# N295UX: 1995 Embraer EMB-120ER, registration cancelled 2010-06-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 30, 2010
- Exported to: Brazil
- Status when cancelled: Valid registration
- Airframe: [Embraer EMB-120ER](https://openairdocs.org/model/embraer-emb-120er) (registry code 3260203)
- Engine: [Pratt & Whitney Canada PW118](https://openairdocs.org/engine/pratt-whitney-canada-pw118) (registry code 52116)
- Data sheets: [TCDS A31SO](https://openairdocs.org/tcds/A31SO), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 120.295
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: February 12, 1995
- Certificate issued: April 15, 2010
- Last registry action: June 4, 2010
- Mode S code: A309E5
- Owner when cancelled: [Intercontinental Jet Inc](https://openairdocs.org/faa-owner/INTERCONTINENTAL%20JET%20INC)
- Location: [Tulsa, OK](https://openairdocs.org/faa-place/OK/Tulsa)
- Owner type: Corporation
- Owner's area on the map: 36.1993° N, 95.9089° W: Placed by OpenAirDocs at the center of ZIP code 74115, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N295UX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=295UX
- Page: https://openairdocs.org/deregistered/N295UX-2010-06-30

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Embraer EMB-120ER: https://openairdocs.org/model/embraer-emb-120er.md

## Service difficulty reports (50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR SWIA200922697](https://openairdocs.org/sdr/SWIA200922697), Sep 19, 2009: BATTERY. DISCHARGED. BACK SECTION OF EMERGENCY LIGHTS DO NOT LIGHT UP. (FLT 6488) INSTALLED SERVICEABLE PACK OF BATTERIES TO THE AFT SECTION.
- [SDR SWIA200820382](https://openairdocs.org/sdr/SWIA200820382), Nov 16, 2008: PCU. FAILED. ON TAKEOFF, RIGHT NP DROPPED TO 99 PERCENT AND DID NOT RECOVER, ABORTED TAKEOFF. REPLACED RIGHT PCU, P/N 782490-46 S/N ON 980810 S/N OFF 890455.
- [SDR SWIA200820075](https://openairdocs.org/sdr/SWIA200820075), Sep 17, 2008: SIGN. BROKEN. EMERGENCY EXIT SIGN AT 6C BROKEN. FLT 5493. REPLACED SIGN. 
- [SDR SWIA200819896](https://openairdocs.org/sdr/SWIA200819896), Jul 19, 2008: ATTACH BRACKET. BROKEN. LT NACELLE FLAP HAS A CRACKED ATTACH BRACKET. (FLIGHT NR 5480) REPLACED THE LT NACELLE FLAP IAW 27-50-03. 
- [SDR SWIA200819583](https://openairdocs.org/sdr/SWIA200819583), Apr 26, 2008: PROBE. CONTAMINATED. FLT 5732 - THE LEFT ENGINE WENT INTO AUTO-FEATHER WHILE ON GROUND. INSPECTED AND REMOVED MOISTURE FROM TORQUE PROBE. OPS CHECK GOOD. 
- [SDR SWIA200819209](https://openairdocs.org/sdr/SWIA200819209), Feb 1, 2008: LIGHT. DAMAGED. EMERGENCY LIGHT AT ROW 6A IS DAMAGED, FLIGHT NR 5723. REPLACED EXIT SIGN PER MM 33-51-02. OPS CHECK OK.
- [SDR SWIA200718878](https://openairdocs.org/sdr/SWIA200718878), Nov 12, 2007: ROLLER. OUT OF ADJUST. FLT 5584 - MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN. ADJUSTED UPPER AFT ROLLER ON PAX DOOR FRAME. OPS CHECKS GOOD. 
- [SDR SWIA200718411](https://openairdocs.org/sdr/SWIA200718411), Jun 30, 2007: DOOR. OUT OF ADJUST. FLT 5774 - MAIN CABIN DOOR GETS JAMMED WHEN TRYING TO OPEN FROM INSIDE. REPLACED THE TOP SHIM STACK ATTACH SCREW AND ADJUSTED GAP TO PROPER CLEARANCES. DOOR OPE
- [SDR SWIA200718299](https://openairdocs.org/sdr/SWIA200718299), May 29, 2007: BATTERY PACK. DISCHARGED. FLOOR LEVEL EMERGENCY LIGHTING IN ROW 9 AND EXIT SIGNS ARE INOP. INSTALLED A SERVICEABLE AFT ELBP. OPS CHECK GOOD.
- [SDR SWIA200718088](https://openairdocs.org/sdr/SWIA200718088), Mar 29, 2007: CONNECTOR. OVERHEATED. RIGHT WINDSHIELD WIPER INOP. REPLACED OVERHEATED PINS AT CONTROLLER CONNECTION.
- [SDR SWIA200616767](https://openairdocs.org/sdr/SWIA200616767), Jun 6, 2006: WINDOW. CRACKED. CAPTAIN'S SIDE WINDOW HAS CRACK. REPLACED CAPTAIN'S DV WINDOW PANEL IAW EMB 120 MM 56-11-01. OPERATIONAL AND LEAK CHECKS GOOD, PN: 163600-3 SN OFF: 1151
- [SDR SWIA200616586](https://openairdocs.org/sdr/SWIA200616586), Apr 10, 2006: LIGHT. INOPERATIVE. FLOOR EMERGENCY LIGHTS ADJACENT GALLEY WILL NOT ILLUMINATE. REMOVED AND REPLACED E-LIGHTING IAW 33-00-00.
- [SDR SWIA200616097](https://openairdocs.org/sdr/SWIA200616097), Jan 4, 2006: SMOKE DETECTOR. CONTAMINATED. LAV SMOKE ALARM ACTIVATES WITH SHIP POWER AND WILL NOT RESET. REMOVED MOISTURE FROM LAV SMOKE DETECTOR SENSOR. OPERATIONAL CHECK GOOD.
- [SDR SWIA200515171](https://openairdocs.org/sdr/SWIA200515171), Jun 19, 2005: LIGHT. INOPERATIVE. ONE RED EMERGENCY LIGHT ON FLOOR INOPERATIVE. REPLACED RED EMERGENCY LIGHT ON FLOOR. OPERATIONAL CHECK GOOD.
- [SDR SWIA200414097](https://openairdocs.org/sdr/SWIA200414097), Nov 6, 2004: RELAY. FAILED. SMOKE COMING FROM F/O'S SIDE PANEL. REPLACED OVERHEATED APU FEEDER PROTECTION RELAY. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413636](https://openairdocs.org/sdr/SWIA200413636), Jul 24, 2004: SERVO. MALFUNCTIONED. AUTOPILOT WANDERS IN PITCH AXIS EXCEEDING COMMAND BARS ABOVE AND THEN BELOW. REMOVED AND REPLACED ELEVATOR SERVO. AUTOPILOT OPERATIONAL CHECK GOOD IAW MM 22-11-
- [SDR SWIA200413320](https://openairdocs.org/sdr/SWIA200413320), May 18, 2004: RIB. CRACKED. LEFT NACELLE FLAP 3RD UPPER RIB SUPPORT (FROM OUTBOARD) CRACKED. DISCOVERED DURING A-CHECK INSPECTION. REMOVED AND REPLACED LEFT NACELLE FLAP WITH SERVICEABLE U
- [SDR SWIA200412795](https://openairdocs.org/sdr/SWIA200412795), Jan 21, 2004: COMPUTER. MALFUNCTIONED. AUTOPILOT ON CAPT'S SIDE DOES NOT PASS FIRST FLIGHT OF DAY CHECKS. REPLACED NR 1 AUTOPILOT COMPUTER. OPS CHECKED GOOD.
- [SDR SWIA200312721](https://openairdocs.org/sdr/SWIA200312721), Dec 25, 2003: ACTUATOR. MALFUNCTIONED. ON TAXI IN TO GATE, FLAP RETRACTION CAUSED DISAGREEMENT - NACELLE FLAPS LAGGING. REMOVED AND REPLACED LT NACELLE ACTUATOR IAW MM 27-50-08. OPS CHECKS GOOD.
- [SDR SWIA200312590](https://openairdocs.org/sdr/SWIA200312590), Nov 17, 2003: COMPUTER. FAULTY. CAPTAIN'S COMMAND BARS ON THE FLIGHT DIRECTOR ALWAYS INDICATE ABOUT 4 DEGREES TOO LOW. REPLACED APC-65B COMPUTER. OPS CHECK GOOD IAW MM 22-11-00.
- [SDR SWIA200312585](https://openairdocs.org/sdr/SWIA200312585), Nov 5, 2003: COMPUTER. MALFUNCTIONED. YAW ENGAGED, RUDDER TRIM AT 6, WHEN AUTO-PILOT ENGAGED, PLANE YAWED LEFT AND RIGHT HARD MOMENTARILY. REMOVED AND REPLACED F/O'S APC 65B IAW MM 22-10-02. OPS CHE
- [SDR SWIA200312575](https://openairdocs.org/sdr/SWIA200312575), Nov 3, 2003: CONTROL PANEL. MALFUNCTIONED. WITH YAW ENGAGED AND RUDDER IN TRIM, THEN ENGAGED AUTO PILOT AND AIRPLANE YAWED AND BALL JUST WENT .5 SCALE TO LT, HAPPENED ON BOTH SIDES. REMOVED AND REPLACED 
- [SDR SWIA200211358](https://openairdocs.org/sdr/SWIA200211358), Oct 23, 2002: ACTUATOR. OUT OF ADJUST. ON TAKEOFF, THE LEFT MAIN GEAR WOULD NOT RETRACT ALL THE WAY. CYCLED GEAR BUT DID NOT CLEAR PROBLEM. RETURNED TO FIELD. ADJUSTED ACTUATOR LENGTH PER MM 32-32-10
- [SDR SWIA200211259](https://openairdocs.org/sdr/SWIA200211259), Aug 30, 2002: FRAME. CRACKED. RT ENGINE FRAME NR 1 CRACKED AT OB TORSION MOUNT WEB. DISCOVERED DURING C-CHECK, C/W SB 120-54-0036 PART 11 FRAME ONE REPLACEMENT.
- [SDR SWIA200211142](https://openairdocs.org/sdr/SWIA200211142), Aug 14, 2002: COMPARATOR. MALFUNCTIONED. AT 70 PERCENT NP, CAPTAIN'S AHARS GOES BLANK, THEN RETURNS WITH HDG FLAG AND COMPASS CARD 30 DEGREES OFF THE HEADING. RETURNED OT SAN. REPLACED NR 1 AHC-85. PER
- [SDR SWIA200211009](https://openairdocs.org/sdr/SWIA200211009), Jul 1, 2002: LATCH. BROKEN. LEFT MAIN GEAR RED LIGHT REMAINED ON AFTER GEAR RETRACTION AND RECYCLE. RETURNED TO SAN. LEFT GEAR FORWARD INBOARD DOOR LATCH BROKEN. REPLACED LATCH AND CYCLED 
- [SDR SWIA200211008](https://openairdocs.org/sdr/SWIA200211008), Jul 1, 2002: WIRE. BROKEN. EXIT SIGN ON ROW 9 OVERHEAD BIN INOP. REPAIRED BROKEN WIRE FOR EMERGENCY EXIT SIGN AT ROW 9 OVERHEAD. OPS CHECK GOOD. NO OTHER DEFECTS NOTED.
- [SDR SWIA200210764](https://openairdocs.org/sdr/SWIA200210764), Mar 29, 2002: FILTER. DIRTY. GREEN HYDRAULIC FILTER LIGHT ILLUMINATED ON TAKEOFF. ALL SYSTEM INDICATORS NORMAL. RETURNED TO SFO. INSTALLED NEW HYDRAULIC RETURN FILTER ON GREEN SYSTEM. PRESS
- [SDR SWIA200210563](https://openairdocs.org/sdr/SWIA200210563), Jan 8, 2002: DEICE SYSTEM. MALFUNCTIONED. LEFT OUTBOARD WING DEICE BOOT INOP LIGHT IN ICING CONDITIONS. RETURNED TO SFO. RE-CHECKED INFLATION OF LEFT AND RIGHT OUTBOARD WING BOOTS. FOUND GOOD. SWAPPED L
- [SDR SWIA200210518](https://openairdocs.org/sdr/SWIA200210518), Jan 2, 2002: COMPUTER. FAULTY. ON TAKEOFF THE FIRST OFFICER'S EADI AND EHIS WENT OUT. SAME OCCURRED ON LANDING. REPLACED K0394, K0396 AND NR 2 DPU. RAN AIRCRAFT AND CYCLED AUXILLARY GENERATOR
- [SDR SWIA200110441](https://openairdocs.org/sdr/SWIA200110441), Dec 14, 2001: WIRE HARNESS. DEFECTIVE. RIGHT MAIN B-GREEN LANDING GEAR INDICATION REMAINS ILLUMINATED WITH GEAR UP. RETURNED TO SFO. REMOVED AND REPLACED UPLOCK HARNESS AND SENSOR. SWUNG GEAR SEVERAL
- [SDR SWIA200110408](https://openairdocs.org/sdr/SWIA200110408), Nov 30, 2001: COMPARATOR. FAILED. UPON APPLICATION OF TAKEOFF POWER CAPTAIN'S SIDE ATTITUDE INDICATOR BECAME INOPERATIVE SHOWING NO HORIZON INFORMATION AND DISPLAYING ATT FLAG. REPLACED CAPTAIN'
- [SDR SWIA200110281](https://openairdocs.org/sdr/SWIA200110281), Oct 29, 2001: RELAY. FAULTY. EFIS & ATT INDICATIONS WHEN POWER LEVER ADVANCED FOR TAKEOFF WITH RIGHT AUX GEN OFF. COULD NOT DUPLICATE DPU FAILURE. RAN ENGINE AND HAD SCREENS FLASH. DPU FAIL
- [SDR SWIA200110047](https://openairdocs.org/sdr/SWIA200110047), Jul 18, 2001: WARNING SYSTEM. ACTIVATED. ON TAKEOFF ROLL AURAL WARNING ''AUTO FEATHER''. SWITCH WAS ON AND TESTED ON TAXI CHECK.COULD NOT DUPLICATE DURING RUNUP. OPS CHECK GOOD.
- [SDR SWIA972611](https://openairdocs.org/sdr/SWIA972611), Jun 2, 2001: PROP HEAT. INTERMITTENT. CREW REPORTS LEFT PROP HEAT FAILS INTERMITTENTLY INFLIGHT. RETURNED TO PDX. MAINTENANCE FOUND THE PROP HAD BEEN STRUCK BY LIGHTNING. REMOVED AND REPLACED LEFT B
- [SDR SWIA972605](https://openairdocs.org/sdr/SWIA972605), May 18, 2001: SWITCH. OUT OF ADJ. FORWARD DOOR LIGHT ILLUMINATED DURING TAKEOFF ROLL. ABORTED AND RETURNED TO GATE. ADJUSTED BOTH FORWARD DOOR SWITCHES. OPS CHECKS GOOD.
- [SDR SWIA972226](https://openairdocs.org/sdr/SWIA972226), Dec 29, 2000: SENSOR. FAILED. TAKEOFF ''TRIM'' AURAL WARNING ON TAKEOFF ROLL WITH TRIM SET AT 32. ABORTED TAKEOFF. REMOVED AND REPLACED RIGHT ELEVATOR PROXIMITY TRIM SENSOR AND ADUSTED IAW E
- [SDR SWIA972161](https://openairdocs.org/sdr/SWIA972161), Dec 9, 2000: SEAL. LEAKING. FLIGHT ATTENDANT REPORTS LOUD RUSHING AIR AT SEAT 6A EXIT DOOR, UNABLE TO PRESSURIZE AIRCRAFT. RETURNED TO PDX.. CLEANED SEAL ON LEFT OVER WING EMERGENCY EXIT. 
- [SDR SWIA972105](https://openairdocs.org/sdr/SWIA972105), Nov 15, 2000: LIGHT. BROKEN. MAIN CABIN DOOR EMERGENCY EXIT LIGHT BROKE OFF. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-51-02. OPS CHECK GOOD.
- [SDR SWIA971962](https://openairdocs.org/sdr/SWIA971962), Aug 28, 2000: LATCH. FAILED. DOOR LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED SINGLE POINT REFUELING ACCESS DOOR CAMLOC IAW MM 28-00-00. OP
- [SDR SWIA971671](https://openairdocs.org/sdr/SWIA971671), Jan 24, 2000: LT PACK. FAILED. LEFT PACK FAILED ON CLIMB THROUGH 700 FOLLOWED BY SMOKE LIGHT ON MAP PANEL AND SMOKE AURAL WARNING. RETURNED TO SFO. REMOVED AND REPLACED LEFT AIR CYCLE MACHINE
- [SDR SWIA971496](https://openairdocs.org/sdr/SWIA971496), Jun 1, 1999: WINDSHIELD. FAILED. LEFT WINDSHIELD SHATTERED CLIMBING THROUGH 12000 FT. REMOVED AND REPLACED LEFT WINDSHIELD IAW MM 56-10-01. NO EVIDENCE OF ANY OTHER DAMAGE.
- [SDR SWIA971160](https://openairdocs.org/sdr/SWIA971160), Apr 3, 1998: SKIN. LIGHTNING STRIKE. AIRCRAFT TOOK A LIGHTNING STRIKE WHILE AIRBORNE. RETURNED TO RDM. RDM, INSPECTED AIRCRAFT PER MM 05-50-01 AND FOUND LIGHTNING STRIKE TO LEFT ELEVATOR. NO OTHER 
- [SDR GLBA97166](https://openairdocs.org/sdr/GLBA97166), Nov 5, 1997: HMU. MALFUNCTIONED. FSD - LEFT ENGINE DID NOT MAKE POWER, ABORTED TAKEOFF, RETURNED TO GATE. REPLACED HMU. (X)
- [SDR GLBA97103](https://openairdocs.org/sdr/GLBA97103), Jun 6, 1997: CONTROL CABLE. WORN. AILERON CONTROL CABLES ARE WORN. REMOVED AND REPLACED AILERON CONTROL CABLES. (X)
- [SDR GLBA97105](https://openairdocs.org/sdr/GLBA97105), May 29, 1997: CONTROL CABLE. WORN. AILERON CONTROL CABLES ARE WORN. REMOVED AND REPLACED AILERON CABLES. (X)
- [SDR GLBA96240](https://openairdocs.org/sdr/GLBA96240), Dec 17, 1996: SWITCH. DIRTY. FSD - AFTER LANDING, UNABLE TO STEER NOSEWHEEL BY TILLER OR RUDDER PEDALS. MAINTENANCE FOUND PROXIMITY SWITCHES STICKING. CLEANED AND OPERATES NORMALLY. (M)
- [SDR GLBA96097](https://openairdocs.org/sdr/GLBA96097), May 23, 1996: TORQUE SENSOR. FAILED. SPI - CREW REPORTED RT TORQUE GAUGE INOPERATIVE (READS ZERO). THEY RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED RT TORQUE SENSOR. OPS CHECK WAS GOOD. (X)
- [SDR 95ZZZX5890](https://openairdocs.org/sdr/95ZZZX5890), Aug 8, 1995: TQ SIG COND. FAILED. OSH - CREW ABORTED TAKEOFF WHEN RT ENGINE TORQUE GAUGE WENT INOP AND THE ENGINE AUTOFEATHERED. MAINTENANCE REPLACED THE TORQUE GAUGE (TORQUE SIGNAL CONDITIONER)
- [SDR 95ZZZX5891](https://openairdocs.org/sdr/95ZZZX5891), Jul 22, 1995: RETRACT MECH. MALFUNCTIONED. ORD - THE CREW ELECTED AN AIR TURN BACK AFTER THE FLAPS STUCK IN THE 15 DEGREE POSITION. AFTER AN UNEVENTFUL LANDING, MAINTENANCE CHECKED THE FAULT SYSTEM IN TH

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