AD 80-12-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Piper Aircraft Inc. | PA-44-180 | Airworthiness Directives; Piper Model PA-44-180 Airplanes |
Unsafe Condition
Nose landing gear retraction during landing rollout or ground operations
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the nose landing gear downlock hook and bushing in accordance with Piper Service Bulletin No. 678 or equivalent manner approved by the FAA, and make appropriate maintenance record entry.
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Compliance Time
within the next 50 hours time in service after the effective date of this AD
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Affected Aircraft
Piper Model PA-44-180, Serial Numbers 44-7995001 through 44-8095020
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Federal Register Abstract
Nose Landing Gear
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_80-12-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 80-12-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Piper Model PA-44-180 Airplanes Subject: Nose Landing Gear Status: Current Citation: This information is not available. Citation Publish Date: 06/05/1980 Effective Date: 06/03/1980 Make: Piper Aircraft Inc. Model: PA-44-180 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: AIR-700: Compliance & Airworthiness Division Office of Primary Responsibility: AIR-720: Operational Safety Branch CFR Part Reference: Part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: 80-12-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-3783 AD NUMBER: 80-12-03 SUBJECT HEADING: Airworthiness Directives; Piper Model PA-44-180 Airplanes ACTION: SUMMARY: DATES: Effective June 3, 1980. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 80-12-03 PIPER AIRCRAFT CORPORATION: Amendment 39-3783. Applies to Model PA-44-180, Serial Numbers 44-7995001 through 44-8095020, airplanes certificated in all categories. Compliance is required within the next 50 hours time in service after the effective date of this AD, unless already accomplished. To prevent nose landing gear retraction during landing rollout or ground operations, accomplish the following: a. Replace the nose landing gear downlock hook and bushing in accordance with Piper Aircraft Corporation Service Bulletin No. 678, dated March 24, 1980, and Piper Service Kit No. 764-010V, or in an equivalent manner approved by the Chief, Engineering and Manufacturing Branch, FAA, Southern Region. b. Make appropriate maintenance record entry. This amendment becomes effective June 3, 1980. FOOTER:
Document Text
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AD Final Rules - DRS_80-12-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 80-12-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Piper Model PA-44-180 Airplanes Subject: Nose Landing Gear Status: Current Citation: This information is not available. Citation Publish Date: 06/05/1980 Effective Date: 06/03/1980 Make: Piper Aircraft Inc. Model: PA-44-180 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: 80-12-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-3783 AD NUMBER: 80-12-03 SUBJECT HEADING: Airworthiness Directives; Piper Model PA-44-180 Airplanes ACTION: SUMMARY: DATES: Effective June 3, 1980. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 80-12-03 PIPER AIRCRAFT CORPORATION: Amendment 39-3783. Applies to Model PA-44-180, Serial Numbers 44-7995001 through 44-8095020, airplanes certificated in all categories. Compliance is required within the next 50 hours time in service after the effective date of this AD, unless already accomplished. To prevent nose landing gear retraction during landing rollout or ground operations, accomplish the following: a. Replace the nose landing gear downlock hook and bushing in accordance with Piper Aircraft Corporation Service Bulletin No. 678, dated March 24, 1980, and Piper Service Kit No. 764-010V, or in an equivalent manner approved by the Chief, Engineering and Manufacturing Branch, FAA, Southern Region. b. Make appropriate maintenance record entry. This amendment becomes effective June 3, 1980. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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