AD 71-21-06

final rule

Airworthiness Directives; Piper Model PA 23-250 Airplanes

AD Number
71-21-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-23-250 (Navy UO-1) Airworthiness Directives; Piper Model PA 23-250 Airplanes

Unsafe Condition

Failure of the existing alternate air flexible duct (P/N 22502-65) could allow fire to pass through the engine firewall in the event of a powerplant fire.

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

Required Actions

Replace the existing alternate air flexible duct P/N 22502-65 with new fireproof duct P/N 48076-02, following Piper Service Bulletin 334 or an equivalent approved duct. Compliance may be requested to be extended by the FAA.

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

Compliance Time

within the next 50 hours' time in service after the effective date of this airworthiness directive unless already accomplished

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

Affected Aircraft

Piper Aircraft Inc. Model PA-23-250 (Navy UO-1) serial numbers 27-4053, 27-4226 through 27-4563 inclusive, 27-4565 through 27-4579 inclusive, 27-4581 through 27-4617 inclusive, 27-4619 through 27-4627 inclusive, 27-4630 through 27-4636 inclusive.

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

Federal Register Abstract

Engine Firewall Flex Duct

Applicability Source Text

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AD Final Rules - DRS_71-21-06.html
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AD Number:
71-21-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Model PA 23-250 Airplanes
Subject:
Engine Firewall Flex Duct
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
10/19/1971
Effective Date:
10/12/1971
Make:
Piper Aircraft Inc.
Model:
PA-23-250 (Navy UO-1)
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
AIR-700: Compliance & Airworthiness Division
Office of Primary Responsibility:
AIR-720: Operational Safety Branch
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 71-21-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1309

AD NUMBER:   71-21-06

SUBJECT HEADING:   Airworthiness Directives; Piper Model PA 23-250 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective October 12, 1971.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
71-21-06 PIPER: Amendment 39-1309. Applies to Turbocharged Type PA 23-250 airplanes Serial Numbers 27-4053, 27-4226 through 27-4563 inclusive, 27-4565 through 27-4579 inclusive, 27-4581 through 27-4617 inclusive, 27-4619 through 27-4627 inclusive, 27-4630 through 27-4636 inclusive.

Compliance required within the next 50 hours' time in service after the effective date of this airworthiness directive unless already accomplished.

To preclude the possibility of fire passing through the engine firewall, in the event of a powerplant fire, replace the existing alternate air flexible duct, P/N 22502-65, with new alternate air duct P/N 48076-02 (fireproof), in accordance with Piper Service Bulletin Number 334 dated 17 March 1971, or later approved revision, or replace with an equivalent alternate air duct approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.

Upon request with substantiating data submitted through an FAA maintenance inspector, the compliance time specified in this AD may be increased by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.

This amendment is effective October 12, 1971.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_71-21-06.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
71-21-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Model PA 23-250 Airplanes
Subject:
Engine Firewall Flex Duct
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
10/19/1971
Effective Date:
10/12/1971
Make:
Piper Aircraft Inc.
Model:
PA-23-250 (Navy UO-1)
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
AIR-700: Compliance & Airworthiness Division
Office of Primary Responsibility:
AIR-720: Operational Safety Branch
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 71-21-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1309

AD NUMBER:   71-21-06

SUBJECT HEADING:   Airworthiness Directives; Piper Model PA 23-250 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective October 12, 1971.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
71-21-06 PIPER: Amendment 39-1309. Applies to Turbocharged Type PA 23-250 airplanes Serial Numbers 27-4053, 27-4226 through 27-4563 inclusive, 27-4565 through 27-4579 inclusive, 27-4581 through 27-4617 inclusive, 27-4619 through 27-4627 inclusive, 27-4630 through 27-4636 inclusive.

Compliance required within the next 50 hours' time in service after the effective date of this airworthiness directive unless already accomplished.

To preclude the possibility of fire passing through the engine firewall, in the event of a powerplant fire, replace the existing alternate air flexible duct, P/N 22502-65, with new alternate air duct P/N 48076-02 (fireproof), in accordance with Piper Service Bulletin Number 334 dated 17 March 1971, or later approved revision, or replace with an equivalent alternate air duct approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.

Upon request with substantiating data submitted through an FAA maintenance inspector, the compliance time specified in this AD may be increased by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.

This amendment is effective October 12, 1971.

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.