# N1110J: 1988 Embraer EMB-120FC, registration cancelled 2024-06-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 25, 2024
- Exported to: Malawi
- Status when cancelled: Sale reported
- Airframe: [Embraer EMB-120FC](https://openairdocs.org/model/embraer-emb-120fc) (registry code 3260204)
- 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: 120.110
- Year built: 1988
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: February 10, 2005
- Last registry action: June 24, 2024
- Mode S code: A0324B
- Location: [Okc, OK](https://openairdocs.org/faa-place/OK/Okc)
- Owner type: Individual
- Owner's area on the map: 35.4676° N, 97.5164° W: Placed by OpenAirDocs: center of Oklahoma City, OK, within about 14 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N1110J
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1110J
- Page: https://openairdocs.org/deregistered/N1110J-2024-06-25

From the FAA registry file of November 5, 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-120FC: https://openairdocs.org/model/embraer-emb-120fc.md

## Service difficulty reports (54, newest 50)

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

- [SDR JIKA20230427401](https://openairdocs.org/sdr/JIKA20230427401), Apr 24, 2023: UNKNOWN. UNKNOWN. THE FLIGHT CREW REPORTED SMOKE IN THE COCKPIT DURING DESCENT INTO KMFR. THE AIRCRAFT LANDED IN KMFR WITHOUT INCIDENT. EMERGENCY VEHICLES WERE DISPATCHED. PDX MA
- [SDR FXGA201212260001](https://openairdocs.org/sdr/FXGA201212260001), Dec 18, 2012: CONTROL UNIT. LEAKING. NR 2 OIL PRESSURE WAS FLUCTUATING BETWEEN 55-40 PSI. NR 2 OIL PRESSURE AURAL WARNING ENGINE "OIL" SHUTDOWN. REPLACED NR 2 PCU IAW MM 61-21-00. GROUND OPS AND LE
- [SDR FXGA20121030001](https://openairdocs.org/sdr/FXGA20121030001), Oct 26, 2012: ATTACH ANGLE. CRACKED. DURING INSPECTION, FOUND RT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED AT THE AFT PRESSURE BULKHEAD.
- [SDR FXGA2012018002](https://openairdocs.org/sdr/FXGA2012018002), Dec 7, 2011: SKIN. CRACKED. DURING "A" CHECK DISCOVERED CRACKS ON LOWER WING SKIN AROUND ACCESS PANELS, 143FB AT WING STATION Y-657, 143BB LT WING STATION Y-657, AND 521AB LT WING STATION 
- [SDR FXGA2012018001](https://openairdocs.org/sdr/FXGA2012018001), Dec 7, 2011: SUPPORT. CORRODED. DURING "A" CHECK, DISCOVERED A CORRODED SUPPORT OF THE MAIN CABIN DOOR WHICH REQUIRED THE SUPPORT REPLACEMENT.
- [SDR FXGA20111006001](https://openairdocs.org/sdr/FXGA20111006001), Aug 31, 2011: ACTUATOR. MALFUNCTIONED. AILERON JAMMED AT TOP OF CLIMB. PULLED AILERON DISCONNECT. RIGHT AILERON THEN APPEARED TO MOVE FREELY. INSPECTED AIRCRAFT AND DETERMINED AILERON TRIM TAB ACTUAT
- [SDR FXGAN1110J8292011](https://openairdocs.org/sdr/FXGAN1110J8292011), Aug 29, 2011: RIVET. MISSING. FOUND LOOSE AND MISSING RIVET ON LOWER WING SKIN STA Y4534 AFT OF STRINGER 10. REPAIRED IAW EMB-120 SRM 51-40-03B.
- [SDR FXGA20110413001](https://openairdocs.org/sdr/FXGA20110413001), Apr 13, 2011: STARTER GEN. FAILED. EMERGENCY BUSS OFF LIGHT ILLUMINATED. REPLACED NR (2) ENGINE STARTER GENERATOR AND RESET CB0471, EMER 1 BUS CIRCUIT BREAKER. OPS CHECKED ALL BUSSES AND TRANSFER
- [SDR FXGA110J](https://openairdocs.org/sdr/FXGA110J), Nov 3, 2010: LATCH. BROKEN. DISCOVERED UPPER RT LATCHING MECHANISM ON FWD DOOR BROKEN, REPLACED BACKSTOP/STOPPER (ASSY PN 120-25452-006) IAW AMM 52-11-00.
- [SDR FXGAN1110J](https://openairdocs.org/sdr/FXGAN1110J), Oct 14, 2010: STRUCTURE. DAMAGED. A DEEP NICK WAS FOUND ON THE MAIN DOOR 1.5" AFT OF FRAME 15, APPROX 12.5" ABOVE DOOR CUTOUT. REPAIRED DAMAGE IAW EO 1051 AND SRM 52-10-01.
- [SDR FXG2007F00001](https://openairdocs.org/sdr/FXG2007F00001), Feb 1, 2007: BUSHING. TIGHT. ON GEAR RETRACTION RED GEAR LIGHTS A AND B REMAINED ON AND LT MAIN GEAR DOOR WOULD NOT SHUT. MAINTENANCE INVESTIGATION REVELED THAT THE PN 19659 BUSHINGS IN BOT
- [SDR SWIA200210811](https://openairdocs.org/sdr/SWIA200210811), Apr 16, 2002: ACTUATOR. FAILED. RIGHT OUTBOARD FLAP CAME DOWN 5 DEGREES SITTING ON RAMP WITH ENGINES OFF AND APU RUNNING. RAN QRH AND FLAP FAILED TO RETRACT. REPLACED RIGHT OUTBOARD FLAP ACTUA
- [SDR SWIA200210784](https://openairdocs.org/sdr/SWIA200210784), Apr 13, 2002: ACTUATOR. LEAKING. TEN MINUTES AFTER TAKEOFF, THE RIGHT SIDE HYDRAULIC RESERVOIR LOW LEVEL LIGHT ILLUMINATED, FOLLOWED SHORTLY BY THE RIGHT SIDE MAIN PUMP LOW PRESSURE LIGHT. RETU
- [SDR SWIA200210533](https://openairdocs.org/sdr/SWIA200210533), Jan 7, 2002: SPRING. OUT OF POSITION. ON DOOR OPENING 3RD AND 4TH STAIRS FROM THE TOP DID NOT EXTEND. REPOSITIONED BOTTOM STEP SPRING AND REPLACED STEP SPRING ON 3RD STEP DOWN FROM TOP. OPS CHECK GO
- [SDR SWIA200110433](https://openairdocs.org/sdr/SWIA200110433), Dec 11, 2001: CONNECTOR. CORRODED. VERTICAL FIN LEADING EDGE DEICE BOOT FAILED INFLIGHT WITH BOTH TIMERS 1 AND 2. FOUND GREEN CORROSION AROUND PIN-B IN CONNECTOR AT S0213 (VERTICAL FIN PRESSURE S
- [SDR SWIA200110121](https://openairdocs.org/sdr/SWIA200110121), Aug 20, 2001: SELECTOR SWITCH. MALFUNCTIONED. FLAP CONTROL FAULT DURING FLAP RETRACTION AND AGAIN WHEN SETTING FLAPS TO 25 DEGREES FOR LANDING. ALL LIGHT BARS FLASHING. QRH RESET PROCEDURE WORKED BOTH TIMES
- [SDR SWIA200110106](https://openairdocs.org/sdr/SWIA200110106), Aug 18, 2001: ACTUATOR. ERRATIC. RT NACELLE FLAP POT IS ERRATIC.REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR. OPS CHECKS GOOD IAW MM 27-50-08.
- [SDR SWIA972643](https://openairdocs.org/sdr/SWIA972643), Jun 18, 2001: INDICATOR. FAILED. ''HIGH SPEED'' AURAL WARNING/TRIPLE CHIME SOUNDED ON TAKEOFF ROLL - IAS APPROXIMATELY 40 KNOTS. TAKEOFF ABORTED. REMOVED AND REPLACED PILOT'S AIRSPEED INDICATOR
- [SDR SWIA972621](https://openairdocs.org/sdr/SWIA972621), Jun 6, 2001: ACTUATOR. MALFUNCTIONED. ON FINAL AFTER SELECTING FLAPS 25, FLAP ASYMMETRY WARNING, FOUR SEGMENTS SHOWING ON RIGHT INBOARD AND ONE SEGMENT ON LEFT INBOARD FLAP INDICATOR. AIRCRAFT WAS C
- [SDR SWIA972232](https://openairdocs.org/sdr/SWIA972232), Dec 28, 2000: DISPLAY. FAILED. ON TAKEOFF ROLL CAPTAINS VSI/TCAS DISPLAY WENT BLANK AND REMAINED BLANK THROUGHOUT ABORTED TAKEOFF. STARTED WORKING DURING TAXI BACK. CHECKED SECURITY OF DISPLA
- [SDR SWIA972043](https://openairdocs.org/sdr/SWIA972043), Oct 21, 2000: CONTROL BOX. FAILED. AFTER TAKEOFF, THE LANDING GEAR WAS SELECTED UP, THE A AND B DOWN PROXIMITY LIGHTS REMAINED LIT, AS WELL AS ALL A AND B DISAGREEMENT LIGHT. AFTER TWO MINUTES, G
- [SDR SWIA971858](https://openairdocs.org/sdr/SWIA971858), Jul 4, 2000: LIGHT. INOPERATIVE. EMERGENCY LIGHTS FRONT LEFT FLOOR AND MIDDLE CEILING AND SIDE INOP. REPLACED FORWARD EMERGENCY LIGHT BATTERY, OPS CHECKS GOOD. S/N: 263, S/N OFF: 12741896.
- [SDR SWIA971857](https://openairdocs.org/sdr/SWIA971857), Jul 4, 2000: LIGHT. INOPERATIVE. EMERGENCY LIGHTING INOP FORWARD FLOOR AND LEFT WALL EXIT SIGN. AFTER PROPER CHARGING, OPS CHECK OF EMERGENCY LIGHTING SYSTEM PER MM 335000 CHECKS GOOD.
- [SDR SWIA971852](https://openairdocs.org/sdr/SWIA971852), Jun 28, 2000: CONTROLLER. MALFUNCTIONED. ON DESCENT, FLAP AND ADVANCED STALL WARNING LIGHTS ILLUMINATED ALONG WITH CONTROL FAULT LIGHT AND SECOND ROW OUTBOARD FLAP LIGHTS ON FLAP PANEL. FOLLOWED QRH AN
- [SDR SWIA971851](https://openairdocs.org/sdr/SWIA971851), Jun 28, 2000: CONTROLLER. MALFUNCTIONED. ON DESCENT, FLAP AND ADVANCED STALL WARNING LIGHTS ILLUMINATED ALONG WITH CONTROL FAULT LIGHT AND SECOND ROW OUTBOARD FLAP LIGHTS ON FLAP PANEL. FOLLOWED QRH AN
- [SDR SWIA971692](https://openairdocs.org/sdr/SWIA971692), Feb 13, 2000: WARNING LIGHT. ILLUMINATED. LEADING EDGE VERTICAL FIN LIGHT ILLUMINATED ON ICE PROTECTION PANEL. RETURNED TO PDX. INSTALLED SERVICEABLE VERTICAL FIN DEICE BOOT IAW 301000, OPS CHECK GOOD. 
- [SDR SWIA971639](https://openairdocs.org/sdr/SWIA971639), Dec 29, 1999: UPLOCK HARNESS. MALFUNCTIONED. AFTER TAKEOFF, SELECTED LANDING GEAR UP, ALL LIGHTS ON GEAR CONTROL PANEL ILLUMINATED. NO GEAR DOOR NOISE OR GEAR RETRACTION HEARD CYCLED LANDING GEAR HANDLE WI
- [SDR SWIA971543](https://openairdocs.org/sdr/SWIA971543), Aug 8, 1999: ALTIMETER. FAILED. CAPTAINS ALTIMETER FAILED CLIMBING THROUGH 13,100. OFF FLAG DISPLAYED. RETURNED TO SEA. REMOVED AND REPLACED CAPTAIN'S ALTIMETER IAW MM 34-12-03. CHECKS GOOD.
- [SDR COMA9710436](https://openairdocs.org/sdr/COMA9710436), Oct 21, 1997: DISAGREE WARNING. ACTIVATED. FLAP DISAGREEMENT WARNING WHEN FLAP SELECTED FOR LANDING APPROACH. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK OF FLAP SYSTEM IAW EMB M/M WAS SATISFACTOR
- [SDR COMA9710422](https://openairdocs.org/sdr/COMA9710422), Oct 3, 1997: TRANSMITTER. MALFUNCTION. GREEN HYDRAULIC SYSTEM LOW LEVEL WARNING INDICATION INFLIGHT. REPLACED THE RESERVOIR QUANTITY TRANSDUCER.
- [SDR COMA9710343](https://openairdocs.org/sdr/COMA9710343), Aug 1, 1997: FLAP TRACKS. DIRTY. WHEN FLAPS SELECTED TO 15 DEGREES FLAP DISAGREEMENT WARNING ON. COULD NOT DUPLICATE DISCREPANCY. CLEANED FLAP TRACKS, OPERATION OF FLAPS NORMAL.
- [SDR COMA9710331](https://openairdocs.org/sdr/COMA9710331), Jul 12, 1997: BATTERY. DISCHARGED. EMERGENCY FLOOR PATH LIGHTING, ROWS 1 THRU 5, IS INOP. REPLACED EMERGENCY LIGHT BATTERY.
- [SDR COMA9710131](https://openairdocs.org/sdr/COMA9710131), Feb 11, 1997: SERVO. BINDING. AILERONS BINDING AND NOISY WHEN MOVED LT OR RT. REPLACED THE AUTO PILOT SERVO. PART TOTAL CYCLES, 20,917.
- [SDR COMA9610395](https://openairdocs.org/sdr/COMA9610395), Dec 11, 1996: BATTERY. DISCHARGED. EMERGENCY EXIT LIGHT AT ROW 5C IS INOP. REPLACED THE EMERGENCY BATTERY PACK.
- [SDR COMA9610310](https://openairdocs.org/sdr/COMA9610310), Oct 25, 1996: AUTO PILOT. MALFUNCTIONED. DURING AUTO PILOT TEST THE ELEVATOR TRIM RUNS WILD. AUTO PILOT SYSTEM PLACED ON DEFERRED MAINTENANCE LIST.
- [SDR COMA9610292](https://openairdocs.org/sdr/COMA9610292), Sep 30, 1996: CIRCUIT BREAKER. FAILED. NR 2 FLIGHT IDLE STOP CB POPPED. REPLACED NR 2 FLIGHT IDLE STOP CIRCUIT BREAKER.
- [SDR COMA9610249](https://openairdocs.org/sdr/COMA9610249), Aug 20, 1996: VALVE. LOW PRESSURE. BOTH LT AND RT COOLING PACKS FAIL TO COOL PROPERLY. REPLACED THE LT AND RT PRESSURE REGULATING VALVES.
- [SDR COMA9610227](https://openairdocs.org/sdr/COMA9610227), Jul 19, 1996: CONTROL BOX. MALFUNCTION. ANTI-SKID LIGHT ILLUMINATED WHEN LANDING GEAR RETRACTED. REPLACED THE ANTI-SKID CONTROL BOX.
- [SDR COMA9610180](https://openairdocs.org/sdr/COMA9610180), Jun 14, 1996: COMPUTER. DEFECTIVE. COPILOTS STICK SHAKER ACTIVATED DURING TAKEOFF ROLL. REPLACED THE STALL WARNING COMPUTER.
- [SDR COMA9610172](https://openairdocs.org/sdr/COMA9610172), Jun 7, 1996: SOLENOID. SHORTED. FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER TRIPPED, WOULD NOT RESET. REPLACED THE FLIGHT IDLE SOLENOID.
- [SDR COMA9610149](https://openairdocs.org/sdr/COMA9610149), May 18, 1996: WINDOW. AIR LEAK. CABIN WILL NOT HOLD PRESSURIZATION. ADJUSTED AND RESEALED PILOT'S DIRECT VISION WINDOW.
- [SDR COMA9610125](https://openairdocs.org/sdr/COMA9610125), Apr 13, 1996: ACTUATOR. MALFUNCTION. FLAP DISAGREEMENT AND CONTROL FAULT WARNINGS. REPLACED THE RT OUTBD FLAP ACTUATOR.
- [SDR COMA9610123](https://openairdocs.org/sdr/COMA9610123), Mar 31, 1996: FCU. MALFUNCTIONED. FLAP CONTROL FAULT WARNING. REPLACED THE FLAP CONTROL UNIT.
- [SDR COMA9610097](https://openairdocs.org/sdr/COMA9610097), Mar 8, 1996: LATCH ASSY. BROKEN. RIGHT MLG DOOR FOUND IN THE OPEN POSITION DURING PREFLIGHT. REPLACED BROKEN DOOR LATCH ASSY.
- [SDR COMA9610059](https://openairdocs.org/sdr/COMA9610059), Feb 3, 1996: ENGINE. FAILED. DURING FLIGHT, RT ENGINE FAILED. REPLACED THE RT ENGINE.
- [SDR COMA9610023](https://openairdocs.org/sdr/COMA9610023), Jan 12, 1996: CIRCUIT BREAKERS. TRIPPED. THE LT AND RT POWER LEVER FLIGHT IDLE STOP SOLENOIDS CIRCUIT BREAKERS WERE TRIPPED. RESET CIRCUIT BREAKERS AND SYSTEM TEST NORMAL.
- [SDR COMA9610019](https://openairdocs.org/sdr/COMA9610019), Jan 10, 1996: AOA. DEFECTIVE. STICK SHAKER CAME ON DURING TAKEOFF ROLL. REPLACED THE LT ANGLE OF ATTACK VANE.
- [SDR COMA9610002](https://openairdocs.org/sdr/COMA9610002), Jan 4, 1996: CONTROL BOX. DEFECTIVE. FLAP ASYMMETRY WARNING DURING LANDING ROLL. REPLACED THE FLAP CONTROL BOX.
- [SDR COMA9512030](https://openairdocs.org/sdr/COMA9512030), Dec 18, 1995: ANGLE. CRACKED. RT WING ROOT FAIRING UPPER ATTACH ANGLE HAS NUMEROUS BROKEN RIVET HEADS AND POSSIBLE CRACKS. REPAIRED FAIRING SUPPORT ANGLE.
- [SDR COMA9511984](https://openairdocs.org/sdr/COMA9511984), Oct 11, 1995: SOLENOID. FAILED. THE RIGHT POWER LEVER FLIGHT IDLE STOP SOLENOID IS INOPERATIVE. REPLACED THE FLIGHT IDLE STOP SOLENOID.

All 54: https://openairdocs.org/deregistered/N1110J-2024-06-25/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA12CA042](https://openairdocs.org/ntsb/DCA12CA042), Feb 16, 2012: Embraer EMB120 (N1110J), Iliamna, AK, substantial damage. Probable cause: the maintenance personnel's failure to install the cotter pins that secured castellated nuts on the left elevator vertical hinge bolts, which resulted in the left elevator partially detaching in…

## FAA accident and incident reports (3)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20120216002539A](https://openairdocs.org/incident/20120216002539A), Feb 16, 2012: Embraer EMB-120FC (N1110J), Iliamna, AK, Substantial damage. On February 16, 2012, everts flight 1291, an EMB-120, N1110J, on an IFR flight plan from anchorage, AK (anc) (panc) to Iliamna, AK (ili) (pail), experienced…
- [Incident 20110831021809I](https://openairdocs.org/incident/20110831021809I), Aug 31, 2011: Embraer EMB-120FC (N1110J), Anchorage, AK, No damage. Ptrs # 201105603NTSB# anc 11 na 090JAMMED aileron at top of climb. Complied with qrh procedure, declared emergency and landing was uneventful. Maintenance…
- [Incident 20050809018149I](https://openairdocs.org/incident/20050809018149I), Aug 9, 2005: Emb EMB120FC (N1110J), Anchorage, AK, Minor damage. (-23) Right hand hydraulic access door, (pn 120-07993-018) departed aircraft in flight causing damage to the ri/h inboard flap, nacelle flap, and shroud. Loss…

## Other aircraft with N1110J

- [Cancelled 1988-04-11](https://openairdocs.org/deregistered/N1110J-1988-04-11): Bell 47G-3B-1, S/N 2906, built 1963. Exported to Mexico. Owner: [Mcdonald James](https://openairdocs.org/faa-owner/MCDONALD%20JAMES), [Phoeniz, AZ](https://openairdocs.org/faa-place/AZ/Phoeniz)

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