N852AL

PILATUS PC-12/45 · 1998 · Valid Registration

Registered owner: METRO AVIATION INC, LA (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
METRO AVIATION, INC (HDNA)Certificate holderMatched by certificate designator

Accident & incident history

Accident · 2001-12-29 Matched by aircraft (N-number)
Pilatus PC-12 None injuryMETRO AVIATION, INC
Source: NTSB case SEA02LA029

Maintenance disclosures

J · 2024-12-16 Matched by certificate designator
ATA 2910

DURING 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 SYSTEM WAS TROUBLESHOT TO A DEFECTIVE HYDRAULIC RELAY P.N. 9740926112.

Source: SDR 2024FA0000964 · FAA SDRS
N · 2016-03-04 Matched by certificate designator
ATA 3418

ON DOWNWIND BEFORE LANDING, THE STICK SHAKER ACTIVATED. THE ACFT WAS WELL ABOVE THE SPEED WHICH THE STICK SHAKER SHOULD HAVE ACTIVATED. ADJUSTED AOA.

Source: SDR HDNA20160304003 · FAA SDRS
N · 2015-05-25 Matched by certificate designator
ATA 3418

STICK 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 OPERATION EMERGENCY CHECKLIST. MAINTENANCE DISCOVERED LT AOA PROBE REQUIRED ADJUSTMENT. ADJUSTED PROBE AND RETURNED ACFT TO SERVICE.

Source: SDR HDNA2015F00074 · FAA SDRS