N848BA

TEXTRON AVIATION INC 208B · 2015 · Fixed-wing single-engine · 1 engine · 12 seats · Valid Registration

Registered owner: BERING AIR INC, AK (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Bering Air, Inc. (FXTA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

5 reports on file, 2017-06-26 – 2019-04-17.

WARNING INDICATION · 2019-04-17 Matched by certificate designator
ATA 2844

Part: PRESSURE SWITCH — FAILED (LOW FUEL) · airframe 3,416 hrs · 7,174 cycles

LOW FUEL PRESSURE LIGHT CAME ON DURING START-UP. SENSOR ON ENGINE HAD FAILED.

Source: SDR FXTA20210505002
WARNING INDICATION · 2019-01-04 Matched by certificate designator
ATA 2844

Part: PRESSURE SWITCH — FAILED (LOW FUEL) · airframe 3,108 hrs · 6,526 cycles

LOW FUEL PRESSURE LIGHT CAME ON DURING START-UP. SENSOR ON ENGINE HAD FAILED.

Source: SDR FXTA20210505003
OTHER · 2018-02-16 Matched by certificate designator
ATA 5511

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 2,207 hrs · 4,767 cycles

THE RIB ON THE LT HORIZONTAL STABILIZER AT HSS 80.60 CRACKED WHERE THE LATERAL STRINGER GOES THROUGH THE RIB.

Source: SDR 2018F00106
OTHER · 2017-11-25 Matched by certificate designator
ATA 3242

Part: PIN — LOOSE (BRAKE ASSY) · airframe 1,963 hrs · 4,243 cycles

BRAKE CALIPER ANCHOR PIN LOOSE IN CALIPER HOUSING. IF ANCHOR PIN FAILS CALIPER WILL CAUSE MAIN WHEEL TO LOCK UP, CAUSING A VERY UNSAFE CONDITION FOR LANDING.

Source: SDR 2017F00201
OTHER · 2017-06-26 Matched by certificate designator
ATA 2730

Part: TORQUE TUBE — LOOSE (ELEVATOR) · airframe 1,573 hrs · 3,422 cycles

ON A NON ROUTINE INSPECTION FOUND THE LEFT AND RIGHT ELEVATOR CONTROL TORQUE TUBES LOOSE WHERE IT ATTACHES TO THE ELEVATOR. THE RIVETS HAD BEEN WORKING IN THE FLANGE THAT ATTACHES THE TORQUE TUBE TO THE ELEVATOR AT THE BUTT RIB INBOARD AND THE SPAR ATTACHMENT OUTBOARD. IF NOT FOUND SOON ENOUGH COULD HAVE LED TO LOSS OF CONTROL OF THE ELEVATOR. THIS A FAIRLY NEW LOW TIME AIRCRAFT TO BE HAVING AN ISSUE LIKE THIS.

Source: SDR 2017F00100