AD 61-16-06

final rule

Airworthiness Directives; Piper Models All PA-24 and PA-24 "250" Aircraft

AD Number
61-16-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
Federal Register: July 29, 1961
Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-24 Airworthiness Directives; Piper Models All PA-24 and PA-24 "250" Aircraft
aircraft Piper Aircraft Inc. PA-24-250 Airworthiness Directives; Piper Models All PA-24 and PA-24 "250" Aircraft

Unsafe Condition

The fuel selector valve handles can be reinstalled with incorrect indexing after disassembly, causing serious fuel system malfunctioning.

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

Required Actions

Replace four-sided valve shafts with Brittain P/N 4018-15 shafts (convex side modification) and verify proper indexing of handles relative to placards after reassembly.

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

Compliance Time

within the next 150 hours' time in service after the effective date or at the next disassembly of fuel selector valves, whichever occurs first

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

Affected Aircraft

Piper Aircraft Inc. models PA-24 and PA-24-250 aircraft modified with Brittain Wing Tip Fuel Tanks (STC SA4-1235 and SA4-1351)

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

Federal Register Abstract

Fuel Selector Valve Handles

Applicability Source Text

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Details
AD Number:
61-16-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Models All PA-24 and PA-24 "250" Aircraft
Subject:
Fuel Selector Valve Handles
Status:
Current
Citation:
Federal Register: July 29, 1961
Citation Publish Date:
07/29/1961
Effective Date:
08/31/1961
Make:
Piper Aircraft Inc.
Model:
PA-24 | PA-24-250
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Superseded AD: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Superseded By: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: 61-16-06
CITATION:   [Federal Register: July 29, 1961]

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   61-16-06

SUBJECT HEADING:   Airworthiness Directives; Piper Models All PA-24 and PA-24 "250" Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective August 31, 1961.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
61-16-06 PIPER: Amdt. 314 Part 507 Federal Register July 29, 1961. Applies to All PA- 24 and PA-24 "250" Aircraft Modified to Incorporate Brittain Wing Tip Fuel Tanks (Supplemental Type Certificates Nos. SA4-1235 and SA4-1351).

Compliance required within the next 150 hours' time in service after the effective date or at the next disassembly of fuel selector valves, whichever occurs first.

The fuel selector valve handles of aircraft equipped with Brittain wing tip fuel tanks can easily be reinstalled with incorrect indexing after the valves have been disassembled for servicing and lubrication. Incorrect indexing can cause serious fuel system malfunctioning and one accident resulting from this condition has been reported. To preclude future incorrect indexing of the fuel selector valve handles, the following must be accomplished:

(a) Remove any valve shafts with four flat sides at the handle end and replace with Brittain P/N 4018-15 shafts, or equivalent. The Brittain P/N 4018-15 shaft is identical to the original except that one of the four sides at the handle end has been modified to a convex shape.

(b) After reassembly and reinstallation of the selector valves, determine that the valve handles are properly indexed with respect to the selector valve placard.

(Brittain Aircraft Enterprises Service Letter No. 4000-1 dated April 26, 1961, covers this same subject.)

This directive effective August 31, 1961.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_61-16-06.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
61-16-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Models All PA-24 and PA-24 "250" Aircraft
Subject:
Fuel Selector Valve Handles
Status:
Current
Citation:
Federal Register: July 29, 1961
Citation Publish Date:
07/29/1961
Effective Date:
08/31/1961
Make:
Piper Aircraft Inc.
Model:
PA-24 | PA-24-250
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: 61-16-06
CITATION:   [Federal Register: July 29, 1961]

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   61-16-06

SUBJECT HEADING:   Airworthiness Directives; Piper Models All PA-24 and PA-24 "250" Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective August 31, 1961.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
61-16-06 PIPER: Amdt. 314 Part 507 Federal Register July 29, 1961. Applies to All PA- 24 and PA-24 "250" Aircraft Modified to Incorporate Brittain Wing Tip Fuel Tanks (Supplemental Type Certificates Nos. SA4-1235 and SA4-1351).

Compliance required within the next 150 hours' time in service after the effective date or at the next disassembly of fuel selector valves, whichever occurs first.

The fuel selector valve handles of aircraft equipped with Brittain wing tip fuel tanks can easily be reinstalled with incorrect indexing after the valves have been disassembled for servicing and lubrication. Incorrect indexing can cause serious fuel system malfunctioning and one accident resulting from this condition has been reported. To preclude future incorrect indexing of the fuel selector valve handles, the following must be accomplished:

(a) Remove any valve shafts with four flat sides at the handle end and replace with Brittain P/N 4018-15 shafts, or equivalent. The Brittain P/N 4018-15 shaft is identical to the original except that one of the four sides at the handle end has been modified to a convex shape.

(b) After reassembly and reinstallation of the selector valves, determine that the valve handles are properly indexed with respect to the selector valve placard.

(Brittain Aircraft Enterprises Service Letter No. 4000-1 dated April 26, 1961, covers this same subject.)

This directive effective August 31, 1961.

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.