- Registered owner
- Ameriflight LLC
- Location
- Dallas, TX
- Owner type
- LLC
- Serial number
- UC57
- Year built
- 1989
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- April 21, 2013
- Certificate issued
- March 21, 2024
- Expires
- March 31, 2031
- Mode S code
- A3B38D
From the FAA registry file of October 22, 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 N338AFMatched 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 N338AFMatched 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 · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR JIKA2026072401Hydraulic System · lowDURING APPROACH, THE FLIGHT CREW REPORTED THAT THE LANDING GEAR HANDLE WAS SELECTED DOWN BUT EMERGENCY EXTENSION PROCEDURES WERE FOLLOWED TO ALLOW THE LANDING GEAR TO BE EXTENDED SAFELY. MAINTENANCE REPORTED THAT UPON INSPECTION IT WAS NOTED THAT THE HYDRAULICSDR JIKA2016050301Bleed Valve · stickingTHE TRAINING CAPTAIN REPORTED WHILE PERFORMING TRAINING STALL MANEUVERS, THE FIRST OFFICER REDUCED POWER, A MOMENTARY COMPRESSOR STALL OCCURRED, BETWEEN 500 - 1000 FT & LBS TORQUE ON THE LT ENG. TRAINING CAPTAIN REDUCED POWER, THIS RESULTED IN ANOTHER STALL.
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