AD 60-18-02

final rule

Airworthiness Directives; VICKERS Model 745D and 810 Series Aircraft

AD Number
60-18-02
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 Vickers-Armstrongs (Aircraft Limited) Viscount 745D Airworthiness Directives; VICKERS Model 745D and 810 Series Aircraft
aircraft Vickers-Armstrongs (Aircraft Limited) Viscount 810 Airworthiness Directives; VICKERS Model 745D and 810 Series Aircraft

Unsafe Condition

Failure of the brake accumulator system due to contamination or blockage of the system components, which could result in loss of braking efficiency or failure of the brake accumulator system.

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

Required Actions

Conduct inspections of the brake accumulator systems as specified in Vickers Preliminary Technical Leaflet (PTL) 222 (700 Series) and PTL 87 (800/810 Series) within the next 300 hours' time in service and at subsequent periodic intervals of 800 hours' time in service. Inspections are not required if filters, Dunlop ACM 18308 or equivalent, are installed in accordance with Vickers Modification Bulletins D.2994 (700 Series) and FG.1796 (800/810 Series).

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

Compliance Time

within the next 300 hours' time in service

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

Affected Aircraft

Vickers-Armstrongs (Aircraft Limited) Viscount 745D and Viscount 810 aircraft

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

Federal Register Abstract

Brake Accumulator

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_60-18-02.html
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Details
AD Number:
60-18-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; VICKERS Model 745D and 810 Series Aircraft
Subject:
Brake Accumulator
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/24/1960
Make:
Vickers-Armstrongs (Aircraft Limited)
Model:
Viscount 745D | Viscount 810
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: 60-18-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   60-18-02

SUBJECT HEADING:   Airworthiness Directives; VICKERS Model 745D and 810 Series Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective August 24, 1960.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
60-18-02 VICKERS: Amdt. 197 Part 507 Federal Register August 24, 1960. Applies To All 745D and 810 Series Aircraft.

Compliance required as indicated.

Conduct inspections of the brake accumulator systems as specified in Vickers Preliminary Technical Leaflet (PTL) 222 (700 Series) and PTL 87 (800/810 Series) within the next 300 hours' time in service and at subsequent periodic intervals of 800 hours' time in service. These inspections are not mandatory when filters, Dunlop ACM 18308 or equivalent, are installed in accordance with Vickers Modification Bulletins D.2994 (700 Series) and FG.1796 (800/810 Series).

This amendment shall become effective 30 days after date of its publication in the Federal Register.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_60-18-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
60-18-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; VICKERS Model 745D and 810 Series Aircraft
Subject:
Brake Accumulator
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/24/1960
Make:
Vickers-Armstrongs (Aircraft Limited)
Model:
Viscount 745D | Viscount 810
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: 60-18-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   60-18-02

SUBJECT HEADING:   Airworthiness Directives; VICKERS Model 745D and 810 Series Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective August 24, 1960.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
60-18-02 VICKERS: Amdt. 197 Part 507 Federal Register August 24, 1960. Applies To All 745D and 810 Series Aircraft.

Compliance required as indicated.

Conduct inspections of the brake accumulator systems as specified in Vickers Preliminary Technical Leaflet (PTL) 222 (700 Series) and PTL 87 (800/810 Series) within the next 300 hours' time in service and at subsequent periodic intervals of 800 hours' time in service. These inspections are not mandatory when filters, Dunlop ACM 18308 or equivalent, are installed in accordance with Vickers Modification Bulletins D.2994 (700 Series) and FG.1796 (800/810 Series).

This amendment shall become effective 30 days after date of its publication in the Federal Register.

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.