AD 82-18-03
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | CL-600-1A11 (CL-600) | Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes |
Unsafe Condition
The breakout forces of the rudder anti-jam mechanisms (Part Number 600-90450) may be outside acceptable limits, which could result in uncommanded rudder movement or jamming.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Measure the anti-jam mechanism breakout forces and re-rig if necessary per Canadair Alert Service Bulletin A600-0030, Revision 1. Alternate means of compliance may be used if approved by the FAA. Special flight permits may be issued under FAR 21.197 and 21.199.
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Compliance Time
within the next 50 hours time in service
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Affected Aircraft
Bombardier Inc. Model CL-600-1A11 (CL-600), serial numbers 1002 and subsequent
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Federal Register Abstract
Anti-Jam Mechanisms
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_82-18-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 82-18-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes Subject: Anti-Jam Mechanisms Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/01/1982 Make: Bombardier Inc. Model: CL-600-1A11 (CL-600) Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 82-18-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4442 AD NUMBER: 82-18-03 SUBJECT HEADING: Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes ACTION: SUMMARY: DATES: Effective September 1, 1982. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 82-18-03 CANADAIR: Amendment 39-4442. Applies to Canadair Model CL-600-1A11 airplanes, serial numbers 1002 and subsequent, certificated in all categories. Compliance is required within the next 50 hours time in service. To ensure that the breakout forces of the two rudder anti-jam mechanisms (Part Number 600-90450) are within acceptable limits, accomplish the following if not already accomplished: 1. Measure the anti-jam mechanism breakout forces and re-rig, if necessary, in accordance with Canadair Alert Service Bulletin A600-0030, Revision 1, dated November 10, 1981. 2. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Mountain Region. 3. 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. 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). This amendment becomes effective September 1, 1982. FOOTER:
Document Text
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AD Final Rules - DRS_82-18-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 82-18-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes Subject: Anti-Jam Mechanisms Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/01/1982 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: 82-18-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4442 AD NUMBER: 82-18-03 SUBJECT HEADING: Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes ACTION: SUMMARY: DATES: Effective September 1, 1982. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 82-18-03 CANADAIR: Amendment 39-4442. Applies to Canadair Model CL-600-1A11 airplanes, serial numbers 1002 and subsequent, certificated in all categories. Compliance is required within the next 50 hours time in service. To ensure that the breakout forces of the two rudder anti-jam mechanisms (Part Number 600-90450) are within acceptable limits, accomplish the following if not already accomplished: 1. Measure the anti-jam mechanism breakout forces and re-rig, if necessary, in accordance with Canadair Alert Service Bulletin A600-0030, Revision 1, dated November 10, 1981. 2. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Mountain Region. 3. 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. 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). This amendment becomes effective September 1, 1982. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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