N125AX

BEECH 1900C · 1988 · Fixed-wing multi-engine · 2 engines · 19 seats · Valid Registration

Registered owner: ALASKA CENTRAL EXPRESS INC, AK (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
ALASKA CENTRAL EXPRESS INC (YADA)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.

5 reports on file, 2018-06-05 – 2025-01-27.

FLUID LOSS · 2025-01-27 Matched by certificate designator
ATA 7261

Part: PUMP — ERODED (SCAVENGE) · airframe 34,008 hrs · 36,891 cycles

MAINTENANCE DISCOVERED A LEAKING ENGINE OIL SCAVENGE PUMP - A PINHOLE WAS VERIFIED IN THE PUMP HOUSING OUTER WALL FROM INTERNAL EROSION - REPLACED SAME.

Source: SDR YADA2025012701
OTHER · 2023-03-06 Matched by certificate designator
ATA 2730

Part: BELLCRANK — CRACKED (ZONE 200) · airframe 31,011 hrs · 34,990 cycles

WHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED WEB.

Source: SDR YADA20230313005
FLUID LOSS · 2022-10-15 Matched by certificate designator
ATA 7920

Part: NONE — ERODED (ZONE 500) · airframe 30,350 hrs · 34,553 cycles

DURING UNRELATED MAINTENANCE, AN OIL LEAK WAS DISCOVERED FROM THE LEFT ENGINE. MAINTENANCE IDENTIFIED THE ENGINE OIL SCAVENGE PUMP AS HAVING A PINHOLE LEAK AND THE PUMP HOUSING WAS REPLACED. INSPECTION DETERMINED THAT CAVITATION EROSION OF THE PUMP BODY IN A CORNER OF THE CAVITY HAD CREATED A HOLE. THIS IS A FREQUENT ON THESE PUMP HOUSINGS. POST REPLACEMENT OF PUMP HOUSING LEAK CHECK WAS GOOD.

Source: SDR YADA2022100301
ENGINE STOPPAGE · 2020-07-01 Matched by certificate designator
ATA 7321

Part: FCU — POWER LOSS (LEFT ENGINE) · airframe 25,687 hrs · 31,436 cycles

PILOT REPORT: LEFT ENGINE FAILURE IN FLIGHT. TORQUE ROLLED BACK SLOWLY TO 0 NG INDICATED APPROX 55 FUEL FLOW 100 PPH. ATTEMPTED STARTER ASSIST AIRSTART. PROP FEATHERED AND UNFEATHERED NORMALLY. SAME INDICATIONS FOR RESTART. SECURED ENGINE. 1300 LBS OF FUEL ON BOARD. MAINTENANCE REPORT: THE CAUSE OF THE FAILURE HAS YET TO BE DETERMINED.

Source: SDR YADA20200702001
WARNING INDICATION · 2018-06-05 Matched by certificate designator
ATA 3020

Part: DUCT — DISCONNECTED (AIR INTAKE) · airframe 23,354 hrs · 30,131 cycles

DURING TAKEOFF ROLL, THE NR 2 ENGINE FIRE LIGHT ILLUMINATED. AFTER RETARDING THE POWER, THE LIGHT DISTINGUISHED. MAINTENANCE PERFORMED INSPECTION OF THE #2 ENGINE AND FOUND THAT THE AIR INTAKE HEATED LIP DUCT WAS DISCONNECTED. MAINTENANCE CONNECTED THE HEATED LIP DUCT.

Source: SDR YADA201806065001