- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 129
- Year built
- 1996
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- January 22, 2009
- Certificate issued
- May 24, 2012
- Expires
- May 31, 2028
- Mode S code
- A075FE
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included below.
On this page
Airworthiness directives that may apply · 76
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1968 | 1 |
|---|---|
| 1969 | 1 |
| 1970 | 1 |
| 1975 | 1 |
| 1977 | 1 |
| 1978 | 2 |
| 1980 | 2 |
| 1986 | 1 |
| 1990 | 1 |
| 1992 | 1 |
| 1994 | 1 |
| 1995 | 1 |
| 1997 | 2 |
| 1998 | 9 |
| 1999 | 6 |
| 2000 | 4 |
| 2001 | 4 |
| 2002 | 5 |
| 2003 | 5 |
| 2004 | 3 |
| 2005 | 7 |
| 2006 | 2 |
| 2007 | 2 |
| 2008 | 3 |
| 2009 | 3 |
| 2011 | 2 |
| 2012 | 1 |
| 2013 | 2 |
| 2014 | 3 |
| 2015 | 2 |
| 2016 | 3 |
| 2017 | 1 |
| 2020 | 1 |
| 2022 | 3 |
| 2023 | 2 |
| 2024 | 2 |
| 2026 | 1 |
See all 93 ADs
Information bulletins that may apply · 13
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N129JWMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Pilatus PC-12/45 aircraft
FAA incident reports
No FAA accident or incident reports matched to N129JWMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Pilatus PC-12/45 aircraft
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2024081620101Control Valve · failedALL 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 AIRPORTS BELOW/NEAR US IF THE SMELL GOT WORSE AND I BECAME MORE CONCERNED ABOUT AN IMMINENT CHANCE SDR QMLA2024021320017Volt Regulator · failedDUAL GENERATOR FAILURE WHEN HEATS/LIGHTS TURNED ONSDR QMLA2024021320016Boot · malfunctionedDE-ICE BOOTS MALFUNCTION AS INDICATED ON "CAWS" PANEL. PILOT WROTE UP DISCREPANCY IN LOG BOOK. AIRCRAFT BOOTS WERE DEFERRED ON MEL AND THE AIRCRAFT WAS RETURNED TO BASE. MAINTENANCE FOUND LH TAIL DE-ICE BOOT HAD A LONG CRACK IN IT.SDR QMLA2024011220003Unknown · unknownAT FL 230 PRESSURIZATION CONTROL WAS SET TO FL 230 AND SHOULD HAVE RESULTED IN A CABIN PRESSURE OF APPROXIMATELY 6,300 FEET. THE CABIN PRESSURE INDICATOR WAS SHOWING 8,000 FEET. AS THE LAST TWO EVENTS, THERE WAS A SLIGHT SMELL, LIKE OVERHEATED RUBBER ON A MANISDR QMLA2023103020098Boot · failedIN-FLIGHT DEICE BOOT FAILURE IN CRUISE FLIGHT. HAD BOOTS ACTIVATED FOR 25MIN AND THEN RECEIVED A CAUTION THAT BOOTS HAD FAILED. RAN QRH AND BOOTS FAILED AGAIN. INSPECTION FOUND AN APPROX. 3 IN TEAR IN LOWER LEFT INBOARD.SDR QMLA2023040520027Timer · unserviceableON A FLIGHT FROM CNY TO GJT USING DE-ICE EQUIPMENT, THE AMBER "DE-ICE" CAWS LIGHT CAME ON WITH A VISUAL AND AURAL CAUTION LIGHT. FOLLOWED PC-12 QRH - GREEN "PROP DE-ICE" WAS NOT FLASHING AS PER CHECK LIST. FOLLOWED PROCEDURE ANYWAY, PROBLEM PERSISTED, PROCEEDESDR QMLA2022040820023None · usedLOSS OF BRAKE FLUID, THE BRAKE CALIPER WAS INSTALLED ON 16 MARCH 2022. THE LINE WAS NOT TOUCHING BUT APPARENTLY WAS INSTALLED WITHOUT SUFFICIENT CLEARANCE. AFTER THE INCIDENT ON 6 APRIL 2022, THE LINE STILL WAS NOT PHYSICALLY TOUCHING BUT THE TIRE HAD APPARENTSDR QMLA2019080879065Battery · hotON CLIMB OUT ON AN IFR FLIGHT PLAN, THE ENTIRE CREW NOTICED WHAT APPEARED TO BE A BURNING SMELL THROUGHOUT THE AIRCRAFT. WE CANCELLED THE IFR FLIGHT PLAN AND ABORTED THE FLIGHT, TURNED TO RTB AND SECURED ALL UNNECESSARY CONSUMERS. UPON RETURN TO BASE, THE MESDR QMLA2018020118012Hinge · crackedON ENTRY TO THE AIRCRAFT, THE ATTACH LUG FOR THE LANYARD THAT HOLDS THE CREW ENTRANCE STEPS UP WAS CRACKED AND BROKE CREATING EXCESSIVE DOWNWARD FORCE AND CAUSING SEVERAL OTHER CRACKS ON THE AIRFRAME SIDE OF THE DOOR HINGE.SDR QMLA2017041717041Fitting · looseOPE ECS/PRESSURIZATION FAIL ON CLIMB AT APPROXIMTELY 13000 FT, ALSO FAILED HOLDING CABIN PRESSURE ON MANUAL MODE. OPEN ACCESS PANEL BELOW COPILOT SEAT. FOUND A AN FITTING SLIGHTLY LOOSE ON CHECK VALVE NEXT TO EJECTOR, JET. REMOVED CHECK VALVE BY REMOVEING THESDR QMLA2013120413172Flap · malfunctionedON APPROACH TO LANDING BELOW 163 KIAS SELECTED FLAP POSITION TO 15 DEGREES. FLAPS FAILED TO MOVE, MASTER CAUTION & AMBER FLAP CAWS LIGHT ILLUMINATED. COMPLETED NO FLAP LANDING WITHOUT FURTHER INCIDENT.
STCs that may be installed · 217
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Pilatus PC-12/45
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller