AD 74-13-09

final rule

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

AD Number
74-13-09
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 Honeywell International Inc. TFE731-2 AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TFE731-2-1C, and -2-2B Engines

Unsafe Condition

Improper configuration of the fuel pump assembly.

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

Required Actions

Inspect the fuel pump assembly per AiResearch Service Bulletin TFE731-73-3004 or later FAA-approved revisions. Equivalent procedures may be approved by the FAA upon submission of substantiation data. Aircraft may be flown to a base for required maintenance under FAR 21.197 and 21.199.

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

Compliance Time

within the next 50 hours time in service after the effective date of this AD, unless already accomplished, and prior to installing replacement fuel pump assemblies identified as P/N 3070851-7 and -8 or later dash numbers

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

Affected Aircraft

AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TFE731-2-1C and -2-2B engines installed in, but not limited to AMD Falcon 10 aircraft

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

Federal Register Abstract

Fuel Pump Assemblies

Applicability Source Text

Show captured applicability text from the source AD
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AD Number:
74-13-09
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TFE731-2-1C, and -2-2B Engines
Subject:
Fuel Pump Assemblies
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/31/1974
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Superseded AD: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Superseded By: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: 74-13-09
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1903

AD NUMBER:   74-13-09

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

ACTION:  

SUMMARY:  

DATES:   Effective July 31, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
74-13-09 AIRESEARCH MANUFACTURING COMPANY OF ARIZONA: Amendment 39-1882 is further amended by Amendment 39-1903. Applies to Model TFE731-2-1C, and -2-2B engines installed in, but not limited to AMD Falcon 10 aircraft, certificated in all categories.

Compliance required within the next 50 hours time in service after the effective date of this AD, unless already accomplished, and prior to installing replacement fuel pump assemblies.

To detect the improper configuration of the fuel pump, accomplish the following:

(a) Inspect the fuel pump assembly in accordance with the instructions contained in AiResearch Service Bulletin TFE731-73-3004, dated June 14, 1974, or later FAA-approved revisions.

(b) The inspection prescribed in paragraph (a), above, need not be accomplished prior to the installation of replacement fuel pumps identified as P/N 3070851-7 and -8, or later dash number designations.

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

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

Amendment 39-1882 became effective June 28, 1974.
This Amendment, 39-1903 becomes effective July 31, 1974.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_74-13-09.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
74-13-09
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TFE731-2-1C, and -2-2B Engines
Subject:
Fuel Pump Assemblies
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/31/1974
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: 74-13-09
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1903

AD NUMBER:   74-13-09

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

ACTION:  

SUMMARY:  

DATES:   Effective July 31, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
74-13-09 AIRESEARCH MANUFACTURING COMPANY OF ARIZONA: Amendment 39-1882 is further amended by Amendment 39-1903. Applies to Model TFE731-2-1C, and -2-2B engines installed in, but not limited to AMD Falcon 10 aircraft, certificated in all categories.

Compliance required within the next 50 hours time in service after the effective date of this AD, unless already accomplished, and prior to installing replacement fuel pump assemblies.

To detect the improper configuration of the fuel pump, accomplish the following:

(a) Inspect the fuel pump assembly in accordance with the instructions contained in AiResearch Service Bulletin TFE731-73-3004, dated June 14, 1974, or later FAA-approved revisions.

(b) The inspection prescribed in paragraph (a), above, need not be accomplished prior to the installation of replacement fuel pumps identified as P/N 3070851-7 and -8, or later dash number designations.

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

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

Amendment 39-1882 became effective June 28, 1974.
This Amendment, 39-1903 becomes effective July 31, 1974.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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