N642PC2005 Pilatus PC-12/45
Safety record in brief:No NTSB accidents or incidents since 198243 ADs may apply8 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Air Methods LLC
- Owner type
- LLC
- City, state
- Greenwood Village, CO
- Certificate issued
- Feb 6, 2014
- Expires
- Feb 28, 2030
- Airworthiness
- Standard · Normal
- Airworthiness date
- Jul 1, 2005
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Pilatus
- Model
- PC-12/45
- Year
- 2005
- Serial number
- 642
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 12
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A86DF1
Engine
- Make and model
- P&W Pt6a Ser
- Type
- Turbo-prop
- Power
- 750 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2014 – nowAir Methods LLCGreenwood Village, CO · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (43)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2024-08-07 | Main Landing Gear Attach Section | Jun 3, 2024 | Airframe (PC-12/45) |
| 2023-09-12 | Air Conditioning System Wiring | Jul 5, 2023 | Airframe (PC-12/45)Certain serial numbers: 466; 467; 725; 861; 1032; 1052; … |
| 2021-24-01 | Aerodynamic Faring | Jan 13, 2022 | Airframe (PC-12/45)Only with: Spectre Lift Platform System installed in accordance with STC No. SA00634DE. |
| 2020-21-23 | Stabilizers | Dec 7, 2020 | Airframe (PC-12/45)Only with: Horizontal stabilizer rear attachment bolt P/N 555.10.12.139 marked with production order number FAUF 10169753, FAUF 10171067, or FAUF 10171267 installed. |
| 2016-18-05 | Power Plant | Oct 6, 2016 | Airframe (PC-12/45)Serial numbers per Figure 1 to paragraph (c)(1) of this AD (affected EMF serial numbers). Only with: Installed with engine mounting frame assembly P/N 571.20.12.036 with serial numbers 0001-1200, 1202-1272, 1275-1323, 1325-1328, 1334-1338, 1340, 1342, 1344-1346, 1348, 1349, 1358, 1361, or 1365. |
Show all 43 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2016-12-01 | Wings | Jul 15, 2016 | Airframe (PC-12/45)Only with: Airplanes delivered before January 1, 2015 (delivery date per issue date of EASA Form 52). |
| 2015-19-15 | Flight Controls | Nov 3, 2015 | Airframe (PC-12/45)Certain serial numbers: 244; 307; 409; 646; 1447–1450; 1461; … |
| 2008-07-11 R1 | PILATUS AIRCRAFT LTD. Airplanes | Mar 25, 2013 | Airframe (PC-12/45) |
| 2009-08-11 | PILATUS AIRCRAFT LTD. Models PC-12 and PC-12/45 Airplanes | May 26, 2009 | Airframe (PC-12/45)Certain serial numbers: 101–320 |
| 2009-05-07 | PILATUS AIRCRAFT LTD. Models PC-12, PC-12/45, PC-12/47, and PC-12/47E Airplanes | Mar 30, 2009 | Airframe (PC-12/45)Certain serial numbers: PC-12 101–544; PC-12 546–888; PC-12/45 101–544; PC-12/45 546–888; PC-12/47 101–544; PC-12/47 546–888; … |
| 2008-02-03 | Pilatus Aircraft Limited Model PC-12, PC-12/45, and PC-12/47 Airplanes | Feb 20, 2008 | Airframe (PC-12/45)Certain serial numbers: 101–749. Only with: Applies where Pilatus PC-12 Service Bulletin No. 32-020 has not been fully incorporated and with MLG assemblies, special bolts, or modification kits of listed P/Ns delivered before December 31, 2006 installed. |
| 2007-03-06 | Pilatus Aircraft Limited PC-12 and PC-12/45 Airplanes | Mar 8, 2007 | Airframe (PC-12/45)Serial numbers per DeCrane Aircraft Mandatory Service Bulletin SB05147 Revision B. Only with: Equipped with DeCrane executive passenger seats Model Number 4006, VPN 403150-1 or 403150-2, with seat serial numbers identified in DeCrane SB05147 Revision B. |
| 2006-16-13 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Sep 18, 2006 | Airframe (PC-12/45)Certain serial numbers: 101–617 |
| 2005-22-13 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Dec 19, 2005 | Airframe (PC-12/45)Certain serial numbers: 101–620 |
| 2005-22-04 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Dec 12, 2005 | Airframe (PC-12/45)Certain serial numbers: 101–625 |
| 2005-11-06 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Jul 18, 2005 | Airframe (PC-12/45)Certain serial numbers: 101–620 |
| 2005-04-16 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Mar 8, 2005 | Airframe (PC-12/45)Certain serial numbers: 322–400 |
| 2005-01-11 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Feb 22, 2005 | Airframe (PC-12/45) |
| 2004-12-11 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Jul 26, 2004 | Airframe (PC-12/45)Only with: Equipped with an inboard and/or outboard flap flexshaft P/N 945.02.02.203 and/or P/N 945.02.02.204. |
| 2004-06-05 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | May 6, 2004 | Airframe (PC-12/45) |
| 2004-04-01 | Pilatus Aircraft Ltd. Models PC-7, PC-12, and PC-12/45 Airplanes | Mar 29, 2004 | Airframe (PC-12/45)Only with: Equipped with Lear Romec engine-driven pump P/N RG9570M or RG9570M1 (PC-7), or P/N RG9570R1 (PC-12, PC-12/45). |
| 2003-20-15 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Oct 10, 2003 | Airframe (PC-12/45)Certain serial numbers: 101–520. Only with: Fuel booster pump P/N 969.84.11.401, 968.84.11.403, or 968.84.11.404 installed. |
| 2003-11-17 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Jul 28, 2003 | Airframe (PC-12/45)Certain serial numbers: 101–380; 382–385; 387–395; 398–406; 408; 409; … |
| 2003-09-11 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Jun 16, 2003 | Airframe (PC-12/45)Serial numbers per Decrane Aircraft, ERDA, Inc., Service Bulletin SB02010, Revision A. Only with: Passenger seat ERDA VPN 403008-1 or 403008-2 (Pilatus P/N 959.30.01.601, 959.30.01.602, 959.30.01.613, or 959.30.01.614) with seat serial number specified in ERDA SB02010 Rev A installed. |
| 2003-07-10 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | May 12, 2003 | Airframe (PC-12/45)Certain serial numbers: 321; 401–457; 463. Only with: Overhead panel P/N 972.81.32.102 (or FAA-approved equivalent) installed that has not been modified to Mod A status. |
| 2001-25-10 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Jan 25, 2002 | Airframe (PC-12/45) |
| 2001-22-15 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Dec 26, 2001 | Airframe (PC-12/45) |
| 2001-11-02 | Pilatus Aircraft LTD Models PC-12 and PC-12/45 Airplanes | Jul 23, 2001 | Airframe (PC-12/45)Certain serial numbers: 101–289 |
| 2000-26-17 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Feb 24, 2001 | Airframe (PC-12/45)Certain serial numbers: 101–320. Only with: Equipped with P/N 959.81.10.107 LH and P/N 959.81.10.108 RH windshields (PPG P/N NP172121-5 LH and NP172121-6 RH or FAA-approved equivalent part numbers). |
| 2000-21-14 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Dec 15, 2000 | Airframe (PC-12/45)Certain serial numbers: 101–301. Only with: Equipped with torque oil-pressure tubes and py pressure pipe assemblies Pilatus P/N 577.11.12.105, P&WC P/N 3119969, or Pilatus P/N 577.11.12.104 (or FAA-approved equivalents). |
| 2000-11-14 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Jun 2, 2000 | Airframe (PC-12/45)Only with: Equipped with pneumatic deicing boots. |
| 2000-02-31 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Mar 27, 2000 | Airframe (PC-12/45)Certain serial numbers: …–180 |
| 99-24-09 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Jan 14, 2000 | Airframe (PC-12/45)Certain serial numbers: 101–300 |
| 99-17-01 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Oct 1, 1999 | Airframe (PC-12/45)Certain serial numbers: 101–239 |
| 99-06-17 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Jun 16, 1999 | Airframe (PC-12/45)Certain serial numbers: 101–180 |
| 99-06-05 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Apr 16, 1999 | Airframe (PC-12/45)Certain serial numbers: 101–227; 232 |
| 98-21-27 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Nov 26, 1998 | Airframe (PC-12/45)Certain serial numbers: 101–230. Only with: Equipped with the corporate commuter cabin layout. |
| 98-20-28 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Nov 4, 1998 | Airframe (PC-12/45) |
| 98-11-01 R2 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Sep 22, 1998 | Airframe (PC-12/45)Certain serial numbers: 101–230 |
| 98-11-20 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Jul 13, 1998 | Airframe (PC-12/45)Certain serial numbers: MSN 101–MSN 180. Only with: Airplanes that incorporate an executive cabin layout. |
| 98-08-26 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | May 29, 1998 | Airframe (PC-12/45)Certain serial numbers: MSN 001–MSN 168 |
| 98-07-18 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Apr 28, 1998 | Airframe (PC-12/45)Certain serial numbers: MSN 101–MSN 153 |
| 98-04-16 | Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes | Apr 2, 1998 | Airframe (PC-12/45)Certain serial numbers: 101–169 |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (8)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Navigation · ehsi · faultedSep 17, 2026
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 EHSI UNIT ONLY AND ALL SURROUNDING AREAS AND WIRING WERE NOT AFFECTED. DETERMINED EHSI UNIT FAILED DUE TO INTERNAL FAILURE. REMOVED AND…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · brake sys · weakNov 3, 2025
UPON LANDING THERE WASN'T ANY BRAKE PRESSURE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · hydraulic system · leakingFeb 25, 2024
ON APPROACH TO LAND TO PATIENT DROP-OFF, WHEN IPUTTING THE LANDING GEAR DOWN THE NOSEWHEEL GEAR INDICATION REMAINED ILLUMINATED "UNSAFE" (RED), AND SIMULTANEOUSLY THE HYDR CAWS LIGHT ILLUMINATED. THE TOWER AT EL PASO TOLD ME THAT THE GEAR LOOKED DOWN, BUT NOT LOCKED. REJECTED THE LANDING, AND…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 8 reportsShow fewer reports
- Flight controls · flap system · malfunctionedNov 13, 2022
AFTER TAKEOFF, WHEN THE FLAPS WERE RAISED FROM 15 TO 0, THEY FROZE AT 14 WITH "FLAP" AND "PUSHER' ANNUNCIATIONS. DECLARED AN EMERGENCY AND LANDED AT KABQ UNEVENTFULLY, FLAPS LOCKED AT 15 DEGREES DUE TO ASYMMETRY FAULT. MAINTENCE ACCOMPLISHED INSPECTION OF THE FLAPS SYSTEM AND ACCOMPLISHED A FLAP…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · relay · inoperativeMar 14, 2016
THE RUDDER TRIM TAB WASN’T OPERATING & STUCK IN FULL RT POSITION. UPON ARRIVING, PROCEEDED TO PERFORM A VISUAL INSPECTION OF RUDDER & TRIM SYS, NO VISUAL DAMAGE WAS FOUND AT THAT TIME. GAINED ACCESS TO THE RUDDER TRIM TAB RELAYS, SWAPPED THE LT & RT RELAYS FOR TROUBLESHOOTING PURPOSE. FOUND THE RT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · terminal block · arcedJun 16, 2013
LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. LANDING GEAR INDICATOR LIGHTS SHOWED 3 RED/UNLOCKED GEAR. HYD LIGHT ILLUMINATED ON CAWS PANEL. BETWEEN 5 AND 10 MINUTES AFTER THE INITIAL FAILURE, THE GEAR CYCLED TO THE UP POSITION WITHOUT ANY PILOT ACTION. THE SYSTEM OPERATED NORMAL ON LANDING. ACFT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · relay · malfunctionedMay 27, 2013
LANDING GEAR FAILED TO RETRACT AFTER TAKE OFF. THE LANDING GEAR INDICATOR LIGHTS SHOWED 3 RED/UNLOCKED GEAR. HYD LIGHT ILLUMINATED ON CAWS PANEL. PERFORMED EMERGENCY GEAR EXTENTION AND RETURNED TO POINT OF DEPARTURE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · tire · failedMar 5, 2011
ACFT LANDED SAFELY AT AIRPORT. DURING TAXI IN BETA MODE, ACFT WAS BREAKING AND PREPARING TO TURN LT ON TO TAXIWAY WHEN THE LT MAIN TIRE BLEW. THE TIRE PN 021-350-0, SN 0246S00343. THIS TIRE HAD A TOTAL OF 7 LANDINGS UNTIL IT FAILED. A NEW TIRE WAS INSTALLED PN 021-350-0, SN 0247S00341 ON 3-5-11…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026