AD 61-16-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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.
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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.
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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
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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)
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Federal Register Abstract
Fuel Selector Valve Handles
Applicability Source Text
Show captured applicability text from the source AD
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Make: Piper Aircraft Inc. Model: PA-24 | PA-24-250 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: AIR-700: Compliance & Airworthiness Division Office of Primary Responsibility: AIR-720: Operational Safety Branch CFR Part Reference: Part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:
Document Text
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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
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