AD 86-02-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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Limited) Model: Viscount 744 | Viscount 745D Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Updated RGL applicability to match AD applicability; CAR C-11-185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:
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Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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