# N241CA: 1990 Embraer EMB-120RT, registration cancelled 2006-11-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 16, 2006
- Status when cancelled: Triennial form not returned
- 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: 120.211
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: March 9, 2000
- Certificate issued: February 20, 2001
- Last registry action: February 17, 2004
- Mode S code: A233E9
- Owner when cancelled: [Boeing Capital Corp](https://openairdocs.org/faa-owner/BOEING%20CAPITAL%20CORP)
- Location: [Long Beach, CA](https://openairdocs.org/faa-place/CA/Long%20Beach)
- Owner type: Corporation
- Owner's area on the map: 33.8089° N, 118.1785° W: Placed by OpenAirDocs at the center of ZIP code 90806, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N241CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=241CA
- Page: https://openairdocs.org/deregistered/N241CA-2006-11-16

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-120RT: https://openairdocs.org/model/embraer-emb-120rt.md

## Service difficulty reports (35)

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

- [SDR COMA9810251](https://openairdocs.org/sdr/COMA9810251), Nov 5, 1998: TORQUE IND. FAILED. RIGHT HAND ENGINE TORQUE INDICATOR FAILED. REPLACED TORQUE INDICATOR.
- [SDR COMA9810240](https://openairdocs.org/sdr/COMA9810240), Oct 20, 1998: LINE. LEAKING. WHILE RUNNING NR 2 ENGINE, IT STARTED LEAKING FUEL. REPLACED RIGHT VENT VALVE MOTIVE FLOW LINE.
- [SDR COMA9810121](https://openairdocs.org/sdr/COMA9810121), May 14, 1998: SOLENOID. SHORTED. FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER TRIPPED. REPLACED SOLENOID.
- [SDR COMA9810112](https://openairdocs.org/sdr/COMA9810112), Apr 20, 1998: WHEEL. CRACKED. MAIN WHEEL ASSEMBLY WAS REMOVED FROM AIRCRAFT BY MECHANIC DUE TO LOW PRESSURE. TIRE SHOP FOUND INBOARD (P/N 300-604-1) WAS MISSING A SECTION OF WHEEL FLANGE APP
- [SDR COMA9810107](https://openairdocs.org/sdr/COMA9810107), Apr 20, 1998: WHEEL. CRACKED. MAIN WHEEL ASSEMBLY WAS REMOVED FROM AIRCRAFT BY MECHANIC DUE TO LOW PRESSURE. TIRE SHOP FOUND INBOARD (P/N 300-604-1) WAS MISSING A SECTION OF WHEEL FLANGE APP
- [SDR COMA9810075](https://openairdocs.org/sdr/COMA9810075), Mar 24, 1998: CONNECTOR. LOOSE. EMERGENCY LIGHT AT ROW 2 INOPERABLE. REPAIRED LOOSE CONNECTION AT BULB.
- [SDR COMA9810063](https://openairdocs.org/sdr/COMA9810063), Mar 6, 1998: EEC. MALFUNCTIONED. TORQUE INDICATION FLUCTUATED +- 20 PERCENT DURING TAKEOFF ROLL. DEFERRED THE ELECTRONIC ENGINE CONTROL SYSTEM.
- [SDR COMA9810062](https://openairdocs.org/sdr/COMA9810062), Mar 4, 1998: BUTTSTRAP. CORROSION. DURING 2C INSPECTION, TASK 5310-131-01I REVEALED CENTER BUTTSTRAP TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BU
- [SDR COMA9810061](https://openairdocs.org/sdr/COMA9810061), Mar 4, 1998: BUTTSTRAP. CORROSION. DURING 2C INSPECTION, TASK 5310-131-01I REVEALED BUTTSTRAP TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP
- [SDR COMA9810060](https://openairdocs.org/sdr/COMA9810060), Mar 4, 1998: BUTTSTRAP. CORROSION. DURING 2C INSPECTION, TASK 5310-131-01I REVEALED BUTTSTRAP THAT WAS CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTST
- [SDR COMA9810059](https://openairdocs.org/sdr/COMA9810059), Mar 4, 1998: CROSSBEAM. CORROSION. DURING 2C INSPECTION, TASK 5310-131-01I REVEALED CROSSBEAM AT FRAME 20 TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEAB
- [SDR COMA9810058](https://openairdocs.org/sdr/COMA9810058), Mar 4, 1998: CROSSBEAM. CORROSION. DURING 2C INSPECTION, TASK 5310-131-01I REVEALED THE CROSSBEAM AT FRAME 16 TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVI
- [SDR COMA9810057](https://openairdocs.org/sdr/COMA9810057), Mar 4, 1998: SILL. CORROSION. DURING 2C INSPECTION, TASK 5310-131-01I REVEALED CABIN SILL TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EM
- [SDR COMA9810056](https://openairdocs.org/sdr/COMA9810056), Mar 4, 1998: SILL. CORRODED. DURING 2C INSPECTION, TASK 5310-131-01I, REVEALED CABIN SILL TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING E
- [SDR COMA9810055](https://openairdocs.org/sdr/COMA9810055), Mar 4, 1998: TCAS TRAY. CORRODED. DURING 2C INSPECTION ZONE 100 TASK 5310-132-01I, FOUND TCAS SUPPORT TRAY CORRODED BEYOND LIMITS. REMOVED CORRODED TRAY AND BUILT UP NEW SERV TRAY IAW STC ST0007
- [SDR COMA9810043](https://openairdocs.org/sdr/COMA9810043), Feb 10, 1998: CONNECTOR. LOOSE. LANDING GEAR CONTROL COULD NOT BE SELECTED UP. GROUND SAFETY LOCK ENGAGED. SECURED LOOSE QUICK DISCONNECT COUPLING AT RIGHT HAND MLG WEIGHT ON WHEELS PROXIMITY 
- [SDR COMA9810037](https://openairdocs.org/sdr/COMA9810037), Feb 8, 1998: LAMP. FAILED. OVERHEAD EMERGENCY LIGHT AT ROW 2B IS INOP. REPLACED THE LIGHT BULB.
- [SDR COMA9810022](https://openairdocs.org/sdr/COMA9810022), Jan 12, 1998: LAMP. FAILED. EMERGENCY LIGHTS AT ROW SIX ARE INOPERATIVE. REPLACED LAMP FOR ROW SIX FLOOR EMERGENCY LIGHT TRACK.
- [SDR COMA9710493](https://openairdocs.org/sdr/COMA9710493), Dec 10, 1997: WIRE. FAILED. LANDING GEAR CANNOT BE SELECTED TO RETRACT. CONTROL SELECTOR CANNOT BE MOVED. REPAIRED WARN WIRING IN RIGHT HAND MLG FOR THE AIR/GROUND WEIGHT ON WHEELS SYTEM.
- [SDR COMA9710373](https://openairdocs.org/sdr/COMA9710373), Aug 20, 1997: SKIN. CORRODED. DURING COMPLIANCE OF E-6 INSPECTION, THE FUSELAGE LOWER SKIN WAS FOUND CORRODED AT FRAMES NR 21, 22 AND 23. THREE SEPARATE REPAIRS WERE PERFORMED. THE DAMAGE AT
- [SDR COMA9710336](https://openairdocs.org/sdr/COMA9710336), Jul 27, 1997: FIRE CONTROL. FAILED. LEFT ENGINE WHEEL WELL FIRE WARNING DURING FLIGHT. ENGINE SECURED AND BOTH FIRE BOTTLES DISCHARGED. FIRE WARNING PERSISTED. FALSE WARNING, REPLACED THE FIRE DET
- [SDR COMA9710313](https://openairdocs.org/sdr/COMA9710313), Jun 14, 1997: SAFETY PIN. NOT REMOVED. NLG DID NOT RETRACT. REMOVED DOWN LOCK SAFETY PIN FROM NLG. AIRCRAFT RETURNED TO SERVICE.
- [SDR COMA9710310](https://openairdocs.org/sdr/COMA9710310), Jun 12, 1997: SKIN. CRACKED. WHILE AIRCRAFT WAS IN THE HANGAR FOR SCHEDULED MAINTENANCE, MECHANIC NOTICED A CRACK IN THE LEFT NACELLE OUTBOARD AFT SKIN, JUST BELOW THE ROLLER SUPPORT FOR TH
- [SDR COMA9710304](https://openairdocs.org/sdr/COMA9710304), May 30, 1997: CONNECTOR. LOOSE. TAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF. REPLACED IMPROPER WIRING CONNECTIONS AT THE ELEVATOR TRIM PROXIMITY SENSORS.
- [SDR COMA9710302](https://openairdocs.org/sdr/COMA9710302), May 29, 1997: AURAL WARNING. SOUNDED. 'TAKEOFF TRIM' AURAL WARNING SOUNDED DURING TAKE OFF. RESET AURAL WARNING COMPUTER. DISCREPANCY WOULD NOT DUPLICATE.
- [SDR COMA9710093](https://openairdocs.org/sdr/COMA9710093), Jan 27, 1997: PROX SENSOR. INOPERATIVE. GEAR HANDLE WOULD NOT MOVE AFTER TAKEOFF. REPLACED RT MLG PROX. SENSOR.
- [SDR COMA9610281](https://openairdocs.org/sdr/COMA9610281), Sep 18, 1996: SOLENOID. MALFUNCTION. FLIGHT IDLE STOP SOLENOID CHECK DOES NOT FUNCTION. REPLACED SOLENOID.
- [SDR COMA9610160](https://openairdocs.org/sdr/COMA9610160), May 31, 1996: HYDRAULIC PUMP. FAILED. GREEN HYDRAULIC SYSTEM ELECTRIC PUMP, FAILED. REPLACED THE GREEN SYSTEM ELECTRIC HYDRAULIC PUMP.
- [SDR COMA9512026](https://openairdocs.org/sdr/COMA9512026), Dec 14, 1995: DNLOCK SENSOR. DEFECTIVE. LANDING GEAR WOULD NOT EXTEND NORMALLY. EMERGENCY EXTENTION SYSTEM USED. REPLACED DEFECTIVE DOWNLOCK PROXIMITY SENSOR.
- [SDR COMA9512013](https://openairdocs.org/sdr/COMA9512013), Nov 27, 1995: ROLLER. WORN. FLAP DISAGREEMENT WARNING CLIMB. OUTBOARD FLAPS DID NOT RETRACT FULLY. REPLACED THE LT OUTBOARD FLAP ASSY ROLLERS.
- [SDR COM11944](https://openairdocs.org/sdr/COM11944), Aug 4, 1995: SENSOR. DAMAGED. DURING LANDING, LEFT MLG INDICATED UNSAFE ON A-SYSTEM AND SAFE ON B-SYSTEM. REPLACED DAMAGED PROXIMITY SENSOR FOR A SYSTEM DOWNLOCK.
- [SDR COM11919](https://openairdocs.org/sdr/COM11919), Jun 17, 1995: SKIN SUPPORT. CRACKED. THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERO-DESIGN REPORT NR 13
- [SDR COM11897](https://openairdocs.org/sdr/COM11897), May 21, 1995: PCU. OUT OF ADJUST. DURING TAKEOFF LT NP INDICATED 99.3 PERCENT. ADJUSTED PCU FOR 100 PERCENT PROPELLER RPM.
- [SDR COM11850](https://openairdocs.org/sdr/COM11850), Mar 31, 1995: CONTL VALVE. DEFECTIVE. ANTI-SKID SYSTEM DOES NOT TEST. REPLACED BRAKE ANTI-SKID CONTROL VALVE.
- [SDR COM11789](https://openairdocs.org/sdr/COM11789), Feb 16, 1995: CONTROL CABLE. BROKEN. GO AROUND BUTTON ON LEFT POWER LEVER IS INOPERATIVE. REPAIRED BROKEN WIRE IN POWER LEVER QUADRANT.

## 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 19970727027159I](https://openairdocs.org/incident/19970727027159I), Jul 27, 1997: Emb EMB120RT (N241CA), Indianapolis, IN. Narrative: on July 27, 1997 comair flight 3199 was enroute from cincinnati, oh to milwaukee, WI and diverted to Indianapolis, IN. The left engine/wheel well…

## Other aircraft with N241CA

- [Cancelled 2024-05-01](https://openairdocs.org/deregistered/N241CA-2024-05-01): Gates Learjet 35A, S/N 142, built 1977. Owner: [Alliance Air Parts Inc](https://openairdocs.org/faa-owner/ALLIANCE%20AIR%20PARTS%20INC), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City)

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