AD 82-25-02

final rule

AVIONS MARCEL DASSAULT - BREGUET AVIATION Model AMD-BA Falcon 10 Airplanes

AD Number
82-25-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

Applicability

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

Unsafe Condition

Potential failure of the landing gear to extend or retract due to issues with the pilot valve ball pushrod, selector solenoid valve, or spring in the landing gear control selector solenoid valve assembly.

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

Required Actions

Inspect and modify or replace the pilot valve ball pushrod, selector solenoid valve, and spring in the landing gear control selector solenoid valve assembly per Service Bulletins F10-0149, F10-0168, F10-0173, and F10-0174. Alternate means of compliance may be approved by the FAA.

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

Compliance Time

within the next 250 hours time in service or 90 days, whichever occurs first, after the effective date of this AD

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

Affected Aircraft

All AMD-BA 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

Landing Gear Retraction System

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_82-25-02.html
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Details
AD Number:
82-25-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
AVIONS MARCEL DASSAULT - BREGUET AVIATION Model AMD-BA Falcon 10 Airplanes
Subject:
Landing Gear Retraction System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/06/1982
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Superseded AD: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Superseded By: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: 82-25-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4502

AD NUMBER:   82-25-02

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

ACTION:  

SUMMARY:  

DATES:   Effective December 6, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
82-25-02 AVIONS MARCEL DASSAULT - BREGUET AVIATION: Amendment 39-4502. Applies to all AMD-BA Falcon 10 airplanes certificated in all categories. Compliance is required within the next 250 hours time in service or 90 days, whichever occurs first, after the effective date of this AD, unless already accomplished.

1. To prevent the potential failure of the landing gear to extend or retract, inspect and modify or replace, if necessary, (a) the pilot valve ball pushrod; (b) the selector solenoid valve; and (c) the spring in the landing gear control selector solenoid valve assembly in accordance with the Accomplishment Instructions of Avions Marcel Dassault-Breguet Aviation Service Bulletin Nos. F10-0149, Revision 1, dated November 22, 1978; F10-0168, Revision 1, dated February 8, 1979; F10-0173 dated November 22, 1978; and F10-0174 dated November 22, 1978.

2. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.

3. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.

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).

This amendment becomes effective December 6, 1982.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_82-25-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
82-25-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
AVIONS MARCEL DASSAULT - BREGUET AVIATION Model AMD-BA Falcon 10 Airplanes
Subject:
Landing Gear Retraction System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/06/1982
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: 82-25-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4502

AD NUMBER:   82-25-02

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

ACTION:  

SUMMARY:  

DATES:   Effective December 6, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
82-25-02 AVIONS MARCEL DASSAULT - BREGUET AVIATION: Amendment 39-4502. Applies to all AMD-BA Falcon 10 airplanes certificated in all categories. Compliance is required within the next 250 hours time in service or 90 days, whichever occurs first, after the effective date of this AD, unless already accomplished.

1. To prevent the potential failure of the landing gear to extend or retract, inspect and modify or replace, if necessary, (a) the pilot valve ball pushrod; (b) the selector solenoid valve; and (c) the spring in the landing gear control selector solenoid valve assembly in accordance with the Accomplishment Instructions of Avions Marcel Dassault-Breguet Aviation Service Bulletin Nos. F10-0149, Revision 1, dated November 22, 1978; F10-0168, Revision 1, dated February 8, 1979; F10-0173 dated November 22, 1978; and F10-0174 dated November 22, 1978.

2. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.

3. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.

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).

This amendment becomes effective December 6, 1982.

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.