AD 83-13-02

final rule

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

AD Number
83-13-02
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

Failure of the passenger door latch mechanism and associated fittings to properly latch the door could result in the door opening during flight, creating an unsafe condition.

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

Required Actions

Within 10 hours time in service after the effective date, inspect and adjust the interior handle per Canadair Alert Service Bulletin No. A600-0203. Within 60 hours time in service, modify the latch mechanism and components per paragraph 2.C. of the service bulletin. Alternate means 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 10 hours time in service after the effective date of this AD and thereafter at intervals not to exceed 25 hours time in service for inspections; modifications must be done within 60 hours time in service after the effective date.

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

Affected Aircraft

Bombardier Inc. Model CL-600-1A11 (CL-600), serial numbers 1024 to 1074 inclusive.

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

Federal Register Abstract

Door Latch Mechanism Assembly

Applicability Source Text

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AD Number:
83-13-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes
Subject:
Door Latch Mechanism Assembly
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/05/1983
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Superseded AD: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Superseded By: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: 83-13-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4670

AD NUMBER:   83-13-02

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

ACTION:  

SUMMARY:  

DATES:   Effective July 5, 1983.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   83-13-02 CANADAIR: Amendment 39-4670. Applies to Model CL-600-1A11 airplanes, serial numbers 1024 to 1074 inclusive, certificated in all categories. To ensure that the passenger door latch mechanism and associated fittings properly latch the door, accomplish the following, unless already accomplished.

1. Within the next 10 hours time in service after the effective date of this AD and thereafter at intervals not to exceed 25 hours time in service, perform the inspection of the interior handle and adjust, as necessary, in accordance with paragraph 2 of Canadair Alert Service Bulletin No. A600-0203 dated September 13, 1982.

2. Within the next 60 hours time in service after the effective date of this AD, modify the latch mechanism and associated components in accordance with paragraph 2.C. of the service bulletin. Accomplishment of this modification terminates the inspection requirements of paragraph 1. above.

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

4. 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 July 5, 1983.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_83-13-02.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
83-13-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes
Subject:
Door Latch Mechanism Assembly
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/05/1983
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: 83-13-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4670

AD NUMBER:   83-13-02

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

ACTION:  

SUMMARY:  

DATES:   Effective July 5, 1983.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   83-13-02 CANADAIR: Amendment 39-4670. Applies to Model CL-600-1A11 airplanes, serial numbers 1024 to 1074 inclusive, certificated in all categories. To ensure that the passenger door latch mechanism and associated fittings properly latch the door, accomplish the following, unless already accomplished.

1. Within the next 10 hours time in service after the effective date of this AD and thereafter at intervals not to exceed 25 hours time in service, perform the inspection of the interior handle and adjust, as necessary, in accordance with paragraph 2 of Canadair Alert Service Bulletin No. A600-0203 dated September 13, 1982.

2. Within the next 60 hours time in service after the effective date of this AD, modify the latch mechanism and associated components in accordance with paragraph 2.C. of the service bulletin. Accomplishment of this modification terminates the inspection requirements of paragraph 1. above.

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

4. 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 July 5, 1983.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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