AD 64-24-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Lavia Argentina S.A. (Laviasa) | PA-25-235 | Airworthiness Directives; Piper Model PA-25-235 Aircraft |
Unsafe Condition
Air leaks permit entrance of engine fumes into the cockpit in the area of the fuselage right main landing gear fittings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install seals, Piper Kit Number 756824 or FAA approved equivalent, at the front and rear right main landing gear fittings as indicated on the sketch of Piper Service Bulletin No. 221 dated August 27, 1964.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 50 hours' time in service after the effective date of this AD unless already accomplished
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Affected Aircraft
Piper Model PA-25-235 Aircraft, Serial Numbers 25-02, 25-2000 through 25-2931.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Fuselage Landing Gear Fitting Seals
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_64-24-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 64-24-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Piper Model PA-25-235 Aircraft Subject: Fuselage Landing Gear Fitting Seals Status: Current Citation: Federal Register: October 24, 1964 Citation Publish Date: 10/24/1964 Effective Date: 10/24/1964 Make: Lavia Argentina S.A. (Laviasa) Model: PA-25-235 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 64-24-05 CITATION: [Federal Register: October 24, 1964] PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 64-24-05 SUBJECT HEADING: Airworthiness Directives; Piper Model PA-25-235 Aircraft ACTION: SUMMARY: DATES: Effective October 24, 1964. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 64-24-05 PIPER: Amdt. 826 Part 507 Federal Register October 24, 1964. Applies to Model PA-25-235 Aircraft, Serial Numbers 25-02, 25-2000 through 25-2931. Compliance required within 50 hours' time in service after the effective date of this AD unless already accomplished. Air leaks, which permit entrance of engine fumes into the cockpit, exist in the area of the fuselage right main landing gear fittings. To correct this condition, accomplish the following: Install seals, Piper Kit Number 756824 or FAA approved equivalent, at the front and rear right main landing gear fittings as indicated on the sketch on the reverse side of Piper Service Bulletin No. 221 dated August 27, 1964. (Piper Service Bulletin No. 221 dated August 27, 1964, pertains to this same subject.) This directive effective October 24, 1964. FOOTER:
Document Text
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AD Final Rules - DRS_64-24-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 64-24-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Piper Model PA-25-235 Aircraft Subject: Fuselage Landing Gear Fitting Seals Status: Current Citation: Federal Register: October 24, 1964 Citation Publish Date: 10/24/1964 Effective Date: 10/24/1964 Make: Lavia Argentina S.A. (Laviasa) Model: PA-25-235 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 64-24-05 CITATION: [Federal Register: October 24, 1964] PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 64-24-05 SUBJECT HEADING: Airworthiness Directives; Piper Model PA-25-235 Aircraft ACTION: SUMMARY: DATES: Effective October 24, 1964. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 64-24-05 PIPER: Amdt. 826 Part 507 Federal Register October 24, 1964. Applies to Model PA-25-235 Aircraft, Serial Numbers 25-02, 25-2000 through 25-2931. Compliance required within 50 hours' time in service after the effective date of this AD unless already accomplished. Air leaks, which permit entrance of engine fumes into the cockpit, exist in the area of the fuselage right main landing gear fittings. To correct this condition, accomplish the following: Install seals, Piper Kit Number 756824 or FAA approved equivalent, at the front and rear right main landing gear fittings as indicated on the sketch on the reverse side of Piper Service Bulletin No. 221 dated August 27, 1964. (Piper Service Bulletin No. 221 dated August 27, 1964, pertains to this same subject.) This directive effective October 24, 1964. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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