# Pilatus Flugzeugwerke PC-12/45

- Type: Aircraft model (FAA registry)
- Registry code: 7090503
- Manufacturer (registry): PILATUS FLUGZEUGWERKE AG
- Model: PC-12/45
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Turbo-prop
- Seats: 11
- Weight class: 12,500 to 19,999 lb
- Certification: Type certificated
- Data sheet: [TCDS A78EU](https://openairdocs.org/tcds/A78EU) (OpenAirDocs)
- Holder: Pilatus Aircraft Ltd.
- Registered aircraft: 8
- Page: https://openairdocs.org/model/pilatus-flugzeugwerke-pc-12-45

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 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2024-08-07](https://openairdocs.org/ad/2024-08-07): Main Landing Gear Attach Section · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Jun 3, 2024
- [AD 2023-09-12](https://openairdocs.org/ad/2023-09-12): Air Conditioning System Wiring · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Jul 5, 2023
- [AD 2021-24-01](https://openairdocs.org/ad/2021-24-01): Aerodynamic Faring · Pilatus PC-12/45, PC-12/47 and PC-12/47E with STC SA00634DE. Effective Jan 13, 2022
- [AD 2020-21-23](https://openairdocs.org/ad/2020-21-23): Stabilizers · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Dec 7, 2020
- [AD 2016-18-05](https://openairdocs.org/ad/2016-18-05): Power Plant · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Oct 6, 2016
- [AD 2016-12-01](https://openairdocs.org/ad/2016-12-01): Wings · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Jul 15, 2016
- [AD 2015-19-15](https://openairdocs.org/ad/2015-19-15): Flight Controls · Pilatus PC-12, PC-12/45 and PC-12/47E. Effective Nov 3, 2015
- [AD 2008-07-11 R1](https://openairdocs.org/ad/2008-07-11-R1): Flight Controls · Pilatus PC-12, PC-12/45 and PC-12/47. Effective Mar 25, 2013
- [AD 2009-08-11](https://openairdocs.org/ad/2009-08-11): Ice and Rain Protection · Pilatus PC-12 and PC-12/45. Effective May 26, 2009
- [AD 2009-05-07](https://openairdocs.org/ad/2009-05-07): Rear stick-pusher cable · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Mar 30, 2009
- [AD 2008-07-11](https://openairdocs.org/ad/2008-07-11): Pitch trim actuator · Pilatus PC-12, PC-12/45 and PC-12/47. Effective May 9, 2008
- [AD 2008-02-03](https://openairdocs.org/ad/2008-02-03): MLG special bolts · Pilatus PC-12, PC-12/45 and PC-12/47. Effective Feb 20, 2008
- [AD 2007-21-11](https://openairdocs.org/ad/2007-21-11): Oil pile assemblies · Pilatus PC-12, PC-12/45 and PC-12/47. Effective Nov 5, 2007
- [AD 2007-03-06](https://openairdocs.org/ad/2007-03-06): Executive seats equipped with pedestal legs · Pilatus PC-12 and PC-12/45. Effective Mar 8, 2007
- [AD 2006-16-13](https://openairdocs.org/ad/2006-16-13): Lug fittings. · Pilatus PC-12 and PC-12/45. Effective Sep 18, 2006
- [AD 2006-08-11](https://openairdocs.org/ad/2006-08-11): Crew seat bucket assemblies · Pilatus PC-12 and PC-12/45. Effective Jun 2, 2006
- [AD 2005-22-13](https://openairdocs.org/ad/2005-22-13): Left and right main landing gear (MLG) assemblies · Pilatus PC-12 and PC-12/45. Effective Dec 19, 2005
- [AD 2005-22-04](https://openairdocs.org/ad/2005-22-04): Nose landing gear (NLG), main landing gear (MLG), and MLG shock absorber  
 assemblies · Pilatus PC-12 and PC-12/45. Effective Dec 12, 2005
- [AD 2005-11-06](https://openairdocs.org/ad/2005-11-06): Pitch actuator · Pilatus PC-12 and PC-12/45. Effective Jul 18, 2005
- [AD 2005-04-16](https://openairdocs.org/ad/2005-04-16): Windshield de-ice wiring system · Pilatus PC-12 and PC-12/45. Effective Mar 8, 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 2005-01-11](https://openairdocs.org/ad/2005-01-11): Main Landing Gear (MLG) Actuator · Pilatus PC-12 and PC-12/45. Effective Feb 22, 2005
- [AD 2004-12-11](https://openairdocs.org/ad/2004-12-11): Outboard flap flexshafts · Pilatus PC-12 and PC-12/45. Effective Jul 26, 2004
- [AD 2004-06-05](https://openairdocs.org/ad/2004-06-05): Main landing gear shock absorber · Pilatus PC-12 and PC-12/45. Effective May 6, 2004
- [AD 2004-04-01](https://openairdocs.org/ad/2004-04-01): Engine-driven pump housing · Pilatus PC-12, PC-12/45 and PC-7. Effective Mar 29, 2004
- [AD 2003-20-15](https://openairdocs.org/ad/2003-20-15): Fuel booster pump · Pilatus PC-12 and PC-12/45. Effective Oct 10, 2003
- [AD 2003-11-17](https://openairdocs.org/ad/2003-11-17): Pressure dome · Pilatus PC-12 and PC-12/45. Effective Jul 28, 2003
- [AD 2003-09-11](https://openairdocs.org/ad/2003-09-11): Pedestal Leg Assembly on Aft Facing Passenger Seats · Pilatus PC-12 and PC-12/45. Effective Jun 16, 2003
- [AD 2003-07-10](https://openairdocs.org/ad/2003-07-10): Push switch caps · Pilatus PC-12 and PC-12/45. Effective May 12, 2003
- [AD 2002-14-22](https://openairdocs.org/ad/2002-14-22): Main Landing Gear (MLG) Assembly Bolts · Pilatus PC-12 and PC-12/45. Effective Aug 29, 2002
- [AD 2002-06-10](https://openairdocs.org/ad/2002-06-10): Connector and Oxygen Tubing and Related Components in Rear Seat Bench · Pilatus PC-12 and PC-12/45. Effective May 6, 2002
- [AD 2001-25-10](https://openairdocs.org/ad/2001-25-10): Flap Control System · Pilatus PC-12 and PC-12/45. Effective Jan 25, 2002
- [AD 2001-22-15](https://openairdocs.org/ad/2001-22-15): Cargo Doors · Pilatus PC-12 and PC-12/45. Effective Dec 26, 2001
- [AD 2001-11-02](https://openairdocs.org/ad/2001-11-02): Generator · Pilatus PC-12 and PC-12/45. Effective Jul 23, 2001
- [AD 2000-26-17](https://openairdocs.org/ad/2000-26-17): Windshield Deicing System · Pilatus PC-12 and PC-12/45. Effective Feb 24, 2001
- [AD 2000-11-14](https://openairdocs.org/ad/2000-11-14): Airframe Pneumatic Deicing Boots · Pilatus PC-12 and PC-12/45. Effective Jul 17, 2000
- [AD 2000-02-31](https://openairdocs.org/ad/2000-02-31): Stick Pusher System · Pilatus PC-12 and PC-12/45. Effective Mar 27, 2000
- [AD 99-24-09](https://openairdocs.org/ad/99-24-09): Flap Inboard Attachment Fittings · Pilatus PC-12 and PC-12/45. Effective Jan 14, 2000
- [AD 99-17-01](https://openairdocs.org/ad/99-17-01): Flap Drive Shafts · Pilatus PC-12 and PC-12/45. Effective Oct 1, 1999
- [AD 99-14-03](https://openairdocs.org/ad/99-14-03): Generator Cables · Pilatus PC-12 and PC-12/45. Effective Aug 17, 1999
- [AD 99-06-17](https://openairdocs.org/ad/99-06-17): Second Generator Control Unit · Pilatus PC-12 and PC-12/45. Effective Jun 16, 1999
- [AD 99-06-05](https://openairdocs.org/ad/99-06-05): Alternate Flap System · Pilatus PC-12 and PC-12/45. Effective Apr 16, 1999
- [AD 98-21-27](https://openairdocs.org/ad/98-21-27): Passenger Seats And Seat Rail Covers · Pilatus PC-12 and PC-12/45. Effective Nov 26, 1998
- [AD 98-20-28](https://openairdocs.org/ad/98-20-28): Airplane Flight Manual (AFM) - Limitations Icing · Pilatus PC-12 and PC-12/45. Effective Nov 4, 1998
- [AD 98-11-01 R2](https://openairdocs.org/ad/98-11-01-R2): Fuel Tank Vent Valves · Pilatus PC-12 and PC-12/45. Effective Sep 22, 1998
- [AD 98-11-20](https://openairdocs.org/ad/98-11-20): Lavatory Wall and Passenger Seat Configuration · Pilatus PC-12 and PC-12/45. Effective Jul 13, 1998
- [AD 98-08-26](https://openairdocs.org/ad/98-08-26): Fuel Tank Underwing Access Panels · Pilatus PC-12 and PC-12/45. Effective May 29, 1998
- [AD 98-07-18](https://openairdocs.org/ad/98-07-18): Propeller De-icing Controller · Pilatus PC-12 and PC-12/45. Effective Apr 28, 1998
- [AD 98-04-16](https://openairdocs.org/ad/98-04-16): Aileron Tie-Rod Jam Nuts · Pilatus PC-12 and PC-12/45. Effective Apr 2, 1998

Historical (superseded or no longer in force):

- [AD 2023-12-17](https://openairdocs.org/ad/2023-12-17) (historical): Horizontal Stabilizer, Spar/Rib · Pilatus PC-12, PC-12/47, PC-12/45 and 1 more. Effective Aug 7, 2023
- [AD 2022-19-03](https://openairdocs.org/ad/2022-19-03) (historical): Rudder Actuator, Main Landing Gear, Main Landing Gear Attach Section · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Oct 27, 2022
- [AD 2016-26-08](https://openairdocs.org/ad/2016-26-08) (historical): Time Limits · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Feb 9, 2017
- [AD 2014-22-01](https://openairdocs.org/ad/2014-22-01) (historical): Time Limits · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Dec 18, 2014
- [AD 2012-26-16](https://openairdocs.org/ad/2012-26-16) (historical): Time Limits · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Mar 26, 2013
- [AD 2009-14-13](https://openairdocs.org/ad/2009-14-13) (historical): Landing gear · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Aug 19, 2009
- [AD 2008-06-17](https://openairdocs.org/ad/2008-06-17) (historical): Rear stick-pusher · Pilatus PC-12, PC-12/45 and PC-12/47. Effective Apr 2, 2008
- [AD 2003-14-07](https://openairdocs.org/ad/2003-14-07) (historical): Nose landing gear (NLG) · Pilatus PC-12 and PC-12/45. Effective Sep 5, 2003
- [AD 2002-01-09](https://openairdocs.org/ad/2002-01-09) (historical): Gasket Material and Relief Valve Attachment Screws · Pilatus PC-12, PC-12/45 and PC-7. Effective Feb 28, 2002
- [AD 2000-21-14](https://openairdocs.org/ad/2000-21-14) (historical): Torque Oil-pressure Tubes and Py Pressure Pipe · Pilatus PC-12 and PC-12/45. Effective Dec 15, 2000
- [AD 99-19-32](https://openairdocs.org/ad/99-19-32) (historical): Actuator Internal Gear Systems · Pilatus PC-12 and PC-12/45. Effective Nov 8, 1999
- [AD 99-17-08](https://openairdocs.org/ad/99-17-08) (historical): Generator · Pilatus PC-12 and PC-12/45. Effective Oct 4, 1999
- [AD 98-11-01 R1](https://openairdocs.org/ad/98-11-01-R1) (historical): Fuel Tank Vent Valves · Pilatus PC-12 and PC-12/45. Effective Sep 22, 1998
- [AD 98-11-01](https://openairdocs.org/ad/98-11-01) (historical): Fuel Tank Vent Valves · Pilatus PC-12 and PC-12/45. Effective Jun 7, 1998
- [AD 97-23-04](https://openairdocs.org/ad/97-23-04) (historical): Fuel Tank Vent Valves · Pilatus PC-12 and PC-12/45. Effective Dec 1, 1997

## Information bulletins (advisory) (8)

- [SAIB CE-17-13](https://openairdocs.org/saib/CE-17-13): Engine Oil Pressure; Torque Transducer Oil Pressure Pipe P-Clamp Installation. Issued May 19, 2017
- [SAIB CE-05-08](https://openairdocs.org/saib/CE-05-08): . Issued Oct 25, 2004
- [SAIB CE-04-70](https://openairdocs.org/saib/CE-04-70): . Issued Jul 8, 2004
- [SAIB CE-04-62](https://openairdocs.org/saib/CE-04-62): . Issued Apr 12, 2004
- [SAIB CE-04-60](https://openairdocs.org/saib/CE-04-60): . Issued Mar 30, 2004
- [SAIB CE-04-52](https://openairdocs.org/saib/CE-04-52): . Issued Feb 13, 2004
- [SAIB CE-03-19](https://openairdocs.org/saib/CE-03-19): . Issued Jan 22, 2003
- [SAIB CE-02-15](https://openairdocs.org/saib/CE-02-15): . Issued Feb 13, 2002

## Registered aircraft (8)

- [N190PE](https://openairdocs.org/aircraft/N190PE): [US Department Of The Interior](https://openairdocs.org/faa-owner/US%20DEPARTMENT%20OF%20THE%20INTERIOR), [Boise, ID](https://openairdocs.org/faa-place/ID/Boise), built 1997, S/N 190
- [N269LG](https://openairdocs.org/aircraft/N269LG): [Coffin Simon P](https://openairdocs.org/faa-owner/COFFIN%20SIMON%20P), Remseck, built 2005, S/N 633
- [N316TR](https://openairdocs.org/aircraft/N316TR): [Tristar Leasing LLC](https://openairdocs.org/faa-owner/TRISTAR%20LEASING%20LLC), [Poteet, TX](https://openairdocs.org/faa-place/TX/Poteet), built 1996, S/N 142
- [N404BF](https://openairdocs.org/aircraft/N404BF): [Mcdunn Air LLC](https://openairdocs.org/faa-owner/MCDUNN%20AIR%20LLC), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City), built 2001, S/N 386
- [N451SS](https://openairdocs.org/aircraft/N451SS): [Targaryen LLC](https://openairdocs.org/faa-owner/TARGARYEN%20LLC), [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas), built 2004, S/N 579
- [N549RD](https://openairdocs.org/aircraft/N549RD): [Neverland Leasing LLC](https://openairdocs.org/faa-owner/NEVERLAND%20LEASING%20LLC), [Middletown, DE](https://openairdocs.org/faa-place/DE/Middletown), built 2004, S/N 549
- [N670WH](https://openairdocs.org/aircraft/N670WH): [Helimax Aviation LLC](https://openairdocs.org/faa-owner/HELIMAX%20AVIATION%20LLC), [Howell, MI](https://openairdocs.org/faa-place/MI/Howell), built 2005, S/N 670
- [N677ST](https://openairdocs.org/aircraft/N677ST): [Laboratory Corporation Of America Holdings](https://openairdocs.org/faa-owner/LABORATORY%20CORPORATION%20OF%20AMERICA%20HOLDINGS), [Burlington, NC](https://openairdocs.org/faa-place/NC/Burlington), built 2005, S/N 677

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20210121000099I](https://openairdocs.org/incident/20210121000099I), Jan 21, 2021: Pilatus Flugzeugwerke Ag PC-12/45 (N451SS), Chicago, IL, Minor damage. On January 21, 2021, at 1816 local time, flight BTQ835, aircraft N451SS, from gogebic-iron county airport, ironwood, mi (kiwd), to o?hare international…

## Service difficulty reports (982, newest 50)

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

- [SDR 2026FA0000896](https://openairdocs.org/sdr/2026FA0000896), Oct 22, 2026: EHSI. SHORTED. WHEN ENROUTE AT CRUISE OVER THE SLC, PILOT SUDDENLY NOTED AN ELECT BURNING ODOR, & NOTICED THE ELECTRONIC HSI SCREEN DARK. THE ODOR PERMEATED THROUGH ENTIRE CAB
- [SDR QMLA2026091720070](https://openairdocs.org/sdr/QMLA2026091720070), Sep 17, 2026: EHSI. FAULTED. FUMES IN CABIN DUE TO EHSI FAILURE. INSPECTED ELECTRICAL CONNECTOR, WIRING, AND ALL AREAS ADJACENT TO EHSI UNIT. ODOR OF ELECTRICAL BURNING WAS ISOLATED TO THE 
- [SDR 4DSR202609010001](https://openairdocs.org/sdr/4DSR202609010001), Sep 1, 2026: SELECTOR VALVE. LEAKING. DURING O.R, FOUND HYDRAULIC LEAK UNDER AIRCRAFT ON PILOT SIDE AND FOUND FLUID LEAKING FROM BELLY PANEL THAT COVERS THE SELECTOR SERVICE VALVE FOR THE LANDING GE
- [SDR QMLA202608122057](https://openairdocs.org/sdr/QMLA202608122057), Aug 11, 2026: WIRE. CHAFED. ERRONEOUS TORQUE INDICATION
- [SDR QMLA2026081320056](https://openairdocs.org/sdr/QMLA2026081320056), Aug 11, 2026: CIRCUIT BREAKER. TRIPPED. BUS TIE CIRCUIT BREAKER POPPED AS LANDING GEAR WAS BEING RAISED
- [SDR G1IA20260810115](https://openairdocs.org/sdr/G1IA20260810115), Aug 10, 2026: WARNING MESSAGE. MULTIPLE IND. HIGH ITT INDICATIONS WITH SUBSEQUENT EIS IND, INCLUDING CAUTION, WARNING & FLASHING ITT TEMP. ITT TEMP INDNS FLUCTUATE BTWN 920 & 960, REGARDLESS OF TORQUE SETT
- [SDR G1IA20260725114](https://openairdocs.org/sdr/G1IA20260725114), Jul 25, 2026: COMPUTER. FAILED. PUSHER/SHAKER MALFUNCTION. CAWS PUSHER ADVISORY, AUDIO AND SHAKER ACTIVATED UPON TAKEOFF WITH AOA INDICATING "SLOW DIAMOND." PUSHER DID NOT ACTIVATE. ALL PERFOR
- [SDR 2026FA0000577](https://openairdocs.org/sdr/2026FA0000577), Jul 10, 2026: MOTOR. WORN. DURING CRUISE FIGHT THE CREW RECEIVED A HYD CAWS ANNUNCIATION. THE LANDING GEAR DID NOT RESPOND TO THE NORMAL GEAR EXTENSION COMMAND. THE CREW EMERGENCY EXTENDE
- [SDR 4DSR2026063001](https://openairdocs.org/sdr/4DSR2026063001), Jun 30, 2026: SELECTOR VALVE. LEAKING. LANDING GEAR HYD. ACCUMULATOR MOTOR CYCLED IN FLIGHT CAUSING CAUTION TO COME ON. AIRCRAFT WAS JACK AND TROUBLESHOT, FOUND SERVICE SELECTOR VALVE TO BE LEAKING I
- [SDR QMLA2026060120034](https://openairdocs.org/sdr/QMLA2026060120034), May 30, 2026: HEATER. FAILED. DURING CRUISE FLIGHT, CABIN FUMES WERE DETECTED, FOLLOWED BY VISIBLE SMOKE. THE FLIGHT CREW EXECUTED THE EMERGENCY PROCEDURES AND CHECKLISTS, WHICH INCLUDED SHU
- [SDR QMLA2026052620032](https://openairdocs.org/sdr/QMLA2026052620032), May 26, 2026: UNKNOWN. ODOR. PILOT SMELLED UNUSUAL ODOR/SMOKE IN COCKPIT DURING CLIMB OUT
- [SDR Q5QA20260421002](https://openairdocs.org/sdr/Q5QA20260421002), Apr 21, 2026: AOA. FAILED. THE PILOT REPORTED THAT AFTER DEPARTURE HE RECEIVED A SLOW SPEED INDICATION WITH AN ACCOMPANYING STICK SHAKER AND ORAL WARNING EVEN THOUGH HE WAS WELL ABOVE THE
- [SDR G1IA20260330107](https://openairdocs.org/sdr/G1IA20260330107), Mar 30, 2026: ALTIMETER. FAILED. CLIMBING THROUGH 190 THE PILOT SIDE ALTIMETER FAILED, ON DECENT IT STARTED WORKING AGAIN UPON REACHING 17,000. DECLARED AN EMERGENCY TO ATC.
- [SDR QMLA2026031820018](https://openairdocs.org/sdr/QMLA2026031820018), Mar 17, 2026: HYDRAULIC SYSTEM. LOW. LEFT MAIN LANDING GEAR IN-TRANSIT LIGHT ILLUMINATES IN FLIGHT. SERVICED HYD SYSTEM, RTS .
- [SDR QMLA2026031620017](https://openairdocs.org/sdr/QMLA2026031620017), Mar 14, 2026: CIRCUIT BREAKER. FAULTED. RED A/P TRIM LIGHT WITH ASSOCIATED ALARMS & CHIMES. PITCH TRIM EXCURSIONS CAUSING ALTITUDE DEVIATION. RESET AP TRIM CB OPS CHECKED GOOD. RTS
- [SDR G1IA20260212105](https://openairdocs.org/sdr/G1IA20260212105), Feb 13, 2026: ALTIMETER. INOPERATIVE. NR 1 ALTIMETER FAILED DURING DESCENT INTO GUP FROM FL230.
- [SDR G1IA20260208104](https://openairdocs.org/sdr/G1IA20260208104), Feb 8, 2026: RELAY. FAILED. VFR LANDING PHASE, ON BASE LEG FOR RUNWAY 32 AT XWA. COMMANDED GEAR DOWN. MAIN GEAR LOWERED & LOCKED INTO PLACE. VERIFIED 2 GREEN LIGHTS. NOSE GEAR REMAINED RED
- [SDR Q5QA20260206001](https://openairdocs.org/sdr/Q5QA20260206001), Jan 30, 2026: STARTER GEN. VIBRATION. THE PILOT NOTICED AN ENGINE VIBRATION ON DECENT INTO READING REGIONAL AIRPORT. THE #1 STARTER- GENERATOR PART NUMBER A 23085-025, SERIAL NUMBER Y0090 WAS FOUND 
- [SDR Q5QA20251106002](https://openairdocs.org/sdr/Q5QA20251106002), Nov 6, 2025: STARTER GEN. INOPERATIVE. THE PC-12 AIRCRAFT WAS IN TRANSITION FROM KGNV (GAINESVILLE FL) TO KVDF (TAMPA FL) WHEN THE PILOT EXPERIENCED A FAILURE OF THE GENERATOR 1 BUSS, THE AIRCRAFT WE
- [SDR QMLA2025110320111](https://openairdocs.org/sdr/QMLA2025110320111), Nov 3, 2025: BRAKE SYS. WEAK. UPON LANDING THERE WASN'T ANY BRAKE PRESSURE.
- [SDR UATA2025110300701](https://openairdocs.org/sdr/UATA2025110300701), Oct 27, 2025: SKIN. WORN. TOP RUDDER STATIC WICK BASE DAMAGED (MAJOR REPAIR). REPLACED DAMAGED SKIN, SEE FORM 337 DATED 10/27/25 FOR FURTHER DETAIL. INSTALLED NEW STATIC IS CHARGE BASE P
- [SDR QMLA2025102320107](https://openairdocs.org/sdr/QMLA2025102320107), Oct 22, 2025: FUEL FILTER. WARNING MESSAGE. FUEL PRESS CAWS INDICATION DURING CRUISE FLIGHT THAT DID NOT EXTINGUISH. FUEL CAWS LIGHT , INSPECTED, REPLACED FUEL FILTER, RTS.
- [SDR G1IA20250909096](https://openairdocs.org/sdr/G1IA20250909096), Sep 9, 2025: CIRCUIT BREAKER. TRIPPED. AFTER TAKEOFF, USED THE GEAR HANDLE TO PULL THE GEAR UP AND SHORTLY AFTER THE HYD CAWS MESSAGE ILLUMINATED AND THE NOSE GEAR INDICATOR WAS RED. RAN EMERGENCY CH
- [SDR QMLA202507262079](https://openairdocs.org/sdr/QMLA202507262079), Jul 19, 2025: COWLING. FAILED. A HAMMER WAS DISCOVERED ON THE ENGINE COWING DURING TAKEOFF AS IT ROLLED ONTO THE WINDSCREEN DURING TAKEOFF. SDR FORM SUBMITTED ON 07/23/2025.
- [SDR QMLA2025061620066](https://openairdocs.org/sdr/QMLA2025061620066), Jun 15, 2025: UNKNOWN. SMOKE. SMOKE SMELL FROM BATTERY FROM BATTERY COMPARTMENT DURING PRE LAUNCH WALK AROUND, UNABLE TO DUPLICATE RTS.
- [SDR 2025FA0000367](https://openairdocs.org/sdr/2025FA0000367), May 20, 2025: LINE. OUT OF POSITION. OUTBOARD DEICE BOOTS, RH WING INFLATING IN INCORRECT SEQUENCE. TWO DEICE HARD LINES WERE INSTALLED IN REVERSED POSITIONS DURING A RECENT WING REPLACEMENT. THE L
- [SDR QMLA2025051920057](https://openairdocs.org/sdr/QMLA2025051920057), May 15, 2025: DAMPENER. FAILED. SHIMMY DAMPENER FAILURE UPON LANDING. REPLACED DAMPER.
- [SDR 9CKC20250402001](https://openairdocs.org/sdr/9CKC20250402001), Mar 7, 2025: WINDSCREEN. CRACKED. ON MARCH 7, 2025, AT ABOUT 17:30 LOCAL ALASKA TIME, WHILE IN CRUISE FLIGHT AT FL270 ENROUTE FROM SCAMMON BAY, AK, RETURNING TO ANCHORAGE, AK, PILATUS PC12-45 N3
- [SDR QMLA2025013020010](https://openairdocs.org/sdr/QMLA2025013020010), Jan 29, 2025: BRAKE ASSY. FAULTED. LEFT BRAKE HAD GRINDING NOISE AND WAS GRABBING UPON BRAKE APPLICATION.
- [SDR QMLA2025011020002](https://openairdocs.org/sdr/QMLA2025011020002), Jan 10, 2025: BOOT. FAILED. HYDRAULIC LIGHT ILLUMINATED DURING LANDING. PROP DE-ICE FAILED IN FLIGHT. - CHECKED FLUID LEVELS AND NITRO PSI. - CLEANED HYD. PSI TRANSMITTER / SWITCH CONNECTI
- [SDR 2024FA0000964](https://openairdocs.org/sdr/2024FA0000964), Dec 16, 2024: RELAY. FAILED. DURING NORMAL APPROACH THE PILOT SELECTED GEAR DOWN, THE HYDRAULIC POWER PACK FAILED TO ENERGIZE RESULTING IN THE LANDING GEAR FAILING TO EXTEND. THE PILOT MANU
- [SDR QMLA2024120320147](https://openairdocs.org/sdr/QMLA2024120320147), Dec 2, 2024: PRESSURE SWITCH. FAULTED. DE-ICE BOOT CAWS WARNING IN FLIGHT, ITEM IS MEL'D CURRENTLY. REMOVED AND REPLACED HORZ. STAB PRESSURE SWITCH WITH NEW UNIT.
- [SDR QMLA2024111420143](https://openairdocs.org/sdr/QMLA2024111420143), Nov 12, 2024: PROPELLER. FAULTED. REPEATED PROP DE-ICE CAWS. AMTS HAVE CLEANED AND REPLACED BRUSH BLOCK, TESTED OAT PROBE, CHECKED WIRING AND PROBLEM KEEPS REPEATING. CHECKED WIRING AND CLEANED 
- [SDR QMLA2024091920120](https://openairdocs.org/sdr/QMLA2024091920120), Sep 18, 2024: FUSIBLE PLUG. FAILED. LANDED ON A 10000 FT RUNWAY AND CLEARED OFF AT THE END. BRAKES WERE NOT USED. AFTER PARKED AND SHUTDOWN, THE CREW PUT THEIR EQUIPMENT INTO THE AMBULANCE AND LEF
- [SDR Q5QA20240918007](https://openairdocs.org/sdr/Q5QA20240918007), Sep 18, 2024: ATTACH BRACKET. CRACKED. DURING A ROUTINE PILATUS 1200HR INSPECTION THE NOSE GEAR ACTUATOR UPPER ATTACH BRACKET (P/N 553.10.12.326) WAS FOUND CRACKED. THE PART WAS ORIGINAL WITH A TOTAL
- [SDR QMLA2024090620107](https://openairdocs.org/sdr/QMLA2024090620107), Sep 4, 2024: WARNING MESSAGE. ILLUMINATED. DURING CLIMB FROM GJT, AT ABOUT 1000 AGL, I RECEIVED A MASTER WARNING ESSENTIAL BUS AND SEVERAL MASTER CAUTION LIGHTS GEN1, GEN2, AND BAT. THE QRH DOESN'T GIVE 
- [SDR 2024F00242](https://openairdocs.org/sdr/2024F00242), Aug 31, 2024: STARTER GEN. FAILED. ROUGHLY 20-30 MINUTES INTO FLIGHT KBOI-KOGD, GEN 1 OFF AND N ESNTL BUS CAWS INDICATIONS ILLUMINATED. PILOT RAN QRH PROCEDURES BY RESETTING GEN 1, THEN PULLING T
- [SDR 2024F00241](https://openairdocs.org/sdr/2024F00241), Aug 31, 2024: STARTER GEN. FAILED. ROUGHLY 20-30 MINUTES INTO FLIGHT KBOI-KOGD, GEN 1 OFF AND N ESNTL BUS CAWS INDICATIONS ILLUMINATED. PILOT RAN QRH PROCEDURES BY RESETTING GEN 1, THEN PULLING T
- [SDR 2024F00240](https://openairdocs.org/sdr/2024F00240), Aug 31, 2024: STARTER GEN. FAILED. ROUGHLY 20-30 MINUTES INTO FLIGHT KBOI-KOGD, GEN 1 OFF AND N ESNTL BUS CAWS INDICATIONS ILLUMINATED. PILOT RAN QRH PROCEDURES BY RESETTING GEN 1, THEN PULLING T
- [SDR G1IA202409104066](https://openairdocs.org/sdr/G1IA202409104066), Aug 24, 2024: BUSS TIE. FAILED. DURING THE INITIAL APPROACH SEGMENT, A DUAL GENERATOR FAILURE OCCURRED - WITH NEGATIVE RESULTS TO RESTORE POWER FOLLOWING THE ESTABLISHED PROCEDURE THROUGH THE 
- [SDR QMLA2024081620101](https://openairdocs.org/sdr/QMLA2024081620101), Aug 13, 2024: CONTROL VALVE. FAILED. ALL OF CREW NOTED A MELTING OR BURNING PLASTIC SMELL. WE WERE ABOUT TO BEGIN OUR DESCENT FOR BASE, AND WERE ONLY ABOUT 15 MINUTES OUT, WITH MULTIPLE ALTERNATIVE
- [SDR QMLA2024072620091](https://openairdocs.org/sdr/QMLA2024072620091), Jul 26, 2024: CIRCUIT BREAKER. TRIPPED. WE TOOK OFF ON A FLIGHT TO A SENDING FACILITY TO PICK UP A PATIENT. DURING CLIMB OUT, THE 'BUS TIE' CIRCUIT BREAKER TRIPPED, ALONG WITH ASSOCIATED WARNINGS AND 
- [SDR QMLA2024072320090](https://openairdocs.org/sdr/QMLA2024072320090), Jul 20, 2024: BRAKE ASSY. LOCKED. DURING TOWING OF THE AIRCRAFT THE RH BRAKE ASSEMBLY LOCKED UP AND WOULD NOT ROTATE. THE BRAKE PLATE BROKE APART AND JAMMED THE WHEEL FROM ROTATING
- [SDR Q5QA20240715006](https://openairdocs.org/sdr/Q5QA20240715006), Jul 15, 2024: ECU. FAILED. THE AIRCRAFT WAS IN ROUTE TO KROA FROM KLZU AT AN ALTITUDE OF 25,000 ON JULY 13, 2024, WHEN THE PILOT EXPERIENCED AN ENVIRONMENTAL CONTROL UNIT FAILURE MASTER W
- [SDR QMLA2024071620086](https://openairdocs.org/sdr/QMLA2024071620086), Jul 13, 2024: WARNING HORN. FALSE ACTIVATION. ESS BUS LT W/ ESS BUS BATTERY AUDIO INTERMITTENTLY COMES ON IN FLIGHT UNABLE TO DUPLICATE FAULT ON GROUND
- [SDR QMLA2024071920088](https://openairdocs.org/sdr/QMLA2024071920088), Jul 6, 2024: BRAKE. UNSERVICEABLE. INSTALL OVERHAULED MAIN WHEEL BRAKE ASSEMBLY ON 07/02/2024. NO ISSUES FOR SEVERAL MISSIONS UNTIL SATURDAY 07/06/2024. PILOT SAID BRAKE PEDDLE SOFT, TECHNICIANS 
- [SDR Q5QA20240627005](https://openairdocs.org/sdr/Q5QA20240627005), Jun 26, 2024: AHRS. MALFUNCTIONED. DURING FLIGHT THE AHRS SYSTEM RESET WHILE ENCOUNTERING SEVERE TURBULENCE REQUIRING EMERGENCY ACTION. ALL SYSTEMS EVENTUALLY CAME BACK ONLINE AFTER EXITING THE T
- [SDR QMLA2024062120065](https://openairdocs.org/sdr/QMLA2024062120065), Jun 21, 2024: RELAY. FAULTED. AFTER TAKEOFF, RETRACTED THE GEAR AND TURNED ON YAW DAMPER, GOT THE RUNAWAY TRIM TONE AND AIRPLANE TRIED TO CLIMB 5000 + FT PER MIN, PUSHED THE TRIM INTERRUPT S
- [SDR QMLA040820035](https://openairdocs.org/sdr/QMLA040820035), Apr 4, 2024: BATTERY. FAILED. BEEN RECEIVING BATTERIES (P N# RG-380E/44)FROM VENDOR ISATAIR IN FLORIDA AS BEING REPAIRED AND NONE ARE HOLDING APM,S WE ARE CONSTANTLY HAVING FLAP RESETS AND O
- [SDR G1IA20240312061](https://openairdocs.org/sdr/G1IA20240312061), Mar 12, 2024: CHIP DETECTOR. UNSERVICEABLE. DISCREPANCY: IN CRUISE FLIGHT THE CHIP CWAS LIGHT STARTED TO CONTINUOUSLY FLASH ON AND OFF, THIS CONTINUED THROUGHOUT THE DESCENT. DECLARED AN EMERGENCY WITH AT

All 982: https://openairdocs.org/model/pilatus-flugzeugwerke-pc-12-45/reports.md

## STCs that may be installed (OpenAirDocs) (160, 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 SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [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 SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA02742NY](https://openairdocs.org/stc/SA02742NY): Installation of MT-Propeller Entwicklung GmbH model MTV-27-1-N-C-F-R(P)/CFR260-65. MT- Propeller Entwicklung GmbH
- [STC SA04763NY](https://openairdocs.org/stc/SA04763NY): Installation of of Gogo Galileo HDX. Pro Star Aviation LLC
- [STC SA03275CH](https://openairdocs.org/stc/SA03275CH): Installation of an antiskid brake system. Lee Air Inc
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc
- [STC SA04841NY](https://openairdocs.org/stc/SA04841NY): Installation of replacement LED recognition lights, LED wingtip lights, LED beacon lights, LED taxi lights, and LED landing lights. Whelen Aerospace Technologies
- [STC SA04278NY](https://openairdocs.org/stc/SA04278NY): Installation of the GPS/Iridium Antenna Provisions. SKYTRAC Systems Ltd
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc
- [STC SA01527CH](https://openairdocs.org/stc/SA01527CH): Installation of a Honeywell KMH 880 Multi-Hazard Awareness System or a Honeywell KTA 870 Traffic Advisory System. Amphenol Cable and Interconnect Technologies Inc
- [STC SA04220NY](https://openairdocs.org/stc/SA04220NY): Installation of Retractable Camera Mount System. Trine Aerospace & Defense
- [STC SA02558SE](https://openairdocs.org/stc/SA02558SE): Installation of a Light Emitting Diode (LED) Landing and Taxi Light. AeroLED's Holdings LLC
- [STC SA04051CH](https://openairdocs.org/stc/SA04051CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC SA00028MC](https://openairdocs.org/stc/SA00028MC): Installation of non-essential antenna and radome. Sierra Nevada Company LLC
- [STC SA03316CH](https://openairdocs.org/stc/SA03316CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development Inc
- [STC SA00229MC](https://openairdocs.org/stc/SA00229MC): Installation of Dual Mode Recognition Lights. Sierra Nevada Company LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02266LA](https://openairdocs.org/stc/SA02266LA): Installation of a Pratt and Whitney PT6A-67P. Finnoff Aviation Products 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 SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA03097AT](https://openairdocs.org/stc/SA03097AT): Installation of Cabin Interior Light Emitting Diode (LED) Reading and Wash Lights and Air Gaspers. Woven Electronics, LLC
- [STC SA01044DE](https://openairdocs.org/stc/SA01044DE): This STC approves the Finnoff Aviation Products installation of the TB44 advanced lithium-ion battery manufactured by True Blue Power in the make and model listed above (Single Battery Configuration). Finnoff Aviation Products
- [STC SA01376CH](https://openairdocs.org/stc/SA01376CH): Installation of Parker Hannifin Wheel/Brake Assembly P/N 40-424/30-244 (conversion kit no. 199-241). 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 SA02254AK](https://openairdocs.org/stc/SA02254AK): Installation of "Single Screen", "2 or 3 Screen", "Dual Screen", or "4 or 6 screen". 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 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 SA02075SE](https://openairdocs.org/stc/SA02075SE): Installation of a Mid-Continent MD835( ) Lithium Ion Battery. Mid-Continent Instrument Co. Inc
- [STC SA04556NY](https://openairdocs.org/stc/SA04556NY): Installation of so-called Seat Slides JG into the cabin. J.G.A
- [STC SA00272LA](https://openairdocs.org/stc/SA00272LA): Installation of a Patient Loading Utility System (PLUS). LifePort LLC
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC SA02427AK](https://openairdocs.org/stc/SA02427AK): Installation of the Max-Viz® Enhanced Vision System (EVS) Model-1500 on Pilatus PC-12 aircraft equipped with a fixed-mounted or panel-mounted Multi-Function Display (MFD) with the ability to display video imagery. PECO Inc
- [STC SA01116WI-D](https://openairdocs.org/stc/SA01116WI-D): Installation of a Honeywell AM-250 Altimeter. Honeywell International Inc
- [STC SA01253WI-D](https://openairdocs.org/stc/SA01253WI-D): Approved for model PC-12/45, S/N 101 and after, not to exceed S/N 540. Group airworthiness approval for Reduced Vertical Separation Minimum (RVSM). Honeywell International Inc
- [STC SA00886WI-D](https://openairdocs.org/stc/SA00886WI-D): Installation of Honeywell KGP 560 General Aviation Enhanced Ground Proximity Warning System (GA-EGPWS) with optional KMD 550/850 Multi-Function Display. Honeywell International Inc
- [STC SA01524WI-D](https://openairdocs.org/stc/SA01524WI-D): Models PC-12, PC-12/45 and PC-12/47 - Installation of the alternate part number EFS 40/50 SG 465 Symbol Generator. Honeywell International Inc
- [STC SA00393BO](https://openairdocs.org/stc/SA00393BO): Installation of the Pratt & Whitney Engine Services FAST System. Pratt & Whitney Engine Services Inc
- [STC SA01865WI](https://openairdocs.org/stc/SA01865WI): Installation of Generator 2 RCCB Upgrade and/or Dual Battery Cockpit Labeling. Finnoff Aviation Products
- [STC SA01855WI](https://openairdocs.org/stc/SA01855WI): Installation of the Send Solutions Airtext Router in 14 CFR Part 23 Aircraft. 3S Certification LLC
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc

All 160: https://openairdocs.org/model/pilatus-flugzeugwerke-pc-12-45/stcs.md

## PMA parts (OpenAirDocs) (990, 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.

- [AA-3074](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126722635620261019152856.0001): Block Assembly Carbon. Aero Accessories LLC · PMA PQ1206CE · Replaces Pilatus P/N: A-3074 968.29.11.375 · Oct 2, 2026
- [TA109770-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190711249620260818171545.0001): Engine Preheat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · Jun 2, 2026
- [TA109770-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159725188520260818171545.0001): Engine Preheat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · Jun 2, 2026
- [68-955-OAA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162016910520260729141226.0001): O-Ring. Omega Aircraft Articles LLC · PMA PQ4191CE · Replaces 68-955 · Jun 1, 2026
- [68-216-OAA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145756719820260729141224.0001): O-Ring. Omega Aircraft Articles LLC · PMA PQ4191CE · Replaces 68-216 · Jun 1, 2026
- [556.20.12.040](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158588691820260527153828.0001): Window, Cabin. Nordam Group Inc, Transparency Division, The · PMA PQ0327SW · Replaces 556.20.12.040 · May 18, 2026
- [556.20.12.029](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145666038220260527153829.0001): Window, Cabin. Nordam Group Inc, Transparency Division, The · PMA PQ0327SW · Replaces 556.20.12.029 · May 18, 2026
- [MCG-1916](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177107511920260324201135.0001): Dampener Hub. Miraj Corporation · PMA PQ0870NE · Replaces 23032-1916 · Mar 4, 2026
- [M23032-2716](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176513850920251223145954.0001): Dampener, Back Plate. Miraj Corporation · PMA PQ0870NE · Replaces 23032-2716 · Dec 19, 2025
- [LSM-500-075](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111587175620251216163756.0001): Boom Beam Installation – Pilatus PC-12. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Dec 1, 2025
- [RG25108ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132496704920250926144300.0001): Coupling, Drive. Aircraft Component Design LLC · PMA PQ2138NE · Replaces RG25108 · Sep 10, 2025
- [01-0790350-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194599937920250811135906.0001): LED GND Recognition LT Upper, Model 9035002. Whelen Aerospace Technologies · PMA PQ0610NE · Replaces 9728769351 · Aug 8, 2025
- [01-0790350-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177334734520250811135906.0001): LED GND Recognition LT Upper, Model 9035003. Whelen Aerospace Technologies · PMA PQ0610NE · Replaces 9728769352 · Aug 8, 2025
- [01-0771375-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171338220520250811135907.0001): Model 7137500 Flasher Assembly. Whelen Aerospace Technologies · PMA PQ0610NE · Replaces 9728787260 · Aug 8, 2025
- [01-0790195-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159706709120250811135905.0001): Landing Light, Model 9019510. Whelen Aerospace Technologies · PMA PQ0610NE · Replaces 9728769438 · Aug 8, 2025
- [01-0790877-17](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153555988820250811135906.0001): Orion 660, Model OR660PG, 28VDC Green. Whelen Aerospace Technologies · PMA PQ0610NE · Replaces 9728769353 · Aug 8, 2025
- [01-0790195-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150820507420250811135905.0001): Taxi Light, Model 9019515. Whelen Aerospace Technologies · PMA PQ0610NE · Replaces 9728769437 · Aug 8, 2025
- [01-0772147-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137771628920250811135906.0001): Recognition Light Assembly. Whelen Aerospace Technologies · PMA PQ0610NE · Replaces 9728769439 · Aug 8, 2025
- [01-0790971-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121863501620250811135907.0001): Model 9097102 Tail Logo Light, Lower. Whelen Aerospace Technologies · PMA PQ0610NE · Replaces 9728769440 · Aug 8, 2025
- [01-0790877-18](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112778357020250811135906.0001): Orion 660, Model OR660PR, 28VDC Red. Whelen Aerospace Technologies · PMA PQ0610NE · Replaces 9728769354 · Aug 8, 2025
- [8003030-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161468877020250722192827.0001): Engine Oil Cooler Assembly. Aero-Classics Heat Transfer Products Inc · PMA PQ2543NM · Replaces 968.32.14.104 · Jul 18, 2025
- [MQAR-Y-XXXXZZZZ#](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188354675220250918135513.0001): miniQAR Installation Kit. Avionica LLC. · PMA PQ1734CE · Modification part · Jun 20, 2025
- [650-0100-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179479213220250918135508.0001): avCM 4G. Avionica LLC. · PMA PQ1734CE · Modification part · Jun 20, 2025
- [804-1201, 804-1205, 804-1205-03, 804-1212, 804-1216](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151454426320250918135505.0001): miniQAR MKIII. Avionica LLC. · PMA PQ1734CE · Modification part · Jun 20, 2025
- [650-0100-05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125525575020250918135511.0001): avCM LTE. Avionica LLC. · PMA PQ1734CE · Modification part · Jun 20, 2025
- [M421B224](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184642443620260325180502.0001): Coverplate,Assy. Ametek Ameron LLC d/b/a Mass Systems · PMA PQ1432NM · Replaces 421B224 · Feb 17, 2025
- [APS93-909-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152042603120250131173807.0001): Wear Pad. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 93-909-1 · Jan 21, 2025
- [APS78-265](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142714934220250131173758.0001): Rivet. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 78-265 · Jan 21, 2025
- [MDL PBA.600.103](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192527057020241213142026.0001): Installation Master Drawing List SPECTRE Lift Platform. Pilatus Business Aircraft Ltd. · PMA PQ05449NM · Modification part · Dec 4, 2024
- [PM-208](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108947571220251118174432.0001): Spinner Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · Nov 20, 2024
- [447883LA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177347097620241107175408.0001): Valve, Safety Assy. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 447883 · Nov 5, 2024
- [SP-KT-106-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158177740620241001200544.0001): Overboard Vent Kit. Spectrum Aeromed LLC · PMA PQ2435CE · Modification part · Oct 1, 2024
- [SP-KT-106-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138923537420241001200544.0001): Pneumatic Routing Kit. Spectrum Aeromed LLC · PMA PQ2435CE · Modification part · Oct 1, 2024
- [SP-KT-105-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123815951320241001200544.0001): Sidewall Pneumatic Kit. Spectrum Aeromed LLC · PMA PQ2435CE · Modification part · Oct 1, 2024
- [MQAR-Y-XXXXZZZZ#](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146041480720240924135408.0001): miniQAR Installation Kit. Avionica LLC. · PMA PQ1734CE · Modification part · Sep 20, 2024
- [SMR20-126](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140181686620241115132949.0001): Seal. SMR Acquisition LLC dba SMR Technologies Inc · PMA PQ0845NE · Replaces 552.20.12.126 · Sep 19, 2024
- [LA01000X200A20B6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153050059720241016174902.0001): O-Ring. LanAir Research and Development Inc · PMA PQ1031NE · Replaces R01000X200A20B6 · Aug 28, 2024
- [LA449039](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125677625320241016174954.0001): Mask Lock. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 449039 · Aug 28, 2024
- [PM-192](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126284581220250709145719.0001): Spinner Mask. PM Research, Inc. · PMA PQ10049NE · Replaces NA · Jul 5, 2024
- [PM-190](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185458904420260702135223.0001): Radome Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · Apr 11, 2024
- [MDL DOC-SNC-000373997](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182030321120240515132153.0001): Replacement Main Battery. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Mar 20, 2024
- [MDL 4052-0000-0021](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159417780320240515132154.0001): Dual Mode Recognition Lights. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Mar 20, 2024
- [MDL 4030-0007-22811](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146614977720240515132154.0001): Non-Essential Radio Rack Communications Equipment and Antennas. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Mar 20, 2024
- [01260001-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199856898620240308150031.0001): K Band Antenna System. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024
- [MDL-01030001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196754748120240308150026.0001): Communications equipment and audio management system(NSAV). Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024
- [0126-0200-4007](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195905770220240308150033.0001): Viasat G-12 Ka Antenna Configuration. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024
- [01260001-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184049340220240308150031.0001): K Band Antenna System. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024
- [01260001-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163279807120240308150031.0001): K Band Antenna System. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024
- [01260001-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159110580120240308150031.0001): K Band Antenna System. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024
- [01260001-05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132308179420240308150031.0001): K Band Antenna System. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024

All of them: https://openairdocs.org/model/pilatus-flugzeugwerke-pc-12-45/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Pilatus PC-12/45](https://openairdocs.org/model/pilatus-pc-12-45): 278 registered aircraft, registry code 7090551
- [Pilatus PC-12/45](https://openairdocs.org/model/pilatus-pc-12-45): 100 registered aircraft, registry code 7090051

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