AD 67-25-07

final rule

Airworthiness Directives; VICKERS Models 744, 745D and 810 Series Airplanes

AD Number
67-25-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Vickers-Armstrongs (Aircraft Limited) Viscount 744 Airworthiness Directives; VICKERS Models 744, 745D and 810 Series Airplanes
aircraft Vickers-Armstrongs (Aircraft Limited) Viscount 745D Airworthiness Directives; VICKERS Models 744, 745D and 810 Series Airplanes
aircraft Vickers-Armstrongs (Aircraft Limited) Viscount 810 Airworthiness Directives; VICKERS Models 744, 745D and 810 Series Airplanes

Unsafe Condition

The Graviner D.1870 or D.1870N/1 loop type overheat detectors and Graviner point type detectors (P/N 4D/3, 13D/3, 68D/3, 150D/07/180) may fail to provide adequate overheat detection, leading to potential fire hazards.

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

Required Actions

Replace Graviner D.1870 or D.1870N/1 loop type overheat detectors with Graviner D.5352N/1 coil overheat detectors. Replace existing point type detectors (P/N 4D/3, 13D/3, 68D/3, 150D/07/180) with specified replacements (P/N 134D/3, 135D/3, 136D/3, 150D/07/210). Perform replacements per BAC Modification Bulletins D.3187 Issue 2 (700 Series) or FG.2055 Issue 2 (810 Series), or equivalent approved method.

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

Compliance Time

within the next 1,000 hours' time in service after the effective date of this AD

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

Affected Aircraft

Vickers-Armstrongs (Aircraft Limited) Viscount Models 744, 745D, and 810 Series airplanes

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

Federal Register Abstract

Heat Detectors

Applicability Source Text

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AD Number:
67-25-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; VICKERS Models 744, 745D and 810 Series Airplanes
Subject:
Heat Detectors
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
09/07/1967
Make:
Vickers-Armstrongs (Aircraft Limited)
Model:
Viscount 744 | 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: 67-25-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-473

AD NUMBER:   67-25-07

SUBJECT HEADING:   Airworthiness Directives; VICKERS Models 744, 745D and 810 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective September 7, 1967.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
67-25-07 VICKERS: Amdt. No. 39-473, Part 39, Federal Register September 7, 1967. Applies to Viscount Models 744, 745D and 810 Series Airplanes.

Within the next 1,000 hours' time in service after the effective date of this AD, unless already accomplished:

Replace Graviner D.1870 or D.1870N/1 loop type overheat detectors with Graviner D.5352N/1 coil overheat detectors. Replace Graviner point type detectors as shown in the following table:

Existing P/N	Replacement P/N
Graviner 4D/3	Graviner 134D/3
Graviner 13D/3	Graviner 135D/3
Graviner 68D/3	Graviner 136D/3
Graviner 150D/07/180	Graviner 150D/07/210

Detectors which are equivalent to the specified Graviner detectors may be used as replacements, subject to the approval of the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region.

Replace the detectors in accordance with British Aircraft Corporation Limited (BAC) Modification Bulletin No. D.3187, Issue 2, (700 Series), and Modification Bulletin No. FG.2055, Issue 2, (810 Series), or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region.

This amendment effective September 7, 1967.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_67-25-07.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
67-25-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; VICKERS Models 744, 745D and 810 Series Airplanes
Subject:
Heat Detectors
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
09/07/1967
Make:
Vickers-Armstrongs (Aircraft Limited)
Model:
Viscount 744 | 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: 67-25-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-473

AD NUMBER:   67-25-07

SUBJECT HEADING:   Airworthiness Directives; VICKERS Models 744, 745D and 810 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective September 7, 1967.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
67-25-07 VICKERS: Amdt. No. 39-473, Part 39, Federal Register September 7, 1967. Applies to Viscount Models 744, 745D and 810 Series Airplanes.

Within the next 1,000 hours' time in service after the effective date of this AD, unless already accomplished:

Replace Graviner D.1870 or D.1870N/1 loop type overheat detectors with Graviner D.5352N/1 coil overheat detectors. Replace Graviner point type detectors as shown in the following table:

Existing P/N	Replacement P/N
Graviner 4D/3	Graviner 134D/3
Graviner 13D/3	Graviner 135D/3
Graviner 68D/3	Graviner 136D/3
Graviner 150D/07/180	Graviner 150D/07/210

Detectors which are equivalent to the specified Graviner detectors may be used as replacements, subject to the approval of the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region.

Replace the detectors in accordance with British Aircraft Corporation Limited (BAC) Modification Bulletin No. D.3187, Issue 2, (700 Series), and Modification Bulletin No. FG.2055, Issue 2, (810 Series), or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region.

This amendment effective September 7, 1967.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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