BERING AIR INC

Operated by BERING AIR INC (per NTSB report)

Operated by Bering Air, Inc. (per NTSB report)

Operated by BERING AIR, INC. (per NTSB report)

Operated by BERING AIR INC (per NTSB report)

Operated by Bering Air Inc. (per NTSB report)

STALL WARNING HORN GOES OFF INTERMITTENTLY AS HIGH AS 140 KTS

PILOT FELT STRONG LEFT RUDDER PRESSURE ON TWO CONSECUTIVE TAKE OFFS

RH MAIN LANDING SCRAPPER SEAL BROKEN AND HANGING FROM BOTTOM OF STRUT.

ON TAKE OFF RIGHT ENGINE LOSS TORQUE INDICATION.

AHRS #1 & 2 FAILED, HEADING RED "X", LOSE OF SYNTHETIC VISION; GRS #1 S/N: 45T003846, GRS #3 S/N: 45T003702, GMU #1 1CM0333444. GMU #2 S/N: 1CM033471, REMOVED, INSPECTED, REINSTALLED. AHRS SYSTEM POST-MX CHECK PERFORMED. AHRS ADJUSTMENT/TEST, PITCH/ROLL OFFSET CALIBRATION, MAGNETOMETER CALIBRATION, HEADING OFFSET CALIBRATION PERFORMED. OPS CHECKED GOOD.

LOW FUEL PRESSURE ANNUNCIATOR WITH ENGINE RUNNING AND ELECTRIC BOOST PUMP ON.

HEADING INDICATOR RED "X" THEN CAME BACK IN A FEW MINUTES, ALL WHILE ON THE GROUND. SYNTHETIC VERSION ALSO LOST BECAUSE OF RED "X". TROUBLESHOOT AND COULD NOT DUPLICATE.

RED X ON AIRSPEED, VSI, TEMP INTERMITTENTLY; SWAPPED TO RH SIDE AND PROBLEM FOLLOWED, UNIT REPLACED

ENGINE FIRE ANNUNCIATION AND AURAL ALERT IN CRUISE & ETM EXCEED (PROP & NG EXCEED). WAS FALSE INDICATIONS. INSPECTED SYSTEMS AND NO FINDINGS NOTED.

ENGINE INSTRUMENTS STOPPED DISPLAYING WHILE IN CRUISE. PILOT DIVERTED TO NEAREST AIRPORT. MECHANIC DISPATCHED TO INSPECT WITH NO FINDINGS.

PROP INSTALLED AND RED OIL NOTED LEAKING FROM PROP BLADE ROOTS AFTER GROUND RUNS. FOLLOWED MANUFACTURES TROUBLESHOOTING AND LEAK CONTINUED. CLEANED/DRIED AND LET SIT OVERNIGHT. FOUND OIL LEAKING FROM BLADE #4 NEXT MORNING WITH PROP STATIC. "0" ENTER FOR PROP CYCLES BECAUSE CYCLES ON PROP ARE NOT TRACKED.

RH MLG STRUT LOW AND NEEDS SERVICED.

CARGO DOOR CONTACTING FORWARD SIDE OF DOOR FRAME WHEN LOADED. FOUND SHIMS MISSING FROM MANUFACTURE

RED OIL LEAKING FROM PROP HUB. DISCOVERED DURING POST FLIGHT INSPECTION. 0 ENTER FOR PROP CYCLES BECAUSE THEY ARE NOT TRACK ON PROPELLERS.

RED OIL FOUND ON HUB. PREFORMED INSPECTIONS PER MPC26 AND PROPELLER STILL LEAKED RED OIL. PROPELLER REMOVED AND REPLACED. CYCLES ARE NOT TRACKED BUT "0" ENTERED TO ALLOW FORM TO SUBMIT.

WHILE IS CRUISE FLIGHT NG WENT HIGH AND BLINKED RED FOLLOWED BY CAS EXCEEDANCE MESSAGE. INSPECTED AND NO FAULTS FOUND. BELIEVED TO BE GLITCH IN GARMIN CAUSING FALSE INDICATIONS BASED ON THE GARMIN RECORDS FROM THE DATA LOGGER CARD. NO OTHER VISUAL OR AUDITABLE INDICATIONS OF NG OVERSPEED BESIDES GAGE FLICKER AND CAS MESSAGE.

LEFT EXHAUST ON LEFT SIDE OF THE ENGINE CRACKED AROUND WELDED TUBE FOR THE HEATED INLET LIP.

LEFT OUTBOARD EXHAUST CRACKED WHERE HEATED LIP TUBE IS WELD TO BOTTOM.

PFD #1 FAILURE IN FLIGHT. NG "X" OUT. NO ABNORMAL ENGINE INDICATIONS.

SHIMMY DAMPENER HAS EXCESSIVE SHIMMY AND LEAKING OIL.

NO CHROME SHOWING ON RIGHT LANDING GEAR STRUT

NOSE SHIMMY ON LANDING AND TAKE OFF. FOUND SHIMMY DAMPENER LOW ON FLUID AND GEAR ON TOP OF THE NOSE LANDING GEAR LOOSE.

FLAP CONTROL LEVER STIFF

PROP DE-ICE CAS MESSAGE ON RUN-UP. FOUND LH & RH LOW OIL PRESSURE SWITCHES WERE FAILED.

FOUND LH ENGINE OIL LOW PRESSURE SWITCH LOOSE IN BOSS.

AFT CABIN DOOR CAS MESSAGE CONTINUOUSLY ON. AFT DOOR PROXIMITY SWITCH NEEDED RE-RIGGED.

BATT TIE OPEN ANNUNCIATOR ILLUMINATED DURING FLIGHT.

RIGHT PITOT MAST HEATING ELEMENT FAILED

CAP ON TOP OF THE VERTICAL THAT BEACON MOUNTS TO CRACKED IN MULTIPLE PLACES ALLOWING THE BEACON TO BECOME LOOSE ON TOP OF THE VERTICAL STABILIZER.

RH INERTIAL SEPARATOR INOPERATIVE. AFTER LANDING MAINTENANCE FOUND ROD END BROKEN THAT CONNECTS THE ELECTRIC ACTUATOR TO THE FIRE WALL.

PILOTS CROTCH SEATBELT STRAP ANCHOR MISSING ATTACHMENT BOLT.

PILOTS CONTROL YOKE ATTACHMENT SCREWS LOOSE

CO-PILOTS YOKE SHAFT ATTACHMENT SCREWS LOOSE.

STANDBY INDICATOR BATTERY FAILED PREFLIGHT TEST AND WOULD NOT CHARGE.

RUDDER BIAS SYSTEM ALLOWING RUDDER TO FAVOR ONE SIDE INSTEAD OF BALANCING AS DESIGNED. MORE PILOT RUDDER INPUT REQUIRE TO COUNTER ACT.

RUDDER PEDAL HARDER TO PUSH WITH RUDDER BIAS ON. FOUND THE RUDDER BIAS AIR CYLINDER LEAKING AIR FROM ONE SIDE CAUSING THE RUDDER TO BIAS THE NON LEAKING SIDE.

BOTH LH AND RH LOWER ENGINE COWLINGS HAVE STRUCTURE CRACKED UNDER THE ATTACHMENT OF THE ICE VANE DOOR LINKAGE CASTINGS. CRACKING WAS NOTICED COMING OUT FROM UNDER THE CASTINGS AND WHEN THE INSPECTION PANELS WERE OPENED TO LOOK AT THE STRUCTURE UNDER THE CASTINGS THERE WAS ADDITION CRACKING LOCATED. LONGERON P/N: 7852121-28, SUPPORT P/N: 7852122-22

BOTH LH AND RH LOWER ENGINE COWLINGS HAVE STRUCTURE CRACKED UNDER THE ATTACHMENT OF THE ICE VANE DOOR LINKAGE CASTINGS. CRACKING WAS NOTICED COMING OUT FROM UNDER THE CASTINGS AND WHEN THE INSPECTION PANELS WERE OPENED TO LOOK AT THE STRUCTURE UNDER THE CASTINGS THERE WAS ADDITION CRACKING LOCATED. LONGERON P/N: 7852121-28, SUPPORT P/N: 7852122-22

LH AND RH AFT ICE VANE DOOR FOUND TO BE CHAFING ON EXIT DUCT CAUSING A GROOVE TO BE WORN INTO THE SKIN WHEN ICE VANE SYSTEM IN THE NORMAL CONFIGURATION.

LH LOWER ENGINE COWLINGS HAVE STRUCTURE CRACKED UNDER THE ICE VANE DOOR LINKAGE CASTING ATTACHMENTS. P/N: 7852122-28 & 7852122-27 CRACKED

LH & RH AFT ICE VANE DOOR FOUND CHAFING ON EXIT DUCT CAUSING A GROOVE TO BE WORN INTO THE SKIN WHEN THE ICE VANES WERE IN THE NORMAL CONFIGURATION.

BLOWER MOTOR MAKING LOUD NOISES DURING OPERATION. WHEN FAN SPUN BY HAND THERE WAS INDICATION OF DRAG OR ROUGHNESS IN MOTOR. MOTOR HAS ONLY BEEN INSTALLED FOR 205.1HRS.

DURING 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 TRAVELING FROM ONE RIVET TO THE NEXT. NO LOOSING OF THE RIVETS WAS OBSERVED. THE OPERATOR DID NOT REPORT ANY OVERSTRESS OF THE ELEVATOR OR ELEVATOR CONTROL SYSTEM AND NO FURTHER DAMAGE WAS FOUND THAT WOULD SUGGEST AN OVERSTRESS CONDITION. FAILURE OF THIS BRACKET WOULD CAUSE LOSS OF ELEVATOR CONTROL ON ONE SIDE AND CAUSE A SERIOUS RISK TO THE SAFETY OF FLIGHT. THE CRACKED BRACKET WAS REPLACED WITH NEW AND THE AIRCRAFT WAS PLACED BACK INTO SERVICE.

LOW FUEL PRESSURE CASS MESSAGE. SENSOR ON ENGINE FAILED

LOW FUEL PRESSURE MESSAGE. SENSOR ON ENGINE FAILED.

LOW FUEL PRESSSSSURE CASS MESSAGE. SENOR ON ENGINE FAILED

LOW FUEL PRESSURE CAS MESSAGE. SENOR ON ENGINE FUEL/OIL HEAT EXCHANGER FAILED.

LOW FUEL PRESSURE CAS MESSAGE. SENSOR ON ENGINE FUEL/OIL HEAT EXCHANGER FAILED.

LOW FUEL PRESSURE CAS MESSAGE. SENSOR ON ENGINE FUEL/OIL HEAT EXCHANGER FAILED.

LOW FUEL PESSURE CASS MESSAGE. SENSOR ON ENGINE FAILED