AD 67-19-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Piper Aircraft Inc. | PA-30 | Airworthiness Directives; Piper Model PA-30 Airplanes |
Unsafe Condition
Cracking of the oxygen cylinder mounting channels and rubbing of the rudder control cable on the oxygen cylinder rear retaining strap.
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Required Actions
Modify the oxygen cylinder mounting installation per Piper Kit No. 757094 or equivalent for serial numbers 30-853, 30-902 through 30-1454. Modify the oxygen cylinder rear retaining strap per Piper Service Bulletin No. 246 and remove rubber strip P/N 13945-85. Compliance time may be extended upon request with FAA approval.
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Compliance Time
within the next 25 hours' time in service after the effective date of this Airworthiness Directive
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Affected Aircraft
Piper Model PA-30 airplanes, serial numbers 30-853, 30-902 through 30-1470, with factory-installed oxygen systems or Piper Oxygen Kits 756981 or 757100.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Oxygen Cylinder Mounting Channels
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_67-19-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-19-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Piper Model PA-30 Airplanes Subject: Oxygen Cylinder Mounting Channels Status: Current Citation: Federal Register: June 2, 1967 Citation Publish Date: 06/02/1967 Effective Date: 06/07/1967 Make: Piper Aircraft Inc. Model: PA-30 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: AIR-700: Compliance & Airworthiness Division Office of Primary Responsibility: AIR-720: Operational Safety Branch CFR Part Reference: Part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: 67-19-05 CITATION: [Federal Register: June 2, 1967] PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-427 AD NUMBER: 67-19-05 SUBJECT HEADING: Airworthiness Directives; Piper Model PA-30 Airplanes ACTION: SUMMARY: DATES: Effective June 7, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-19-05 PIPER: Amdt. 39-427, Part 39, Federal Register June 2, 1967. Applies to Type PA-30 airplanes, Serial Numbers 30-853, 30-902 Through 30-1470, Which Incorporate Factory Installed Oxygen System or Piper Oxygen Kits 756981 or 757100. Compliance required within the next 25 hours' time in service after the effective date of this Airworthiness Directive, unless already accomplished. To prevent cracking of the oxygen cylinder mounting channels and prevent the rudder control cable from rubbing on the oxygen cylinder rear retaining strap, accomplish the following: (a) On airplanes, Serial Numbers 30-853, 30-902 through 30-1454, modify the oxygen cylinder mounting installation in accordance with the Installation Instructions contained in Piper Oxygen Cylinder Mounting Modification Kit No. 757094 or equivalent modification, approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region. (b) On all airplanes modify the Oxygen Cylinder Rear Retaining Strap P/N 758109 and remove the Rubber Strip P/N 13945-85 as shown on the sketch contained in Piper Service Bulletin No. 246, dated March 21, 1967, or equivalent modification approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region. (c) Upon request, with substantiating data submitted through an FAA maintenance inspector, compliance time may be increased by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region. (Piper Service Bulletin No. 236, dated December 29, 1966, also pertains to the subject of paragraph (a)). This amendment effective June 7, 1967. FOOTER:
Document Text
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AD Final Rules - DRS_67-19-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-19-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Piper Model PA-30 Airplanes Subject: Oxygen Cylinder Mounting Channels Status: Current Citation: Federal Register: June 2, 1967 Citation Publish Date: 06/02/1967 Effective Date: 06/07/1967 Make: Piper Aircraft Inc. Model: PA-30 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: 67-19-05 CITATION: [Federal Register: June 2, 1967] PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-427 AD NUMBER: 67-19-05 SUBJECT HEADING: Airworthiness Directives; Piper Model PA-30 Airplanes ACTION: SUMMARY: DATES: Effective June 7, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-19-05 PIPER: Amdt. 39-427, Part 39, Federal Register June 2, 1967. Applies to Type PA-30 airplanes, Serial Numbers 30-853, 30-902 Through 30-1470, Which Incorporate Factory Installed Oxygen System or Piper Oxygen Kits 756981 or 757100. Compliance required within the next 25 hours' time in service after the effective date of this Airworthiness Directive, unless already accomplished. To prevent cracking of the oxygen cylinder mounting channels and prevent the rudder control cable from rubbing on the oxygen cylinder rear retaining strap, accomplish the following: (a) On airplanes, Serial Numbers 30-853, 30-902 through 30-1454, modify the oxygen cylinder mounting installation in accordance with the Installation Instructions contained in Piper Oxygen Cylinder Mounting Modification Kit No. 757094 or equivalent modification, approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region. (b) On all airplanes modify the Oxygen Cylinder Rear Retaining Strap P/N 758109 and remove the Rubber Strip P/N 13945-85 as shown on the sketch contained in Piper Service Bulletin No. 246, dated March 21, 1967, or equivalent modification approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region. (c) Upon request, with substantiating data submitted through an FAA maintenance inspector, compliance time may be increased by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region. (Piper Service Bulletin No. 236, dated December 29, 1966, also pertains to the subject of paragraph (a)). This amendment effective June 7, 1967. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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