AD 49-43-01

final rule

CONVAIR Model 240 Aircraft

AD Number
49-43-01
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 Model 240 Aircraft

Unsafe Condition

Cracks or burned areas in the corrugated augmenter tube may lead to a possible fire hazard.

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

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).

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

Compliance Time

Compliance required as noted below: To be accomplished immediately and each day thereafter; and at each No. 1 inspection.

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

Affected Aircraft

CONVAIR Model 240 Aircraft with Muff Type Augmenter Installation.

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

Federal Register Abstract

Augmenter Tube

Applicability Source Text

Show captured applicability text from the source AD
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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Superseded AD: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Superseded By: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

Show stored source text (verify against official source)
AD Final Rules - DRS_49-43-01.html
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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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