# N200CD: 1990 Embraer EMB-120RT, registration cancelled 2006-04-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 25, 2006
- Exported to: South Africa
- 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: 120.200
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: August 31, 1990
- Certificate issued: February 21, 2006
- Last registry action: February 21, 2006
- Mode S code: A19239
- Owners when cancelled: [Fhe Inc DBA](https://openairdocs.org/faa-owner/FHE%20INC%20DBA), [International Aviation Support](https://openairdocs.org/faa-owner/INTERNATIONAL%20AVIATION%20SUPPORT)
- Location: [Carrollton, TX](https://openairdocs.org/faa-place/TX/Carrollton)
- Owner type: Corporation
- Owner's area on the map: 32.9619° N, 96.8993° W: Placed by OpenAirDocs at the center of ZIP code 75006, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N200CD
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=200CD
- Page: https://openairdocs.org/deregistered/N200CD-2006-04-25

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

## Service difficulty reports (61, newest 50)

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

- [SDR 2006FA0000065](https://openairdocs.org/sdr/2006FA0000065), Jan 11, 2006: WINDOW FRAME. CRACKED. PILOT`S SIDE WINDOW LOWER STRUCTURAL BEAM IS CRACKED AT LT WINDSHIELD AFT BEAM. NORMAL OPERATIONS. (K)
- [SDR 2006FA0000046](https://openairdocs.org/sdr/2006FA0000046), Jan 11, 2006: WINDOW FRAME. CRACKED. COPILOTS SIDE WINDOW LOWER STRUCTURAL BEAM IS CRACKED AT RT WINDSHIELD AFT BEAM. NORMAL OPS. (K)
- [SDR SWIA200210545](https://openairdocs.org/sdr/SWIA200210545), Jan 5, 2002: LANDING GEAR. MALFUNCTIONED. AFTER GEAR RETRACTION, BOTH RED AND GREEN A-SYSTEM NOSE LIGHTS REMAINED ILLUMINATED. PRESS TO TEST DISPLAYED ALL B-LIGHTS ON AND ONLY A-NOSE LIGHTS ON. ATTEMPTE
- [SDR SWIA200110253](https://openairdocs.org/sdr/SWIA200110253), Oct 15, 2001: BOLT. BROKEN. UPON GEAR RETRACTION LEFT MAIN GEAR DOOR STAYED OPEN. RECYCLED GEAR AND IT STILL REMAINED OPEN. FOUND A BROKEN BOLT ON THE LEFT INBOARD FORWARD DOOR ACTUATOR AR
- [SDR SWIA200110220](https://openairdocs.org/sdr/SWIA200110220), Oct 2, 2001: FCU. MALFUNCTIONED. ON TAKEOFF WE GOT THE FLAP AND ADVANCED SWS ON MAP AND CONTROL FAULT. ASYMMETRY AND DISAGREEMENT ON OVERHEAD FLAP PANEL AND FLAP DEG. INDICATOR WENT TO 0 DEGREE
- [SDR SWIA200110204](https://openairdocs.org/sdr/SWIA200110204), Sep 21, 2001: STRAP. OUT OF POSITION. CLIMBING THROUGH 22,000 CABIN ALT LIGHT ON MAP. CABIN WOULD NOT RESPOND IN AUTO. SWITCH TO MANUAL, WOULD NOT RESPOND. AFTER ABOUT 30 SECONDS CABIN STARTED DESCE
- [SDR SWIA200110179](https://openairdocs.org/sdr/SWIA200110179), Sep 8, 2001: ENGINE. MALFUNCTIONED. LEFT ENGINE LOST POWER INFLIGHT, PRECAUTIONARY ENGINE SHUT DOWN CHECK COMPLETED.REMOVED AND REPLACED LEFT ENGINE ASSY WITH SERVICEABLE UNIT. COMPLIED WITH ALL I
- [SDR SWIA200110167](https://openairdocs.org/sdr/SWIA200110167), Aug 18, 2001: FRAME. CRACKED. LEFT NACELLE FRAME 1 CRACKED AT INBOARD TORSION MOUNT.REPLACED LEFT NACELLE FRAME 1 IAW SB120-54-0036 PART 2.
- [SDR SWIA200110166](https://openairdocs.org/sdr/SWIA200110166), Aug 18, 2001: FRAME. CRACKED. RIGHT NACELLE FRAME 1 CRACKED AT OUTBOARD TORSION MOUNT.REPLACED RIGHT NACELLE FRAME 1 IAW SB120-54-0036 PART 2.
- [SDR SWIA200110165](https://openairdocs.org/sdr/SWIA200110165), Aug 18, 2001: STRINGER. CRACKED. CRACKED LOWER STRINGER IN FUEL BAY LEFT WING AT NR 2 FUEL ACCESS PANEL BAY FWD.REPAIRED IAW EMB120 SRM 57-20-03.
- [SDR SWIA200110164](https://openairdocs.org/sdr/SWIA200110164), Aug 18, 2001: STRINGER. CRACKED. CRACKED LOWER STRINGER IN FUEL BAY LEFT WING AT NR 2 FUEL ACCESS PANEL BAY AFT.REPAIRED IAW EMB120 SRM 57-20-03.
- [SDR SWIA200110163](https://openairdocs.org/sdr/SWIA200110163), Aug 18, 2001: STRINGER. CRACKED. RIGHT MOST INBOARD FUEL PANEL FORWARD STRINGER CRACKED. REPAIRED IAW EMB120 SRM 57-20-03 AS OUTLINED.
- [SDR SWIA200110162](https://openairdocs.org/sdr/SWIA200110162), Aug 18, 2001: BEARING. CORRODED. RIGHT NACELLE FLAP HINGE BEARINGS 2 EA. CORRODED AND WORN.REPLACED NACELLE FLAP WITH SERVICEABLE FLAP ASSEMBLY AS NEEDED.P/N: 120-40327-002 S/N OFF: 120212
- [SDR SWIA200110161](https://openairdocs.org/sdr/SWIA200110161), Aug 18, 2001: SWIVEL. CORRODED. NOSE GEAR AFT DOORS RODS AND SWIVELS WORN AND CORRODED.REMOVED AND REPLACED NOSE LANDING GEAR AFT DOORS RODS AND SWIVELS WITH SERVICEABLE PARTS AS REQUIRED.
- [SDR SWIA972654](https://openairdocs.org/sdr/SWIA972654), Jun 11, 2001: WARNING SYSTEM. ACTIVATED. AURAL WARNING AND MAP LIGHT ILLUMINATED ON TAKEOFF WITH ABORT BELOW 80 KTS. RESET AURAL WARNING SYSTEM. OPS CHECK GOOD.
- [SDR SWIA972289](https://openairdocs.org/sdr/SWIA972289), Jan 13, 2001: BOOT. FAILED. INBOARD STABILIZER AND INBOARD WING DEICE BOOTS FAILED AFTER TAKEOFF. RETURNED TO SEA. REMOVED AND REPLACED INBOARD STABILIZER AND WING EJECTOR VALVE WITH SERVI
- [SDR SWIA972247](https://openairdocs.org/sdr/SWIA972247), Jan 4, 2001: WIRE. GROUNDED. ON APPROACH SELECTED FLAPS 25 THE RT OUTBOARD WENT 1 LIGHT BAR PAST FLAPS 25 AND CAUSED AN ASYMETRY. WE LANDED, PERFORMED THE QRH, THEN SELECTED FLAPS UP AND TH
- [SDR SWIA972235](https://openairdocs.org/sdr/SWIA972235), Dec 31, 2000: ACTUATOR. FAILED. RIGHT OUTBOARD FLAP GOES TO 45 DEGREES WHEN 25 DEGREES WAS COMMANDED. THERES NO INDICATION WITH THE OVERHEAD PANEL OR MAP. REPLACED RIGHT OUTBOARD ACTUATOR. OPS
- [SDR SWIA972199](https://openairdocs.org/sdr/SWIA972199), Dec 17, 2000: ACTUATOR. FAILED. DURING SELECTION OF FLAPS 15 ON TAXI THE OUTBOARD PAIR WOULD ONLY EXTEND TO 1 LIGHT BAR. WE RECEIVED A CONTROL FAULT AND ASWS WARNING. WERE UNABLE TO EXTEND OR 
- [SDR SWIA972174](https://openairdocs.org/sdr/SWIA972174), Dec 10, 2000: ACTUATOR. FAILED. DURING CRUISE FLIGHT, ''CONTROL FAUL'' FLAP WARNING INDICATOR ALONG WITH OUTBOARD PAIR OF FLAPS ILLUMINATED ON OVERHEAD PANEL. ADVANCED SWS AND FLAP LIGHTS ON M
- [SDR SWIA972173](https://openairdocs.org/sdr/SWIA972173), Dec 9, 2000: CONNECTOR. CONTAMINATED. CONTROL FAULT IN OUTBOARD PAIR OF FLAPS DURING APPROACH WITH ASSOCIATED ''FLAP'' AND ''ADVANCED SWS'' ON MAP. ATTEMPTED TO RESET AS PER QRH WHICH WAS UNSUCCESSF
- [SDR SWIA972141](https://openairdocs.org/sdr/SWIA972141), Nov 30, 2000: CONNECTOR. CONTAMINATED. ON DESCENT FLAP, ADVANCED SWS, CONTROL FAULT, OUTBOARD PAIR FLASHING. QRH WAS FOLLOWED BUT SYSTEM DID NOT RESET. FOUND MOISTURE IN CANNON PLUGS, CLEANED. USING 
- [SDR SWIA972111](https://openairdocs.org/sdr/SWIA972111), Nov 20, 2000: LANDING GEAR. MALFUNCTIONED. LEFT MAIN LANDING GEAR WOULD NOT RETRACT. SECURED LEFT GEAR INBOARD FOWARD DOOR. SWUNG GEAR, OPS CHECKS GOOD IAW MM 32-32-00.
- [SDR SWIA972125](https://openairdocs.org/sdr/SWIA972125), Nov 11, 2000: CONTROL UNIT. FAILED. DURING CRUISE FLIGHT, REEIVED 4 INDICATIONS: CONTROL FAULT, OUTBOARD FLAP PAIR SECOND SEGMENT FLASHING, MAP FLAP AND ADVANCED SWS CAPTIONS. QRH RESET UNSUCCESSF
- [SDR SWIA971921](https://openairdocs.org/sdr/SWIA971921), Aug 9, 2000: ROD END. DAMAGED. BOTH RIGHT MAIN ''''RED'''' DISAGREEMENT LIGHTS REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED. RETURNED TO SFO. REPLACED RIGHT MLG RETRACTING ACTUATOR ROD END A
- [SDR SWIA971752](https://openairdocs.org/sdr/SWIA971752), Apr 4, 2000: WARNING SYSTEM. FALSE INDICATION. AFTER TAKEOFF SINGLE CHIME AURAL WARNING CHIMED CONTINUED WITH GEAR DOWN BUT STOPPED WHEN REACHING THE GATE. UNSCHEDULED LANDING. REPLACED AURAL WARNING UNIT IA
- [SDR SWIA971450](https://openairdocs.org/sdr/SWIA971450), Apr 9, 1999: RELAY. FAILED. LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR RELAY BOX IAW MM 32-31-02. GEAR SWING CHECKS GOOD.
- [SDR COMA9810068](https://openairdocs.org/sdr/COMA9810068), Mar 10, 1998: CABLE. CORRODED. DURING 2C INSPECTION TASK 813-01A, FOUND CARGO DOOR FORWARD INNER CABLE TO BE CORRODED. REMOVED CORRODED CABLE AND INSTALLED SERV CABLE IAW EMB120 MM.
- [SDR COMA9710426](https://openairdocs.org/sdr/COMA9710426), Oct 10, 1997: DISAGREE LIGHT. MALFUNCTIONED. WHEN LANDING GEAR SELECTED UP, THE RIGHT HAND MLG DISAGREE LIGHTS REMAINED ON. COULD NOT DUPLICATE DISCREPANCY. LANDING GEAR RETRACT CHECKS NORMAL.
- [SDR COMA9710401](https://openairdocs.org/sdr/COMA9710401), Sep 8, 1997: DRAG BRACE. STIFF. LEFT HAND MLG DID NOT DOWNLOCK DURING FREE FALL CHECK. RESHIMMED THE LANDING GEAR DRAG BRACE.
- [SDR COMA9710238](https://openairdocs.org/sdr/COMA9710238), May 4, 1997: PROX SENSOR. FALSE WARN. TAKEOFF TRIM AURAL WARNING DURING TAKEOFF. REPLACED THE LT ELEVATOR TRIM PROXIMITY SENSOR.
- [SDR COMA9710160](https://openairdocs.org/sdr/COMA9710160), Feb 24, 1997: PROX SENSOR. FAILED. AFTER TAKEOFF AND GEAR SELECTED UP, THE LEFT HAND MLG 'A' LIGHT REMAINED ON. LANDING GEAR DID NOT RETRACT UNTIL EMERGENCY SYSTEM WAS ACTIVATED. REPLACED THE LEF
- [SDR COMA9710074](https://openairdocs.org/sdr/COMA9710074), Jan 21, 1997: CYLINDER. CRACKED. HYD LEAK COMING FROM NOSE GEAR STEERING AREA. REPLACED LEFT STEERING CYLINDER.
- [SDR COMA9710045](https://openairdocs.org/sdr/COMA9710045), Jan 18, 1997: ROLLER. WORN. LEFT OUTBOARD FLAP FAILS TO RETRACT WITH OTHERS. REPLACED LEFT OUTBOARD FLAP ROLLLRS, OPERATIONAL CHECK GOOD.
- [SDR COMA9710029](https://openairdocs.org/sdr/COMA9710029), Jan 13, 1997: ACTUATOR. INOPERATIVE. FLAP DISAGREEMENT UPON FLAP RETRACTION AFTER TAKEOFF. REPLACED LEFT OUTBOARD FLAP ACTUATOR OPERATIONAL CHECK GOOD. PART TOTAL CYCLES, 16,190.
- [SDR COMA9610308](https://openairdocs.org/sdr/COMA9610308), Oct 18, 1996: WIRE. CHAFED. LT BLEED AIR DUCT LEAK WARNING CAME ON DURING CLIMB. REPAIRED CHAFED WIRING AT DUCT LEAK SENSOR.
- [SDR COMA9610151](https://openairdocs.org/sdr/COMA9610151), May 19, 1996: SKIN SUPPORT. CRACKED. DURING 400FC INSPECTION, FOUND ONE RIVET AT FRAME 9 JUST BELOW RIGHT DIRECT WINDOW TO BE DEFORMED. FURTHER INSPECTION REVEALED SKIN SUPPORT TO BE CRACKED. REPLA
- [SDR COMA9610109](https://openairdocs.org/sdr/COMA9610109), Mar 23, 1996: ROLLERS. WORN. FLAPS DISAGREEMENT WARNING AFTER TAKEOFF WHEN FLAPS SELECTED UP. REPLACED WORN ROLLERS AND TRACKS ON RT INBD FLAP.
- [SDR COMA9610103](https://openairdocs.org/sdr/COMA9610103), Mar 11, 1996: DOOR LATCH. BROKEN. OIL INSPECTION DOOR ON ENGINE COWLING WILL NOT STAY CLOSED. REPAIRED BROKEN SHEET METAL LATCH RETAINER.
- [SDR COMA9610096](https://openairdocs.org/sdr/COMA9610096), Mar 7, 1996: OAT PROBE HEAT. FAILED. OUTSIDE AIR TEMPERATURE PROBE HEAT IS INOPERATIVE. REPLACED THE TRUE AIR TEMP PROBE. PART TOTAL CYCLES, 12,082.
- [SDR COMA9610075](https://openairdocs.org/sdr/COMA9610075), Feb 6, 1996: LINES. FROZEN. LEFT AND RIGHT HYDRAULIC RESERVOIR LOW PRESS WARNINGS ILLUMINATED. THAWED THE FROZEN MOISTURE THAT WAS BLOCKING THE HYDRAULIC RESERVOIR BLEED AIR PRESSURIZATION
- [SDR COMA9610068](https://openairdocs.org/sdr/COMA9610068), Feb 5, 1996: SENSOR. MALFUNCTIONED. NOSE LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER RETRACTION. COUD NOT DUPLICATE DISCREPANCY. REPLACED A-SYSTEM PROXIMITY SENSOR, WHILE TROUBLESHOOTING.
- [SDR COMA9610065](https://openairdocs.org/sdr/COMA9610065), Feb 4, 1996: CONTROL BOX. DEFECTIVE. NOSE LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER GEAR RETRACTION. REPLACED THE LANDING GEAR CONTROL ASSY.
- [SDR COMA9610047](https://openairdocs.org/sdr/COMA9610047), Jan 30, 1996: RETRACT MECH. ICED UP. NOSE LANDING, GEAR INTRANSIT LIGHTS REMAINED ON AFTER GEAR RETRACTION. REMOVED ICE FROM LANDING GEAR, RETRACT CHECKS NORMAL, AND ACFT RETURNED TO SERVICE.
- [SDR COMA9610033](https://openairdocs.org/sdr/COMA9610033), Jan 19, 1996: UPLOCK HOOK. LACK OF LUBE. LT MLG WILL NOT RETRACT. FOUND UPLOCK HOOK ASSY TO BE BINDING. CLEANED AND LUBED UPLOCK ASSY AND SYSTEM OPERATES NORMALLY.
- [SDR COMA9512020](https://openairdocs.org/sdr/COMA9512020), Dec 9, 1995: UPLOCK. DIRTY. WHEN LANDING GEAR SELECTED UP, LT MLG INTRANSIT LIGHTS REMAINED ON. CLEANED LT MLG UPLOCK, RETRACTION CHECK NORMAL AND ACFT RETURNED TO SERVICE.
- [SDR COMA9512002](https://openairdocs.org/sdr/COMA9512002), Nov 12, 1995: SEPARATOR. LEAKING. RT DUCT LEAK WARNING ACTIVATED. REPLACED LEAKING AIR FOIL DE-ICE WATER SEPARATOR.
- [SDR COMA9511990](https://openairdocs.org/sdr/COMA9511990), Oct 20, 1995: WARNING LIGHT. ILLUMINATED. CARGO DOOR WARNING ILLUMINATED DURING FLIGHT. PLACED CARGO DOOR WARNING SYSTEM ON DEFERRED MAINTENANCE LIST.
- [SDR COM11937](https://openairdocs.org/sdr/COM11937), Jul 31, 1995: LINK ROD. FAILED. AIRCRAFT ON APPROACH TO FPO, CREW SELECTED GEAR DOWN. THE MLG INDICATED DOWN AND LOCKED AND THE NLG INDICATED UNSAFE. MAINTENANCE INSPECTED THE NLG AND FOUND TH
- [SDR COM11931](https://openairdocs.org/sdr/COM11931), Jul 21, 1995: LATCH ASSY. BROKEN. LEFT ENGINE INBD NACELLE LATCH IS BROKEN. REPLACED LATCH.

All 61: https://openairdocs.org/deregistered/N200CD-2006-04-25/reports.md

## FAA accident and incident reports (2)

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 20000227002219I](https://openairdocs.org/incident/20000227002219I), Feb 27, 2000: Emb EMB120RT (N200CD), Redding, CA. (-23) Aircraft encountered what the pilot described as severe clear air turbulence with a large downdraft followed by a sudden updraft during the approach to…
- [Incident 19950517021159I](https://openairdocs.org/incident/19950517021159I), May 17, 1995: Emb EMB120RT (N200CD), Chicago, IL. Lost oil pressure left engine diverted mdw. Oil pressure fitting at regulator broke.

## Other aircraft with N200CD

- [Cancelled 2008-08-22](https://openairdocs.org/deregistered/N200CD-2008-08-22): Cirrus Design SR20, S/N 2000, built 2008. Exported to United Kingdom. Owner: [Anglo Services Inc Trustee](https://openairdocs.org/faa-owner/ANGLO%20SERVICES%20INC%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)

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