AD 82-01-01

final rule

Airworthiness Directives; CANADAIR Model CL-600 Airplanes

AD Number
82-01-01
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 Airplanes
aircraft Bombardier Inc. CL-600-2A12 (CL-601) Airworthiness Directives; CANADAIR Model CL-600 Airplanes
aircraft Bombardier Inc. CL-600-2B16 (CL-601-3A) Airworthiness Directives; CANADAIR Model CL-600 Airplanes
aircraft Bombardier Inc. CL-600-2B16 (CL-601-3R) Airworthiness Directives; CANADAIR Model CL-600 Airplanes
aircraft Bombardier Inc. CL-600-2B16 (CL-604) Airworthiness Directives; CANADAIR Model CL-600 Airplanes
aircraft Bombardier Inc. CL-600-2B19 (Regional Jet Series 100) Airworthiness Directives; CANADAIR Model CL-600 Airplanes

Unsafe Condition

Asymmetric spoiler deployment due to improper rigging of left and right controlex cables (parts numbers 600-91305-5 and 600-91305-7).

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

Required Actions

Visually inspect and adjust the left and right controlex cables for compliance with Canadair Alert Service Bulletin A600-0024, Revision 1, or an approved method. Airplanes may be flown under FAR 21.197 to a maintenance base for inspection.

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

Compliance Time

within ten days after the effective date of this AD

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

Affected Aircraft

Bombardier Inc. Model CL-600 airplanes with serial number 1002 to 1050 inclusive

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

Federal Register Abstract

Left and Right Controlex Cables

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_82-01-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
82-01-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CANADAIR Model CL-600 Airplanes
Subject:
Left and Right Controlex Cables
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/04/1982
Make:
Bombardier Inc.
Model:
CL-600-1A11 (CL-600) | CL-600-2A12 (CL-601) | CL-600-2B16 (CL-601-3A) | CL-600-2B16 (CL-601-3R) | CL...Show more
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: 82-01-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4288

AD NUMBER:   82-01-01

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

ACTION:  

SUMMARY:  

DATES:   Effective January 4, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
82-01-01 CANADAIR: Amendment 39-4288. Applies to Model CL-600 airplanes with serial number 1002 to 1050 inclusive. To prevent asymmetric spoiler deployment, accomplish the following within ten days after the effective date of this AD, unless already accomplished:

1. Visually inspect and adjust, if necessary, the left and right controlex cables (parts numbers 600-91305-5 and 600-91305-7) for compliance with the revised rigging procedure specified in Canadair Alert Service Bulletin A600-0024, Revision 1, dated November 6, 1981, or in a manner 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.

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 January 4, 1982.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_82-01-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
82-01-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CANADAIR Model CL-600 Airplanes
Subject:
Left and Right Controlex Cables
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/04/1982
Make:
Bombardier Inc.
Model:
CL-600-1A11 (CL-600) | CL-600-2A12 (CL-601) | CL-600-2B16 (CL-601-3A) | CL-600-2B16 (CL-601-3R) | CL...Show more
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: 82-01-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4288

AD NUMBER:   82-01-01

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

ACTION:  

SUMMARY:  

DATES:   Effective January 4, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
82-01-01 CANADAIR: Amendment 39-4288. Applies to Model CL-600 airplanes with serial number 1002 to 1050 inclusive. To prevent asymmetric spoiler deployment, accomplish the following within ten days after the effective date of this AD, unless already accomplished:

1. Visually inspect and adjust, if necessary, the left and right controlex cables (parts numbers 600-91305-5 and 600-91305-7) for compliance with the revised rigging procedure specified in Canadair Alert Service Bulletin A600-0024, Revision 1, dated November 6, 1981, or in a manner 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.

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 January 4, 1982.

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.