- Registered owner
- Wright Air Service Inc
- Location
- Fairbanks, AK
- Owner type
- Corporation
- Serial number
- 208B5194
- Year built
- 2015
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- March 18, 2015
- Certificate issued
- July 26, 2022
- Expires
- July 31, 2029
- Mode S code
- AA1B94
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 21
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1988 | 1 |
|---|---|
| 1990 | 2 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 2 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 2 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 3 |
| 2021 | 1 |
| 2023 | 1 |
See all 26 ADs
Information bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N750RVMatched 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 Cessna 208B aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EPUA20180928001Master Cylinder · failedNO BRAKES WERE NOTED BY PILOT FOR LEFT TIRE. MAINTENANCE INSPECTED AIRCRAFT AND DETERMINED THAT THE LEFT BRAKE MASTER CYLINDER HAD FAILED. THE UNIT IS SUSPECTED TO HAVE INTERNAL LEAKAGE. UNIT WAS REPLACED AND NO FURTHER ISSUES WERE NOTEDSDR EPUA20170807001Bolt · brokenDURING AIRCRAFT GROUND OPERATIONS, IT WAS NOTED THAT THE LEFT WHEEL BRAKE CALIPER WAS DISCOVERED BROKEN. MAINTENANCE INSPECTED THE DEFECT AND NOTED THAT THE LEFT MAIN LANDING GEAR BRAKE CALIPER ANCHOR BOLT BROKEN. REPLACED THE BRAKE ASSEMBLY, TORQUE PLATE, ASDR EPUA20170718001Rivet · looseTHE RIGHT ELEVATOR HAS SMOKING RIVETS ON THE INBOARD BUTT RIB WHERE THE TORQUE TUBE ATTACHES. VISUAL INSPECTION INDICATES THAT ALL OF THE ATTACH RIVETS EXCEPT FOR THREE ARE SMOKING. THE LEFT ELEVATOR LOOKS CONSIDERABLY BETTER THAN THE RIGHT SIDE BUT ONE RIVESDR EPUA20160422001Drive Assy · separatedSTANDBY POWER ANNUNCIATOR LIGHT WON’T GO OUT. INSPECTED ACFT & FOUND THAT THE RETAINING RING FOR THE STANDBY ALTERNATOR DRIVE PULLEY HAD FAILED. DUE TO THIS FAILURE THE DRIVE PULLEY HAD MIGRATED OUT OF THE HOUSING ASSEMBLY & WAS LYING IN THE ENG COWLING ASSE
STCs that may be installed · 300
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.