AD 85-26-05

final rule

Airworthiness Directives; GULFSTREAM AEROSPACE Model GA-7 (Cougar) Airplanes

AD Number
85-26-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

TypeManufacturerModelDetails
aircraft SOCATA - Groupe Aerospatiale GA-7 Airworthiness Directives; GULFSTREAM AEROSPACE Model GA-7 (Cougar) Airplanes

Unsafe Condition

Failure of the rudder torque tube due to corrosion or cracks.

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

Required Actions

Visually inspect the rudder torque tube for corrosion or cracks. If cracks or excessive corrosion are found, replace the rudder torque tube P/N 7CS10500-11. If no cracks and only light surface corrosion exist, apply corrosion protection treatment.

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

Compliance Time

within 50 hours time-in-service after the effective date of this AD unless previously accomplished

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

Affected Aircraft

GULFSTREAM AEROSPACE Model GA-7 (Cougar) airplanes, all serial numbers, certified in any category

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

Federal Register Abstract

Rudder Torque Tube

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_85-26-05.html
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Details
AD Number:
85-26-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; GULFSTREAM AEROSPACE Model GA-7 (Cougar) Airplanes
Subject:
Rudder Torque Tube
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/03/1986
Make:
SOCATA - Groupe Aerospatiale
Model:
GA-7
Product Type:
Aircraft
Product Subtype:
Small 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Superseded AD: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Superseded By: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: 85-26-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5203

AD NUMBER:   85-26-05

SUBJECT HEADING:   Airworthiness Directives; GULFSTREAM AEROSPACE Model GA-7 (Cougar) Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective January 3, 1986.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
85-26-05 GULFSTREAM AEROSPACE: Amendment 39-5203. Applies to Model GA-7 (Cougar) airplanes, all serial numbers, certified in any category.

COMPLIANCE: Required within 50 hours time-in-service after the effective date of this AD unless previously accomplished.

To prevent failure of the rudder torque tube, accomplish Paragraphs (a), (b) and (c) of the following AD in accordance with Gulfstream Aerospace Corporation (GAC) Service Bulletin (S/B) No. ME-21, dated November 1, 1985:

(a) Visually inspect the rudder torque tube for corrosion or cracks.

(b) If any cracks or excessive corrosion is found, prior to further flight replace the rudder torque tube, P/N 7CS10500-11.

(c) If no cracks are found and no corrosion or only light surface corrosion exists on the rudder torque tube, prior to further flight apply corrosion protection treatment to the torque tube.

(d) Aircraft may be flown in accordance with Federal Aviation Regulation 21.197 to a location where this AD can be accomplished.

(e) An equivalent method of compliance with this AD, if used, must be approved by the Manager, Atlanta Aircraft Certification Office, 1075 Inner Loop Road, College Park, Georgia 30337; telephone (404) 763-7428.

All persons affected by this directive may obtain copies of the documents referred to herein upon request to Gulfstream Aerospace Corporation, P.0. Box 2206, Savannah, Georgia 31402- 2206, or the FAA, Rules Docket, Office of the Regional Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106.

This amendment becomes effective on January 3, 1986.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_85-26-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
85-26-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; GULFSTREAM AEROSPACE Model GA-7 (Cougar) Airplanes
Subject:
Rudder Torque Tube
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/03/1986
Make:
SOCATA - Groupe Aerospatiale
Model:
GA-7
Product Type:
Aircraft
Product Subtype:
Small 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: 85-26-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5203

AD NUMBER:   85-26-05

SUBJECT HEADING:   Airworthiness Directives; GULFSTREAM AEROSPACE Model GA-7 (Cougar) Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective January 3, 1986.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
85-26-05 GULFSTREAM AEROSPACE: Amendment 39-5203. Applies to Model GA-7 (Cougar) airplanes, all serial numbers, certified in any category.

COMPLIANCE: Required within 50 hours time-in-service after the effective date of this AD unless previously accomplished.

To prevent failure of the rudder torque tube, accomplish Paragraphs (a), (b) and (c) of the following AD in accordance with Gulfstream Aerospace Corporation (GAC) Service Bulletin (S/B) No. ME-21, dated November 1, 1985:

(a) Visually inspect the rudder torque tube for corrosion or cracks.

(b) If any cracks or excessive corrosion is found, prior to further flight replace the rudder torque tube, P/N 7CS10500-11.

(c) If no cracks are found and no corrosion or only light surface corrosion exists on the rudder torque tube, prior to further flight apply corrosion protection treatment to the torque tube.

(d) Aircraft may be flown in accordance with Federal Aviation Regulation 21.197 to a location where this AD can be accomplished.

(e) An equivalent method of compliance with this AD, if used, must be approved by the Manager, Atlanta Aircraft Certification Office, 1075 Inner Loop Road, College Park, Georgia 30337; telephone (404) 763-7428.

All persons affected by this directive may obtain copies of the documents referred to herein upon request to Gulfstream Aerospace Corporation, P.0. Box 2206, Savannah, Georgia 31402- 2206, or the FAA, Rules Docket, Office of the Regional Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106.

This amendment becomes effective on January 3, 1986.

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.