AD 86-02-05

final rule

Airworthiness Directives; BRITISH AEROSPACE Model 700 Series Airplanes

AD Number
86-02-05
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 Vickers-Armstrongs (Aircraft Limited) Viscount 744 Airworthiness Directives; BRITISH AEROSPACE Model 700 Series Airplanes
aircraft Vickers-Armstrongs (Aircraft Limited) Viscount 745D Airworthiness Directives; BRITISH AEROSPACE Model 700 Series Airplanes

Unsafe Condition

Nose landing gear collapse as a result of a faulty hydraulic cut out valve (Part Number AIR 41916).

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

Required Actions

Modify the aircraft hydraulic system cut out valve (Part Number AIR 41916) in accordance with Automotive Products Modification Standard SA 3490 dated December 16, 1959. Alternate means of compliance may be used if approved by the FAA.

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

Compliance Time

Within the next 1000 hours time-in-service or nine months after the effective date of this AD, whichever occurs first.

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

Affected Aircraft

Vickers-Armstrongs (Aircraft Limited) Viscount 744 and Viscount 745D models, all serial numbers.

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

Federal Register Abstract

Hydraulic System Cut Out Valve

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_86-02-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
86-02-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AEROSPACE Model 700 Series Airplanes
Subject:
Hydraulic System Cut Out Valve
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/03/1986
Make:
Vickers-Armstrongs (Aircraft Limited)
Model:
Viscount 744 | Viscount 745D
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Superseded AD: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Superseded By: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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 86-02-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5204

AD NUMBER:   86-02-05

SUBJECT HEADING:   Airworthiness Directives; BRITISH AEROSPACE Model 700 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective February 3, 1986.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   86-02-05 BRITISH AEROSPACE: Amendment 39-5204. Applies to Vickers Viscount Model 700 series airplanes certificated in any category. Compliance is required as follows, unless previously accomplished. To prevent nose landing gear collapse as a result of a faulty hydraulic cut out valve, accomplish the following:

A. Within the next 1000 hours time-in-service or nine months after the effective date of this AD, whichever occurs first, modify the aircraft hydraulic system cut out valve, Part Number AIR 41916, in accordance with Automotive Products Modification Standard SA 3490, dated December 16, 1959 (reference BAe Technical News Sheet No. 369, Issue 1, dated August 5, 1985).

B. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

C. 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.

All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to British Aerospace Inc., Box 17414, Dulles International Airport, Washington, D.C. 20041. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective February 3, 1986.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_86-02-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
86-02-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AEROSPACE Model 700 Series Airplanes
Subject:
Hydraulic System Cut Out Valve
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/03/1986
Make:
Vickers-Armstrongs (Aircraft Limited)
Model:
Viscount 744 | Viscount 745D
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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 86-02-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5204

AD NUMBER:   86-02-05

SUBJECT HEADING:   Airworthiness Directives; BRITISH AEROSPACE Model 700 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective February 3, 1986.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   86-02-05 BRITISH AEROSPACE: Amendment 39-5204. Applies to Vickers Viscount Model 700 series airplanes certificated in any category. Compliance is required as follows, unless previously accomplished. To prevent nose landing gear collapse as a result of a faulty hydraulic cut out valve, accomplish the following:

A. Within the next 1000 hours time-in-service or nine months after the effective date of this AD, whichever occurs first, modify the aircraft hydraulic system cut out valve, Part Number AIR 41916, in accordance with Automotive Products Modification Standard SA 3490, dated December 16, 1959 (reference BAe Technical News Sheet No. 369, Issue 1, dated August 5, 1985).

B. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

C. 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.

All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to British Aerospace Inc., Box 17414, Dulles International Airport, Washington, D.C. 20041. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective February 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.