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N852AL

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1998 Pilatus PC-12/45 · Pratt & Whitney Canada PT6A-60A

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Registered owner
Metro Aviation Inc
Location
Shreveport, LA
Owner type
Corporation
Serial number
213
Year built
1998
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
June 21, 2000
Certificate issued
June 15, 2012
Expires
June 30, 2028
Mode S code
ABAED1
Pilatus PC-12/45Airframe model · 12 seats · 1 engine · 378 registeredTCDS A78EUAirframe · Pilatus PC-12/45TCDS E4EAEngine · Pratt & Whitney Canada PT6A-60A

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 52

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
See all 67 ADs

Information bulletins that may apply · 10

Advisory, not mandatory.

NTSB investigations · 1

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

NTSB SEA02LA029Accident · No injuriesLimited investigationFinal reportSunriver, ORThe pilot's failure to maintain directional control during the landing roll. An icy runway and a snow bank were factors.Dec 29, 2001 · Substantial damage

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.

Accident 20011229035689ABend, OR(.19) On December 29, 2001, at 0155 pacific standard time, a Pilatus PC-12, N852AL, registered to st. charles medical center, and operated by air methods as a 14 CFR part 91 positioning flight, ran off the side of the runway at Sunriver, Oregon, and collided…Dec 29, 2001 · No damage

Service difficulty reports · 3

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

SDR 2024FA0000964Relay · failedDURING NORMAL APPROACH THE PILOT SELECTED GEAR DOWN, THE HYDRAULIC POWER PACK FAILED TO ENERGIZE RESULTING IN THE LANDING GEAR FAILING TO EXTEND. THE PILOT MANUALLY EXTENDED THE LANDING GEAR AND LANDED THE AIRCRAFT NORMALLY RESULTING IN NO DAMAGE. THE SYSTEMDec 16, 2024 · N852AL · Pilats PC1245 · Hydraulic System, MainSDR HDNA20160304003Aoa · out of adjustON DOWNWIND BEFORE LANDING, THE STICK SHAKER ACTIVATED. THE ACFT WAS WELL ABOVE THE SPEED WHICH THE STICK SHAKER SHOULD HAVE ACTIVATED. ADJUSTED AOA.Mar 4, 2016 · N852AL · Pilats PC1245 · Stall Warning SystemSDR HDNA2015F00074Probe · out of adjustSTICK SHAKER ACTIVATED ON TAKEOFF AT 600 FT AGL. PILOT INTERRUPTED THE SYS USING THE YOKE MOUNTED INTERRUPT BUTTON, DECREASED AOA, INCREASED AIRSPEED AND OPENED THE STICK SHAKER CIRCUIT BREAKER AS A PRECAUTION. ONCE AT A SAFE ALTITUDE RAN INADVERTENT SHAKER OMay 25, 2015 · N852AL · Pilats PC1245 · Stall Warning System

STCs that may be installed · 166

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 166 STCs