AD 88-25-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aerostar Aircraft Corporation | PA-60-601 (Aerostar 601) | Airworthiness Directives; PIPER (AEROSTAR) Models PA-60-601, PA-60-601P, PA-60-602P, PA-60-700P Airplanes |
| aircraft | Aerostar Aircraft Corporation | PA-60-601P (Aerostar 601P) | Airworthiness Directives; PIPER (AEROSTAR) Models PA-60-601, PA-60-601P, PA-60-602P, PA-60-700P Airplanes |
| aircraft | Aerostar Aircraft Corporation | PA-60-602P (Aerostar 602P) | Airworthiness Directives; PIPER (AEROSTAR) Models PA-60-601, PA-60-601P, PA-60-602P, PA-60-700P Airplanes |
| aircraft | Aerostar Aircraft Corporation | PA-60-700P (Aerostar 700P) | Airworthiness Directives; PIPER (AEROSTAR) Models PA-60-601, PA-60-601P, PA-60-602P, PA-60-700P Airplanes |
Unsafe Condition
Damage to the oil supply hoses could result in an in-flight fire, oil starvation and/or engine failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace and modify the engine fluid-carrying hoses and associated hardware in accordance with Piper Service Bulletins 761 (for applicable models except PA-60-700P) and 815 (for all affected models). Allow flight under FAR 21.197 to a location where this AD can be accomplished. Equivalent compliance may be approved by the Atlanta Aircraft Certification Office.
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 (AEROSTAR) Models PA-60-601 (S/N 61-0001-004 through 61-0880-8162157), PA-60-601P (S/N 61P-0157-001 through 61P-0860-8163455), PA-60-602P (S/N 62P-0750-8165001 and 62P-0861-8165002 through 60-8365010), PA-60-700P (S/N 60-8423001 through 60-8423025) airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Engine Fluid-Carrying Hoses
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_88-25-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 88-25-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; PIPER (AEROSTAR) Models PA-60-601, PA-60-601P, PA-60-602P, PA-60-700P Airplanes Subject: Engine Fluid-Carrying Hoses Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/26/1988 Make: Aerostar Aircraft Corporation Model: PA-60-601 (Aerostar 601) | PA-60-601P (Aerostar 601P) | PA-60-602P (Aerostar 602P) | PA-60-700P (Aer...Show more Product Type: Aircraft Product Subtype: Large 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: 88-25-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-6080 AD NUMBER: 88-25-02 SUBJECT HEADING: Airworthiness Directives; PIPER (AEROSTAR) Models PA-60-601, PA-60-601P, PA-60-602P, PA-60-700P Airplanes ACTION: SUMMARY: DATES: Effective December 26, 1988. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 88-25-02 PIPER (AEROSTAR): Amendment 39-6080. Applies to Models PA-60-601 equipped with an automatic waste gate controller per Retrofit Option 106 (S/N 61-0001-004 through 61-0334-111), PA-60-601 (S/N 61-0342-112 through 61-0880-8162157), PA-60-601P (S/N 61P-0157-001 through 61P-0860-8163455), PA-60-602P (S/N 62P-0750-8165001, and 62P-0861-8165002 through 60-8365010), PA-60-700P (S/N 60-8423001 through 60-8423025) airplanes certificated in any category. Compliance: Required within the next 50 hours time-in-service after the effective date of this AD unless already accomplished. To reduce the possibility of damage to the oil supply hoses which, if not corrected, could result in an in-flight fire, oil starvation and/or engine failure, accomplish the following: (a) For all the above applicable airplanes except Model PA-60-700P (S/N 60- 8423001 through 60-8423025) airplanes, replace and modify the engine fluid-carrying hoses and associated hardware in accordance with the instructions contained in Piper Service Bulletin (SB) No. 761, dated April 18, 1983, and Piper SB No. 815, dated January 3, 1986. (b) For Model PA-60-700P Aerostars (S/N 60-8423001 through 60- 8423025) airplanes replace and modify the engine fluid-carrying hoses and associated hardware in accordance with the instructions contained in Piper SB No. 815, dated January 3, 1986. (c) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished. (d) An equivalent means of compliance with this AD may be used if approved by the Manager, Atlanta Aircraft Certification Office, ACE-115A, Federal Aviation Administration, 1669 Phoenix Parkway, Suite 210C, Atlanta, Georgia 30349. All persons affected by this directive may obtain copies of the documents referred to herein upon request to Piper Aircraft Corporation, 2926 Piper Drive, Vero Beach, Florida 32960; or may examine these documents at the FAA, Office of the Assistant Chief Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106. This amendment, 39-6080, becomes effective on December 26, 1988. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_88-25-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 88-25-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; PIPER (AEROSTAR) Models PA-60-601, PA-60-601P, PA-60-602P, PA-60-700P Airplanes Subject: Engine Fluid-Carrying Hoses Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/26/1988 Make: Aerostar Aircraft Corporation Model: PA-60-601 (Aerostar 601) | PA-60-601P (Aerostar 601P) | PA-60-602P (Aerostar 602P) | PA-60-700P (Aer...Show more Product Type: Aircraft Product Subtype: Large 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: 88-25-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-6080 AD NUMBER: 88-25-02 SUBJECT HEADING: Airworthiness Directives; PIPER (AEROSTAR) Models PA-60-601, PA-60-601P, PA-60-602P, PA-60-700P Airplanes ACTION: SUMMARY: DATES: Effective December 26, 1988. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 88-25-02 PIPER (AEROSTAR): Amendment 39-6080. Applies to Models PA-60-601 equipped with an automatic waste gate controller per Retrofit Option 106 (S/N 61-0001-004 through 61-0334-111), PA-60-601 (S/N 61-0342-112 through 61-0880-8162157), PA-60-601P (S/N 61P-0157-001 through 61P-0860-8163455), PA-60-602P (S/N 62P-0750-8165001, and 62P-0861-8165002 through 60-8365010), PA-60-700P (S/N 60-8423001 through 60-8423025) airplanes certificated in any category. Compliance: Required within the next 50 hours time-in-service after the effective date of this AD unless already accomplished. To reduce the possibility of damage to the oil supply hoses which, if not corrected, could result in an in-flight fire, oil starvation and/or engine failure, accomplish the following: (a) For all the above applicable airplanes except Model PA-60-700P (S/N 60- 8423001 through 60-8423025) airplanes, replace and modify the engine fluid-carrying hoses and associated hardware in accordance with the instructions contained in Piper Service Bulletin (SB) No. 761, dated April 18, 1983, and Piper SB No. 815, dated January 3, 1986. (b) For Model PA-60-700P Aerostars (S/N 60-8423001 through 60- 8423025) airplanes replace and modify the engine fluid-carrying hoses and associated hardware in accordance with the instructions contained in Piper SB No. 815, dated January 3, 1986. (c) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished. (d) An equivalent means of compliance with this AD may be used if approved by the Manager, Atlanta Aircraft Certification Office, ACE-115A, Federal Aviation Administration, 1669 Phoenix Parkway, Suite 210C, Atlanta, Georgia 30349. All persons affected by this directive may obtain copies of the documents referred to herein upon request to Piper Aircraft Corporation, 2926 Piper Drive, Vero Beach, Florida 32960; or may examine these documents at the FAA, Office of the Assistant Chief Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106. This amendment, 39-6080, becomes effective on December 26, 1988. FOOTER:
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