AD 88-25-02

final rule

Airworthiness Directives; PIPER (AEROSTAR) Models PA-60-601, PA-60-601P, PA-60-602P, PA-60-700P Airplanes

AD Number
88-25-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
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

AI-generated summary from the source AD text. Verify against the official source before acting.

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
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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
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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:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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