AD 49-43-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Kelowna Flightcraft R & D Ltd. | 240 Series | CONVAIR Model 240 Aircraft |
Unsafe Condition
Cracks or burned areas in the corrugated augmenter tube may lead to a possible fire hazard.
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Required Actions
Inspect the corrugated augmenter tube for cracks or burned areas immediately and each day thereafter using an extension mirror and light or equivalent means. Inspect the tube from both front and rear ends during each No. 1 inspection. Replace cracked or burned tubes unless defects meet specific allowable limits (cracks less than 3/4-inch long, no more than three cracks, and no two within 6 inches).
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Compliance Time
Compliance required as noted below: To be accomplished immediately and each day thereafter; and at each No. 1 inspection.
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Affected Aircraft
CONVAIR Model 240 Aircraft with Muff Type Augmenter Installation.
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Federal Register Abstract
Augmenter Tube
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_49-43-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 49-43-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: CONVAIR Model 240 Aircraft Subject: Augmenter Tube Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Kelowna Flightcraft R & D Ltd. Model: 240 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 49-43-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 49-43-01 SUBJECT HEADING: CONVAIR Model 240 Aircraft ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 49-43-01 CONVAIR: Applies to All Model 240 Aircraft With Muff Type Augmenter Installation. Compliance required as noted below. 1. To be accomplished immediately and each day thereafter: To avoid a possible fire hazard inspect corrugated augmenter tube for cracks or burned areas. This inspection is to be conducted from the rear end of the augmenter by means of an extension mirror and light, or equivalent means. 2. To be accomplished at each No. 1 inspection. Inspect the augmenter tube from both the front and rear ends for cracks or burned areas as described above. 3. Cracked or burned augmenters are to be replaced immediately unless the defects fall within the following limits: (a) Augmenter tubes which are found to have a crack, or cracks, in the outer shell may be flown in scheduled operation to a base station for replacement if the cracks are less than 3/4-inch long, no more than three cracks exist in the outer shell, and no two cracks are within 6 inches of each other. (b) Augmenter tubes found to have small cracks at the ends of seam welds on the wear band (doubler) at the forward end of the outer shell, are considered airworthy. Such cracks, when confined to the wear band, do not affect the safety of the tube and have shown no tendency to progress to a dangerous condition. 4. The inspections specified in 1 and 2 are not necessary on the following augmenter types: CVAC P/N 240-6220195 with any of the following forward augmenter sections: 240- 6221107, 240-622107-250, -252, -260, -262, -264, -268, -280, -290, -300, -314, -360. This supersedes AD 48-40-03. FOOTER:
Document Text
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AD Final Rules - DRS_49-43-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 49-43-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: CONVAIR Model 240 Aircraft Subject: Augmenter Tube Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Kelowna Flightcraft R & D Ltd. Model: 240 Series 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: 49-43-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 49-43-01 SUBJECT HEADING: CONVAIR Model 240 Aircraft ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 49-43-01 CONVAIR: Applies to All Model 240 Aircraft With Muff Type Augmenter Installation. Compliance required as noted below. 1. To be accomplished immediately and each day thereafter: To avoid a possible fire hazard inspect corrugated augmenter tube for cracks or burned areas. This inspection is to be conducted from the rear end of the augmenter by means of an extension mirror and light, or equivalent means. 2. To be accomplished at each No. 1 inspection. Inspect the augmenter tube from both the front and rear ends for cracks or burned areas as described above. 3. Cracked or burned augmenters are to be replaced immediately unless the defects fall within the following limits: (a) Augmenter tubes which are found to have a crack, or cracks, in the outer shell may be flown in scheduled operation to a base station for replacement if the cracks are less than 3/4-inch long, no more than three cracks exist in the outer shell, and no two cracks are within 6 inches of each other. (b) Augmenter tubes found to have small cracks at the ends of seam welds on the wear band (doubler) at the forward end of the outer shell, are considered airworthy. Such cracks, when confined to the wear band, do not affect the safety of the tube and have shown no tendency to progress to a dangerous condition. 4. The inspections specified in 1 and 2 are not necessary on the following augmenter types: CVAC P/N 240-6220195 with any of the following forward augmenter sections: 240- 6221107, 240-622107-250, -252, -260, -262, -264, -268, -280, -290, -300, -314, -360. This supersedes AD 48-40-03. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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