AD 77-09-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | CL-215-1A10 | Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes |
Unsafe Condition
Structural failure of the nose landing gear door closing rods, P/N 215-85009, and the sequencing redundancy mechanism rod, P/N 215-85026, which could compromise structural integrity.
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Required Actions
Inspect and rework in accordance with Canadair Service Information Circular No. 101-CL-215 dated May 6, 1975, or an equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.
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Compliance Time
Compliance is required as indicated unless already accomplished. For aircraft in service 12 months or more, compliance is required and flight operations are restricted to land operations until compliance. For aircraft in service less than 12 months, compliance is required before achieving 12 months in service.
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Affected Aircraft
Canadair Model CL-215-1A10 airplanes, Serial Numbers 1001 to 1040 inclusive.
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Federal Register Abstract
Nose Landing Gear
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_77-09-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 77-09-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes Subject: Nose Landing Gear Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/09/1977 Make: Bombardier Inc. Model: CL-215-1A10 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 77-09-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2886 AD NUMBER: 77-09-05 SUBJECT HEADING: Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes ACTION: SUMMARY: DATES: Effective May 9, 1977. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 77-09-05 CANADAIR: Amendment 39-2886. Applies to Canadair CL-215-1A10 airplanes, Serial Numbers 1001 to 1040 inclusive, in all categories. Compliance is required as indicated unless already accomplished. To assure the structural integrity of the nose landing gear door closing rods, P/N 215- 85009, and the sequencing redundancy mechanism rod, P/N 215-85026, accomplish the following: (a) On aircraft that have been in service for 12 months or more, compliance with paragraph (c) is required and flight operations are restricted to land operations until compliance is shown. (b) On aircraft that have been in service less than 12 months, compliance with paragraph (c) is required before achieving 12 months in service. (c) Inspect and rework in accordance with Canadair Service Information Circular No. 101-CL-215 dated May 6, 1975, or an equivalent method of compliance. A later revision and an equivalent method of compliance must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region. (d) Upon request, with substantiating data submitted through an FAA Maintenance Inspector, the compliance time specified in this AD may be increased by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region. This amendment becomes effective May 9, 1977. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_77-09-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 77-09-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes Subject: Nose Landing Gear Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/09/1977 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: 77-09-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2886 AD NUMBER: 77-09-05 SUBJECT HEADING: Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes ACTION: SUMMARY: DATES: Effective May 9, 1977. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 77-09-05 CANADAIR: Amendment 39-2886. Applies to Canadair CL-215-1A10 airplanes, Serial Numbers 1001 to 1040 inclusive, in all categories. Compliance is required as indicated unless already accomplished. To assure the structural integrity of the nose landing gear door closing rods, P/N 215- 85009, and the sequencing redundancy mechanism rod, P/N 215-85026, accomplish the following: (a) On aircraft that have been in service for 12 months or more, compliance with paragraph (c) is required and flight operations are restricted to land operations until compliance is shown. (b) On aircraft that have been in service less than 12 months, compliance with paragraph (c) is required before achieving 12 months in service. (c) Inspect and rework in accordance with Canadair Service Information Circular No. 101-CL-215 dated May 6, 1975, or an equivalent method of compliance. A later revision and an equivalent method of compliance must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region. (d) Upon request, with substantiating data submitted through an FAA Maintenance Inspector, the compliance time specified in this AD may be increased by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region. This amendment becomes effective May 9, 1977. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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