AD 82-05-02

final rule

Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes

AD Number
82-05-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Bombardier Inc. CL-600-1A11 (CL-600) Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes

Unsafe Condition

Loss of electrical power

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

Required Actions

Inspect and repair if necessary in accordance with Canadair Alert Service Bulletin No. A600-0087, Revision 1, dated September 3, 1981, or a later revision approved by the Chief, Seattle Area Aircraft Certification Office. Airplanes may be flown under FAR 21.197 to a maintenance base for the inspection. Alternate methods of compliance may be used if approved.

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

Compliance Time

Within the next 50 flight hours or within the next 15 calendar days after the effective date of this Airworthiness Directive, whichever comes first

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

Affected Aircraft

Canadair Model CL-600-1A11 airplanes, serial numbers 1005 thru 1007, 1010 thru 1014, and 1016 thru 1022

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

Federal Register Abstract

Loss Of Electrical Power

Applicability Source Text

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AD Number:
82-05-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes
Subject:
Loss Of Electrical Power
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/11/1982
Make:
Bombardier Inc.
Model:
CL-600-1A11 (CL-600)
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Superseded AD: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Superseded By: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: 82-05-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4327

AD NUMBER:   82-05-02

SUBJECT HEADING:   Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 11, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   82-05-02 CANADAIR: Amendment 39-4327. Applies to Canadair Model CL-600-1A11 airplanes, serial numbers 1005 thru 1007, 1010 thru 1014, and 1016 thru 1022. To prevent loss of electrical power, unless already accomplished, accomplish the following:

1. Within the next 50 flight hours, or within the next 15 calendar days after the effective date of this Airworthiness Directive, whichever comes first, inspect, and repair if necessary, in accordance with accomplishment instructions contained in Canadair Alert Service Bulletin No. A600-0087, Revision 1, dated September 3, 1981, or a later revision approved by the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Mountain Region.

2. Airplanes may be flown in accordance with FAR 21.197 to a maintenance base for accomplishment of the inspection required by this AD.

3. Alternate methods of compliance with this AD may be used when they provide an equivalent level of safety and are approved by the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Mountain Region.

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to the addresses listed above. These documents may also be examined at FAA Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington 98108.

This amendment becomes effective March 11, 1982.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_82-05-02.html
Copy URL
Print/Save as PDF
Document Versions
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Details
AD Number:
82-05-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes
Subject:
Loss Of Electrical Power
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/11/1982
Make:
Bombardier Inc.
Model:
CL-600-1A11 (CL-600)
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: 82-05-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4327

AD NUMBER:   82-05-02

SUBJECT HEADING:   Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 11, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   82-05-02 CANADAIR: Amendment 39-4327. Applies to Canadair Model CL-600-1A11 airplanes, serial numbers 1005 thru 1007, 1010 thru 1014, and 1016 thru 1022. To prevent loss of electrical power, unless already accomplished, accomplish the following:

1. Within the next 50 flight hours, or within the next 15 calendar days after the effective date of this Airworthiness Directive, whichever comes first, inspect, and repair if necessary, in accordance with accomplishment instructions contained in Canadair Alert Service Bulletin No. A600-0087, Revision 1, dated September 3, 1981, or a later revision approved by the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Mountain Region.

2. Airplanes may be flown in accordance with FAR 21.197 to a maintenance base for accomplishment of the inspection required by this AD.

3. Alternate methods of compliance with this AD may be used when they provide an equivalent level of safety and are approved by the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Mountain Region.

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to the addresses listed above. These documents may also be examined at FAA Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington 98108.

This amendment becomes effective March 11, 1982.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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