AD 72-15-04

final rule

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

AD Number
72-15-04
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

Flame propagation in the engine fire zone due to unmodified oil system and hydraulic system hoses.

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

Required Actions

Modify the oil system and hydraulic system hoses in accordance with Canadair Service Bulletins CL-215-138 (rev. A or later) and CL-215-140 (or later approved revisions).

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

Compliance Time

within the next 125 hours' time in service after the effective date of this AD

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

Affected Aircraft

Bombardier Inc. Model CL-215-1A10 airplanes with serial numbers 1005, 1006, 1010, 1011, 1013 through 1018, 1021, and 1023 through 1030.

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

Federal Register Abstract

Flame Propagation In Engine Fire Zone

Applicability Source Text

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AD Final Rules - DRS_72-15-04.html
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AD Number:
72-15-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes
Subject:
Flame Propagation In Engine Fire Zone
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/25/1972
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Superseded AD: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Superseded By: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: 72-15-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1485

AD NUMBER:   72-15-04

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

ACTION:  

SUMMARY:  

DATES:   Effective July 25, 1972.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
72-15-04 CANADAIR: Amdt. 39-1485. Applies to Canadair Limited Type CL-215-1A10 airplanes, Serial Nos. 1005, 1006, 1010, 1011, 1013 through 1018, 1021, and 1023 through 1030.

Compliance required within the next 125 hours' time in service, unless already accomplished, after the effective date of this AD. To reduce the risk of flame propagation in the event of a fire in the engine fire zone, modify the oil system and hydraulic system hoses in accordance with the instructions and effectivities listed in the following Canadair Service Bulletins or an equivalent modification approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

(a) Canadair Service Bulletin CL-215-138 dated February 2, 1971, and revision "A" dated April 23, 1971 or later approved revision.

(b) Canadair Service Bulletin CL-215-140 dated January 18, 1971 or later approved revision.

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 is effective July 25, 1972.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_72-15-04.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
72-15-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes
Subject:
Flame Propagation In Engine Fire Zone
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/25/1972
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: 72-15-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1485

AD NUMBER:   72-15-04

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

ACTION:  

SUMMARY:  

DATES:   Effective July 25, 1972.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
72-15-04 CANADAIR: Amdt. 39-1485. Applies to Canadair Limited Type CL-215-1A10 airplanes, Serial Nos. 1005, 1006, 1010, 1011, 1013 through 1018, 1021, and 1023 through 1030.

Compliance required within the next 125 hours' time in service, unless already accomplished, after the effective date of this AD. To reduce the risk of flame propagation in the event of a fire in the engine fire zone, modify the oil system and hydraulic system hoses in accordance with the instructions and effectivities listed in the following Canadair Service Bulletins or an equivalent modification approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

(a) Canadair Service Bulletin CL-215-138 dated February 2, 1971, and revision "A" dated April 23, 1971 or later approved revision.

(b) Canadair Service Bulletin CL-215-140 dated January 18, 1971 or later approved revision.

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 is effective July 25, 1972.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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