AD 70-15-03

final rule

Airworthiness Directives: BEECH Models 23, A23, A23A, B23, A23-24 and A23-19 and 19A Airplanes

AD Number
70-15-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 19A Airworthiness Directives: BEECH Models 23, A23, A23A, B23, A23-24 and A23-19 and 19A Airplanes
aircraft Textron Aviation Inc. 23 Airworthiness Directives: BEECH Models 23, A23, A23A, B23, A23-24 and A23-19 and 19A Airplanes
aircraft Textron Aviation Inc. A23 Airworthiness Directives: BEECH Models 23, A23, A23A, B23, A23-24 and A23-19 and 19A Airplanes
aircraft Textron Aviation Inc. A23-19 Airworthiness Directives: BEECH Models 23, A23, A23A, B23, A23-24 and A23-19 and 19A Airplanes
aircraft Textron Aviation Inc. A23-24 Airworthiness Directives: BEECH Models 23, A23, A23A, B23, A23-24 and A23-19 and 19A Airplanes
aircraft Textron Aviation Inc. A23A Airworthiness Directives: BEECH Models 23, A23, A23A, B23, A23-24 and A23-19 and 19A Airplanes
aircraft Textron Aviation Inc. B23 Airworthiness Directives: BEECH Models 23, A23, A23A, B23, A23-24 and A23-19 and 19A Airplanes

Unsafe Condition

Stiff operation, binding, and seizing of Beech P/N 169-920000-127 fuel selector valve assembly

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

Required Actions

Modify the fuel selector valve assembly in accordance with Beechcraft Service Instructions No. 0364-289 or later FAA approved revision, or an equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

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

Compliance Time

Within 25 hours' time in service after the effective date of this AD

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

Affected Aircraft

BEECH Models 23, A23, A23A, B23 (Serial Numbers M-1 through M-1162); A23-24 (Serial Numbers MA-1 through MA-333); and A23-19 and 19A (Serial Numbers MB-1 through MB-392)

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

Federal Register Abstract

Fuel Selector Valve

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_70-15-03.html
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AD Number:
70-15-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives: BEECH Models 23, A23, A23A, B23, A23-24 and A23-19 and 19A Airplanes
Subject:
Fuel Selector Valve
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/21/1970
Make:
Textron Aviation Inc.
Model:
19A | 23 | A23 | A23-19 | A23-24 | A23A | B23
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: 70-15-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1037

AD NUMBER:   70-15-03

SUBJECT HEADING:   Airworthiness Directives: BEECH Models 23, A23, A23A, B23, A23-24 and A23-19 and 19A Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective July 21, 1970.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
70-15-03 BEECH: Amdt. 39-1037. Applies to Models 23, A23, A23A and B23 (Serial Numbers M-1 through M-1162); A23-24 (Serial Numbers MA-1 through MA-333); and A23-19 and 19A (Serial Numbers MB-1 through MB-392) Airplanes.

Compliance: Required as indicated, unless already accomplished.

To prevent stiff operation, binding and seizing of Beech P/N 169-920000-127 fuel selector valve assembly, accomplish the following:

Within 25 hours' time in service after the effective date of this AD, modify Beech P/N 169-920000-127 fuel selector valve assembly in accordance with Beechcraft Service Instructions No. 0364-289, or later FAA approved revision, or an equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

This amendment becomes effective July 21, 1970.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_70-15-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
70-15-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives: BEECH Models 23, A23, A23A, B23, A23-24 and A23-19 and 19A Airplanes
Subject:
Fuel Selector Valve
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/21/1970
Make:
Textron Aviation Inc.
Model:
19A | 23 | A23 | A23-19 | A23-24 | A23A | B23
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: 70-15-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1037

AD NUMBER:   70-15-03

SUBJECT HEADING:   Airworthiness Directives: BEECH Models 23, A23, A23A, B23, A23-24 and A23-19 and 19A Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective July 21, 1970.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
70-15-03 BEECH: Amdt. 39-1037. Applies to Models 23, A23, A23A and B23 (Serial Numbers M-1 through M-1162); A23-24 (Serial Numbers MA-1 through MA-333); and A23-19 and 19A (Serial Numbers MB-1 through MB-392) Airplanes.

Compliance: Required as indicated, unless already accomplished.

To prevent stiff operation, binding and seizing of Beech P/N 169-920000-127 fuel selector valve assembly, accomplish the following:

Within 25 hours' time in service after the effective date of this AD, modify Beech P/N 169-920000-127 fuel selector valve assembly in accordance with Beechcraft Service Instructions No. 0364-289, or later FAA approved revision, or an equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

This amendment becomes effective July 21, 1970.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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