AD 64-06-01

final rule

Airworthiness Directives; Beech Model 23 Aircraft

AD Number
64-06-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
Federal Register: March 11, 1964

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 23 Airworthiness Directives; Beech Model 23 Aircraft

Unsafe Condition

Failures of the cabin heater/muffler weld assembly, Beech P/N 169-950010-21, have occurred. Such failures can cause hazardous quantities of carbon monoxide to enter the cabin when cabin heat is used.

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

Required Actions

Install a stainless steel dam around the exhaust tube between the muffler assembly and heater shroud assembly in accordance with Beechcraft Service Bulletin No. 64-1 dated January 13, 1964; or render the cabin heat and windshield defrost system inoperative by positively securing in the closed position the sliding doors of both the cabin heat and the defrost valves in the airplane firewall.

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

Compliance Time

within 10 hours' time in service after the effective date of this AD, unless already accomplished

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

Affected Aircraft

All Model 23 Aircraft Prior to Serial Number M-555 Except Serial Number M-1

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

Federal Register Abstract

Cabin Heater/Muffler Weld Assembly

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_64-06-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
64-06-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Beech Model 23 Aircraft
Subject:
Cabin Heater/Muffler Weld Assembly
Status:
Current
Citation:
Federal Register: March 11, 1964
Citation Publish Date:
03/11/1964
Effective Date:
03/17/1964
Make:
Textron Aviation Inc.
Model:
23
Product Type:
Aircraft
Product Subtype:
Small 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Superseded AD: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Superseded By: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: 64-06-01
CITATION:   [Federal Register: March 11, 1964]

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   64-06-01

SUBJECT HEADING:   Airworthiness Directives; Beech Model 23 Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective March 17, 1964.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
64-06-01 BEECH: Amdt. 703 Part 507 Federal Register March 11, 1964. Applies to All Model 23 Aircraft Prior to Serial Number M-555 Except Serial Number M-1.

Compliance required within 10 hours' time in service after the effective date of this AD, unless already accomplished.

Failures of the cabin heater/muffler weld assembly, Beech P/N 169-950010-21, have occurred. Such failures can cause hazardous quantities of carbon monoxide to enter the cabin when cabin heat is used. To preclude carbon monoxide contamination of cabin air, accomplish either of the following:

(a) Install a stainless steel dam around the exhaust tube between the muffler assembly and heater shroud assembly in accordance with Beechcraft Service Bulletin No. 64-1 dated January 13, 1964; or

(b) Render the cabin heat and windshield defrost system inoperative by positively securing in the closed position the sliding doors of both the cabin heat and the defrost valves in the airplane firewall.

This directive effective March 17, 1964.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_64-06-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
64-06-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Beech Model 23 Aircraft
Subject:
Cabin Heater/Muffler Weld Assembly
Status:
Current
Citation:
Federal Register: March 11, 1964
Citation Publish Date:
03/11/1964
Effective Date:
03/17/1964
Make:
Textron Aviation Inc.
Model:
23
Product Type:
Aircraft
Product Subtype:
Small 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: 64-06-01
CITATION:   [Federal Register: March 11, 1964]

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   64-06-01

SUBJECT HEADING:   Airworthiness Directives; Beech Model 23 Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective March 17, 1964.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
64-06-01 BEECH: Amdt. 703 Part 507 Federal Register March 11, 1964. Applies to All Model 23 Aircraft Prior to Serial Number M-555 Except Serial Number M-1.

Compliance required within 10 hours' time in service after the effective date of this AD, unless already accomplished.

Failures of the cabin heater/muffler weld assembly, Beech P/N 169-950010-21, have occurred. Such failures can cause hazardous quantities of carbon monoxide to enter the cabin when cabin heat is used. To preclude carbon monoxide contamination of cabin air, accomplish either of the following:

(a) Install a stainless steel dam around the exhaust tube between the muffler assembly and heater shroud assembly in accordance with Beechcraft Service Bulletin No. 64-1 dated January 13, 1964; or

(b) Render the cabin heat and windshield defrost system inoperative by positively securing in the closed position the sliding doors of both the cabin heat and the defrost valves in the airplane firewall.

This directive effective March 17, 1964.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.