# N269CA: 1992 Embraer EMB-120RT, registration cancelled 2022-09-19

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 19, 2022
- Status when cancelled: Valid registration
- Airframe: [Embraer EMB-120RT](https://openairdocs.org/model/embraer-emb-120rt) (registry code 3260202)
- 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: 120263
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: April 2, 1992
- Certificate issued: February 1, 2022
- Last registry action: February 1, 2022
- Mode S code: A2A09F
- Owner when cancelled: [Ameriflight LLC](https://openairdocs.org/faa-owner/AMERIFLIGHT%20LLC)
- Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas)
- Owner type: LLC
- Owner's area on the map: 32.9032° N, 97.0531° W: Placed by OpenAirDocs at the center of ZIP code 75261, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N269CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=269CA
- Page: https://openairdocs.org/deregistered/N269CA-2022-09-19

From the FAA registry file of November 7, 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-120RT: https://openairdocs.org/model/embraer-emb-120rt.md

## Service difficulty reports (72, newest 50)

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

- [SDR COMA0210028](https://openairdocs.org/sdr/COMA0210028), Jul 21, 2002: WIRE. FLIGHT 5080 TAKE OFF TRIM CONFIG WARNING DURING T/O.REPAIRED BROKEN WIRE AT ELEVATOR TAB PROX SENSOR.
- [SDR COMA0210020](https://openairdocs.org/sdr/COMA0210020), May 19, 2002: EEC. DEFECTIVE. FLIGHT 5023 DURING CLIMB OUT OF MCO THE #2 ENGINE POWER LEVER INPUT WAS IN EXCESS OF ONE INCH BEFORE IT TOOK EFFECT.REPLACED THE #2 EEC.
- [SDR COMA0210004](https://openairdocs.org/sdr/COMA0210004), Feb 9, 2002: LATCH. BROKEN. FLIGHT 5021 L/H MLG, INBD GEAR DOOR, DOES NOT CLOSE AFTER GEAR RETRACTION.REPLACED THE DOOR LATCH.
- [SDR COMA0210002](https://openairdocs.org/sdr/COMA0210002), Feb 4, 2002: HANDLE. DEFECTIVE. FLIGHT 5021 L/H MLG INDICATED INTRANSIT AFTER GEAR RETRACTION.REPLACED THE L/H INBD GEAR DOOR LATCH.
- [SDR COMA0210001](https://openairdocs.org/sdr/COMA0210001), Jan 11, 2002: DOOR LATCH. FLIGHT 5070 L/H MLG DID NOT RETRACT WHEN GEAR SELECTED UP.FOUND L/H MLG DOOR UNLATCH - SECURED DOOR LATCH, NO OTHER DEFECTS FOUND.
- [SDR COMA0110164](https://openairdocs.org/sdr/COMA0110164), Dec 21, 2001: SWITCH. OUT OF ADJ. FLIGHT 5028 - SERVICE DOOR WARNING LIGHT AFTER T/O.ADJUSTED THE FUEL SERVICE DOOR MICRO SWITCH.
- [SDR COMA0110160](https://openairdocs.org/sdr/COMA0110160), Dec 1, 2001: POWER LEVER. FLIGHT #5056. POWER LEVER SPLIT DURING T/O.POWER LEVER SPLIT WITHIN LIMITS. AIRCRAFT RETURNED TO SERVICE.
- [SDR COMA0110158](https://openairdocs.org/sdr/COMA0110158), Nov 25, 2001: RIB. CRACKED. DURING A SERVICE CHECK, MECHANIC NOTICED A CRACK LOCATED AT THE COCKPIT OVERHEAD CREW ASSIST HANDLE MOUNT ON LEFT SIDE.DAMAGE WAS REMOVED FROM THE RIB. A FILLER
- [SDR COMA0110157](https://openairdocs.org/sdr/COMA0110157), Nov 16, 2001: SENSOR. MALFUNCTIONED. FLIGHT 5049 - THREE KNOB POWER LEVER SPLIT DURING T/O. REPLACED THE RT ENGINE T2 SENSOR.
- [SDR COMA0110134](https://openairdocs.org/sdr/COMA0110134), Aug 6, 2001: COMPUTER. MALFUNCTIONED. DURING LANDING APPROACH INTO MCO WHEN FLAPS WERE SELECTED FROM 25 TO 45 DEGREES AUDIBLE FLAP CAUTION ACTIVATED, CREW DECLARED AN EMERGENCY AND LANDED SAFELY. IN
- [SDR COMA0110133](https://openairdocs.org/sdr/COMA0110133), Aug 6, 2001: FLAP TRACK. DURING LANDING APPROACH INTO EYW WHEN FLAPS WERE SELECTED FROM 25 TO 45 DEGREES, FLAP DISAGREE CAUTION ACTIVATED.REPLACED THE FLAP ROLLERS FOR THE LEFT INBOARD 
- [SDR COMA0110043](https://openairdocs.org/sdr/COMA0110043), Mar 10, 2001: FAN. FAILED. LAVATORY SMOKE DETECTOR ACTIVATED, SMOKE SMELL IN COCKPIT. REPLACED THE LEFT HAND GROUND COOLING FAN.
- [SDR COMA0110038](https://openairdocs.org/sdr/COMA0110038), Mar 1, 2001: LANDING GEAR. MALFUNCTIONED. LANDING GEAR SLOW TO EXTEND, AND INDICATED UNSAFE. RECYCLED GEAR WITH SAME RESULTS. COULD NOT DUPLICATE. LANDING GEAR RETRACTION CHECKS WERE NORMAL.
- [SDR COMA0110037](https://openairdocs.org/sdr/COMA0110037), Feb 23, 2001: SHEAR TIE. CRACKED. DURING A 400 FLIGHT CYCLE CHECK, A CRACKED RIVET HEAD WAS DISCOVERED ON THE RIGHT SIDE OF AIRCRAFT FUSELAGE ALONG FRAME 9. UPON FURTHER INVESTIGATION, THE SKIN 
- [SDR COMA0110036](https://openairdocs.org/sdr/COMA0110036), Feb 23, 2001: SHEAR TIE. CRACKED. DURING A 400 FLIGHT CYCLE CHECK, A CRACKED RIVET HEAD WAS DISCOVERED ON THE RIGHT SIDE OF AIRCRAFT FUSELAGE ALONG FRAME 9. UPON FURTHER INVESTIGATION, THE SKIN 
- [SDR COMA0110035](https://openairdocs.org/sdr/COMA0110035), Feb 19, 2001: SPRING. BROKEN. ON POST-FLIGHT INSPECTION, CREW NOTICED OIL LEAKING FROM LEFT PROPELLER. MAINTENANCE DETERMINED SOURCE TO BE THE NR 1 PROP BLADE. THE BLADE WAS REMOVED, AND THE
- [SDR COMA0110034](https://openairdocs.org/sdr/COMA0110034), Feb 19, 2001: SPRING. BROKEN. ON POST-FLIGHT INSPECTION CREW NOTICED OIL LEAKING FROM LEFT PROPELLER. MAINTENANCE DETERMINED SOURCE TO BE THE NR 1 PROP BLADE. THE BLADE WAS REMOVED, AND THE 
- [SDR COMA0010366](https://openairdocs.org/sdr/COMA0010366), Sep 21, 2000: SMOKE DETECTOR. MALFUNCTIONED. THE LAVATORY SMOKE DETECTOR ACTIVATED DURING TAXI, AIRCRAFT RETURNED TO THE GATE. DEFERRED THE LAVATORY SMOKE DETECTOR.
- [SDR COMA0010161](https://openairdocs.org/sdr/COMA0010161), Jun 7, 2000: BATTERY. DISCHARGED. OVERHEAD EMERGENCY LIGHT AT ROW 6 IS INOPERABLE. REPLACED BATTERY PACK.
- [SDR COMA0010065](https://openairdocs.org/sdr/COMA0010065), May 11, 2000: PCU. OUT OF RIG. RIGHT PROPELLER NP INDICATED 97 PERCENT MAX. FOUND TRANSFER TUBE TO PCU RIGGING DISCREPANCY. ADJUSTED RIGGING AND ACFT. RETURNED TO SERVICE.
- [SDR COMA0010035](https://openairdocs.org/sdr/COMA0010035), Mar 1, 2000: SENSOR. MALFUNCTIONED. NLG INTRANSIT LIGHT REMAINED ON AFTER GEAR RETRACTED. REPLACED THE NLG DOWNLOCK SENSOR.
- [SDR COMA0010027](https://openairdocs.org/sdr/COMA0010027), Feb 20, 2000: SIGN. INOPERATIVE. CABIN DOOR EMERGENCY LIGHT WAS INOPERABLE. REPLACED LIGHT ASSY.
- [SDR COMA0010021](https://openairdocs.org/sdr/COMA0010021), Feb 2, 2000: SIGN. BROKEN. EXIT SIGN AT ROW 8 WAS BROKEN. REPLACED EXIT SIGN.
- [SDR COMA0010015](https://openairdocs.org/sdr/COMA0010015), Jan 27, 2000: INDICATOR. MALFUNCTIONED. RIGHT HAND HYDRAULIC RESERVOIR, LOW LEVEL, WARNING. REPLACED THE QUANTITY GAUGE.
- [SDR COMA0010009](https://openairdocs.org/sdr/COMA0010009), Jan 12, 2000: BATTERY. DISCHARGED. AFT SECTION CABIN EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.
- [SDR COMA9910191](https://openairdocs.org/sdr/COMA9910191), Dec 15, 1999: INDICATOR. ERRATIC. RT ENGINE T6 INDICATOR FLUCTUATED FULL SCALE. REPLACED T6 INDICATOR GAUGE.
- [SDR COMA9910183](https://openairdocs.org/sdr/COMA9910183), Dec 11, 1999: SENSOR. OUT OF ADJUST. TRIM WARNING DURING TAKEOFF. ADJUSTED THE ELEVATOR TRIM PROXIMITY SENSORS.
- [SDR COMA9910178](https://openairdocs.org/sdr/COMA9910178), Nov 13, 1999: WIRE. DAMAGED. TAKEOFF TRIM AURAL WARNING. REPAIRED DAMAGED WIRE SPLICE AT THE ELEVATOR TRIM PROXIMITY SENSORS.
- [SDR COMA9910152](https://openairdocs.org/sdr/COMA9910152), Sep 21, 1999: SENSOR. FAIELD. AFTER TAKEOFF AND GEAR RETRACTION, NOSE GEAR INDICATION WAS RED B, LIGHTS REMAINED ON AFTER CYCLING GEAR. REMOVED AND REPLACED NOSE LANDING GEAR PROX SENSOR FOR
- [SDR COMA9910136](https://openairdocs.org/sdr/COMA9910136), Aug 18, 1999: FUEL HEATER. LEAKING. FUEL LEAKING FROM LEFT ENGINE. REPLACED THE FUEL HEATER.
- [SDR COMA9910075](https://openairdocs.org/sdr/COMA9910075), May 10, 1999: CHECK VALVE. FAILED. SMOKE FLOWED HEAVILY FROM COCKPIT GASPERS DURING DESCENT THRU 14,000 FT. TORQUE REDUCED TO 20 PERCENT. REMOVED AND REPLACED LEFT ENGINE OIL PRESSURE CHECK VALVE
- [SDR COMA9910074](https://openairdocs.org/sdr/COMA9910074), May 10, 1999: OUTFLOW VALVE. FAILED. AUTO PRESSURIZATION INOPERATIVE. REMOVED AND REPLACED PRESS OUTFLOW VALVE.
- [SDR COMA9910070](https://openairdocs.org/sdr/COMA9910070), May 2, 1999: VALVE. MALFUNCTIONED. SMOKE IN COCKPIT COMING FROM AIRCRAFT VENTS. REPLACED THE LEFT ENGINE 2.5 SWITCHING VALVE.
- [SDR COMA991066](https://openairdocs.org/sdr/COMA991066), Apr 22, 1999: AIR DIST. ODOR. SMOKE IN COCKPIT AND CABIN, FOR APPROXIMATELY 20 SECONDS DURING LANDING APPROACH. INSPECTED AIRCRAFT COOLING AND RECIRCULATION SYSTEM. NO DEFECTS FOUND.
- [SDR COMA9910023](https://openairdocs.org/sdr/COMA9910023), Jan 23, 1999: ACTUATOR. FAILED. WHEN SELECTING FLAPS TO 45 DEGREES, THE FLAP DISAGREE CAUTION ACTIVATED. REPLACED THE EIGHT OUTBOARD FLAP ACTUATOR.
- [SDR COMA9810271](https://openairdocs.org/sdr/COMA9810271), Nov 28, 1998: WARNING. ACTIVATED. FUEL WARNING ON MAP DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE.
- [SDR COMA9810216](https://openairdocs.org/sdr/COMA9810216), Sep 17, 1998: SOCKET. SHORTED. NAVIGATION LIGHTS CIRCUIT BREAKER TRIPPED TWICE. REPLACED DEFECTIVE LIGHT SOCKET.
- [SDR COMA9810129](https://openairdocs.org/sdr/COMA9810129), May 28, 1998: AHRS. FAILED. PILOTS AHRS FAILED. REPLACED NR 1 AHRS.
- [SDR COMA9810116](https://openairdocs.org/sdr/COMA9810116), May 11, 1998: BOX CONTROL. MALFUNCTIONED. WHEN LANDING GEAR EXTENDED BOTH GREEN AND RED INDICATOR LIGHTS ILLUMINATED, AND ANTI-SKID FAIL INDICATION. COULD NOT DUPLICATE DISCREPANCY. REPLACED LANDING GEA
- [SDR COMA9810067](https://openairdocs.org/sdr/COMA9810067), Mar 12, 1998: RELAY BOX. FAILED. TAKEOFF AURAL WARNING SOUNDED AFTER TAKEOFF. REPLACED THE LANDING GEAR RELAY BOX.
- [SDR COMA9810064](https://openairdocs.org/sdr/COMA9810064), Mar 11, 1998: LIGHT ASSY. OVERHEATED. SMOKE IN CABIN DURING TAXI OPERATIONS. REPLACED OVERHEATED FLUORESCENT LIGHT ASSY AT SEAT 4B.
- [SDR COMA9810048](https://openairdocs.org/sdr/COMA9810048), Feb 22, 1998: RELAY BOX. MALFUNCTION. UNABLE TO RAISE LANDING GEAR AFTER TAKEOFF. BOTH INTRANSIT RED AND GREEN SAFE INDICATORS WERE ON. REPLACED THE LANDING GEAR RELAY BOX.
- [SDR COMA081341](https://openairdocs.org/sdr/COMA081341), Aug 2, 1997: BATTERY. DISCHARGED. NUMEROUS EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY BATTERY.
- [SDR COMA9710321](https://openairdocs.org/sdr/COMA9710321), Jun 27, 1997: INDICATION. MALFUNCTIONED. WHEN LANDING GEAR RETRACTED, THE B-SYSTEM INTRANSIT LIGHTS REMAINED ON. COULD NOT DUPLICATE DISCREPANCY. LANDING GEAR EXTENSION AND RETRACTION CHECKS NORMAL.
- [SDR COMA9710260](https://openairdocs.org/sdr/COMA9710260), May 8, 1997: SKIN. DENTED. FUSELAGE RT SKIN WAS PREVIOUSLY FOUND TO HAVE A LARGE DENT BETWEEN FRAMES 14 AND 15, AND STRINGERS 12R AND 13R. THE DENT WAS DEFERRED PER SRM LIMITATIONS. AT TH
- [SDR COMA9710259](https://openairdocs.org/sdr/COMA9710259), May 8, 1997: OMEGA BEAM. CORRODED. ON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT FWD CENTER OMEGA BEAM WAS FOUND TO HAVE A SMALL AREA OF CORROSION THROUGH THE PART. THE OMEGA BEAM WAS REPAIRED
- [SDR COMA9710258](https://openairdocs.org/sdr/COMA9710258), May 8, 1997: ANGLE. CORRODED. ON 4C TASK 5320-152-01I, THE SUPPORT ANGLE FOR THE AFT EMERGENCY EXIT LOWER GUIDE PIN RECEPTACLES, WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.
- [SDR COMA9710257](https://openairdocs.org/sdr/COMA9710257), May 8, 1997: ANGLE. CORRODED. ON 2C TASK 5310-131-01I, THE FWD FLOOR SUPPORT ANGLE UNDER THE PAX DOOR ENTRANCE THRESHOLD WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.
- [SDR COMA9710256](https://openairdocs.org/sdr/COMA9710256), May 8, 1997: SILL. CORRODED. ON 4C TASK 5330-162-01I, THE RT FWD FLOOR SUPPORT SILL IN THE CARGO COMPARTMENT WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.
- [SDR COMA9710255](https://openairdocs.org/sdr/COMA9710255), May 8, 1997: CROSSBEAM. CORRODED. ON 4C TASK 5320-142-01I, THE RT CABIN FLOORBEAM CROSSBEAM AT FRAME 36 WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.

All 72: https://openairdocs.org/deregistered/N269CA-2022-09-19/reports.md

## FAA accident and incident reports (1)

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.

- [Incident 19930629044339I](https://openairdocs.org/incident/19930629044339I), Jun 29, 1993: Emb EMB120RT (N269CA), Washington, DC, Minor damage. Left wing tip collided with jetway while departing from gate.

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