- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 642
- Year built
- 2005
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- July 1, 2005
- Certificate issued
- February 6, 2014
- Expires
- February 28, 2030
- Mode S code
- A86DF1
From the FAA registry file of October 22, 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 N642PCMatched 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 N642PCMatched 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 · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2026091720070Ehsi · faultedFUMES 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 FAILSDR QMLA2025110320111Brake Sys · weakUPON LANDING THERE WASN'T ANY BRAKE PRESSURE.SDR QMLA2024022520020Hydraulic System · leakingON 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 NOTSDR QMLA2022111720075Flap System · malfunctionedAFTER 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 THESDR QMLA2016031416026Relay · inoperativeTHE 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 FSDR QMLA2013061613081Terminal Block · arcedLANDING 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.SDR QMLA2013052713072Relay · malfunctionedLANDING 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.SDR RMXA379348Tire · failedACFT 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
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.
See all 217 STCs