- Registered owner
- Martinaire Aviation LLC
- Location
- Addison, TX
- Owner type
- LLC
- Serial number
- 208B0167
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Certificate issued
- October 26, 2006
- Expires
- October 31, 2028
- Mode S code
- A5BAA2
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 N4687BMatched 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 · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2024F00250Servo · lockedPITCH TRIM SERVO LOCKS UP WITH AUTOPILOT ENGAGEDSDR 2024FA0000769Servo · bindsTHE ROLL TRIM SERVO IS LOCKING UP.SDR 2017FA0000568Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.SDR 2012FA0000421Hose · unserviceable12.5" LONG HOSE TO THE SECONDARY EXHAUST WAS FOUND TO HAVE SWOLLEN UP INTERNALLY.SDR 2010FA0001063Case · brokenPILOT REPORTED TO MX THAT WITH THE THROTTLE LEVER AT THE GATE (FWD SIDE OF GATE) THE ENGINE WAS GOING INTO REVERSE. THE SUBSEQUENT INSP FOUND THE REVERSE ROPE CASING HAD BROKEN AT THE SWIVEL JOINT. THE REVERSE ROPE ITSELF WAS STILL ATTACHED.SDR MT92008F00008Transistor · burnedTHE PILOT REPORTED SMOKE IN THE COCKPIT TO ATC, DECLARED AN EMERGENCY, AND RETURNED TO DEPARTURE. THE SMOKE THAT WAS SEEN BY THE PILOT APPEARED TO BE COMING FROM UNDER THE GLARE SHIELD ABOVE THE FUEL FLOW AND FUEL QUANTITY INDICATORS. THE PILOT SAID THERE WASDR 95ZZZX1894Bracket · brokenPILOT REPORTED FLAP C/B TRIPPED DURING FLAP RETRACTION. DURING TROUBLESHOOTING, FOUND PN 2611144-1 WING FLAP MOTOR BRACKET BROKEN CAUSING THE MOTOR TRANSMISSION ASSY TO BIND. POSSIBLE CAUSES FOR THIS PROBLEM ARE (1) EXCESSIVE USE OF THE STBY FLAP SYSTEM, THE
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.