AD 87-11-02

final rule

Airworthiness Directives; DEHAVILLAND Model DHC-7 Series Airplanes

AD Number
87-11-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Viking Air Limited DHC-7-1 Airworthiness Directives; DEHAVILLAND Model DHC-7 Series Airplanes
aircraft Viking Air Limited DHC-7-100 Airworthiness Directives; DEHAVILLAND Model DHC-7 Series Airplanes
aircraft Viking Air Limited DHC-7-101 Airworthiness Directives; DEHAVILLAND Model DHC-7 Series Airplanes
aircraft Viking Air Limited DHC-7-102 Airworthiness Directives; DEHAVILLAND Model DHC-7 Series Airplanes
aircraft Viking Air Limited DHC-7-103 Airworthiness Directives; DEHAVILLAND Model DHC-7 Series Airplanes

Unsafe Condition

Flames may penetrate the rear cargo compartment liner to the fuselage primary structure.

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

Required Actions

Modify the DHC-7 rear cargo liner in accordance with DH Modification No. 7/2499, as detailed in DeHavilland Service Bulletin No. 7-25-49, Revision A, dated July 11, 1986, or later revisions approved by the Manager, New York Certification Office, FAA, New England Region. Alternate means of compliance may be used when approved by the Manager, New York Aircraft Certification Office, FAA, New England Region.

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

Compliance Time

Within the next 6 months 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-7 series airplanes, certificated in any category

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

Federal Register Abstract

Rear Cargo Liner

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_87-11-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
87-11-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DEHAVILLAND Model DHC-7 Series Airplanes
Subject:
Rear Cargo Liner
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
06/21/1987
Make:
Viking Air Limited
Model:
DHC-7-1 | DHC-7-100 | DHC-7-101 | DHC-7-102 | DHC-7-103
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: 87-11-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5625

AD NUMBER:   87-11-02

SUBJECT HEADING:   Airworthiness Directives; DEHAVILLAND Model DHC-7 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective June 21, 1987.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   87-11-02 THE DEHAVILLAND AIRCRAFT COMPANY OF CANADA, A DIVISION OF BOEING OF CANADA, LTD.: Amendment 39-5625. Applies to all Model DHC-7 series airplanes, certificated in any category. Compliance is required as indicated, unless already accomplished.

To assure that flames will not penetrate the rear cargo compartment liner to the fuselage primary structure, accomplish the following:

A. Within the next 6 months after the effective date of this AD, modify the DHC-7 rear cargo liner in accordance with DH Modification No. 7/2499, as detailed in DeHavilland Service Bulletin No. 7-25-49, Revision A, dated July 11, 1986, or later revisions approved by the Manager, New York Certification Office, FAA, New England Region.

B. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, New York Aircraft Certification Office, FAA, New England Region.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to The de Havilland Aircraft Company of Canada, A Division of Boeing of Canada, Ltd., Garratt Boulevard, Downsview, Ontario M3K 1Y5, Canada. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or FAA, New England Region, New York Aircraft Certification Office, 181 South Franklin Avenue, Room 202, Valley Stream, New York.

This amendment becomes effective June 21, 1987.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_87-11-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
87-11-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DEHAVILLAND Model DHC-7 Series Airplanes
Subject:
Rear Cargo Liner
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
06/21/1987
Make:
Viking Air Limited
Model:
DHC-7-1 | DHC-7-100 | DHC-7-101 | DHC-7-102 | DHC-7-103
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: 87-11-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5625

AD NUMBER:   87-11-02

SUBJECT HEADING:   Airworthiness Directives; DEHAVILLAND Model DHC-7 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective June 21, 1987.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   87-11-02 THE DEHAVILLAND AIRCRAFT COMPANY OF CANADA, A DIVISION OF BOEING OF CANADA, LTD.: Amendment 39-5625. Applies to all Model DHC-7 series airplanes, certificated in any category. Compliance is required as indicated, unless already accomplished.

To assure that flames will not penetrate the rear cargo compartment liner to the fuselage primary structure, accomplish the following:

A. Within the next 6 months after the effective date of this AD, modify the DHC-7 rear cargo liner in accordance with DH Modification No. 7/2499, as detailed in DeHavilland Service Bulletin No. 7-25-49, Revision A, dated July 11, 1986, or later revisions approved by the Manager, New York Certification Office, FAA, New England Region.

B. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, New York Aircraft Certification Office, FAA, New England Region.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to The de Havilland Aircraft Company of Canada, A Division of Boeing of Canada, Ltd., Garratt Boulevard, Downsview, Ontario M3K 1Y5, Canada. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or FAA, New England Region, New York Aircraft Certification Office, 181 South Franklin Avenue, Room 202, Valley Stream, New York.

This amendment becomes effective June 21, 1987.

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.