AD 74-23-05

final rule

AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TFE731-2-2B and -2-1C Engines

AD Number
74-23-05
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Honeywell International Inc. TFE731-2 AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TFE731-2-2B and -2-1C Engines

Unsafe Condition

Fuel pumps (P/N 3070851-2, -4, -5, and -6) may fail due to insufficient service life limit, exceeding 25 hours total time in service.

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

Required Actions

Replace fuel pumps with less than 25 hours total time in service before exceeding 25 hours. Replace fuel pumps with more than 25 hours total time immediately. Inspect and re-identify eligible pumps per AiResearch Service Bulletin TFE731-73-3005.

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

Compliance Time

before exceeding 25 hours total time in service

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

Federal Register Abstract

Fuel Pumps

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_74-23-05.html
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AD Number:
74-23-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TFE731-2-2B and -2-1C Engines
Subject:
Fuel Pumps
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/14/1974
Make:
Honeywell International Inc.
Model:
TFE731-2
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Superseded AD: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Superseded By: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: 74-23-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2008

AD NUMBER:   74-23-05

SUBJECT HEADING:   AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TFE731-2-2B and -2-1C Engines

ACTION:  

SUMMARY:  

DATES:   Effective November 14, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
74-23-05 AIRESEARCH MANUFACTURING COMPANY OF ARIZONA: Amendment 39-2008. Applies to AiResearch Model TFE731-2-2B and -2-1C engines installed in, but not limited to, AMD Falcon DA-10 and Lear-Gates Models 35 and 36 aircraft certificated in all categories.

(A) Upon receipt of this telegram, except as authorized in (C) below, P/N 3070851-2, -4, -5, and -6 fuel pumps with less than 25 hours total time in service must be replaced before exceeding 25 hours total time in service. Fuel pumps with more than 25 hours total time in service must be replaced before further flight.

(B) The maximum service life of P/N 3070851-2, -4, -5, and -6 fuel pumps is 25 hours total time in service since new or overhaul.

(C) AiResearch Service Bulletin TFE731-73-3005, dated July 10, 1974, provides instructions for inspecting and re-identifying P/N 3070851-5 and -6 fuel pumps which have been determined to conform to the -7 and -8 configuration.

(D) P/N 3070851-7 and -8 fuel pumps are not subject to the service life limit prescribed in (A) above and may be installed in accordance with AiResearch Service Bulletin TFE731-73-3005, dated July 10, 1974, or later FAA-approved revisions.

(E) Equivalent procedures may be approved by the Chief, Aircraft Engineering Division, FAA Western Region, upon submission of adequate substantiation data.

(F) Aircraft may be flown to a base for performance of maintenance required by the AD per FAR's 21.197 and 21.199.

This supersedes telegram dated June 4, 1974 and AD 74-13-08.

This amendment becomes effective November 14, 1974, for all persons except those to whom it was made effective immediately by telegram dated June 4, 1974.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_74-23-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
74-23-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TFE731-2-2B and -2-1C Engines
Subject:
Fuel Pumps
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/14/1974
Make:
Honeywell International Inc.
Model:
TFE731-2
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: 74-23-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2008

AD NUMBER:   74-23-05

SUBJECT HEADING:   AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TFE731-2-2B and -2-1C Engines

ACTION:  

SUMMARY:  

DATES:   Effective November 14, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
74-23-05 AIRESEARCH MANUFACTURING COMPANY OF ARIZONA: Amendment 39-2008. Applies to AiResearch Model TFE731-2-2B and -2-1C engines installed in, but not limited to, AMD Falcon DA-10 and Lear-Gates Models 35 and 36 aircraft certificated in all categories.

(A) Upon receipt of this telegram, except as authorized in (C) below, P/N 3070851-2, -4, -5, and -6 fuel pumps with less than 25 hours total time in service must be replaced before exceeding 25 hours total time in service. Fuel pumps with more than 25 hours total time in service must be replaced before further flight.

(B) The maximum service life of P/N 3070851-2, -4, -5, and -6 fuel pumps is 25 hours total time in service since new or overhaul.

(C) AiResearch Service Bulletin TFE731-73-3005, dated July 10, 1974, provides instructions for inspecting and re-identifying P/N 3070851-5 and -6 fuel pumps which have been determined to conform to the -7 and -8 configuration.

(D) P/N 3070851-7 and -8 fuel pumps are not subject to the service life limit prescribed in (A) above and may be installed in accordance with AiResearch Service Bulletin TFE731-73-3005, dated July 10, 1974, or later FAA-approved revisions.

(E) Equivalent procedures may be approved by the Chief, Aircraft Engineering Division, FAA Western Region, upon submission of adequate substantiation data.

(F) Aircraft may be flown to a base for performance of maintenance required by the AD per FAR's 21.197 and 21.199.

This supersedes telegram dated June 4, 1974 and AD 74-13-08.

This amendment becomes effective November 14, 1974, for all persons except those to whom it was made effective immediately by telegram dated June 4, 1974.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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