N422CA
Registered owner: BERING AIR INC, AK (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Bering Air, Inc. (FXTA) | Certificate holder | — | Matched 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.
9 reports on file, 1997-02-27 – 2015-12-04.
Part: G SWITCH — INOPERATIVE (ELT) · airframe 15,967 hrs · 15,375 cycles
G-SWITCH IN ELT FAILED TO TEST. NO MATTER HOW HARD YOU HIT THE ELT IT WOULD NOT TRIP THE G-SWITCH.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 13,898 hrs · 13,318 cycles
CORROSION ON FUSELAGE CHINE ANGLE BELOW THE COCKPIT FLOOR.
Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 3 · airframe 13,898 hrs · 13,318 cycles
CORROSION ON FUSELAGE TO HORIZONTAL STABILIZER ATTACH FITTINGS.
Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 13,898 hrs · 13,318 cycles
CORROSION ON FUSELAGE TO HORIZONTAL STABILIZER ATTACH FITTINGS.
Part: SPAR CAP — CORRODED (CENTER WING) · corrosion level 3 · airframe 13,898 hrs · 13,318 cycles
CORROSION ON CTR WING UPPER SPAR CAP "T" ON THE LOWER SURFACE OF THE FWD FLANGE UNDER NUTPLATE AT CWS 1821.
Part: SPAR CAP — CORRODED (CENTER WING) · corrosion level 3 · airframe 13,898 hrs · 13,318 cycles
(KGBR) CORROSION ON CTR WING UPPER SPAR CAP "T" ON THE LOWER SURFACE OF THE FWD FLANGE UNDER NUTPLATE AT CWS 1821.
Part: ENGINE — MAKING METAL (NR 2)
ON DOWNWIND LEG AT 2000 FT PILOT NOTICED NR 2 ENGINE TORQUE GAGE READ 0. COPILOT VISUAL OF NR 2 PROP REPORTED AS FEATHERED EMERGENCY HANDLE ACTIVATED AND UNEVENTFUL LANDING MADE. SUBSQUENT ENGINE START FAILED. NEXT START ATTEMPT FOLLOWING DAY FOR TROUBLESHOOTING NORMAL, AFTER 2 MINUTE GROUND RUN NR 2 ENGINE CHIP DETECTOR ILLUMINATED AND ENGINE WAS SHUT DOWN. OIL FILTER INSPECTION REVEALED NO METAL CONTENT. ENGINE REMOVED FROM SERVICE.
Part: ENGINE — FAILED (NR 2)
ON DOWNWIND LEG AT 2000 FEET, AGL PILOT NOTICED NR 2 ENGINE TQ. GAUGE READ 0. COPILOT VISUAL OF NR 2 PROP REPORTED AS FEATHERED. E HANDLE ACTIVATED AND UNEVENTFUL LANDING MADE. SUBSEQUENT ENGINE START FAILED. NEXT START ATTEMPT FOLLOWING DAY FOR TROUBLESHOOTING NORMAL, AFTER 2 MINUTE GROUND RUN NR 2 ENGINE CHIP DETECTOR ILLUMINATED AND ENGINE WAS SHUT DOWN. OIL FILTER INSPECTION REVEALED NO METAL CONTENT. ENGINE REMOVE FROM SERVICE AND SENT TO REPAIR FACILITY FOR INSPECTION/ REPAIR.
Part: ENGINE — FAILED (NR 1)
THE FOLLOWING DETAILS WERE REPORTED BY THE PILOT. THEY OCCURRED WHILE EN ROUTE. A/C YAWED TO LEFT. NR 1 TQ INDICATOR SPOOLED DOWN RAPIDLY. CHIP DET LT LIGHT ILLUMINATED ON WARNING ANNUNCIATOR PANEL. NR 1 RPM INDICATOR SPOOLED DOWN. NR 1 OIL PRESSURE, FUEL FLOW, AND EGT SPOOLED DOWN. AIR SPEED REDUCED FROM 160 KIAS TO 125. AT THE TIME OF THE INCIDENT, ENGINE TSN: 8028.6; TSO: 3410.0; CYCLES: 3177. THERE WERE 208.7 HOURS SINCE THE LAST HSI AND G/B INSP. PRIMARY FOCUS IS ON THE GEARBOX; HOWEVER, TEAR DOWN HAS NOT OCCURRED.