Registered owner
Air Methods LLC
Owner type
LLC
Serial number
236
Year built
1998
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
November 20, 1998
Certificate issued
May 26, 2016
Expires
May 31, 2029
Mode S code
A316F5

From the FAA registry file of October 22, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PT6A-66 model are included below.

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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.

1997In forceSuperseded2026
ADs by the year they took effect: 68 ADs
19972
19989
19996
20004
20013
20024
20035
20043
20056
20062
20072
20083
20093
20121
20132
20141
20151
20162
20171
20201
20222
20232
20242
20261
See all 68 ADs

Information bulletins that may apply · 8

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N299AMMatched 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 · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 5

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR QMLA2022101420069Landing Gear · malfunctionedTOOK OFF FROM KLBL, DEPARTED ON RUNWAY 17 AND HEADED TO KDDC. NO MORE USABLE RUNWAY. THEN PUT THE GEAR UP AND TURNED LEFT TO GET ON THE COURSE AND SET FLAPS TO 0. THEN MADE A SECOND LEFT TO GET TO DDC. DURING CLIMBING, ENGAGED THE AUTOPILOT. ABOUT 1 MIN LATOct 5, 2022 · N299AM · Pilats PC12 · Landing Gear Retraction/Extension SystemSDR QMLA2019060529052Wire · chafedAIR CONDITIONING WIRING TO PRESSURE SWITCH FOR THE COMPRESSOR MOTOR WERE CHAFED THROUGH, AND SHORTING TO THE MOTOR MOUNT. REPAIRED THE WIRING IAW AC43-13 AND PILATUS PC-12/45 WIRING DIAGRAM AND FUNCTION CHECKED PER PILATUS PC-12 AMM, WIRES WERE SECURED SO NOT Jun 2, 2019 · N299AM · Pilats PC1245 · Air Conditioning System WiringSDR QMLA2018071018078Unknown · malfunctionedAUTO PILOT DISCONNECTED PASSING ABOUT 11K FEET CLIMBING TO 15K FT. CLEAR SKIES AND NO TURBULENCE. ATTEMPTED RECONNECT AND IMMEDIATELY THE AUTO PILOT DISCONNECTED AGAIN. OBSERVED CONTROL WHEEL SHAKING INDICATED AIRSPEED ABOUT 150 KNOTS AND AOA INDICATOR PASSINGJul 7, 2018 · N299AM · Pilats PC1245 · Stall Warning SystemSDR QML201805108057Governor · intermittentON DEPARTURE PROPELLER RPM WAS VERY LOW. 1635 VS 1700 GOOD TORQUE, PLANE ACCELERATED RPM STARTED TO INCREASE AND YELLOW LIGHT WENT OUT BUT STILL LOW. MOVING TOO FAST TO ABORT AND UNSURE THE REVERSE WOULD EFFECTIVE, ELECTED TO TAKE IT IN FLIGHT AND HANDLE AS ANMay 10, 2018 · N299AM · Pilats PC1245 · Propeller GovernorSDR QML2001F00000Actuator · failedFLAP SYSTEM MALFUNCTION. FLAPS FROZE AT APPROXIMATELY 15 DEGREES, WHILE BEING RETRACTED IMMEDIATELY FOLLOWING TAKEOFF. DEFECTIVE FLAP ACTUATOR. FAULTY FLAP ACTUATOR REMOVED AND REPLACED.Jun 1, 2001 · N299AM · Pilats PC1245 · Trailing Edge Flap Actuator

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.

See all 162 STCs