Owner type Corporation
Year built 1998
Type Fixed wing single engine
Engine Turbo-prop
Airworthiness Standard, normal
Airworthiness date August 20, 1998
Certificate issued November 19, 1998
Expires March 31, 2029 From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PT6A-66 model are included below.
On this page Registration Potential ADs 53 Information bulletins 8 NTSB investigations 0 FAA incident reports 2 Difficulty reports 6 Potential STCs 162 Related links Airworthiness directives that may apply · 53 Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
1997 In force Superseded2026 ADs by the year they took effect: 68 ADs 1997 2 1998 9 1999 6 2000 4 2001 3 2002 4 2003 5 2004 3 2005 6 2006 2 2007 2 2008 3 2009 3 2012 1 2013 2 2014 1 2015 1 2016 2 2017 1 2020 1 2022 2 2023 2 2024 2 2026 1
See all 68 ADs Information bulletins that may apply · 8 Advisory, not mandatory.
NTSB investigations No NTSB investigations matched to N970NA Matched 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 · 2 FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20150827015219I Taxi · Midland, TX On August 27, 2015, at 0806 local time, a 1998 PC-12/45 aircraft bearing registration number N970NA, registered to native air, was taxiing to the hangar after landing in (kmaf) Midland, Texas following a part 135 repositioning flight from (E38) alpine, Texas.… Aug 27, 2015 · Minor damage Incident 20130606009059I Landing: Rollout · Albuquerque, NM On June 6, 2013, at 22:00 MST, a Pilatus PC-12/45 registered to native American air service inc. and operated by air methods corp. blew out a left main tire on landing and departed the left side of runway 3 at Sunport International Airport, Albuquerque, new… Jun 6, 2013 · Minor damage
Service difficulty reports · 6 Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2025011020002 Boot · failed HYDRAULIC LIGHT ILLUMINATED DURING LANDING. PROP DE-ICE FAILED IN FLIGHT. - CHECKED FLUID LEVELS AND NITRO PSI. - CLEANED HYD. PSI TRANSMITTER / SWITCH CONNECTIONS. PROP DE-ICE INSPECTED WITH NO PROBLEMS NOTED. Jan 10, 2025 · N970NA · Pilats PC1245 · Airfoil Anti/De-ice System SDR QMLA122820121 Altimeter · unknown RIGHT AFTER TAKEOFF PILOT ALTIMETER FAILED. ATC CONFIRMD NO ALTITUDE READOUT.WE RETURNED TO RAP UNEVENTFULLY AND WROTE UP THE DISCREPANCY. Dec 23, 2023 · N970NA · Pilats PC1245 · Altimeter, Barometric/Encoder SDR QMLA2023080720059 Unknown · unknown AUTO PILOT FAILURE WHILE CLIMBING OUT OF PINE RIDE TRIED TO SET CLIMB AT 130 KTS IT WOULDN’T CAPTURE ALTITUDE ALERTER KEPT RINGING THROUGHOUT FLIGHT WHEN DECENDING INTO RAP SET 1200 FT/MIN AIRCRAFT DIDN’T CAPTURE RATE JUST WENT INTO A MUCH STEEPER RATE. SHUT Aug 5, 2023 · N970NA · Pilats PC12 · Auto Flight System SDR QMLA2014072514091 Unknown · odor AFTER ENG STARTUP & DURING TAXI TO RUNWAY, PILOT & MEDICAL CREW SMELLED A BURNING WIRE SMELL. PILOT TURNED AROUND BEFORE TAKEOFF & RETURNED TO HANGAR WITH NO OTHER INCIDENCE. A 15 MINUTE GND RUN UP WAS PERFORMED WITH THE ACFT IN FULL TAKEOFF CONFIGURATION. Jul 25, 2014 · N970NA · Pilats PC1245 · Air Distribution System SDR 2010F00241 Pressure Switch · leaking ABOUT 25 MILES OUT, ENROUTE, MEDICAL CREW INFORMED ME THAT THEY HAD HEARD A LOUD SOUND FOLLOWED BY A "THUD" THAT THEY FELT UNDERNEATH THE LT SIDE OF THE ACFT. DID NOT HEAR OF FEEL OR HEAR WHAT THEY HAD JUST EXPERIENCED, ASKED THEM TO SHOW SPECIFICALLY WHERE TH Nov 14, 2010 · N970NA · Pilats PC1245 · Hydraulic System, Main SDR RMXA029H226080609 Skin · cracked WHILE INSTALLATION OF THE ELEVATOR FOLLOWING MAINTENANCE A SUSPECTED CRACK WAS FOUND IN THE SHEET METAL SKIN ON THE RH SIDE OF THE VERTICAL STABILIZER. THE CRACK IS LOCATED AT THE RH FORWARD MOUNT HOLE FOR THE 32CT FAIRING. THE CRACK EMANATES FORWARD FROM THE Aug 5, 2009 · N970NA · Pilats PC1245 · Vertical Stabilizer, Plate/Skin STCs that may be installed · 162 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 See all 162 STCs