- Registered owner
- M E S LLC
- Location
- Anchorage, AK
- Owner type
- LLC
- Serial number
- AC-583
- Year built
- 1984
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- May 31, 1984
- Certificate issued
- December 1, 2015
- Expires
- December 31, 2028
- Mode S code
- A34D73
From the FAA registry file of October 27, 2026. The registry lists only the engine series, so ADs for every AiResearch TPE331 model are included below.
On this page
NTSB investigations
No NTSB investigations matched to N3114GMatched 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 Fairchild SA227-AC 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.
Airworthiness directives that may apply · 93
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1972 | 1 |
|---|---|
| 1974 | 2 |
| 1975 | 2 |
| 1976 | 1 |
| 1979 | 2 |
| 1980 | 2 |
| 1982 | 1 |
| 1983 | 1 |
| 1984 | 3 |
| 1986 | 2 |
| 1987 | 2 |
| 1988 | 1 |
| 1989 | 1 |
| 1990 | 3 |
| 1991 | 2 |
| 1992 | 3 |
| 1993 | 8 |
| 1994 | 2 |
| 1995 | 3 |
| 1996 | 8 |
| 1997 | 6 |
| 1998 | 5 |
| 1999 | 1 |
| 2000 | 5 |
| 2001 | 2 |
| 2002 | 5 |
| 2003 | 2 |
| 2004 | 1 |
| 2005 | 3 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 2 |
| 2011 | 2 |
| 2012 | 2 |
| 2014 | 3 |
| 2015 | 3 |
| 2016 | 4 |
| 2017 | 2 |
| 2018 | 4 |
| 2026 | 1 |
See all 113 ADs
Information bulletins that may apply · 18
Advisory, not mandatory.
See all 19 bulletins
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR TN8A2015011500001Valve · failedFLIGHT RETURNING TO BASE AFTER FREIGHT CHARTER FLIGHT. UPON APPROACH PILOT SELECTED GEAR DOWN BUT DID NOT RECEIVE A GREEN LIGHT INDICATION FOR THE NOSE GEAR. PILOT RECYCLED GEAR AND REQUESTED TO TERMINATE LANDING. PILOT MANUAL EXTENDED THE LANDING GEAR IAW SDR M0501Windshield · crackedNR 1 WINDSHIELD CRACKED AT DESCENT FROM CRUISE, CREW DEPRESSURIZED AIRCRAFT, DESCENDED TO PROPER ALTITUDE, AND DIVERTED TO LAND WITHOUT INCIDENT. OAT WAS -40C, WINDSHIELD HEAT WAS ON "LOW". MAINTENANCE FOUND INNER PANE EXTENSIVELY CRACKED.SDR 2005FA0000065Windshield · crackedMRR-M05-01, NR 1 WINDSHIELD CRACKED IN FLIGHT JUST AS CREW STARTED DESCENT. CREW DEPRESSURIZED AC, DESCENDED TO AN APPROPRIATE ALTITUDE FOR NON-PRESSURIZED FLIGHT, AND DIVERTED TO AN AIRPORT WITH VMC CONDITIONS. CREW LANDED WITH NO FURTHER INCIDENT. OAT WASSDR 2005FA0000060Smoke · detectedMRR-M04-19, CREW NOTICED SMOKE IN COCKPIT AS THEY WERE CLIMBING THROUGH 12,000 FT, DESCENDED TO 10,000 FT, DEPRESSURIZED, TURNED OFF BLEEDS, AND CONTINUED TO STATION UNPRESSURIZED. SUSPECTED ACM FAILURE OR BLEED HEAT CNTRL VALVE FAILURE. RAN BOTH ENG FOR 20 SDR 2005FA0000059Fire Bottle · emptyMRR-M04-18, DURING FLIGHT THE LT FIRE EXTINGUISHER (E) LIGHT CAME ON BRIEFLY SEVERAL TIMES. THE CREW MONITORED THE LIGHT AND THE FLIGHT WAS CONTINUED TO THE DESTINATION WITH NO INCIDENT. FIRE EXTINGUISHER (E) LIGHT WAS FOUND ON, AND THE FIRE EXTINGUISHER BOTSDR SDR02060432Shaft · fracturedUPON LANDING, DURING ROLL OUT PILOT REPORTED A HEAVY VIBRATION FOLLOWED BY AN ABRUPT PULL TO THE LEFT. INSPECTION OF THE LT MAIN GEAR ASSEMBLY REVEALED A BROKEN LOWER SCISSOR ASSEMBLY SHAFT WHICH ALLOWED THE YOKE TO ROTATE.SDR 99ZZZM318Torque Indicator · inoperativeDURING TAKEOFF ROLL AT LCH, THERE WAS NO RIGHT TORQUE INDICATION AND THE TAKEOFF WAS ABORTED. MAINTENANCE REMOVED AND REPLACED THE RIGHT TORQUE INDICATOR AND COMPLIED WITH AN OPERATIONS CHECK. THE CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVISDR 99ZZZM2Wire · brokenUPON LANDING ROLLOUT AT SLU, A/C BEGAN DRIFTING TO THE RT, WITH THE NOSE WHEEL STEERING ARMED. THE PILOT MAINTAINED THE RUNWAY CENTERLINE WITH THE RUDDER BUT AS THE A/C SLOWED, THE RUDDER BECAME LESS EFFECTIVE AND NOSEWHEEL STEERING STILL DID NOT RESPOND. PISDR 98ZZZM935Line · brokenWHILE EN ROUTE FROM SJU TO BGI, THE AIRCRAFT EXPERIENCED COMPLETE HYDRAULIC FAILURE ON THE LEFT ENGINE. BOTH HYDRAULIC LIGHTS ILLUMINATED AND THE HYDRAULIC GAUGE INDICATED ZERO PRESSURE. AFTER ACCOMPLISHING EMERGENCY GEAR EXTENSION PROCEDURE, THE AIRCRAFT LASDR 98ZZZM637Actuator · inoperativeAFTER TAKEOFF OUT OF MIQ, THE CREW HAD TO RECYCLE THE NOSE LANDING GEAR IN ORDER TO GET THE GEAR LIGHT TO EXTINGUISH. THE RED INTRANSIT LIGHT WENT ON AND OFF 3 TIMES BEFORE EXTINGUISHING. THE AIRCRAFT LANDED AT SJU WITHOUT FURTHER INCIDENT. MAINTENANCE REMOSDR 97ZZZM899Radar Indicator · failedDEPARTING SJU-CUR, WHILE ADDING POWER FOR TAKEOFF, THE CREW SUDDENLY SMELLED SMOKE IN THE COCKPIT. THE SMELL INDICATED THAT THE SMOKE WAS OF THE ELECTRICAL TYPE. THE TAKEOFF WAS ABORTED. MAINTENANCE REPLACED THE RADAR INDICATOR. AIRCRAFT WAS RELEASED AND DSDR 97ZZZM740Srl Computer · malfunctionedON TAKEOFF ROLL OUT OF SJU, THE LEFT ENGINE EGT AND TORQUE INDICATIONS BECAME ERRATIC. THE PILOT ABORTED THE TAKEOFF AND ASKED FOR CLEARANCE TO A SECLUDED AREA TO PERFORM AN ENG RUNUP CHECK. DURING THE RUNUP CHECK THE PILOT TURNED OFF THE LT SRL AND THE LT E
STCs that may be installed · 130
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Fairchild SA227-AC
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