AD 81-05-02

final rule

AVIONS MARCEL DASSAULT - BREGUET AVIATION Model Falcon 10 Airplanes

AD Number
81-05-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
aircraft Dassault Aviation Falcon 10 AVIONS MARCEL DASSAULT - BREGUET AVIATION Model Falcon 10 Airplanes

Unsafe Condition

Overheating of the air conditioning system's freon compressor motor starting resistor, which could lead to a potential fire hazard.

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

Required Actions

Remove the compressor motor starting resistor and thermostat, and install a time-delay device in the starting system following Service Bulletin F10 0177 or FAA-approved revisions.

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

Compliance Time

Prior to May 1, 1981

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

Affected Aircraft

All Model Falcon 10 airplanes certificated in all categories.

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

Federal Register Abstract

Compressor Starting Circuit

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_81-05-02.html
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AD Number:
81-05-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
AVIONS MARCEL DASSAULT - BREGUET AVIATION Model Falcon 10 Airplanes
Subject:
Compressor Starting Circuit
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/02/1981
Make:
Dassault Aviation
Model:
Falcon 10
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 81-05-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4048

AD NUMBER:   81-05-02

SUBJECT HEADING:   AVIONS MARCEL DASSAULT - BREGUET AVIATION Model Falcon 10 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 2, 1981.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
81-05-02 AVIONS MARCEL DASSAULT - BREGUET AVIATION: Amendment 39-4048. Applies to all Model Falcon 10 airplanes certificated in all categories. Compliance required as indicated.

To prevent overheating of the air conditioning system - freon compressor motor starting resistor and thus avoid the attendant potential fire hazard accomplish the following, unless already accomplished:

Prior to May 1, 1981, remove the compressor motor starting resistor and thermostat, and install a time-delay device in the starting system in accordance with Avions Marcel Dassault- Breguet Aviation Service Bulletin No. F10 0177, dated December 5, 1978, or later FAA- approved revisions, or in a manner acceptable to the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Region.

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to the addresses listed above. These documents may also be examined at FAA Northwest Region, 9010 East Marginal Way South, Seattle, Washington 98108.

This amendment supersedes AD 78-22-03.

This amendment becomes effective March 2, 1981.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_81-05-02.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
81-05-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
AVIONS MARCEL DASSAULT - BREGUET AVIATION Model Falcon 10 Airplanes
Subject:
Compressor Starting Circuit
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/02/1981
Make:
Dassault Aviation
Model:
Falcon 10
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 81-05-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4048

AD NUMBER:   81-05-02

SUBJECT HEADING:   AVIONS MARCEL DASSAULT - BREGUET AVIATION Model Falcon 10 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 2, 1981.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
81-05-02 AVIONS MARCEL DASSAULT - BREGUET AVIATION: Amendment 39-4048. Applies to all Model Falcon 10 airplanes certificated in all categories. Compliance required as indicated.

To prevent overheating of the air conditioning system - freon compressor motor starting resistor and thus avoid the attendant potential fire hazard accomplish the following, unless already accomplished:

Prior to May 1, 1981, remove the compressor motor starting resistor and thermostat, and install a time-delay device in the starting system in accordance with Avions Marcel Dassault- Breguet Aviation Service Bulletin No. F10 0177, dated December 5, 1978, or later FAA- approved revisions, or in a manner acceptable to the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Region.

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to the addresses listed above. These documents may also be examined at FAA Northwest Region, 9010 East Marginal Way South, Seattle, Washington 98108.

This amendment supersedes AD 78-22-03.

This amendment becomes effective March 2, 1981.

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.