AD 70-01-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | CL-215-1A10 | Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes |
Unsafe Condition
Loss of chine spray strips due to cracks and/or deformation in left and right chine spray strips P/N 215-30058-2, -3 and their attaching bolts.
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Required Actions
Visually inspect left and right chine spray strips P/N 215-30058-2, -3 and their attaching bolts for cracks and/or deformation before further flight. Repeat inspections within 25 water scoop and drop sequences or before first flight each day, whichever occurs first. Replace cracked or deformed parts before further flight.
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Compliance Time
Prior to further flight
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Affected Aircraft
Bombardier Inc. Model CL-215-1A10 airplanes certificated in all categories utilized in seaplane operation.
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Federal Register Abstract
Chine Spray Strips
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_70-01-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 70-01-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes Subject: Chine Spray Strips Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/08/1970 Make: Bombardier Inc. Model: CL-215-1A10 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 70-01-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-1117 AD NUMBER: 70-01-05 SUBJECT HEADING: Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes ACTION: SUMMARY: DATES: Effective December 8, 1970. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 70-01-05 CANADAIR: Amdt. 39-900 as amended by Amendment 39-1117. Applies to CL-215-1A10 airplanes certificated in all categories utilized in seaplane operation. To prevent hazards associated with the loss of the chine spray strips, accomplish the following: (a) Prior to further flight visually inspect the left and right chine spray strips P/N 215-30058-2, -3 and the bolts attaching the strips to the hull for cracks and/or deformation. These inspections are to be repeated within 25 water scoop and drop sequences or before the first flight of each day of operation, whichever occurs first. Replace cracked or deformed parts before further flight, except that the airplane may be flown in accordance with FAR 21.197 to a base where the installation can be performed. (b) The inspection required by this AD constitute preventive maintenance and may be performed by persons authorized to perform preventive maintenance under FAR 43. (c) The compliance times of the repetitive inspections may be increased by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region, upon receipt of substantiating data submitted through an FAA Maintenance Inspector. (d) The repetitive inspection specified in (a) may be discontinued when the modification defined in Canadair Modification Summary Number IC-1510 and contained in Service Bulletin CL-215-51 has been incorporated, or an equivalent modification approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region, has been incorporated. Amendment 39-900 effective January 6, 1970. This Amendment 39-1117 is effective December 8, 1970. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_70-01-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 70-01-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes Subject: Chine Spray Strips Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/08/1970 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: 70-01-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-1117 AD NUMBER: 70-01-05 SUBJECT HEADING: Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes ACTION: SUMMARY: DATES: Effective December 8, 1970. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 70-01-05 CANADAIR: Amdt. 39-900 as amended by Amendment 39-1117. Applies to CL-215-1A10 airplanes certificated in all categories utilized in seaplane operation. To prevent hazards associated with the loss of the chine spray strips, accomplish the following: (a) Prior to further flight visually inspect the left and right chine spray strips P/N 215-30058-2, -3 and the bolts attaching the strips to the hull for cracks and/or deformation. These inspections are to be repeated within 25 water scoop and drop sequences or before the first flight of each day of operation, whichever occurs first. Replace cracked or deformed parts before further flight, except that the airplane may be flown in accordance with FAR 21.197 to a base where the installation can be performed. (b) The inspection required by this AD constitute preventive maintenance and may be performed by persons authorized to perform preventive maintenance under FAR 43. (c) The compliance times of the repetitive inspections may be increased by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region, upon receipt of substantiating data submitted through an FAA Maintenance Inspector. (d) The repetitive inspection specified in (a) may be discontinued when the modification defined in Canadair Modification Summary Number IC-1510 and contained in Service Bulletin CL-215-51 has been incorporated, or an equivalent modification approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region, has been incorporated. Amendment 39-900 effective January 6, 1970. This Amendment 39-1117 is effective December 8, 1970. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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