# Pilatus Flugzeugwerke PC-12/47

- Type: Aircraft model (FAA registry)
- Registry code: 7090504
- Manufacturer (registry): PILATUS FLUGZEUGWERKE AG
- Model: PC-12/47
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Turbo-prop
- Seats: 11
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS A78EU](https://openairdocs.org/tcds/A78EU) (OpenAirDocs)
- Holder: Pilatus Aircraft Ltd.
- Registered aircraft: 6
- Page: https://openairdocs.org/model/pilatus-flugzeugwerke-pc-12-47

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 2015-14-10](https://openairdocs.org/ad/2015-14-10): Flight Controls · Pilatus PC-12/47 and PC-12/47E. Effective Aug 20, 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 2009-05-07](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

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

## Information bulletins (advisory) (1)

- [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

## Registered aircraft (6)

- [N561GG](https://openairdocs.org/aircraft/N561GG): [N561gg LLC](https://openairdocs.org/faa-owner/N561GG%20LLC), [Dover, DE](https://openairdocs.org/faa-place/DE/Dover), built 2007, S/N 830
- [N72DZ](https://openairdocs.org/aircraft/N72DZ): [US Air Force Special Operations Command/Askm](https://openairdocs.org/faa-owner/US%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND%2FASKM), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), S/N 777
- [N796PC](https://openairdocs.org/aircraft/N796PC): [Air Methods LLC](https://openairdocs.org/faa-owner/AIR%20METHODS%20LLC), [Greenwood Village, CO](https://openairdocs.org/faa-place/CO/Greenwood%20Village), built 2007, S/N 796
- [N801J](https://openairdocs.org/aircraft/N801J): [Little Family Farms Lllp](https://openairdocs.org/faa-owner/LITTLE%20FAMILY%20FARMS%20LLLP), [Kenmore, WA](https://openairdocs.org/faa-place/WA/Kenmore), built 2007, S/N 801
- [N821CT](https://openairdocs.org/aircraft/N821CT): [Axiom Aviation Group LLC](https://openairdocs.org/faa-owner/AXIOM%20AVIATION%20GROUP%20LLC), [Webb City, MO](https://openairdocs.org/faa-place/MO/Webb%20City), built 2006, S/N 713
- [N96MV](https://openairdocs.org/aircraft/N96MV): [US Air Force Special Operations Command](https://openairdocs.org/faa-owner/US%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), S/N 793

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (273, newest 50)

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

- [SDR 2026F00122](https://openairdocs.org/sdr/2026F00122), Jun 6, 2026: STRAKE. CRACKED. LH & RH STRAKES WERE REPLACED DUE TO CRACKED MOUNT SPIGOTS AT FRAME 40 ON 12/22/2025 AT TAT 11997.50 TAC 10962. SERVICEABLE UNITS WERE INSTALLED FROM PC-12/47 R
- [SDR 2026FA0000239](https://openairdocs.org/sdr/2026FA0000239), Mar 30, 2026: WIRE. BROKEN. PILOT REPORTED DURING DESCENT INTO PSO WHILE REDUCING POWER TO SLOW, ALL ELECTRICAL POWER WAS LOST FOR APPROXIMATELY 3 SECONDS. ALL SCREENS WENT BLACK. ALL INTE
- [SDR HVUA202605120811](https://openairdocs.org/sdr/HVUA202605120811), Jan 28, 2026: OUTFLOW VALVE. FOD. NEARING TOP OF CLIMB THE CABIN CONTINUED A SHALLOW CLIMB PAST THE SCHEDULED CABIN ALTITUDE. IN RESPONSE THE PILOT DONNED HIS OXYGEN MASK AND INSTRUCTED PASSENGE
- [SDR QMLA2026010620001](https://openairdocs.org/sdr/QMLA2026010620001), Jan 4, 2026: RELAY. MALFUNCTIONED. PRE-TAKEOFF, TAXI, & TAKEOFF NORMAL. AFTER LIFTING & CLIMBING, AUTOPILOT WOULD NOT ENGAGE WHEN TURNED ON. CONTINUED FLT. DURING CLIMB, DISPLAY 2 STARTED PULSING
- [SDR 4GIA2026012700000](https://openairdocs.org/sdr/4GIA2026012700000), Dec 17, 2025: BRACKET. CRACKED. LEFT & RIGHT AFT MOUNT BRACKETS ON STRAKES CRACKED/BROKEN. LH PN: 553-26-12-375 RH PN: 553-26-12-376.
- [SDR QMLA2025080520084](https://openairdocs.org/sdr/QMLA2025080520084), Aug 5, 2025: ELECTRICAL SYS. FAILED. ELECTRICAL SYSTEM FAILURE ON TAXI. BUS TIE OPENED, MULTIPLE SYSTEMS SHUT DOWN, CAWS, MASTER WARNING AND CAUTION ILLUMINATED. UPON SHUT DOWN, SMOKE AND FUMES FOU
- [SDR QMLA2025072620080](https://openairdocs.org/sdr/QMLA2025072620080), Jul 24, 2025: O-RING. PINCHED. CABIN PRESSURIZATION DUMPED WHEN CLIMBING THROUGH FL200. SYSTEM WOULD NOT RESPOND TO ANY INPUTS TO THE CONTROLLER. IS AIRCRAFT HAS BEEN RETURNED TO REVENUE SERV
- [SDR QMLA2025042020050](https://openairdocs.org/sdr/QMLA2025042020050), Apr 20, 2025: THROTTLE. FAULTED. DURING CLIMBOUT, AT 8,000 FEET MSL, THERE WAS NO THROTTLE RESPONSE FOR APPROXIMATELY THE LAST 20% OF THROTTLE LEVER TRAVEL. THE THROTTLE OPERATED NORMALLY THROU
- [SDR 2025FA0000315](https://openairdocs.org/sdr/2025FA0000315), Apr 17, 2025: ENGINE. DAMAGED. TOOK 15 MINUTES TO CLIMB TO 17,000 AND WERE LEVEL FOR APPROXIMATELY 25 MINUTES WHEN A RAPID SERIES OF BLAST NOISES CAME FROM THE ENGINE ACCOMPANIED BY LARGE AMO
- [SDR QMLA2025022720029](https://openairdocs.org/sdr/QMLA2025022720029), Feb 27, 2025: BLEED VALVE. MALFUNCTIONED. UPON DEPARTURE, SET MY POWER TO ROUGHLY 34.5 TORQUE & AFTER ROTATION, ATTEMPTED TO ADD MORE POWER. WHEN ADDED MORE POWER NOTHING HAPPENED & TORQUE STAYED AROUND
- [SDR QMLA2025022120023](https://openairdocs.org/sdr/QMLA2025022120023), Feb 23, 2025: FILTER. BYPASSING. AFTER TAKEOFF OUT KLBF, DURING THE CLIMB OUT, THE CAWS PANEL FUEL PRESSURE LIGHT ILLUMINATED. I RAN THROUGH THE QRH CHECKLIST FOR THAT ANNUNCIATOR WHICH EXTINGU
- [SDR Q5QA20250128001](https://openairdocs.org/sdr/Q5QA20250128001), Jan 28, 2025: ACTUATOR. FAILED. THE AIRCRAFT WAS MOVED TO MAINTENANCE FOR A RIGHT MAIN LANDING GEAR ACTUATOR INDICATION PROBLEM, IT WAS DETERMINED THAT THE PROBLEM WAS INTERNAL TO THE ACTUATOR
- [SDR QMLA2025010620001](https://openairdocs.org/sdr/QMLA2025010620001), Dec 31, 2024: PUMP. INOPERATIVE. LOW FUEL PRESSURE LIGHT ILLUMINATED IN FLIGHT DURING DESCENT. PER QRH, TURNED BOOST PUMPS TO ON AND CONTINUED DESCENT TRYING TO GET TO WARMER AIR. LOW PRESSURE 
- [SDR QMLA2024102220137](https://openairdocs.org/sdr/QMLA2024102220137), Oct 19, 2024: CIRCUIT BREAKER. TRIPPED. AFTER TAKEOFF, THE LANDING GEAR REMAINED DOWN, I WAS CALLED BY THE CONTROL TOWER, I HAD 3 GREEN LIGHTS, AND THE LANDING GEAR LEVER WAS UP, I PROCEEDED TO MAINTA
- [SDR QMLA2024080220095](https://openairdocs.org/sdr/QMLA2024080220095), Aug 2, 2024: AOA. FAULTED. IMMEDIATELY AFTER TAKEOFF THE STICK SHAKER ACTIVATED CONTINUOUSLY WITH THE PUSHER CAWS LIGHT ILLUMINATED. RETURNED TO AIRPORT FOR LANDING.
- [SDR QMLA2024061020061](https://openairdocs.org/sdr/QMLA2024061020061), Jun 10, 2024: CIRCUIT BREAKER. TRIPPED. DURING TAKE OFF THE GEAR DID NOT RETRACT SO THE FLIGHT WAS ABORTED AFTER FINDING THE CIRCUIT BREAKER WAS OUT. MAINTENANCE FOUND THAT THE HYD. CTR (NON ESSENTIAL
- [SDR QMLA2024050120046](https://openairdocs.org/sdr/QMLA2024050120046), Apr 29, 2024: PUMP. FAULTED. WE WERE AT FLIGHT LEVEL 210 IN NORMAL CRUISE. WE HAD BEEN AIRBORNE FOR 2+ HOURS. THE MASTER CAUTION ILLUMINATED SPORADICALLY SEVERAL TIMES BEFORE I COULD SEE IT
- [SDR 2024FA0000257](https://openairdocs.org/sdr/2024FA0000257), Mar 15, 2024: STARTER GEN. FAILED INSP. DURING VISUAL INSPECTION IT WAS NOTED THAT THE STARTER-GENERATOR BRUSHES WERE WORN TO NEAR 1/4 LIFE REMAINING MARKS. UPON REVIEWING THE HISTORY ON THIS STARTER-
- [SDR 2024F00040](https://openairdocs.org/sdr/2024F00040), Feb 18, 2024: STARTER GEN. FAILED. DURING ENGINE START, STARTER-GENERATOR FAILED. STARTER-GENERATOR HAD 20.5 HOURS TSO. OVERHAUL WAS PERFORMED BY FREEDOM AERO, CRS 25FR283B, ON WORK ORDER W29131 
- [SDR 2024F00041](https://openairdocs.org/sdr/2024F00041), Jan 25, 2024: STARTER GEN. FAILED. DURING ENGINE START, STARTER-GENERATOR FAILED. STARTER-GENERATOR HAD 675.4 HOURS TSO. BRUSHES WERE FOUND TO BE WORN TO LIMITS (PREMATURE FAILURE). OVERHAUL WAS 
- [SDR 15DA2023100973501](https://openairdocs.org/sdr/15DA2023100973501), Oct 9, 2023: UNKNOWN. UNKNOWN. ENGINE START AND TAXI WERE BOTH NORMAL IN GROUND IDLE. UPON ACCELERATION AND ROTATION IN FLIGHT IDLE, A DISTINCT SMELL OF "BURNING RUBBER" WAS NOTICED THAT PROG
- [SDR PCPR202308221](https://openairdocs.org/sdr/PCPR202308221), Aug 22, 2023: SCREW. CORRODED. DURING UNSCHEDULED REMOVAL OF LEFT AILERON FOUND BALANCE WEIGHT ATTACH SEVERELY TO MILDLY CORRODED. RIGHT AILERON BALANCE WEIGHT ATTACH SCREWS ALSO FOUND CORROD
- [SDR QMLA2023073120057](https://openairdocs.org/sdr/QMLA2023073120057), Jul 27, 2023: UNKNOWN. UNKNOWN. EN ROUTE TO HOME STATION, THE HYDRAULIC CAWS LIGHT ILLUMINATED. QRH PROCEDURES WERE FOLLOWED AND THE LANDING GEAR WAS PUMPED DOWN MANUALLY. AIRCRAFT LANDED WITH
- [SDR 2024FA0000187](https://openairdocs.org/sdr/2024FA0000187), Jul 11, 2023: STARTER GEN. FAILED. CLICKING SOUND AND NO ROTATION UPON ATTEMPTED START. FOUND SPLINE SHART SLIGHTLY OUT OF ROUND AND BRUSHES WORN BEYOND LIMITS. FAILED STARTER-GEN WAS OVERHAULED 
- [SDR QMLA2023062920051](https://openairdocs.org/sdr/QMLA2023062920051), Jun 29, 2023: UNKNOWN. UNKNOWN. I TOOK OFF FROM RUNWAY 30 AT KLBF AND, AFTER GEAR AND FLAP RETRACTION AT ABOUT 500FT AGL, THE BUS TIE POPPED OFFLINE ALONG WITH THE NON ESSENTIAL BUS. AFTER RUN
- [SDR HVUA20210517001](https://openairdocs.org/sdr/HVUA20210517001), May 16, 2021: CONTROL PANEL. FAILED. "GEN 1 OFF" "BAT OFF" CAWS WARNING WITH MULTIPLE OTHER CAWS WARNINGS FOLLOWED BY SMOKE AND BURNING SMELL FROM OVERHEAD CONTROL PANEL. GEN 1 WAS OFFLINE AND POSS
- [SDR 2B5A719DEC20](https://openairdocs.org/sdr/2B5A719DEC20), Dec 12, 2020: BRAKE. MALFUNCTIONED. NO RIGHT HAND BRAKE ACTUATION WHEN APPLIED DURING TAXI.
- [SDR 2B5A202010250001](https://openairdocs.org/sdr/2B5A202010250001), Oct 22, 2020: GROUND STUD. CORRODED. INSPECTION REVEALED CORROSION AT THE BATTERY GROUND POINT. THIS IS THE THIRD ONE IN THE FLEET IN RECENT WEEKS. ONE WAS TOTAL ELECTRIC FAILURE IN FLIGHT.
- [SDR 2B5A202010250002](https://openairdocs.org/sdr/2B5A202010250002), Oct 16, 2020: GROUND STUD. CORRODED. TOTAL ELECTRICAL FAILURE ON APPROACH GEN 1 & 2 AND BATTERY WERE PROVIDING NO POWER TO THE AIRCRAFT. A SAFE LANDING WAS MADE. CORROSION WAS FOUND AT FRAME 38 UND
- [SDR 2B5A202009140001](https://openairdocs.org/sdr/2B5A202009140001), Sep 13, 2020: BEARING. SEIZED. INNER WHEEL BEARING FAILED WHEEL BECAME LOOSE AND COCKED AND SLID BREAKING THE BEAD AND DEFLATING. AIRCRAFT STOPPED BEFORE ANY FURTHER DAMAGE.
- [SDR FXGA20208173001](https://openairdocs.org/sdr/FXGA20208173001), Aug 13, 2020: WARNING MESSAGE. FALSE ACTIVATION. "HYDRAULIC" CAUTION ANNUNCIATOR CAME ON ABOUT 10 MINUTES INTO FLIGHT. HAD TO PUMP GEAR DOWN BY HAND. MAINTENANCE FOUND HYDRAULIC PUMP PRESSURE ABOVE MAX LIMIT A
- [SDR Q5QA20200309303](https://openairdocs.org/sdr/Q5QA20200309303), Mar 3, 2020: CONTROL CABLE. DEFECTIVE. WHILE PERFORMING ROUTINE MAINTENANCE, THE TECHNICIAN DISCOVERED AN UNUSUAL SOUND COMING FROM THE LH FLAP DRIVE SYSTEM. IT WAS DETERMINED THAT THE SOUND WAS COMI
- [SDR GBBR2019111105](https://openairdocs.org/sdr/GBBR2019111105), Nov 5, 2019: DRAG BRACE. DAMAGED. NOSE LANDING FAILED TO EXTEND TO DOWN AND LOCKED POSITION. NOSE GEAR HUNG UP AT A 45 DEGREE ANGLE
- [SDR 2020FA0000020](https://openairdocs.org/sdr/2020FA0000020), Oct 7, 2019: BOOT. SHORTED. PROPELLER DE-ICE BOOT SHORTED INTERNALLY. THE PROPELLER WAS REMOVED AND WAS SENT TO A HARTZELL SERVICE CENTER. THE BLADE REQUIRED REPAIR.
- [SDR 9JLA2018091717806](https://openairdocs.org/sdr/9JLA2018091717806), Sep 3, 2018: TIMER. DEFECTIVE. CREW REPORTED THAT THE AIRCRAFT DE-ICE BOOT SYSTEM INOPERATIVE. THEY WERE UNABLE TO COMPLETE FLIGHT DUE TO ICING ALONG ROUTE OF FLIGHT. "DE-ICE" CAS MESSAGE IN 
- [SDR 2018FA0000510](https://openairdocs.org/sdr/2018FA0000510), Aug 28, 2018: DISC. FAILED. PILOT REPORTED LH BRAKE PARTIALLY LOCKED UP DURING LOW SPEED ROLL OUT AFTER LANDING. LESS THAN 20 KTS. ALSO GRINDING NOISE COMING FROM BRAKES. UPON REMOVAL OF T
- [SDR 6CBA2018033018175](https://openairdocs.org/sdr/6CBA2018033018175), Mar 26, 2018: BULKHEAD. CORRODED. DURING ANNUAL INSPECTION, CORROSION WAS FOUND ON FORWARD PRESSURE BULKHEAD, LT AND RT SIDE OF FRAME 15. THE CORROSION ON THE LT SIDE WAS LOCATED JUST INBOARD OF
- [SDR 6CBA2018032218174](https://openairdocs.org/sdr/6CBA2018032218174), Mar 17, 2018: UNKNOWN. ODOR. PILOT REPORTED THAT DURING TAKEOFF, A STRONG ODOR FROM ECS. INSPECTED THE ENGINE INLET AND EXTERIOR FOR OIL LEAKS AND DEBRIS. NO LEAKS OR DEBRIS NOTED. REMOVED,
- [SDR 3SDR20180213005](https://openairdocs.org/sdr/3SDR20180213005), Jan 24, 2018: SPACER. CHAFED. DURING LIFE EXTENSION INSPECTION IAW SB 04-009, FOUND CHAFE DAMAGE FROM AILERON CABLE CHAIN RUBBING THE CHAIN CONNECTING ROD AND ASSOCIATED SPACER. WITH AILERON
- [SDR 3SDR20180212004](https://openairdocs.org/sdr/3SDR20180212004), Jan 24, 2018: SPACER. CHAFED. DURING LIFE EXTENSION INSPECTION IAW SB 04-009, FOUND CHAFE DAMAGE FROM AILERON CABLE CHAIN RUBBING THE CHAIN CONNECTING ROD AND ASSOCIATED SPACER. WITH AILERON
- [SDR QMLA2017100717113](https://openairdocs.org/sdr/QMLA2017100717113), Oct 23, 2017: HEATER. MALFUNCTIONED. NOMINAL TAKEOFF RWY 30 LBF. DURING CLIMB, PASSING APPROXIMATELY 10,000' MSL BUS TIE CAWS LIGHT AND BUS TIE CB OPENED ALSO UF HEATER CB OPENED. NO SMOKE OR FUMES
- [SDR 6CBA2017081517171](https://openairdocs.org/sdr/6CBA2017081517171), Aug 15, 2017: TRANSPONDER. FAILED. ENROUTE, THE FLIGHT CREW REPORTED AN ELECTRICAL BURNING ODOR, POSSIBLY TRANSPONDER, ATC CONFIRMED THAT THEY WERE NOT RECEIVING TRANSPONDER DATA. DIVERTED AND MA
- [SDR 6CBA2017063017168](https://openairdocs.org/sdr/6CBA2017063017168), Jun 30, 2017: SKIN. CRACKED. RIGHT FLAP BOTTOM SKIN IS CRACKED BETWEEN TWO RIVETS ON FORWARD LAP JOINT BETWEEN FORWARD AND AFT FLAP SPARS, BETWEEN FLAP RIBS FIVE AND SIX. REMOVED DAMAGE AND
- [SDR 6CBA2017063017167](https://openairdocs.org/sdr/6CBA2017063017167), Jun 30, 2017: SKIN. CRACKED. LEFT FLAP BOTTOM SKIN IS CRACKED BETWEEN TWO RIVETS ON FORWARD LAP JOINT BETWEEN FORWARD AND AFT FLAP SPARS, BETWEEN FLAP RIBS FIVE AND SIX. REMOVED DAMAGE AND 
- [SDR 6CBA2017062217164](https://openairdocs.org/sdr/6CBA2017062217164), Jun 22, 2017: STATIC WICK. DAMAGED. LEFT FLAP BOTTOM SKIN IS CRACKED BETWEEN TWO RIVETS ON FORWARD LAP JOINT BETWEEN FORWARD AND AFT FLAP SPARS, BETWEEN FLAP RIBS FIVE AND SIX. REMOVED DAMAGE AND 
- [SDR 6CBA2017050117160](https://openairdocs.org/sdr/6CBA2017050117160), May 1, 2017: STRUCTURE. DAMAGED. DURING INSPECTION, DAMAGE WAS FOUND ON THE LT ELEVATOR TRAILING EDGE. THE ELEVATOR WAS REPAIRED IAW THE SRM 12-A-55-20-00-00A-664A-A .
- [SDR PCPR201701171](https://openairdocs.org/sdr/PCPR201701171), Dec 28, 2016: BOLT. SHEARED. AFTER TAKEOFF PILOT COULD NOT RETRACT GEAR. DETERMINED BY MAINTENANCE CREW THAT THE LANDING GEAR HYDRAULIC POWER PACK MOTOR CAGE BOLT HAD SHEARED AND BACKED OUT
- [SDR 6CBA2016102416154](https://openairdocs.org/sdr/6CBA2016102416154), Oct 24, 2016: LIGHT. INOPERATIVE. AFTER DEPARTING FOK, FLT CREW REPORTED, WITH GEAR RETRACTION RED NOSE GEAR INDICATION DID NOT EXTINGUISH, WHEN GEAR WAS EXTENDED FOR LANDING WE DID NOT GET A GR
- [SDR FXGA2016FA0000344](https://openairdocs.org/sdr/FXGA2016FA0000344), Jul 28, 2016: WARNING SYSTEM. ACTIVATED. REPEATED FLAPS CAWS WARNING ANNUNCIATOR ILLUMINATES. CAS ANALYST RECORDED THE RECURRING EVENT ON THE FOLLOWING DAYS. FLAPS CAWS WARNING LIGHT ON. ADJUSTED FLAPS
- [SDR FXGA2016FA0000343](https://openairdocs.org/sdr/FXGA2016FA0000343), Jul 28, 2016: WARNING SYSTEM. ACTIVATED. REPEATED FLAPS CAWS WARNING ANNUNCIATOR ILLUMINATES. CAS ANALYST RECORDED THE RECURRING EVENT ON THE FOLLOWING DAYS. FLAPS CAWS WARNING LIGHT ON. DESCRIPTION OF

All 273: https://openairdocs.org/model/pilatus-flugzeugwerke-pc-12-47/reports.md

## STCs that may be installed (OpenAirDocs) (123, 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 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 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 SA03476CH](https://openairdocs.org/stc/SA03476CH): Installation of Patient Loading and Utility System (PLUS). LifePort LLC
- [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 SA02683SE](https://openairdocs.org/stc/SA02683SE): Installation of a Supplemental Lighting System. Aviation Specialties Unlimited 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
- [STC SA02677LA](https://openairdocs.org/stc/SA02677LA): Modification to upgrade the existing Mode S Transponder system by installing the ACSS NXT-700 Transponder with ADS-B Out and optionally install the ACSS NXG-900 GPS as the position source for ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA02678LA](https://openairdocs.org/stc/SA02678LA): Modification to upgrade the existing Mode S Transponder system by installing the ACSS NXT-600 Transponder with ADS-B Out and optionally install the ACSS NXG-900 GPS as the position source for ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC

All 123: https://openairdocs.org/model/pilatus-flugzeugwerke-pc-12-47/stcs.md

## PMA parts (OpenAirDocs) (920, 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
- [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-206](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114901396720260625165551.0001): Navigation Light Lens to De-Ice Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · Nov 20, 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
- [AD-549-1324-06](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162453647620240620212612.0001): Battery Storage. Aero Design Inc/A HEICO Aerospace Company · PMA PQ1465CE · Replaces 549-1324-06 · May 21, 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

All of them: https://openairdocs.org/model/pilatus-flugzeugwerke-pc-12-47/pma.md

## The same model under other registry codes

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

- [Pilatus PC-12/47](https://openairdocs.org/model/pilatus-pc-12-47): 119 registered aircraft, registry code 7090552

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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.