# Aerostar PA-60-601

- Type: Aircraft model (FAA registry)
- Registry code: 7106017
- Manufacturer (registry): AEROSTAR
- Model: PA-60-601
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Reciprocating
- Seats: 6
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS A17WE](https://openairdocs.org/tcds/A17WE) (OpenAirDocs)
- Holder: Aerostar Aircraft Corporation
- Registered aircraft: 0
- Page: https://openairdocs.org/model/aerostar-pa-60-601

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2003-22-01](https://openairdocs.org/ad/2003-22-01): Auxiliary fuel transfer pumps · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Nov 17, 2003
- [AD 2002-24-07](https://openairdocs.org/ad/2002-24-07): Roto-Master and Rajay scavenge pumps · Aerostar PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P) and 1 more. Effective Jan 17, 2003
- [AD 2001-08-10](https://openairdocs.org/ad/2001-08-10): Main Landing Gear Lower Side Brace Assemblies · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Jun 12, 2001
- [AD 98-24-29](https://openairdocs.org/ad/98-24-29): Wing Upper Spar Cap · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Jan 8, 1999
- [AD 98-04-23](https://openairdocs.org/ad/98-04-23): AFM - Limitations Section - Icing · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Mar 13, 1998
- [AD 95-23-11](https://openairdocs.org/ad/95-23-11): Upper And Lower Horizontal Flanges · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 1 more. Effective Nov 30, 1995
- [AD 94-15-13](https://openairdocs.org/ad/94-15-13): Nose Landing Gear Drag Link Assembly · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Sep 12, 1994
- [AD 93-13-08](https://openairdocs.org/ad/93-13-08): Torque Links · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Aug 20, 1993
- [AD 90-01-02](https://openairdocs.org/ad/90-01-02): Service Bulletin 920 - Fire Prevention · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Mar 1, 1990
- [AD 89-03-04](https://openairdocs.org/ad/89-03-04): Cabin Door · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Feb 24, 1989
- [AD 88-25-02](https://openairdocs.org/ad/88-25-02): Engine Fluid-Carrying Hoses · Aerostar PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P) and 1 more. Effective Dec 26, 1988
- [AD 88-21-05](https://openairdocs.org/ad/88-21-05): Exhaust Systems (STC SA980NM) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Nov 6, 1988
- [AD 87-21-01](https://openairdocs.org/ad/87-21-01): Fuel Filler Openings · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 14 more. Effective Nov 2, 1987
- [AD 87-07-09](https://openairdocs.org/ad/87-07-09): Exhaust System Components · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective May 15, 1987
- [AD 83-14-07 R3](https://openairdocs.org/ad/83-14-07-R3): Limitations Section -- CG Limit · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 1 more. Effective Nov 25, 1983
- [AD 80-18-03](https://openairdocs.org/ad/80-18-03): Fuel Pressure System · Aerostar PA-60-601 (Aerostar 601) and PA-60-601P (Aerostar 601P). Effective Oct 6, 1980
- [AD 80-19-14](https://openairdocs.org/ad/80-19-14): Horizontal/Vertical Stabilizer · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) and PA-60-601P (Aerostar 601P). Effective Sep 25, 1980
- [AD 80-17-04](https://openairdocs.org/ad/80-17-04): Fuel Flow Transducers · Aerosonic Fuel Flow Transducers, PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) and 9 more. Effective Aug 13, 1980
- [AD 80-12-14](https://openairdocs.org/ad/80-12-14): Engine Fire · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) and PA-60-601P (Aerostar 601P). Effective Jun 19, 1980
- [AD 79-01-05](https://openairdocs.org/ad/79-01-05): Fuel Starvation · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) and PA-60-601P (Aerostar 601P). Effective Dec 27, 1979
- [AD 79-18-10](https://openairdocs.org/ad/79-18-10): Cabin Door Latching Mechanism · Aerostar PA-60-600 (Aerostar 600) and PA-60-601 (Aerostar 601). Effective Aug 29, 1979
- [AD 79-08-05](https://openairdocs.org/ad/79-08-05): Engine Nacelles · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) and PA-60-601P (Aerostar 601P). Effective May 24, 1979
- [AD 78-18-05](https://openairdocs.org/ad/78-18-05): Wing Tank Fuel Quantity Indicator · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) and PA-60-601P (Aerostar 601P). Effective Sep 13, 1978
- [AD 74-25-02](https://openairdocs.org/ad/74-25-02): Electrical Attitude And Directional Gyros · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) and PA-60-601P (Aerostar 601P) with STC SA2336WE or SA2367WE. Effective Dec 4, 1974
- [AD 71-17-07](https://openairdocs.org/ad/71-17-07): Wing Flap Attachment Rib · Aerostar PA-60-600 (Aerostar 600) and PA-60-601 (Aerostar 601). Effective Aug 23, 1971
- [AD 70-23-04](https://openairdocs.org/ad/70-23-04): Wing Flap Tracks · Aerostar PA-60-600 (Aerostar 600) and PA-60-601 (Aerostar 601). Effective Aug 23, 1971
- [AD 71-10-02](https://openairdocs.org/ad/71-10-02): Overvoltage Relay Ground · Aerostar PA-60-600 (Aerostar 600) and PA-60-601 (Aerostar 601). Effective May 14, 1971
- [AD 71-05-06](https://openairdocs.org/ad/71-05-06): Main Landing Gear · Aerostar PA-60-600 (Aerostar 600) and PA-60-601 (Aerostar 601). Effective Apr 5, 1971
- [AD 71-02-05](https://openairdocs.org/ad/71-02-05): Main Cabin Door Lock Pins · Aerostar PA-60-600 (Aerostar 600) and PA-60-601 (Aerostar 601). Effective Jan 23, 1971
- [AD 70-25-09](https://openairdocs.org/ad/70-25-09): Microphone Jack Connection · Aerostar PA-60-600 (Aerostar 600) and PA-60-601 (Aerostar 601). Effective Dec 18, 1970
- [AD 70-23-05](https://openairdocs.org/ad/70-23-05): Fuel Pressure Indicators · Aerostar PA-60-600 (Aerostar 600) and PA-60-601 (Aerostar 601). Effective Nov 16, 1970

## Information bulletins (advisory) (2)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-03-55](https://openairdocs.org/saib/CE-03-55): . Issued Sep 18, 2003

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (28)

As reported by operators and repair stations, by the model named in the report.

- [SDR CA060419002](https://openairdocs.org/sdr/CA060419002), Apr 17, 2006: SPAR. CRACKED. CRACK WAS NOTICED DURING AN ANNUAL INSPECTION WITH THE AID OF FLASHLIGHT AND MIRROR. THE DEFECT AREA IS JUST AFT OF THE NR 2 ENGINE FIREWALL THROUGH AN INSPECTI
- [SDR TZRA200600001](https://openairdocs.org/sdr/TZRA200600001), Mar 10, 2006: ROCKER COVER. BROKEN. LT ENG BEGAN TO RUN ROUGH & LEAK OIL ONTO COWLING INBD SIDE. ENG CONTINUED TO MAKE PWR & OIL PRESS REMAINED NORM, DEACTIVATED TURBOS AS PRECAUTION. EXAM REVEALE
- [SDR TZR2005F00014](https://openairdocs.org/sdr/TZR2005F00014), Mar 17, 2005: CYLINDER. CRACKED. CYLINDER HAS A CRACK IN THE INTAKE VALVE SEAT. (K)
- [SDR 2004FA0000902](https://openairdocs.org/sdr/2004FA0000902), Nov 19, 2004: CHANNEL. CRACKED. ON INSPECTION, FOUND PART CRACKED AT RIVET HOLES WHERE ATTACHED TO P/N 210056-031 CHANNEL.
- [SDR 7529S](https://openairdocs.org/sdr/7529S), Nov 19, 2004: CHANNEL. CRACKED. ON INSPECTION, FOUND PART CRACKED AT RIVET HOLES WHERE ATTACHED TO P/N 210056-031 CHANNEL.
- [SDR TZR2004F00003](https://openairdocs.org/sdr/TZR2004F00003), Dec 10, 2003: CRANKCASE. CRACKED. PILOT REPORTED A HARD DOWNDRAFT (REPORTED THAT HE HIT HIS HEAD ON CEILING) APPROX 20 SECONDS LATER NR 2 ENGINE LOST POWER AND HE SHUT THE ENGINE DOWN. HE LANDED
- [SDR 2003FA0001047](https://openairdocs.org/sdr/2003FA0001047), Sep 26, 2003: BOOT. LOOSE. DEICE BOOT (FAST BOOT) DOES NOT PROPERLY ADHERE TO BLADE.
- [SDR TZR2004F00001](https://openairdocs.org/sdr/TZR2004F00001), Jul 29, 2003: TORQUE LINK. BROKEN. TORQUE LINK ATTACH POINT ON THE RT STRUT BROKE AT LANDING. THIS ALLOWED THE RT MLG TIRE TO ROTATE AND PULL THE AIRCRAFT OFF THE RUNWAY. THE RESULTING SIDE LOAD 
- [SDR 2003FA0000823](https://openairdocs.org/sdr/2003FA0000823), Jul 29, 2003: STRUT. BROKEN. TORQUE LINK ATTACH POINT ON THE RIGHT STRUT BROKE AT LANDING. THIS ALLOWED THE RIGHT MLG TIRE TO ROTATE AND PULL THE AIRCRAFT OFF THE RUNWAY. THE RESULTING SIDE
- [SDR GXPA0303](https://openairdocs.org/sdr/GXPA0303), May 9, 2003: ENGINE. LEAKING. AIRCRAFT DOWN IN EL DORADO, AR DUE TO LOW OIL PRESSURE IN RT ENGINE. CORRECTIVE ACTION WILL BE COMMUNICATED WHEN TROUBLESHOOTING IS COMPLETED.
- [SDR MHJ2002F00003](https://openairdocs.org/sdr/MHJ2002F00003), Jul 1, 2002: DOOR. DEPARTED. UPPER CABIN DOOR DEPARTED IN FLIGHT. ABOUT 1 HOUR INTO FLIGHT PILOT REPORTED CREAKING SOUND. SHORTLY AFTERWARD, DOOR DEPARTED. PILOT LANDED WITHOUT INCIDENT.
- [SDR 2002FA0000150](https://openairdocs.org/sdr/2002FA0000150), Dec 18, 2001: RIB. CRACKED. DURING ANNUAL INSPECTION THE VERTICAL STABILIZER LOWER FORWARD RIB WAS FOUND CRACKED AT THE 90 DEGREE BEND ADJACENT TO THE FORWARD SPAR. THIS AREA NEEDS CLOSE I
- [SDR 2002FA0000149](https://openairdocs.org/sdr/2002FA0000149), Dec 18, 2001: SUPPORT. CRACKED. DURING ROUTINE MAINTENANCE TO REPLACE MAIN TIRES, THE AIRCRAFT WAS JACKED. THE NOSE LANDING GEAR HAD EXCESSIVE MOVEMENT. THE NOSE LANDING GEAR ACTUATOR SUPPORT 
- [SDR MHJ2001F00001](https://openairdocs.org/sdr/MHJ2001F00001), Nov 1, 2001: MAIN BEARING. DELAMINATED. FOUND NONFERROUS METAL IN SUCTION OIL SCREEN, CUT OPEN OIL FILTER AND FOUND NONFERROUS METAL IN OIL FILTER, DISASSEMBLED ENGINE, FOUND NR 2 AND NR 4 MAIN BEARIN
- [SDR GXPA0117](https://openairdocs.org/sdr/GXPA0117), Aug 14, 2001: CONNECTOR. MALFUNCTIONED. ARTIFICIAL HORIZON TUMBLED AND SHOWED 10 DEGREES LEFT BANK IN STRAIGHT LEVEL FLIGHT. CLEANED CANNON PLUG AND CLEARED FOR TEST FLIGHT. OPS CHECKED GOOD. TEST FLI
- [SDR AUS20011043](https://openairdocs.org/sdr/AUS20011043), Jul 5, 2001: TAILPIPE. CRACKED. (AUS) RH ENGINE TAILPIPE CRACKED ALLOWING HOT EXHAUST GAS TO ACTIVATE FIRE WARNING SYSTEM.
- [SDR AU000679](https://openairdocs.org/sdr/AU000679), Sep 1, 2000: BRACE. CRACKED. (AUS) LEFT MAIN LANDING GEAR LOWER SIDE BRACE CRACKED. FOUND DURING INSPECTION IAW TSA-SB600-134A. (X)
- [SDR GXPA00008](https://openairdocs.org/sdr/GXPA00008), May 5, 2000: WINDOW. BLEW OUT. AIRCRAFT EMERGENCY WINDOW BLEW OUT, WHILE IN CRUISE, AFTER TAKEOFF FROM TOLEDO. AIRCRAFT LANDED BACK IN TOLEDO. AIRCRAFT GROUNDED DUE TO AWAITING REPLACEMENT WI
- [SDR CA981006002](https://openairdocs.org/sdr/CA981006002), Sep 25, 1998: ROD. FAILED. (CAN) DURING CRUISE, THE PILOT NOTED THE NR 1 ENGINE WAS RUNNING ROUGH. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO BASE. POST-FLIGHT INSPECTION REVEA
- [SDR AU981107](https://openairdocs.org/sdr/AU981107), Sep 1, 1998: ROD. CORRODED. (AUS) NOSE LANDING GEAR BUNGEE ROD CORRODED AND BINDING. NOSE LANDING GEAR COLLAPSED.
- [SDR 98ZZZX3005](https://openairdocs.org/sdr/98ZZZX3005), Jun 26, 1998: BOLT. FAILED. WHEEL ASSEMBLY FOUND WITH INCORRECT BOLTS INSTALLED. INSTALLED NEW P/N AN5-35A BOLTS.
- [SDR GXPA97011](https://openairdocs.org/sdr/GXPA97011), May 8, 1997: MAGNETO. SEIZED. ACFT'S RT ENG FAILED IN-FLIGHT. ACFT LANDED AT FDY. NLG COLLA PSED ON LANDING.INSP AND TEAR DOWN OF ENG NOTED THAT RT MAG WAS S EIZED. CRANKSHAFT DRIVE GEAR HAD
- [SDR 96ZZZX4817](https://openairdocs.org/sdr/96ZZZX4817), Aug 24, 1996: BELLCRANK. FAILED. AFTER TAKEOFF, PILOT RETRACTED GEAR AND GOT NO UP LIGHT. COULD SEE INBOARD DOOR TRAILING. PILOT LOWERED AND LANDED. BELLCRANK WAS FOUND IN SEVERAL PIECES. OUTBO
- [SDR AU961150](https://openairdocs.org/sdr/AU961150), Jul 30, 1996: PROPELLER. GROUND STRIKE. (AUS) RH ENGINE SUFFERED A PROPELLER STRIKE - ALL THREE BLADES DAMAGED IN AREA APPROXIMATELY 50.8MM (2IN) FROM TIP
- [SDR 95ZZZX4356](https://openairdocs.org/sdr/95ZZZX4356), Jul 13, 1995: EXIT. DEPARTED. EMERGENCY EXIT DEPARTED AIRCRAFT AFTER LEVELLNG OFF AT 9,500 FEET. THE AIRCRAFT SUSTAINED NO DAMAGE TO EXIT FRAME OR TAIL SURFACES. INVESTIGATION REVEALED THE F
- [SDR 95ZZZX2279](https://openairdocs.org/sdr/95ZZZX2279), Mar 31, 1995: BEARING. WRONG PART. DURING AN ANNUAL INSPECTION, OUTBOARD AILERON BEARING BRACKET APPEARED TO HAVE WORKING RIVETS. REMOVAL OF THE BRACKET REVEALED CRACKS IN THE RIB IN TWO OF THE R
- [SDR 95ZZZX2278](https://openairdocs.org/sdr/95ZZZX2278), Mar 31, 1995: RIB. CRACKED. DURING AN ANNUAL INSPECTION, OUTBOARD AILERON BEARING BRACKET APPEARED TO HAVE WORKING RIVETS. REMOVAL OF THE BRACKET REVEALED CRACKS IN THE RIB IN TWO OF THE R
- [SDR 95ZZZX1274](https://openairdocs.org/sdr/95ZZZX1274), Feb 8, 1995: ENGINE. FAILED. LEFT ENGINE SHUT DOWN IN-FLIGHT, ACFT LANDED. REMOVED AND REPLACED ENGINE, CAUSE FOR FAILURE UNKNOWN AT THIS TIME.

## STCs that may be installed (OpenAirDocs) (227, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA01147WI](https://openairdocs.org/stc/SA01147WI): Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. Concorde Battery Corporation
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC
- [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics
- [STC SA35GL](https://openairdocs.org/stc/SA35GL): Install Cleveland Acft Products wheel and brake conversion kit, P/N 199-51. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA04452NY](https://openairdocs.org/stc/SA04452NY): Installation of MT-Propeller Entwicklung GmbH model MTV-14-B-C-F/CF(L)188-30g 4-blade, constant speed, full feathering propellers and spinners. MT- Propeller Entwicklung GmbH
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King)
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA04182NY](https://openairdocs.org/stc/SA04182NY): Installation of BendixKing KA 310 Autopilot Adapter. Honeywell International Inc
- [STC SA09764DS](https://openairdocs.org/stc/SA09764DS): Installation of an S-TEC 01326 Digital Flight Control System (DFCS). S-TEC Corporation
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA1184CE](https://openairdocs.org/stc/SA1184CE): Installation of King KFC 200 2 axis(3 optional) Flight Control System with King KCS 55 (or -55A) compass and a King KI 255 (or -256) Flight Command Indicator or a KG 258 Attitude Horizon Gyro with a KC 292 Mode Controller. Honeywell International Inc
- [STC SA1530CE-D](https://openairdocs.org/stc/SA1530CE-D): Installation of King KAS 297 altitude selector option. Honeywell International Inc
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA2207WE](https://openairdocs.org/stc/SA2207WE): Installation of electrically-driven Freon air-conditioning system. Air Comm Corporation
- [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE Inc
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA01828SE](https://openairdocs.org/stc/SA01828SE): Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System. J. P. Instruments
- [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine
- [STC SA04060NY](https://openairdocs.org/stc/SA04060NY): Installation of the Replacement Hydraulic Accumulator Piston. Marsh Brothers Aviation Inc
- [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation

All 227: https://openairdocs.org/model/aerostar-pa-60-601/stcs.md

## PMA parts (OpenAirDocs) (over 1,000, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [RAP164-05006](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173488801620260722154724.0001): Brake Disc. Rapco Inc. · PMA PQ2101CE · Replaces 164-05006 · Jun 3, 2026
- [AG5221-222](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126006627420260616140346.0001): Spool, Pilot Valve. Aero Accessories LLC · PMA PQ1206CE · Replaces Woodward P/N:5221-222 · May 27, 2026
- [MDL TD 031851](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118069681220250508133537.0001): VA-1A( )AndAccessories. Electronics International Inc · PMA PQ0088NM · Modification part · Apr 10, 2025
- [20002A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105416877020250303152537.0001): Air-Oil Cooler. Boyd Niagara LLC · PMA PQ0872NE · Replaces 8526250 · Oct 30, 2024
- [3111-022ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162012168820240917173615.0001): Shim, Brass. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 3111-022 · Sep 4, 2024
- [01-7079-24](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136170424120231108124805.0001): LIGHT-ASSY, StarLight. AeroLEDs LLC · PMA PQ5259NM · Replaces WA7079B-24NLI7079-24CMA-7079B-24A7079B… · Nov 3, 2023
- [APS68-01700](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131577670320231102131428.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01700 · Sep 25, 2023
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195100709020220706160036.0001): Whelen Aerospace Technologies · PMA PQ1372CE · Jun 21, 2022
- [EA-22000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187055246220220525194331.0001): Controller Wire Harness (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-21000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180869754820220525194157.0001): Six-Cylinder Ignition Controller. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-22000T](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151952144920220525194443.0001): Controller Wire Harness- Twin (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [AA2J4-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108664051520220725142936.0001): Filter Assembly. Aero Accessories LLC · PMA PQ1206CE · Replaces Airborne1J4-4Aero Accessories AA1J4-4 · Mar 14, 2022
- [89000026-003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174241017120240229155312.0001): Final Assembly KCP 100 Control Panel(Landscape). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000020-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135386137120240229155256.0001): Final Assembly KSD 100 Primary Flight Display (PFD). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000023-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121615886720240229155301.0001): Final Assembly KG 71 Air Data Attitude and Heading Reference System (ADHRS). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000026-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104792557320240229155307.0001): Final Assembly KCP 100 Control Panel. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [MC153-00900](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID749574486520211021173347.0001): Ring. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 153-00900, 153-9, 755-964 · Sep 9, 2021
- [MC153-01500](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID559779322202110211733540.0001): Ring. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 153-01500, 153-15, 755-930 · Sep 9, 2021
- [MC153-00300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID311331069320211021173332.0001): Ring. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 153-00300, 755-929, A39070 · Sep 9, 2021
- [MC154-01400](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID275286721320211021173430.0001): Felt. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 154-01400, 154-14, 751-819 · Sep 9, 2021
- [MC155-00100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID246865560202110211734530.0001): Retaining Ring. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 155-00100, 155-1, 3023, 752-830 · Sep 9, 2021
- [MC154-01300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168798577720211021173428.0001): Felt. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 154-01300, 154-13, 751-810 · Sep 9, 2021
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID761274132202109231437480.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID261034086720210921142531.0001): SkyTrax 100B/200 ADS-B Receiver. Avidyne Corporation · PMA PQ4035CE · Replaces ModificationPart · Jul 28, 2021
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159699760202109231436460.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [ST-984](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID986409859320210810161807.0001): Installation of S-TEC 01326 Digital Flight Control System (DFCS)). S-TEC Corporation · PMA PQ0445SW · Modification part · Apr 8, 2021
- [ST-984-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID981785173520210810161808.0001): Installation of S-TEC 01326 Digital Flight Control System (DFCS). S-TEC Corporation · PMA PQ0445SW · Modification part · Apr 8, 2021
- [ST-984-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID783193906320210810161807.0001): Installation of S-TEC 01326 Digital Flight Control System (DFCS). S-TEC Corporation · PMA PQ0445SW · Modification part · Apr 8, 2021
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID909759096020210702175208.0001): Aspen Avionics · PMA PQ03868SW · Jan 20, 2021
- [1049-4000-03-001C](https://drs.faa.gov/browse/excelExternalWindow/FB6A4D62429A217F86258633006145AB.0001): Roll Steering Converter. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4201-20](https://drs.faa.gov/browse/excelExternalWindow/ED78E4F8D3C63347862586330061461D.0001): Annunciator Kit GDC31. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4200-20](https://drs.faa.gov/browse/excelExternalWindow/CBC6239248334CCE86258633006145E5.0001): Connector Kit GDC31. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4200-50](https://drs.faa.gov/browse/excelExternalWindow/86CBD103649292948625863300614693.0001): Isolation Coupler Installation Kit. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4000-03-001B](https://drs.faa.gov/browse/excelExternalWindow/6583D9B2B4E75DBE862586330061451A.0001): E50Roll Steering Converter. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4801-01](https://drs.faa.gov/browse/excelExternalWindow/39A0DF401545910A8625863300614652.0001): Isolation Coupler. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [APS68-01700](https://drs.faa.gov/browse/excelExternalWindow/51CDE584B1A22102862586290049EFF5.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01700 · Nov 4, 2020
- [ALE-2008AE-AC](https://drs.faa.gov/browse/excelExternalWindow/E2B30B020A91DE91862585DE00509F79.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AE, as used in alternators ALT… · Sep 1, 2020
- [RA154-03000](https://drs.faa.gov/browse/excelExternalWindow/DD82997F649BC443862585E40035802A.0001): Molded Grease Seal. Rapco Inc · PMA PQ2101CE · Replaces Cleveland Wheels & Brakes 154-03000 · Sep 1, 2020
- [ALE-2008AA-AC](https://drs.faa.gov/browse/excelExternalWindow/C617AAB83C6B799B862585DE0050A01D.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AA, as used in alternators ALY… · Sep 1, 2020
- [XA-943FS-AC](https://drs.faa.gov/browse/excelExternalWindow/B7CC6ECA46AA2F14862585DE00509E71.0001): Pos. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-943FS, as used in alternators ALE… · Sep 1, 2020
- [ALE-1013AS-AC](https://drs.faa.gov/browse/excelExternalWindow/9F424D3467678943862585DE00509EFC.0001): Alternator Brush. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-1013AS, as used in alternators ALE… · Sep 1, 2020
- [ALU-3045BS-AC](https://drs.faa.gov/browse/excelExternalWindow/68353ACEF594EACF862585DE0050A127.0001): Brush Assembly. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALU-3045BS, as used in alternators ALE… · Sep 1, 2020
- [ALE-2008ABS-AC](https://drs.faa.gov/browse/excelExternalWindow/6583E821C11FC24F862585DE0050A086.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008ABS, as used in alternators… · Sep 1, 2020
- [XA-944JS-AC](https://drs.faa.gov/browse/excelExternalWindow/0388185039CFC4DD862585DE00509DDD.0001): Neg. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-944JS, as used in alternators ALE… · Sep 1, 2020
- [APS068-01700](https://drs.faa.gov/browse/excelExternalWindow/068001A41B0BCCA9862585EC004522B5.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01700 · Aug 26, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID887550545520220125131316.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID761917634820220125131457.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID519877368620220125131335.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID253032526202201251314340.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID231190298420220125131352.0001): DAC International · PMA PQ0986SW · Jul 31, 2020

All of them: https://openairdocs.org/model/aerostar-pa-60-601/pma.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.