- Registered owner
- Alaska Central Express Inc
- Location
- Anchorage, AK
- Owner type
- Corporation
- Serial number
- UC44
- Year built
- 1988
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- May 24, 2018
- Certificate issued
- April 12, 2018
- Expires
- April 30, 2028
- Mode S code
- A0665B
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 41
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1987 | 3 |
|---|---|
| 1989 | 1 |
| 1992 | 1 |
| 1993 | 1 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 3 |
| 1997 | 7 |
| 1998 | 3 |
| 1999 | 4 |
| 2000 | 2 |
| 2001 | 2 |
| 2003 | 3 |
| 2004 | 5 |
| 2005 | 3 |
| 2006 | 2 |
| 2009 | 2 |
| 2011 | 1 |
| 2012 | 1 |
| 2014 | 2 |
| 2023 | 1 |
See all 50 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N125AXMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Beech 1900C aircraft
FAA incident reports
No FAA accident or incident reports matched to N125AXMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Beech 1900C aircraft
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR YADA2025012701Pump · erodedMAINTENANCE DISCOVERED A LEAKING ENGINE OIL SCAVENGE PUMP - A PINHOLE WAS VERIFIED IN THE PUMP HOUSING OUTER WALL FROM INTERNAL EROSION - REPLACED SAME.SDR YADA20230313005Bellcrank · crackedWHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED
WEB.SDR YADA2022100301None · erodedDURING 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 ASDR YADA20200702001Fcu · power lossPILOT 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 FUSDR YADA201806065001Duct · disconnectedDURING 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 HEATE
STCs that may be installed · 177
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 1900C
STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light ControllerSTC SA04837NYInstallation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights