AD 67-30-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Piper Aircraft Inc. | PA-32-300 | Airworthiness Directives; Piper Models PA-32-300 Series and PA-32S-300 Series Airplanes |
| aircraft | Piper Aircraft Inc. | PA-32S-300 | Airworthiness Directives; Piper Models PA-32-300 Series and PA-32S-300 Series Airplanes |
Unsafe Condition
Possibility of restricting air flow through the engine air induction system due to the existing engine air inlet duct configuration.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the engine air inlet duct with parts and per instructions in Piper Modification Kit 760159. Compliance may be adjusted up to a maximum of 10 hours to coincide with annual or 100-hour inspections.
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 AD, unless already accomplished.
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Affected Aircraft
Piper Models PA-32-300 and PA-32S-300 Series Airplanes with serial numbers 32-15, 32-40000 through 32-40399.
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Federal Register Abstract
Engine Air Induction System
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_67-30-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-30-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Piper Models PA-32-300 Series and PA-32S-300 Series Airplanes Subject: Engine Air Induction System Status: Current Citation: This information is not available. Citation Publish Date: 12/28/1967 Effective Date: 12/22/1967 Make: Piper Aircraft Inc. Model: PA-32-300 | PA-32S-300 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: AIR-700: Compliance & Airworthiness Division Office of Primary Responsibility: AIR-720: Operational Safety Branch CFR Part Reference: Part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: Amdt. should be 39-526. https://www.govinfo.gov/content/pkg/FR-1967-12-28/pdf/FR-1967-12-28.pdf AIRWORTHINESS DIRECTIVES FINAL RULES: 67-30-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-508 AD NUMBER: 67-30-06 SUBJECT HEADING: Airworthiness Directives; Piper Models PA-32-300 Series and PA-32S-300 Series Airplanes ACTION: SUMMARY: DATES: Effective December 22, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-30-06 PIPER: Amdt. 39-508, Part 39, Federal Register November 8, 1967. Applies to Models PA-32-300, PA-32S-300 Series Airplanes. Serial Numbers 32-15, 32-40000 through 32- 40399. Compliance required within the next 50 hours' time in service after the effective date of this AD, unless already accomplished. To prevent the possibility of restricting air flow through the engine air induction system accomplish the following: (a) Replace the engine air inlet duct, Piper Part No. 457599 or 63633-50, with parts and per instructions contained in Piper Modification Kit 760159. (b) The compliance time may be adjusted up to a maximum of 10 hours to coincide with aircraft annual or 100-hour scheduled inspections. (c) Piper Service Bulletin No. 260 dated November 8, 1967, covers the same subject. Other means of compliance with the requirements of this directive may be utilized, if approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region. This amendment effective December 22, 1967. FOOTER:
Document Text
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AD Final Rules - DRS_67-30-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-30-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Piper Models PA-32-300 Series and PA-32S-300 Series Airplanes Subject: Engine Air Induction System Status: Current Citation: This information is not available. Citation Publish Date: 12/28/1967 Effective Date: 12/22/1967 Make: Piper Aircraft Inc. Model: PA-32-300 | PA-32S-300 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: Amdt. should be 39-526. https://www.govinfo.gov/content/pkg/FR-1967-12-28/pdf/FR-1967-12-28.pdf AIRWORTHINESS DIRECTIVES FINAL RULES: 67-30-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-508 AD NUMBER: 67-30-06 SUBJECT HEADING: Airworthiness Directives; Piper Models PA-32-300 Series and PA-32S-300 Series Airplanes ACTION: SUMMARY: DATES: Effective December 22, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-30-06 PIPER: Amdt. 39-508, Part 39, Federal Register November 8, 1967. Applies to Models PA-32-300, PA-32S-300 Series Airplanes. Serial Numbers 32-15, 32-40000 through 32- 40399. Compliance required within the next 50 hours' time in service after the effective date of this AD, unless already accomplished. To prevent the possibility of restricting air flow through the engine air induction system accomplish the following: (a) Replace the engine air inlet duct, Piper Part No. 457599 or 63633-50, with parts and per instructions contained in Piper Modification Kit 760159. (b) The compliance time may be adjusted up to a maximum of 10 hours to coincide with aircraft annual or 100-hour scheduled inspections. (c) Piper Service Bulletin No. 260 dated November 8, 1967, covers the same subject. Other means of compliance with the requirements of this directive may be utilized, if approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region. This amendment effective December 22, 1967. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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