AD 66-20-02

final rule

Airworthiness Directives; Hawker Siddeley de Havilland Model 104 Dove Series Airplanes

AD Number
66-20-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
Federal Register: August 13, 1966
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 1A Airworthiness Directives; Hawker Siddeley de Havilland Model 104 Dove Series Airplanes
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 2A Airworthiness Directives; Hawker Siddeley de Havilland Model 104 Dove Series Airplanes
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 5A Airworthiness Directives; Hawker Siddeley de Havilland Model 104 Dove Series Airplanes
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 5BA Airworthiness Directives; Hawker Siddeley de Havilland Model 104 Dove Series Airplanes
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 6A Airworthiness Directives; Hawker Siddeley de Havilland Model 104 Dove Series Airplanes
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 6BA Airworthiness Directives; Hawker Siddeley de Havilland Model 104 Dove Series Airplanes
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 7A Airworthiness Directives; Hawker Siddeley de Havilland Model 104 Dove Series Airplanes
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 7AXC Airworthiness Directives; Hawker Siddeley de Havilland Model 104 Dove Series Airplanes
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 8A Airworthiness Directives; Hawker Siddeley de Havilland Model 104 Dove Series Airplanes
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 8AXC Airworthiness Directives; Hawker Siddeley de Havilland Model 104 Dove Series Airplanes

Unsafe Condition

The absence of 0.25 inch diameter radial holes in the engine air intake fire extinguishing system nozzle assembly (P/N P.117) and improper installation of fire extinguisher bottles and flexible hoses may prevent effective fire suppression, leading to potential engine fire hazards.

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

Required Actions

Inspect and replace nozzle jets without 0.25 inch diameter radial holes with P/N P.117e. Inspect and replace improper fire extinguisher bottles and flexible hoses per Hawker Siddeley Technical News Sheet CT (104) No. 196 or FAA-approved equivalent.

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

Compliance Time

within the next 100 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

de Havilland Model 104 Dove Series Airplanes equipped with an engine fire extinguisher system.

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

Federal Register Abstract

Engine Fire Extinguishing System

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_66-20-02.html
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Details
AD Number:
66-20-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Hawker Siddeley de Havilland Model 104 Dove Series Airplanes
Subject:
Engine Fire Extinguishing System
Status:
Current
Citation:
Federal Register: August 13, 1966
Citation Publish Date:
08/13/1966
Effective Date:
08/13/1966
Make:
de Havilland Aircraft Co., Ltd., The
Model:
D.H. 104 Dove Series 1A | D.H. 104 Dove Series 2A | D.H. 104 Dove Series 5A | D.H. 104 Dove Series 5...Show more
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: 66-20-02
CITATION:   [Federal Register: August 13, 1966]

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-273

AD NUMBER:   66-20-02

SUBJECT HEADING:   Airworthiness Directives; Hawker Siddeley de Havilland Model 104 Dove Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 13, 1966.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
66-20-02 HAWKER SIDDELEY: Amdt. 39-273, Part 39, Federal Register August 13, 1966. Applies to de Havilland Model 104 Dove Series Airplanes Equipped With an Engine Fire Extinguisher System.

Compliance required within the next 100 hours' time in service after the effective date of this AD, unless already accomplished.

(a) Inspect the engine air intake fire extinguishing system nozzle assembly to determine that 0.25 inch diameter radial holes are present in nozzle jet, P/N P.117. Replace each nozzle jet without 0.25 inch diameter radial holes with jet, P/N P.117e, with 0.25 inch diameter radial holes.

(b) Inspect the engine fire extinguishing system to determine that proper fire extinguisher bottle and flexible hoses from the fire extinguisher bottle to the firewall and from the firewall to the distributor are installed in accordance with Hawker Siddeley Aviation Ltd. Technical News Sheet CT (104) No. 196, Issue 1, or later ARB-approved issue or an FAA- approved equivalent. Replace improper fire extinguisher bottles and flexible hoses.

Hawker Siddeley Aviation Limited Technical News Sheet Dove (104) Series CT (104) No. 195, Issue 1, pertains to this subject.)

This directive effective August 13, 1966.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_66-20-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
66-20-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Hawker Siddeley de Havilland Model 104 Dove Series Airplanes
Subject:
Engine Fire Extinguishing System
Status:
Current
Citation:
Federal Register: August 13, 1966
Citation Publish Date:
08/13/1966
Effective Date:
08/13/1966
Make:
de Havilland Aircraft Co., Ltd., The
Model:
D.H. 104 Dove Series 1A | D.H. 104 Dove Series 2A | D.H. 104 Dove Series 5A | D.H. 104 Dove Series 5...Show more
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: 66-20-02
CITATION:   [Federal Register: August 13, 1966]

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-273

AD NUMBER:   66-20-02

SUBJECT HEADING:   Airworthiness Directives; Hawker Siddeley de Havilland Model 104 Dove Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 13, 1966.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
66-20-02 HAWKER SIDDELEY: Amdt. 39-273, Part 39, Federal Register August 13, 1966. Applies to de Havilland Model 104 Dove Series Airplanes Equipped With an Engine Fire Extinguisher System.

Compliance required within the next 100 hours' time in service after the effective date of this AD, unless already accomplished.

(a) Inspect the engine air intake fire extinguishing system nozzle assembly to determine that 0.25 inch diameter radial holes are present in nozzle jet, P/N P.117. Replace each nozzle jet without 0.25 inch diameter radial holes with jet, P/N P.117e, with 0.25 inch diameter radial holes.

(b) Inspect the engine fire extinguishing system to determine that proper fire extinguisher bottle and flexible hoses from the fire extinguisher bottle to the firewall and from the firewall to the distributor are installed in accordance with Hawker Siddeley Aviation Ltd. Technical News Sheet CT (104) No. 196, Issue 1, or later ARB-approved issue or an FAA- approved equivalent. Replace improper fire extinguisher bottles and flexible hoses.

Hawker Siddeley Aviation Limited Technical News Sheet Dove (104) Series CT (104) No. 195, Issue 1, pertains to this subject.)

This directive effective August 13, 1966.

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.