AD 77-10-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | CL-215-1A10 | Airworthiness Directives; CANADAIR MODEL CL-215-1A10 Airplanes |
Unsafe Condition
Failure of the main landing gear actuator attachment fitting P/N 215-34014-1 and -2 could result in loss of main landing gear structural integrity.
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Required Actions
Inspect and alter main landing gear actuator attachment fitting P/N 215-34014-1 and -2 in accordance with Canadair Service Information Circular No. 136-CL-215, page 2 of 3 dated June 11, 1976, or an approved equivalent. Equivalent inspections and parts must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.
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Compliance Time
prior to U.S. Airworthiness certification
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Affected Aircraft
Canadair CL-215-1A10 Airplanes, Serial Numbers 1001 through 1040 and 1046 certificated in all categories that have not been altered in accordance with Canadair Service Information Circular No. 136-CL-215
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Federal Register Abstract
Main Landing Gear Actuator
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_77-10-14.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 77-10-14 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CANADAIR MODEL CL-215-1A10 Airplanes Subject: Main Landing Gear Actuator Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/26/1977 Make: Bombardier Inc. Model: CL-215-1A10 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 77-10-14 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2908 AD NUMBER: 77-10-14 SUBJECT HEADING: Airworthiness Directives; CANADAIR MODEL CL-215-1A10 Airplanes ACTION: SUMMARY: DATES: Effective May 26, 1977. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 77-10-14 CANADAIR: Amendment 39-2908. Applies to Canadair CL-215-1A10 Airplanes, Serial Numbers 1001 through 1040 and 1046 certificated in all categories that have not been altered in accordance with Canadair Service Information Circular No. 136-CL-215. Compliance required prior to U.S. Airworthiness certification. Inspect and alter main landing gear actuator attachment fitting P/N 215-34014-1 and -2 in accordance with Canadair Service Information Circular No. 136-CL-215, page 2 of 3 dated June 11, 1976, or an approved equivalent. Equivalent inspections and parts must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region. This amendment becomes effective May 26, 1977. FOOTER:
Document Text
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AD Final Rules - DRS_77-10-14.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 77-10-14 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CANADAIR MODEL CL-215-1A10 Airplanes Subject: Main Landing Gear Actuator Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/26/1977 Make: Bombardier Inc. Model: CL-215-1A10 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: 77-10-14 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2908 AD NUMBER: 77-10-14 SUBJECT HEADING: Airworthiness Directives; CANADAIR MODEL CL-215-1A10 Airplanes ACTION: SUMMARY: DATES: Effective May 26, 1977. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 77-10-14 CANADAIR: Amendment 39-2908. Applies to Canadair CL-215-1A10 Airplanes, Serial Numbers 1001 through 1040 and 1046 certificated in all categories that have not been altered in accordance with Canadair Service Information Circular No. 136-CL-215. Compliance required prior to U.S. Airworthiness certification. Inspect and alter main landing gear actuator attachment fitting P/N 215-34014-1 and -2 in accordance with Canadair Service Information Circular No. 136-CL-215, page 2 of 3 dated June 11, 1976, or an approved equivalent. Equivalent inspections and parts must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region. This amendment becomes effective May 26, 1977. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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