Registered owner
Bering Air Inc
Location
Nome, AK
Owner type
Corporation
Serial number
UE-148
Year built
1995
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, commuter
Airworthiness date
May 13, 1995
Certificate issued
April 13, 2004
Expires
January 31, 2030
Mode S code
A0C202

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PT6A-6 model are included below.

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Airworthiness directives that may apply · 66

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1968In forceSuperseded2026
ADs by the year they took effect: 74 ADs
19681
19691
19701
19751
19771
19802
19921
19941
19954
19965
199710
19985
19998
20002
20015
20022
20035
20043
20053
20062
20081
20092
20111
20122
20142
20161
20231
20241
See all 74 ADs

Information bulletins that may apply · 9

Advisory, not mandatory.

NTSB investigations · 2

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

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.

Service difficulty reports · 13

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

SDR 2022F00440Adapter · crackedDURING ROUTINE INSPECTION WHILE PERFORMING INSPECTION "I" CHECK PROCEDURE (5-00-I0) TABLE 1 ITEM 30. IT WAS DISCOVERED THAT THE ELEVATOR HORN TO ELEVATOR ATTACH BRACKET P/N:101-610017-1 WAS CRACKED 85% AROUND THE CIRCUMFERENCE OF THE BRACKET WITH THE CRACK TRANov 1, 2022 · N148SK · Beech 1900D · Elevator Control SystemSDR S2YA02046Engine · malfunctionedSHORTLY AFTER TAKEOFF OF FLIGHT 1053 MKE-CMH THE CREW NOTICED THE RIGHT ENGINE WAS NOT PRODUCING ENOUGH TORQUE. THE CREW MADE AN AIR-TURN-BACK TO MKE. MECHANIC INSPECTED THE RIGHT ENGINE AND FOUND THERE WAS AN OBSTRUCTION IN THE P3 LINE THAT GOES TO THE BLEENov 14, 2002 · N148SK · Beech 1900D · Engine (Turbine/Turboprop)SDR S2YA00014Shutoff Valve · inoperativeFLT 1024 - MKE-CVG - DURING FLIGHT, THE CABIN ALT HI ANNUNCIATOR ILLUMINATED AT FL 230. THE FLIGHT CREW NOTED THE CABIN ALTITUDE WAS AT FL 100 AND CLIMBING. SO THE CREW DEPLOYED THE OXYGEN MASKS, DIVERTED TO FWA AND MADE AN UNEVENTFUL LANDING. THE CREW CONTJun 9, 2000 · N148SK · Beech 1900D · Cabin Pressure Control SystemSDR S2YA00007Engine · leakingFLT 1064 - SDF-MKE - THE LEFT ENGINE OIL PRESSURE FLUCTUATED BETWEEN 60-90 PSI. THE CREW DIVERTED TO IND AND HAD OUTSTATION MAINTENANCE SERVICE AND INSPECT THE LEFT ENGINE. THE A/C CONTINUED ONTO MKE AND MAINTENANCE INSPECTED THE ENGINE AGAIN. THE OIL CONSUMar 28, 2000 · N148SK · Beech 1900D · Turbine Engine Oil SystemSDR S2YA97007Pressure Switch · inoperativeDURING THE MONTH OF JANUARY, SIX FUEL PRESSURE SWITCHES, P/N 100-389018-21 WERE REPLACED. THE TBR FOR THE SWITCHES WAS: 3,933.2 HRS FROM N NR 148SK; 1,418.2 HRS FROM N NR 831SK; 1,479.7 HRS FROM N NR 87SK; 2,525.6 HRS FROM N NR 881SK; 1,715.7 HRS FROM N NR 8Mar 25, 1997 · N148SK · Beech 1900D · Fuel Pressure IndicatorSDR S2YA960036Trim Tab · frozenTHE FLT CREW, FOUND THE ELEVATOR TRIM TABS FROZEN WHEN THEY LEVELED OFF AT CRUISING ALTITUDE. WHEN THE AIRCRAFT LANDED, THE FREEZING ELEVATOR TRIM TABS WERE WRITTEN UP. MAINTENANCE LUBED THE ELEVATOR TRIM TAB ACTUATORS. OPS CHECKED GOOD MANUALLY AND ELECTRINov 27, 1996 · N148SK · Beech 1900D · Elevator Tab Control SystemSDR S2YA960035Door Warning · illuminatedFLT 1263 - DAY-BNA - AFTER TAKEOFF THE CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLT. THE CO-PILOT INSPECTED THE DOOR LOCK CAMS IN FLIGHT TO CHECK FOR AN UNSAFE CONDITION, NONE WERE FOUND TO BE OUT OF ALIGNMENT. THE CREW MADE A SAFE LANDING IN DAY. MAINTENANCE INov 19, 1996 · N148SK · Beech 1900D · Door Warning SystemSDR S2YA960008Blower · failedFLT 1199 - IND-MKE - EN ROUTE THE FLIGHT CREW REPORTED SMOKE IN THE CABIN. THEY MADE AN AIR TURN BACK TO IND TAKING EMERGENCY PRECAUTIONS DURING AND AFTER LANDING. MX WAS CALLED TO INSPECT THE AIRCRAFT AND FOUND THE FWD VENT BLOWER SEIZED, BURNED OR BURNED SMay 23, 1996 · N148SK · Beech 1900D · Air Distribution FanSDR S2YA950019Generator · off lineAFTER THE FLIGHT CREW LEFT MKE ON FLT NR 1124, THEY FOUND THAT THE RT DC GENERATOR WAS OFF LINE. THEY PROCEEDED TO TURN BACK TO MKE. MAINTENANCE PARALLELED THE GENERATOR CIRCUIT PER BEECH MM AND OPS CHECK GOOD. (M)Aug 16, 1995 · N148SK · Beech 1900D · DC Generating SystemSDR S2YA950013Deice Supp Line · chafedFOUND THE TAIL DEICE SUPPLY LINE CHAFED AT THE POINT OF EXIT FROM THE CLEAR PLASTIC ROUTING 'PROTECTION' TUBE. THE LOCATION IS THE BASE OF THE VERTICAL STABILIZER, LOWER ZONE 331. THE LINE WAS REPAIRED AND REST OF THE FLEET IS BEING CHECKED. (X)Jun 22, 1995 · N148SK · Beech 1900D · Airfoil Anti/De-ice SystemSDR S2YA950010Acm Inlet Duct · improper instlFOUND THE AIR CYCLE MACHINE INLET DUCT INSTALLED BACKWARDS ON THE BOTTOM OF THE LT WING PANEL WELD ASSEMBLY. REMOVED AND REINSTALLED THE LOUVER IN THE PROPER POSITION. THIS HAD ALSO OCCURRED ON AIRCRAFT S/N UE-145, BOTH FROM THE FACTORY. (X)May 20, 1995 · N148SK · Beech 1900D · Cabin Cooling SystemSDR S2YA950009Axle · incorrect diaDISCOVERED BOTH INNER AND OUTER WHEEL BEARINGS, PN 13899, WERE FROZEN IN PLACE ON NLG STRUT ASSY AXLE SHAFT, PN 114-820026-1, WHILE TRYING TO REMOVE THE NOSE WHEEL AND TIRE ASSY. ATTEMPTED DRY ICE AND HEATING OF THE BEARING RACE TO FACILITATE REMOVAL, TO NO AMay 19, 1995 · N148SK · Beech 1900D · Nose/Tail Landing Gear Strut/AxleSDR S2YA950008Radome · leaksTHE RADOME TO FUSELAGE MOUNT AREA AT FS 30.00 HAD TO BE SEALED TO PREVENT PREMATURE RADAR FAILURES DUE TO MOISTURE. AS THE RADAR TRANSIT/RECEIVER IS HIGHLY SUSCEPTIBLE TO ANY WATER. WE HAVE HAD MULTIPLE FAILURES DUE TO THIS PROBLEM. THE REST OF FLEET WAS SEMay 19, 1995 · N148SK · Beech 1900D · Aerodynamic Fairings

STCs that may be installed · 203

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

See all 203 STCs