AD 56-04-02

final rule

CONVAIR Models 240 and 340 Aircraft

AD Number
56-04-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Kelowna Flightcraft R & D Ltd. 240 Series CONVAIR Models 240 and 340 Aircraft
aircraft Kelowna Flightcraft R & D Ltd. 340 CONVAIR Models 240 and 340 Aircraft

Unsafe Condition

A recent accident involving a nacelle fire highlighted the need for additional fire protection in the wheel well area (zone 3), specifically addressing aluminum alloy fuel supply lines, flexible hose assemblies, propeller pump suction lines, oil hose assemblies, and micarta pulleys which could contribute to fire hazards.

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

Required Actions

Replace aluminum alloy engine fuel supply lines, sleeves, nuts, and tube unions with steel lines in the wheel well area (zone 3). Replace flexible hose assemblies with steel tubing or fireproof flexible lines. Replace aluminum alloy propeller pump suction lines with steel lines. Protect oil hose assemblies with asbestos sleeves or equivalent. Replace micarta pulleys with aluminum alloy pulleys.

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

Compliance Time

Not later than February 1, 1957, for Model 240 and August 1, 1957, for Model 340.

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

Affected Aircraft

CONVAIR Models 240 and 340 Aircraft, all serial numbers.

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

Federal Register Abstract

Fuel Supply Lines

Applicability Source Text

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AD Final Rules - DRS_56-04-02.html
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Details
AD Number:
56-04-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
CONVAIR Models 240 and 340 Aircraft
Subject:
Fuel Supply Lines
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Kelowna Flightcraft R & D Ltd.
Model:
240 Series | 340
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Superseded AD: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Superseded By: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: 56-04-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   56-04-02

SUBJECT HEADING:   CONVAIR Models 240 and 340 Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
56-04-02 CONVAIR: Applies to All 240 and 340 Aircraft.

Compliance required as soon as possible but not later than February 1, 1957, for Model 240 and August 1, 1957, for Model 340.

As a result of a recent accident involving a nacelle fire, additional fire protection for the nacelle is required.

The following changes or equivalent must be made to accomplish the above:

1. Replace aluminum alloy engine fuel supply lines, and sleeves, nuts and tube unions, with steel lines in the wheel well area (zone 3), except for lines and fittings outboard of the main landing gear beam. This does not apply to lines and fittings between cross-feed valves.

2. Replace present flexible hose assemblies in the engine fuel supply system in the wheel well area (zone 3), including AN fittings, with steel tubing and/or fireproof flexible lines, except for lines and fittings outboard of the main landing gear beam. Flexible lines qualifying as fireproof may incorporate either steel or aluminum fittings.

3. (a) CV-340 airplanes only. Replace aluminum alloy propeller pump suction line in left-hand nacelle wheel well (zone 3) with a steel line.

(b) CV-240 airplanes only. Replace aluminum alloy propeller pump suction line in wheel well area (zone 3) with a steel line. (Both nacelles.) (Original flexible hose connections will be satisfactory if provided with a steel liner.)

4. Protect existing oil hose assemblies in wheel well area (zone 3) with asbestos sleeves or equivalent.

5. Replace all micarta pulleys in wheel well area (zone 3) with aluminum alloy pulleys.
(Convair Service Bulletins Numbers 240-467 and 340-167 cover items 1 through 4. Convair Service Bulletins Numbers 240-468 and 340-166 cover item 5. These bulletins also contain some items which are not mandatory but are recommended.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_56-04-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
56-04-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
CONVAIR Models 240 and 340 Aircraft
Subject:
Fuel Supply Lines
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Kelowna Flightcraft R & D Ltd.
Model:
240 Series | 340
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: 56-04-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   56-04-02

SUBJECT HEADING:   CONVAIR Models 240 and 340 Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
56-04-02 CONVAIR: Applies to All 240 and 340 Aircraft.

Compliance required as soon as possible but not later than February 1, 1957, for Model 240 and August 1, 1957, for Model 340.

As a result of a recent accident involving a nacelle fire, additional fire protection for the nacelle is required.

The following changes or equivalent must be made to accomplish the above:

1. Replace aluminum alloy engine fuel supply lines, and sleeves, nuts and tube unions, with steel lines in the wheel well area (zone 3), except for lines and fittings outboard of the main landing gear beam. This does not apply to lines and fittings between cross-feed valves.

2. Replace present flexible hose assemblies in the engine fuel supply system in the wheel well area (zone 3), including AN fittings, with steel tubing and/or fireproof flexible lines, except for lines and fittings outboard of the main landing gear beam. Flexible lines qualifying as fireproof may incorporate either steel or aluminum fittings.

3. (a) CV-340 airplanes only. Replace aluminum alloy propeller pump suction line in left-hand nacelle wheel well (zone 3) with a steel line.

(b) CV-240 airplanes only. Replace aluminum alloy propeller pump suction line in wheel well area (zone 3) with a steel line. (Both nacelles.) (Original flexible hose connections will be satisfactory if provided with a steel liner.)

4. Protect existing oil hose assemblies in wheel well area (zone 3) with asbestos sleeves or equivalent.

5. Replace all micarta pulleys in wheel well area (zone 3) with aluminum alloy pulleys.
(Convair Service Bulletins Numbers 240-467 and 340-167 cover items 1 through 4. Convair Service Bulletins Numbers 240-468 and 340-166 cover item 5. These bulletins also contain some items which are not mandatory but are recommended.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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