AD 76-13-06

final rule

Airworthiness Directives; de Havilland Model DHC- 6 Series Twin Otter Aircraft

AD Number
76-13-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Viking Air Limited DHC-6-1 Airworthiness Directives; de Havilland Model DHC- 6 Series Twin Otter Aircraft
aircraft Viking Air Limited DHC-6-100 Airworthiness Directives; de Havilland Model DHC- 6 Series Twin Otter Aircraft
aircraft Viking Air Limited DHC-6-200 Airworthiness Directives; de Havilland Model DHC- 6 Series Twin Otter Aircraft
aircraft Viking Air Limited DHC-6-300 Airworthiness Directives; de Havilland Model DHC- 6 Series Twin Otter Aircraft

Unsafe Condition

Excessive removal of lightning strike protection bonding strap material during installation of wing tip strobe lights compromises aircraft lightning strike protection.

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

Required Actions

Accomplish alteration to wing tips per DeHavilland Service Bulletin No. 6/318 or equivalent approved alteration. Compliance must be within 100 hours in service after the AD's effective date, with possible extension upon request and FAA approval.

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

Compliance Time

Within the next 100 hours 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

DeHavilland Model DHC-6 series Twin Otter aircraft serial nos. 1 thru 430 with wing tip strobe lighting installed.

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

Federal Register Abstract

Lightning Protection

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_76-13-06.html
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AD Number:
76-13-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; de Havilland Model DHC- 6 Series Twin Otter Aircraft
Subject:
Lightning Protection
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/06/1976
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Superseded AD: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: 76-13-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2654

AD NUMBER:   76-13-06

SUBJECT HEADING:   Airworthiness Directives; de Havilland Model DHC- 6 Series Twin Otter Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective July 6, 1976.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
76-13-06 DEHAVILLAND: Amendment 39-2654. Applies to DeHavilland Model DHC- 6 series Twin Otter aircraft serial nos. 1 thru 430 incorporating wing tip strobe lighting.

Compliance required as indicated:

To restore the aircraft lightning strike protection to its original status, as a result of excessive removal of lightning strike protection bonding strap material, during the installation of the wing tip strobe lights, accomplish the following:

(a) Within the next 100 hours in service after the effective date of this AD, accomplish the alteration to the aircraft wing tips in accordance with "Accomplishment Instructions" in DeHavilland DHC-6 Service Bulletin No. 6/318, dated January 3, 1975, or later revision, or equivalent alteration approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.

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

This amendment is effective July 6, 1976.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_76-13-06.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
76-13-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; de Havilland Model DHC- 6 Series Twin Otter Aircraft
Subject:
Lightning Protection
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/06/1976
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: 76-13-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2654

AD NUMBER:   76-13-06

SUBJECT HEADING:   Airworthiness Directives; de Havilland Model DHC- 6 Series Twin Otter Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective July 6, 1976.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
76-13-06 DEHAVILLAND: Amendment 39-2654. Applies to DeHavilland Model DHC- 6 series Twin Otter aircraft serial nos. 1 thru 430 incorporating wing tip strobe lighting.

Compliance required as indicated:

To restore the aircraft lightning strike protection to its original status, as a result of excessive removal of lightning strike protection bonding strap material, during the installation of the wing tip strobe lights, accomplish the following:

(a) Within the next 100 hours in service after the effective date of this AD, accomplish the alteration to the aircraft wing tips in accordance with "Accomplishment Instructions" in DeHavilland DHC-6 Service Bulletin No. 6/318, dated January 3, 1975, or later revision, or equivalent alteration approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.

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

This amendment is effective July 6, 1976.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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