- Registered owner
- N208ee Inc
- Location
- Addison, TX
- Owner type
- Corporation
- Serial number
- 208B1213
- Year built
- 2006
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- December 23, 2014
- Certificate issued
- June 27, 2019
- Expires
- June 30, 2029
- Mode S code
- A1B024
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 26
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 | 2 |
| 1998 | 2 |
| 2001 | 2 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 2 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 3 |
| 2012 | 1 |
| 2014 | 1 |
| 2015 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
See all 32 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
Airframe · Cessna 208B
SAIB CE-18-32Engine Oil System (Airframe Furnished): Flapper Check Valve FailureSAIB CE-17-25ELEVATOR TORQUE TUBE Inspections for cracks and corrosion in elevator torque tubesSAIB CE-09-42Lights - Landing Light, Beacon Light and Taxi Light Switch ApplicationsEngine · Pratt & Whitney Canada PT6A-114A
SAIB NE-12-04Turbine/ Turboprop Engine: Reduction GearboxSAIB NE-10-47Turbine Engine Compressor SectionNTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
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 · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 141A202504110001Wheel · noiseON APPROACH TO STL, CREW KEPT HEARING LOUD CRACKING/POPPING SOUNDS. THE SOUND WAS COMING FROM LH SIDE NEAR TIRE ASSY.. CREW ASK APPROACH FOR A SLOWER THAN NORMAL APPROACH FOR ISSUE. ATC DECLARED THE EMERGENCY. THROUGH POST FLIGHT INSPECTION FOUND NO ISSUESSDR 2023F00195Belt · brokenSMELL OF BURNT RUBBER FOLLOWED BY SMOKE IN THE COCKPIT DUE TO AIR CONDITIONING BELT BREAKING AND RUBBING ON COMPRESSOR PULLEYSDR 2023F00040None · wornCREW REPORTED PROPELLER HEAT INOP-SHOWS 8-9 AMPS IN BOTH AUTO AND MANUAL. MODES. CORRECTIVE ACTION: REMOVED PROPELLER ANTI-ICE LEADS. INSTALLED THREE NEW PROPELLER DE-ICE LEADS. PROPELLER ANTI-ICE SYSTEMS CHECK GOOD ON ENGINE GROUND RUN. SUBSEQUENT FLIGHT WAS SDR MUIA20190212001Connector · contaminatedCREW PERFORMED AIR RETURN AFTER RESERVOIR LOW FUEL LIGHT ILLUMINATED ON ANNUNCIATOR PANEL WITH LH & RH WING LOW FUEL LIGHTS ILLUMINATED ON ANNUNCIATOR PANEL WHEN DAY-NIGHT SWITCH MOVED TO "DAY" MODE. FOUND MOISTURE ACCUMULATION UNDER FLOOR IN AREA OF FUEL RESESDR MUIA201806216001Engine · power lossCREW REJECTED TAKEOFF AND REPORTED INSUFFICIENT ENGINE TORQUE. PERFORMED GROUND RUN WITH CREW WITH NO FAULTS. FOUND CREW DISCUSSED THE EFFECTS OF HIGH OUTSIDE AIR TEMPERATURE AND ELEVATED DENSITY ALTITUDE ON AIRCRAFT AND ENGINE PERFORMANCE WITH DIRECTOR OF OPESDR MUIA201806011001Connector · contaminatedREJECTED TAKEOFF, DUE TO THE FUEL RESERVOIR LOW LIGHT ILLUMINATING DURING THE TAKEOFF ROLL. FOUND AND CLEARED MOISTURE FROM ANNUNCIATOR PANEL CONNECTOR WITH INDICATION GOING AWAY AND NOT RETURNING DURING A REPO FLIGHT.SDR MUIA20180119001Screw · looseTHE SCREW THAT WAS LOOSE WAS THE FWD SCREW ON THE PILOT-SIDE KICK PANEL. IT HAD LAST BEEN REMOVED 138.2 HRS PRIOR TO THIS EVENT DURING NORMAL INSPECTION REQUIREMENTS AND WAS MOST LIKELY UNDER TORQUED DURING INSTALLATION.SDR MUIA20170209001Engine · stalledCREW REPORTED ENGINE SHUTDOWN (STALL) DURING TAXI. PERFORMED GENERAL VISUAL INSPECTION OF ENTIRE ENGINE. PERFORMED BORESCOPE OF 1ST STAGE COMPRESSOR. PERFORMED POWER ASSURANCE RUN OF AIRCRAFT WITH ALL RESULTS NORMAL, NO DEFECTS FOUND. NO PREVIOUS REPORTS OF THSDR MUIA20160824001Brake · unserviceableCREW REPORTED BRAKE FAILURE AND WAS TOWED BACK TO HANGAR. MAINTENANCE PERFORMED VISUAL INSPECTION OF BRAKE SYS AND FOUND NO LEAKS OR OBVIOUS MECHANICAL DEFECTS. REPLACED LT BRAKE AT WHEEL WITH SERVICEABLE UNIT AND REPLACED LT MLG BRAKE LININGS AS A PRECAUTIONSDR MUIA20160125001Fcu · malfunctionedFLIGHT CREW STATED THAT WHILE IN CRUISE THEY LOST 300 LBS OF TORQUE & FELT JOLT IN ACFT. THEY CONTINUALLY HAD A DEGRADATION OF POWER UNTIL LANDING. THE BEST THEY COULD OBTAIN WAS 1,100 LBS OF TORQUE UPON LANDING. ACFT WAS INSPECTED AT SITE OF EMER LANDING &
STCs that may be installed · 306
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.