE: Replacement procedure reference material is contained in General Electric Alert Service Bulletin (CT58) A73-68.

This amendment becomes effective December 10, 1974.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_74-25-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
74-25-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
GENERAL ELECTRIC COMPANY Model CT58-140 Engine
Subject:
Fuel System Hose
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/10/1974
Make:
General Electric Company
Model:
CT58-140-1 | CT58-140-2
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: 74-25-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2009

AD NUMBER:   74-25-01

SUBJECT HEADING:   GENERAL ELECTRIC COMPANY Model CT58-140 Engine

ACTION:  

SUMMARY:  

DATES:   Effective December 10, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   74-25-01 GENERAL ELECTRIC COMPANY: Amendment 39-2009. Applies to General Electric Company CT58-140 engine fuel system hose, P/N 3007T22P02 (VIN SR 9844CC6-00910).

Compliance required unless already accomplished, within the next fifteen (15) days time in service after the effective date of this AD.

To prevent possible failure of the fuel filter to flow divider hose, remove hose P/N 3007T22P02 (VIN SR 9844CC6-00910) with identification bands bearing date and/or serial number as follows:

November 72 or December 72 (3 parts total), and hoses dated December 73 having Serial Numbers 1507, 1508, 1509, 1510, 1512, 1514, 1516, 1517, 1519, 1520, 1522, and 1525 (12 parts total).

Replace hoses removed with new hose, P/N 3007T22P02 (VIN SR 9844CC6-00910) or P/N 3007T22P02 (VIN 95387), which are hoses other than those of serial nubmer and/or date identified for removal above.

Upon request of the operator, an FAA Maintenance Inspector, subject to prior approval of the Chief, Engineering and Manufacturing Branch, FAA, New England Region, may adjust the inspection interval specified in this AD to permit compliance at an established inspection period of the operator if the request contains substantiating data to justify the increase for that operator.

NOTE: Replacement procedure reference material is contained in General Electric Alert Service Bulletin (CT58) A73-68.

This amendment becomes effective December 10, 1974.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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