AD 75-12-02

final rule

Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes

AD Number
75-12-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
aircraft Bombardier Inc. CL-215-1A10 Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes

Unsafe Condition

Incorrect connection to the engine Firex bottles could occur, which may preclude proper operation of the engine fire suppression system.

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

Required Actions

Modify the routing of the wire harness to the engine Firex bottles in accordance with Canadair Service Information Circular No. 66-CL-215, Revision A, dated August 13, 1974, or an equivalent modification approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

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

Compliance Time

next twenty-five hours' time in service after the effective date of this AD unless already accomplished

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

Affected Aircraft

Canadair Model CL-215-1A10 airplanes certificated in all categories.

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

Federal Register Abstract

Engine Fire Bottles

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_75-12-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-12-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes
Subject:
Engine Fire Bottles
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/30/1975
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Superseded AD: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Superseded By: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: 75-12-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2220

AD NUMBER:   75-12-02

SUBJECT HEADING:   Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective May 30, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-12-02 CANADAIR: Amendment 39-2220. Applies to Canadair CL-215-1A10 airplanes certificated in all categories.

Compliance required with the next twenty-five hours' time in service after the effective date of this AD unless already accomplished.

To preclude the possibility of incorrect connection being made to the engine Firex bottles, accomplish the following:

Modify the routing of the wire harness to the engine Firex bottles in accordance with Canadair Service Information Circular No. 66-CL-215, Revision A, dated August 13, 1974, or an equivalent modification approved by Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

This amendment is effective May 30, 1975.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_75-12-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-12-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes
Subject:
Engine Fire Bottles
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/30/1975
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: 75-12-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2220

AD NUMBER:   75-12-02

SUBJECT HEADING:   Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective May 30, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-12-02 CANADAIR: Amendment 39-2220. Applies to Canadair CL-215-1A10 airplanes certificated in all categories.

Compliance required with the next twenty-five hours' time in service after the effective date of this AD unless already accomplished.

To preclude the possibility of incorrect connection being made to the engine Firex bottles, accomplish the following:

Modify the routing of the wire harness to the engine Firex bottles in accordance with Canadair Service Information Circular No. 66-CL-215, Revision A, dated August 13, 1974, or an equivalent modification approved by Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

This amendment is effective May 30, 1975.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.