AD 56-24-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Kelowna Flightcraft R & D Ltd. | 240 Series | CONVAIR Models 240, 340 and 440 Series Aircraft |
| aircraft | Kelowna Flightcraft R & D Ltd. | 340 | CONVAIR Models 240, 340 and 440 Series Aircraft |
| aircraft | Kelowna Flightcraft R & D Ltd. | 440 | CONVAIR Models 240, 340 and 440 Series Aircraft |
Unsafe Condition
Engine cylinder failures, specifically involving stud failures or flange failures of the No. 8 cylinder, can dislodge the cylinder and sever the feathering line, preventing propeller feathering and creating an additional fire hazard from oil being pumped onto the engine.
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Required Actions
Reroute the propeller feathering line between cylinders either by following Convair Service Bulletins (240-479, 340-205, 440-23) or route the line between front row cylinders, allowing adequate flexibility if passing over a rear row cylinder.
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Compliance Time
by September 1, 1957
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Affected Aircraft
CONVAIR Models 240, 340, and 440 Series Aircraft
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Federal Register Abstract
Cylinder
Applicability Source Text
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AD Final Rules - DRS_56-24-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 56-24-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: CONVAIR Models 240, 340 and 440 Series Aircraft Subject: Cylinder Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Kelowna Flightcraft R & D Ltd. Model: 240 Series | 340 | 440 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 56-24-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 56-24-01 SUBJECT HEADING: CONVAIR Models 240, 340 and 440 Series Aircraft ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 56-24-01 CONVAIR: Applies to All 240, 340 and 440 Series Aircraft. Compliance recommended at the next engine overhaul but required on all aircraft by September 1, 1957. Several cases of engine cylinder failures have occurred in which it was subsequently impossible to feather the propeller. The feathering line is presently routed over the top of the No. 8 cylinder and when this cylinder is dislodged, due to stud failures or flange failure, the feathering line is severed thus preventing feathering and causing an additional fire hazard from oil being pumped onto the engine. The record of cylinder failures from studs loosening or breaking indicates that the front row cylinders are mainly involved. To prevent loss of feathering control from such failures, either of the following actions is required: 1. The propeller feathering line is to be rerouted between cylinders. (Convair Service Bulletins Nos. 240-479, 340-205 and 440-23 cover an acceptable method of complying with this modification on Models 240, 340 and 440, respectively.) 2. The propeller feathering line is to be routed between cylinders on the front row of cylinders. It shall be acceptable for the line to pass over the top of a rear row cylinder provided there is adequate flexibility in the line assembly to allow for some displacement without breaking line or fittings in the event of a cylinder failure. FOOTER:
Document Text
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AD Final Rules - DRS_56-24-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 56-24-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: CONVAIR Models 240, 340 and 440 Series Aircraft Subject: Cylinder Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Kelowna Flightcraft R & D Ltd. Model: 240 Series | 340 | 440 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: 56-24-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 56-24-01 SUBJECT HEADING: CONVAIR Models 240, 340 and 440 Series Aircraft ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 56-24-01 CONVAIR: Applies to All 240, 340 and 440 Series Aircraft. Compliance recommended at the next engine overhaul but required on all aircraft by September 1, 1957. Several cases of engine cylinder failures have occurred in which it was subsequently impossible to feather the propeller. The feathering line is presently routed over the top of the No. 8 cylinder and when this cylinder is dislodged, due to stud failures or flange failure, the feathering line is severed thus preventing feathering and causing an additional fire hazard from oil being pumped onto the engine. The record of cylinder failures from studs loosening or breaking indicates that the front row cylinders are mainly involved. To prevent loss of feathering control from such failures, either of the following actions is required: 1. The propeller feathering line is to be rerouted between cylinders. (Convair Service Bulletins Nos. 240-479, 340-205 and 440-23 cover an acceptable method of complying with this modification on Models 240, 340 and 440, respectively.) 2. The propeller feathering line is to be routed between cylinders on the front row of cylinders. It shall be acceptable for the line to pass over the top of a rear row cylinder provided there is adequate flexibility in the line assembly to allow for some displacement without breaking line or fittings in the event of a cylinder failure. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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