AD 83-21-03

final rule

Airworthiness Directives; DeHavilland Model DHC-7 Airplanes

AD Number
83-21-03
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 Airplanes
aircraft Viking Air Limited DHC-7-100 Airworthiness Directives; DeHavilland Model DHC-7 Airplanes
aircraft Viking Air Limited DHC-7-101 Airworthiness Directives; DeHavilland Model DHC-7 Airplanes
aircraft Viking Air Limited DHC-7-102 Airworthiness Directives; DeHavilland Model DHC-7 Airplanes
aircraft Viking Air Limited DHC-7-103 Airworthiness Directives; DeHavilland Model DHC-7 Airplanes

Unsafe Condition

Failure of the pilot valve of the ground spoiler valve No. 2 could result in uncommanded operation of the ground spoilers during flight, leading to potential loss of control.

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

Required Actions

Perform an operational check of the ground spoiler system within 25 flight hours from the AD effective date, and repeat the functional checks every 800 flight hours. Use DeHavilland Alert Service Bulletin A7-27-56 for instructions. Alternate means of compliance may be approved.

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

Compliance Time

Within 25 flight hours from 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 airplanes equipped with ground spoiler valves per modification No. 7/1732, including DHC-7-1, DHC-7-100, DHC-7-101, DHC-7-102, DHC-7-103 models.

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

Federal Register Abstract

Ground Spoiler System

Applicability Source Text

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AD Number:
83-21-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DeHavilland Model DHC-7 Airplanes
Subject:
Ground Spoiler System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/02/1983
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Superseded AD: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: 83-21-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4753

AD NUMBER:   83-21-03

SUBJECT HEADING:   Airworthiness Directives; DeHavilland Model DHC-7 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective November 2, 1983.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   83-21-03 DEHAVILLAND AIRCRAFT OF CANADA, LTD.: Amendment 39-4753. Applies to DeHavilland model DHC-7 airplanes, certificated in all categories, which are equipped with ground spoiler valves installed in accordance with DeHavilland modification No. 7/1732. To detect failures of the pilot valve of the ground spoiler valve No. 2, accomplish the following, unless previously accomplished:

A. Within 25 flight hours from the effective date of this AD, perform an operational check of the ground spoiler system, and take appropriate corrective action, if necessary, in accordance with the Accomplishment Instructions of DeHavilland Aircraft of Canada, Ltd., Alert Service Bulletin A7-27-56, dated June 28, 1983.

B. Repeat the functional checks of paragraph A. at intervals not to exceed 800 flight hours.

C. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.

D. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.

This amendment becomes effective November 2, 1983.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_83-21-03.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
83-21-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DeHavilland Model DHC-7 Airplanes
Subject:
Ground Spoiler System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/02/1983
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: 83-21-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4753

AD NUMBER:   83-21-03

SUBJECT HEADING:   Airworthiness Directives; DeHavilland Model DHC-7 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective November 2, 1983.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   83-21-03 DEHAVILLAND AIRCRAFT OF CANADA, LTD.: Amendment 39-4753. Applies to DeHavilland model DHC-7 airplanes, certificated in all categories, which are equipped with ground spoiler valves installed in accordance with DeHavilland modification No. 7/1732. To detect failures of the pilot valve of the ground spoiler valve No. 2, accomplish the following, unless previously accomplished:

A. Within 25 flight hours from the effective date of this AD, perform an operational check of the ground spoiler system, and take appropriate corrective action, if necessary, in accordance with the Accomplishment Instructions of DeHavilland Aircraft of Canada, Ltd., Alert Service Bulletin A7-27-56, dated June 28, 1983.

B. Repeat the functional checks of paragraph A. at intervals not to exceed 800 flight hours.

C. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.

D. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.

This amendment becomes effective November 2, 1983.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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