Aerostar Aircraft Corporation Airworthiness Directives

55 ADs indexed for Aerostar Aircraft Corporation aircraft.

Models

PA-60-601 (Aerostar 601) 29 ADs PA-60-600 (Aerostar 600) 26 ADs PA-60-601P (Aerostar 601P) 22 ADs PA-60-602P (Aerostar 602P) 15 ADs PA-60-700P (Aerostar 700P) 14 ADs RX-6 6 ADs S-50A 6 ADs S-55A 6 ADs S-60A 6 ADs Various 5 ADs RX-7 4 ADs S-40A 4 ADs S-66A 4 ADs S-77A 3 ADs W100LB 3 ADs RX-8 2 ADs S-49A 2 ADs S-52A 2 ADs S-57A 2 ADs Fuel Cylinders 2 ADs Fuel Cylinders 1 AD F.260 1 AD F.260B 1 AD F.260C 1 AD F.260D 1 AD F.260E 1 AD F.260F 1 AD S.205 - 18/F 1 AD S.205 - 18/R 1 AD S.205 - 20/F 1 AD S.205 - 20/R 1 AD 110C 1 AD 110P 1 AD 78C 1 AD 90C 1 AD ARKY 1 AD BAG 1 AD BEAR 1 AD BRAIN 1 AD Skysailor 105 1 AD Skysailor 90 1 AD 335 1 AD 340A 1 AD 402B 1 AD 404 1 AD 414A 1 AD 421C 1 AD Fuel Flow Transducers 1 AD PA-60-600 (Aerostar 600) 1 AD PA-60-601 (Aerostar 601) 1 AD PA-60-601P (Aerostar 601P) 1 AD AT-302 1 AD AT-400 1 AD BN-2 1 AD BN-2A 1 AD BN-2A-3 1 AD H.P. 137 Jetstream Mk. 1 1 AD Nord 262A Series 1 AD PA-60-600 (Aerostar 600) 1 AD PA-60-601 (Aerostar 601) 1 AD PA-60-601P (Aerostar 601P) 1 AD AEIO-320-D1B 1 AD AEIO-320-D2B 1 AD AEIO-320-E1A 1 AD AEIO-320-E1B 1 AD AEIO-320-E2A 1 AD AEIO-320-E2B 1 AD AEIO-360-B1B 1 AD AEIO-360-B1D 1 AD AEIO-360-B1F 1 AD AEIO-360-B1F6 1 AD 114B 1 AD 114TC 1 AD 208 1 AD 208B 1 AD 58 1 AD 95-55 1 AD 95-C55 1 AD A36 1 AD B36TC 1 AD PA-60-700P (Aerostar 700P) 1 AD 172L 1 AD 172P 1 AD 172RG 1 AD 182P 1 AD 182Q 1 AD 182R 1 AD 210R 1 AD F182P 1 AD F182Q 1 AD PA-60-700P (Aerostar 700P) 1 AD PA-31 1 AD PA-31-300 1 AD PA-31-325 1 AD PA-31-350 1 AD PA-31P 1 AD PA-31P-350 1 AD PA-60-600 (Aerostar 600) 1 AD PA-60-601 (Aerostar 601) 1 AD PA-60-601P (Aerostar 601P) 1 AD PA-60-602P (Aerostar 602P) 1 AD PA-60-700P (Aerostar 700P) 1 AD 110P 1 AD 78C 1 AD 90C 1 AD CTS 1 AD QUBE-80 1 AD RXS-8 1 AD S-57S 1 AD S-60S 1 AD S-71A 1 AD SPII 1 AD Burners 1 AD 328-100 1 AD F.260 1 AD F.260B 1 AD F.260C 1 AD F.260D 1 AD F.260E 1 AD GTX 33 1 AD GTX 330 1 AD GTX 330D 1 AD GTX 33D 1 AD

Recent ADs

2025-21-01 Recurring

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Airworthiness Directives; Cameron Balloons Ltd. Fuel Cylinders

Unsafe Condition: Cracks on the upper hex portion of pressure relief valve (PRV) adaptors could lead to uncontrolled leakage of liquefied petroleum gas (LPG), resulting in an in-flight fire and consequent emergency ...

Effective: Oct 27, 2025 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Cameron Balloons Ltd. Fuel Cylinders

2023-17-09

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Airworthiness Directives; Cameron Balloons Ltd. Fuel Cylinders

Unsafe Condition: cracks in the weld between the cylinder valve plate and the upper dished end of Cameron fuel cylinder part number (P/N) CB2990/A

Effective: Sep 13, 2023 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Cameron Balloons Ltd. Fuel Cylinders

2023-09-09 Recurring

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Airworthiness Directives; Various Airplanes, Helicopters, and Engines

Unsafe Condition: Multiple failures of spot-welded, multi-segment v-band couplings at the tailpipe to the turbocharger exhaust housing flange.

Effective: Jul 17, 2023 Category: engine Compliance: Within 50 flight hours after the effective date of this AD.

Why matched: Airworthiness Directives; Various Airplanes, Helicopters, and Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2022-15-02 Recurring

final rule

Airworthiness Directives; Cameron Balloons Ltd. Burner Assemblies

Unsafe Condition: fatigue cracking of the weld on Stratus double burner hangers, caused mainly during ground transportation with the burner erect, combined with an overload event

Effective: Aug 25, 2022 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Cameron Balloons Ltd. Burner Assemblies

2022-03-15

final rule

Airworthiness Directives; Various Airplanes

Unsafe Condition: The displayed fuel quantity can have an error as much as four gallons/fuel tank with the display indicating four gallons with an empty tank. In the context of this event, the end level effect is th...

Effective: Mar 21, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Airplanes

Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

2022-01-06

final rule

Airworthiness Directives; Cameron Balloons Ltd. Fuel Cylinders

Unsafe Condition: Certain Cameron Hot Air Balloon fuel cylinders are supplied with liquid offtakes that consist of a quarter turn ball valve mounted on a flanged adaptor ([part number] P/N CB437, see [CAA AD] figure...

Effective: Jan 18, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Cameron Balloons Ltd. Fuel Cylinders

2020-24-10 Recurring

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Airworthiness Directives; Aerostar Aircraft Corporation Airplanes

Unsafe Condition: Corrosion on the elevator and aileron balance tubes, which may be hidden by rubber boots, could result in failure of the aileron and elevator balance tubes, jamming of the aileron and/or elevator b...

Effective: Jan 22, 2021 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Aerostar Aircraft Corporation Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

2013-03-10

final rule

Airworthiness Directives; Lindstrand Hot Air Balloons Ltd Appliances

Unsafe Condition: Insufficient tightness of the threaded hose connector in the assembly area that could result in fuel leakage.

Effective: Mar 19, 2013 Category: aircraft Compliance: Within 60 days after the effective date of March 19, 2013.

Why matched: Airworthiness Directives; Lindstrand Hot Air Balloons Ltd Appliances

2006-12-07

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Airworthiness Directives; Engine Components Inc. (ECi) Reciprocating Engine Cylinder Assemblies

Unsafe Condition: Cracks in the cylinder assemblies and possible engine failure caused by separation of a cylinder head.

Effective: Jul 11, 2006 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Engine Components Inc. (ECi) Reciprocating Engine Cylinder Assemblies

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2005-18-20

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Airworthiness Directives; Goodrich De-icing and Specialty Systems “FASTprop” Propeller De-icers

Unsafe Condition: Goodrich De-icing and Specialty Systems 'FASTprop' propeller de-icers becoming loose or debonded, and detaching from propeller blades during operation.

Effective: Oct 14, 2005 Category: propeller Compliance: Before further flight

Why matched: Airworthiness Directives; Goodrich De-icing and Specialty Systems "FASTprop" Propeller De-icers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2005-01-19

final rule

Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

Unsafe Condition: The GTX 33/33D/330/330D Mode S transponders may detect the S1 (suppression) interrogating pulse below the minimum trigger level (MTL) and, in some circumstances, not reply. This could lead to inacc...

Effective: Feb 23, 2005 Category: aircraft Compliance: Within 12 months of the effective date (February 23, 2005).

Why matched: Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

2003-22-01 Recurring

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Airworthiness Directives; Aerostar Aircraft Corporation Models PA-60-600, PA-60-601, PA-60-601P, PA-60-602P, and PA-60-700P Airplanes

Unsafe Condition: Fuel leaking from the auxiliary fuel transfer pumps installed below the auxiliary fuel tank, which could result in fire or explosion in the cargo/passenger compartment.

Effective: Nov 17, 2003 Category: aircraft Compliance: Within the next 10 hours time-in-service after November 17, 2003 (initial inspection); repetitive...

Why matched: Airworthiness Directives; Aerostar Aircraft Corporation Models PA-60-600, PA-60-601, PA-60-601P, PA-60-602P, and PA-60-700P Airplanes

Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

2002-24-07

final rule

Airworthiness Directives; Aerostar Aircraft Corporation Models PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P), and PA-60-700P (Aerostar 700P) Airplanes

Unsafe Condition: Inadequate retention of the existing left-hand (LH) oil scavenge pump rotor allows the rotor to machine its way through the LH end plate. Axial migration of the right-hand (RH) scavenge pump rotor ...

Effective: Jan 17, 2003 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Aerostar Aircraft Corporation Models PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P), and PA-60-700P (Aerostar 700P) Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2001-10-09

final rule

Airworthiness Directives; Honeywell KC 225 Automatic Flight Control Systems

Unsafe Condition: The Honeywell KC 225 automatic flight control system (AFCS) is disconnecting without warning during flight in a gross mistrim configuration, which could result in an undesirable autotrim command th...

Effective: Jun 15, 2001 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Honeywell KC 225 Automatic Flight Control Systems

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

2001-08-10

final rule

Airworthiness Directives; Aerostar Aircraft Corporation Models PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P), and PA-60-700P (Aerostar 700P) Airplanes

Unsafe Condition: Cracking of the main landing gear lower side brace at the upper bolt lug where the upper and lower side braces connect, which could result in failure of the main landing gear lower side brace.

Effective: Jun 12, 2001 Category: aircraft Compliance: Within the next 50 hours time-in-service after June 12, 2001, unless already performed.

Why matched: Airworthiness Directives; Aerostar Aircraft Corporation Models PA-60-600 (Aerostar 600), PA-60- 601 (Aerostar 601), PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P), and PA-60-700P (Aerostar 700P) Airplanes

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

Amdt-39-10916 Recurring

final rule

Airworthiness Directives; Aerostar Aircraft Corporation PA-60-600 and PA-60-700 Series Airplanes

Unsafe Condition: Fatigue cracking of the wing upper spar cap, which could result in structural failure of the wing spar to the point of failure with consequent loss of control of the airplane.

Effective: Jan 8, 1999 Category: aircraft Compliance: Within 100 hours time-in-service after the effective date, and thereafter at intervals not to exc...

Why matched: Airworthiness Directives; Aerostar Aircraft Corporation PA-60-600 and PA-60-700 Series Airplanes

Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure

98-24-29

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Airworthiness Directives; Aerostar Aircraft Corporation PA-60-600 and PA-60-700 Series Airplanes

Unsafe Condition: Fatigue cracking of the wing upper spar cap above the main landing gear fitting in the top of the wheel well, which could result in structural failure of the wing spar to the point of failure with ...

Effective: Jan 8, 1999 Category: aircraft Compliance: Within the next 100 hours time-in-service after the effective date of this AD, unless already acc...

Why matched: Airworthiness Directives; Aerostar Aircraft Corporation PA-60-600 and PA-60-700 Series Airplanes

Amdt-39-10335

final rule

Airworthiness Directives; Aerostar Aircraft Corporation Models PA-60-600, PA-60-601, PA-60-601P, PA-60-602P, and PA-60-700P Airplanes

Unsafe Condition: Operating in severe icing conditions without clear procedures and limitations may lead to adverse flight control behavior or aircraft performance degradation.

Effective: Mar 13, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Aerostar Aircraft Corporation Models PA-60-600, PA-60-601, PA-60-601P, PA-60-602P, and PA-60-700P Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

98-04-23

final rule

Airworthiness Directives; Aerostar Aircraft Corporation Models PA-60-600, PA-60-601, PA-60-601P, PA-60-602P, and PA-60-700P Airplanes.

Unsafe Condition: Flight in freezing rain, freezing drizzle, or mixed icing conditions may result in ice build-up on protected surfaces exceeding the capability of the ice protection system, or may result in ice for...

Effective: Mar 13, 1998 Category: aircraft Compliance: Within 30 days after the effective date of this AD

Why matched: Airworthiness Directives; Aerostar Aircraft Corporation Models PA-60-600, PA-60-601, PA-60-601P, PA-60-602P, and PA-60-700P Airplanes.

95-23-11

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Airworthiness Directives; Aerostar Aircraft Corporation PA-60-600 (Aerostar 600) Series (formerly Piper Aircraft Corporation) Airplanes.

Unsafe Condition: Cracked fuselage horizontal stabilizer attach fittings could result in the fuselage horizontal stabilizer separating from the airplane while in flight with subsequent loss of control of the airplane.

Effective: Nov 30, 1995 Category: aircraft Compliance: Initially within the next 25 hours time-in-service (TIS) after the effective date or within the n...

Why matched: Airworthiness Directives; Aerostar Aircraft Corporation PA-60-600 (Aerostar 600) Series (formerly Piper Aircraft Corporation) Airplanes.

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