AD 87-07-09

final rule
Data completeness: 70%

Airworthiness Directives; PIPER AIRCRAFT CORPORATION TED SMITH AEROSTAR) Models PA-60-600, PA-60-601, PA-60-601P, PA-60-602P and PA-60-700P Airplanes

AD Number
87-07-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Aerostar Aircraft Corporation PA-60-600 (Aerostar 600) Airworthiness Directives; PIPER AIRCRAFT CORPORATION TED SMITH AEROSTAR) Models PA-60-600, PA-60-601, PA-60-601P, PA-60-602P and PA-60-700P Airplanes
aircraft Aerostar Aircraft Corporation PA-60-601 (Aerostar 601) Airworthiness Directives; PIPER AIRCRAFT CORPORATION TED SMITH AEROSTAR) Models PA-60-600, PA-60-601, PA-60-601P, PA-60-602P and PA-60-700P Airplanes
aircraft Aerostar Aircraft Corporation PA-60-601P (Aerostar 601P) Airworthiness Directives; PIPER AIRCRAFT CORPORATION TED SMITH AEROSTAR) Models PA-60-600, PA-60-601, PA-60-601P, PA-60-602P and PA-60-700P Airplanes
aircraft Aerostar Aircraft Corporation PA-60-602P (Aerostar 602P) Airworthiness Directives; PIPER AIRCRAFT CORPORATION TED SMITH AEROSTAR) Models PA-60-600, PA-60-601, PA-60-601P, PA-60-602P and PA-60-700P Airplanes
aircraft Aerostar Aircraft Corporation PA-60-700P (Aerostar 700P) Airworthiness Directives; PIPER AIRCRAFT CORPORATION TED SMITH AEROSTAR) Models PA-60-600, PA-60-601, PA-60-601P, PA-60-602P and PA-60-700P Airplanes

Unsafe Condition

Failed exhaust system components, including cracks, pin holes, leaks, binding, unserviceable clamps, bolts, supports, slip joints, flange mating surfaces, turbocharger mounting flanges, and gaskets.

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

Required Actions

Inspect exhaust system components using dye penetrant for cracks and pin holes, check clamps, bolts, supports, slip joints, flanges, and gaskets. Remove exhaust stacks, replace unserviceable parts, and reinstall with specific lubricants, torque settings, and spacing requirements. Compliance must be within 50 hours time-in-service after the effective date.

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 Aircraft Corporation models PA-60-600 (serials 60-0001-003 through 60-0933-8161262), PA-60-601 (61-0001-004 through 61-0880-8162157), PA-60-601P (61P-0157-001 through 61P-0860-8163455), PA-60-602P (62P-0750-8165001, 62P-0861-8165002 through 62P-0932-8165055, and 60-8265001 through 60-8365021), and PA-60-700P (60-8423001 through 60-8423025).

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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