AD 67-33-01

final rule

Airworthiness Directives; de Havilland Aircraft Type DHC-6 Series Airplanes

AD Number
67-33-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
Federal Register: December 30, 1967

Applicability

TypeManufacturerModelDetails
aircraft Viking Air Limited DHC-6-1 Airworthiness Directives; de Havilland Aircraft Type DHC-6 Series Airplanes
aircraft Viking Air Limited DHC-6-100 Airworthiness Directives; de Havilland Aircraft Type DHC-6 Series Airplanes
aircraft Viking Air Limited DHC-6-200 Airworthiness Directives; de Havilland Aircraft Type DHC-6 Series Airplanes
aircraft Viking Air Limited DHC-6-300 Airworthiness Directives; de Havilland Aircraft Type DHC-6 Series Airplanes

Unsafe Condition

The noncompliance of the Grimes 41905-1 Anti-Collision Light causes a hazardous condition.

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

Required Actions

Install a placard stating 'AIRCRAFT LIMITED TO DAY VFR FLIGHT ONLY' within 50 hours' time in service after the effective date. The placard may be removed after replacing the light with Grimes G8400A-24 per de Havilland Modification No. 6/1116 or equivalent approved installation.

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

Compliance Time

Within the next 50 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 Aircraft Type DHC-6 Airplanes incorporating Grimes 41905-1 Anti-Collision Light

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

Federal Register Abstract

Anti-collision Light

Applicability Source Text

Show captured applicability text from the source AD
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Details
AD Number:
67-33-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; de Havilland Aircraft Type DHC-6 Series Airplanes
Subject:
Anti-collision Light
Status:
Current
Citation:
Federal Register: December 30, 1967
Citation Publish Date:
12/30/1967
Effective Date:
12/30/1967
Make:
Viking Air Limited
Model:
DHC-6-1 | DHC-6-100 | DHC-6-200 | DHC-6-300
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Superseded AD: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Superseded By: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: 67-33-01
CITATION:   [Federal Register: December 30, 1967]

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-529

AD NUMBER:   67-33-01

SUBJECT HEADING:   Airworthiness Directives; de Havilland Aircraft Type DHC-6 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective December 30, 1967.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
67-33-01 de HAVILLAND AIRCRAFT: Amdt. 39-529, Part 39, Federal Register December 30, 1967. Applies to Type DHC-6 Airplanes Incorporating Grimes 41905-1 Anti- Collision Light.

Compliance required as indicated.

To prevent the occurrence of a hazardous condition, caused by the noncompliance of the Grimes 41905-1 Anti-Collision Light, accomplish the following:

(a) Within the next 50 hours' time in service after the effective date of this AD, unless already accomplished, install the following placard in full view of the pilot: "AIRCRAFT LIMITED TO DAY VFR FLIGHT ONLY."

(b) The placard required by paragraph (a) may be removed when the light is replaced by the Grimes G8400A-24 Anti-Collision Light in accordance with the "Procedure" outlined in de Havilland Modification No. 6/1116, dated October 26, 1967, or later revision or equivalent installation approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.

(c) Upon request with substantiating data submitted through an FAA maintenance inspector, the compliance time specified in this AD may be increased by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.

This amendment effective December 30, 1967.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_67-33-01.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
67-33-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; de Havilland Aircraft Type DHC-6 Series Airplanes
Subject:
Anti-collision Light
Status:
Current
Citation:
Federal Register: December 30, 1967
Citation Publish Date:
12/30/1967
Effective Date:
12/30/1967
Make:
Viking Air Limited
Model:
DHC-6-1 | DHC-6-100 | DHC-6-200 | DHC-6-300
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: 67-33-01
CITATION:   [Federal Register: December 30, 1967]

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-529

AD NUMBER:   67-33-01

SUBJECT HEADING:   Airworthiness Directives; de Havilland Aircraft Type DHC-6 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective December 30, 1967.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
67-33-01 de HAVILLAND AIRCRAFT: Amdt. 39-529, Part 39, Federal Register December 30, 1967. Applies to Type DHC-6 Airplanes Incorporating Grimes 41905-1 Anti- Collision Light.

Compliance required as indicated.

To prevent the occurrence of a hazardous condition, caused by the noncompliance of the Grimes 41905-1 Anti-Collision Light, accomplish the following:

(a) Within the next 50 hours' time in service after the effective date of this AD, unless already accomplished, install the following placard in full view of the pilot: "AIRCRAFT LIMITED TO DAY VFR FLIGHT ONLY."

(b) The placard required by paragraph (a) may be removed when the light is replaced by the Grimes G8400A-24 Anti-Collision Light in accordance with the "Procedure" outlined in de Havilland Modification No. 6/1116, dated October 26, 1967, or later revision or equivalent installation approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.

(c) Upon request with substantiating data submitted through an FAA maintenance inspector, the compliance time specified in this AD may be increased by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.

This amendment effective December 30, 1967.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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