# N47722: 1990 Embraer EMB-120ER, registration cancelled 2012-03-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 7, 2012
- 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: 120.166
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: July 10, 1996
- Certificate issued: March 29, 2007
- Last registry action: December 17, 2010
- Mode S code: A5DDD4
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N47722
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=47722
- Page: https://openairdocs.org/deregistered/N47722-2012-03-07

From the FAA registry file of October 28, 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 (54, newest 50)

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

- [SDR C2XA01IA063](https://openairdocs.org/sdr/C2XA01IA063), Feb 5, 2001: PROXIMITY SWITCH. INOPERATIVE. IAH - FLIGHT 3580, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED
- [SDR C2XA00IA476](https://openairdocs.org/sdr/C2XA00IA476), Dec 22, 2000: CONNECTOR. BENT. TYR - FLT 4379 - THE CREW REPORTED THAT ON TAKEOFF ROLL RECEIVED ELECTRIC AND DOOR WARNINGS AND LOST NOSE WHEEL STEERING. THE CREW ABORTED TAKEOFF AND RETURNED 
- [SDR C2XAOOIA396](https://openairdocs.org/sdr/C2XAOOIA396), Oct 30, 2000: HEATER. DAMAGED. DURING TAKE-OFF ROLL CREW REPORTED A FUEL LOW PRESSURE LIGHT ON #2 ENGINE. TAKE-OFF WAS ABORTED WITHOUT INCIDENT, AND THE CREW NOTICED FUEL LEAKING OUT OF #2 NA
- [SDR C2XA00IA268](https://openairdocs.org/sdr/C2XA00IA268), Sep 6, 2000: BULB. INOPERATIVE. IAH - DURING A CHECK INSPECTION, TWO AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULBS, AND TH
- [SDR C2XA00IA192](https://openairdocs.org/sdr/C2XA00IA192), Jul 4, 2000: DOOR. DISCONNECTED. IAH - FLT 3581 - THE CREW REPORTED THAT THE LEFT FORWARD NOSE GEAR DOOR WOULD NOT CLOSE AND A LOUD NOISE COMING FROM THE NOSE LANDING GEAR COMPARTMENT. THE AIRC
- [SDR C2XA00IA131](https://openairdocs.org/sdr/C2XA00IA131), May 19, 2000: WIRE. BROKEN. EFD - DURING MAINTENANCE INSPECTION, SEVERAL AISLE PATH EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE LIGHT TRAC
- [SDR C2XA00IA124](https://openairdocs.org/sdr/C2XA00IA124), May 13, 2000: BATTERY PACK. DISCHARGED. IAH - DURING 1A INSPECTION, THE RIGHT UPPER OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PAC
- [SDR C2XA00IA114](https://openairdocs.org/sdr/C2XA00IA114), May 5, 2000: BATTERY PACK. DISCHARGED. IAH - DURING SERVICE CHECK INSPECTION, THE AFT EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTE
- [SDR C2XA00IA048](https://openairdocs.org/sdr/C2XA00IA048), Mar 2, 2000: PROXIMITY SWITCH. MISALIGNED. IAH - FLIGHT 3664 - THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR POSITION A LIGHT ILLUMINATED INFLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHO
- [SDR C2XAOOIA045](https://openairdocs.org/sdr/C2XAOOIA045), Feb 20, 2000: FRAME. CRACKED. DURING CONTINENTAL EXPRESS AIRLINES C-CHECK, FOUND LT NACELLE NR 1 FRAME CRACKED. REMOVED AND REPLACED NR 1 FRAME IAW EC5410-01034. AIRCRAFT APPROVED FOR RETURN
- [SDR C2XA99IA589](https://openairdocs.org/sdr/C2XA99IA589), Nov 3, 1999: RELAY BOX. INOPERATIVE. IAH - FLT 3455, THE CREW REPORTED THAT THE LANDING GEAZR WOULD NOT RETRACT. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED 
- [SDR C2XA99IA384](https://openairdocs.org/sdr/C2XA99IA384), Jul 23, 1999: BATTERY PACK. DISCHARGED. IAH - A-CHECK INSPECTION, THE AFT FOUR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW E
- [SDR C2XA99IA181](https://openairdocs.org/sdr/C2XA99IA181), Mar 4, 1999: LENS. BROKEN. IAH - DURING POST-FLT INSPECTION, A RED EMERGENCY AISLE PATH EMERGENCY LIGHT WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LENS, AND THE
- [SDR C2XA99IA179](https://openairdocs.org/sdr/C2XA99IA179), Mar 4, 1999: WIRE. BROKEN. IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AND THE AIRCRAFT WAS APPROVE
- [SDR C2XA98CL072](https://openairdocs.org/sdr/C2XA98CL072), Nov 6, 1998: FUSE. FAILED. CLE - FLT 3351 - CREW REPORTED THE EMERGENCY ESCAPE FLOOR LIGHTS DO NOT WORK FROM ROW 9 TO ROW 11. MAINTENANCE INSPECTED THE EMERGENCY LIGHTING SYSTEM THEN REMO
- [SDR C2XA98IA211](https://openairdocs.org/sdr/C2XA98IA211), Jun 17, 1998: BATTERY PACK. DISCHARGED. IAH - DURING C-CHECK INSPECTION, THE FORWARD FLOOR EMERGENCY LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK FOR 
- [SDR C2XA98IA210](https://openairdocs.org/sdr/C2XA98IA210), Jun 17, 1998: CREASE BEAM. CORRODED. IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 39 AND 44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION 
- [SDR C2XA98IA209](https://openairdocs.org/sdr/C2XA98IA209), Jun 17, 1998: BUTTSTRAP. CORRODED. IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 38-44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION
- [SDR C2XA98IA208](https://openairdocs.org/sdr/C2XA98IA208), Jun 17, 1998: BUTTSTRAP. CORRODED. IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER BUTTSTRAP BETWEEN FRAMES 34 AND 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE EFFECTED SEC
- [SDR C2XA98IA207](https://openairdocs.org/sdr/C2XA98IA207), Jun 17, 1998: T-PROFILE. CORRODED. IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 40 RIGHT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE EFFECTED T-PROFILE IAW EMB120 SR
- [SDR C2XA98IA206](https://openairdocs.org/sdr/C2XA98IA206), Jun 17, 1998: TEE. CORRODED. IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 38 RIGHT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE EFFECTED T-PROFILE IAW EMB120 SR
- [SDR C2XA98IA205](https://openairdocs.org/sdr/C2XA98IA205), Jun 17, 1998: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMVOED AND REPLACED THE EFFECTED SEAT TRACK IAW EMBL-120 
- [SDR C2XA98IA204](https://openairdocs.org/sdr/C2XA98IA204), Jun 17, 1998: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, THE RIGHT WING NUMBER TWO UPPER SKIN SUPPORT AT RIB 21 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE EFFECTED S
- [SDR C2XA98IA200](https://openairdocs.org/sdr/C2XA98IA200), Jun 17, 1998: ANGLE. CRACKED. IAH - DURING C-CHECK INSPECTION, THE LEFT DRAG ANGLE ON THE VERTICLE STABILIZER WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE DAMAGED SECTION OF THE DRAG ANG
- [SDR C2XA98IA199](https://openairdocs.org/sdr/C2XA98IA199), Jun 17, 1998: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER REPA
- [SDR C2XA98IA198](https://openairdocs.org/sdr/C2XA98IA198), Jun 17, 1998: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER IAW E
- [SDR C2XA97CL048](https://openairdocs.org/sdr/C2XA97CL048), Apr 30, 1997: ENGINE. FAILURE. CLE - FLT 3184 - CREW REPORTED WHILE CLIMBING THROUGH 6,000 FEET, RIGHT HAND ENGINE NP INCREASED AND THE OIL PRESSURE DROPPED TO ZERO. CREW ATTEMPTED A SHUTDOWN
- [SDR C2XA97CL021](https://openairdocs.org/sdr/C2XA97CL021), Mar 10, 1997: ACTUATOR. FAILED. PIT - FLT 3610 - CREW REPORTED, RECEIVED A FLAP CONTROL FAULT IN FLIGHT WHICH WOULD NOT RESET. AIRCRAFT LANDED IN PIT WITHOUT INCIDENT. THE AIRCRAFT WAS MAINTEN
- [SDR C2XA96IA292](https://openairdocs.org/sdr/C2XA96IA292), Dec 2, 1996: STRINGER. CRACKED. IAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER NR 10 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE AFFECTED PORTION OF STRINGER AND THE AIRCRAFT W
- [SDR C2XA96CL009](https://openairdocs.org/sdr/C2XA96CL009), Jan 31, 1996: ACTUATOR. STICKING. CLT - FLT NR 3340 - CREW REPORTED, THAT AFTER TAKEOFF AND FLAP RETRACTION, THE LEFT AND RIGHT OUTBOARD FLAPS STAYED AT 15 DEGREES WITHOUT RECEIVING A DISAGREEME
- [SDR C2XA96CL008](https://openairdocs.org/sdr/C2XA96CL008), Jan 30, 1996: CONTROL UNIT. FAILED. CLE - FLIGHT NR 3286 - CREW REPORTED THAT ON APPROACH WHEN THE FLAPS WERE SELECTED TO 25 DEGREES FROM 15 DEGREES, THE LEFT AND RIGHT OUTBOARD FLAPS STAYED AT 15
- [SDR C2XA96CL007](https://openairdocs.org/sdr/C2XA96CL007), Jan 30, 1996: ACTUATOR. LINKAGE BINDING. ROC - FLIGHT NR 3113 - CREW REPORTED THAT ON APPROACH WITH FLAPS SELECTED TO 15 DEGREES, A FLAP ASYMMETRY OCCURRED THEN CHANGED TO A FLAP DISAGREEMENT. THE CREW
- [SDR C2XA96CL006](https://openairdocs.org/sdr/C2XA96CL006), Jan 28, 1996: CONTROL UNIT. FAILED. CLT - FLT NR 3372 - CREW REPORTED, THAT DURING APPROACH THEY RECEIVED A FLAP CONTROL FAULT, THE CREW RESET THE SYSTEM BUT RECEIVED ANOTHER FLAP CONTROL FAULTY W
- [SDR C2XA96CL005](https://openairdocs.org/sdr/C2XA96CL005), Jan 25, 1996: CONTROL UNIT. FAILED. ROC - FLT NR 3113 - CREW REPORTED THAT DURING LANDING WHEN THE FLAPS WERE SELECTED TO 15 DEGREES, THE RIGHT OUTBOARD EXTENDED TO 10 DEGREES AND THE LEFT OUTBOAR
- [SDR C2XA95CL116](https://openairdocs.org/sdr/C2XA95CL116), Sep 23, 1995: ENGINE. FAILED. FLT NR 3230 - DAY - CLE - RIGHT POWER LEVER HAD VERY NOTICEABLE VIBRATION WITH PROPELLER IN FEATHER AND MINIMUM RPM. MAINTENANCE REMOVED AND REPLACED RIGHT ENGI
- [SDR C2XA95IA180](https://openairdocs.org/sdr/C2XA95IA180), Aug 8, 1995: T-CAP. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND THE T-CAP AT FRAME 40 TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-CAP, AND THE AIRCRAFT WAS APPROVED 
- [SDR C2XA95IA179](https://openairdocs.org/sdr/C2XA95IA179), Aug 8, 1995: CROSS BEAM. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND THE CROSS BEAM BETWEEN FRAMES 35 TO 38, TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF CROSSBEA
- [SDR C2XA95IA178](https://openairdocs.org/sdr/C2XA95IA178), Aug 8, 1995: CROSSBEAM. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND CROSSBEAM AT FRAME 16 TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF CROSSBEAM, AND THE AIRCRAF
- [SDR C2XA95IA177](https://openairdocs.org/sdr/C2XA95IA177), Aug 8, 1995: SKIN SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 4 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED F
- [SDR C2XA95IA175](https://openairdocs.org/sdr/C2XA95IA175), Aug 8, 1995: SKIN SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 2 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED F
- [SDR C2XA95IA174](https://openairdocs.org/sdr/C2XA95IA174), Aug 8, 1995: SKIN SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 3 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED F
- [SDR C2XA95IA173](https://openairdocs.org/sdr/C2XA95IA173), Aug 8, 1995: SKIN SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 5 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED F
- [SDR C2XA95IA172](https://openairdocs.org/sdr/C2XA95IA172), Aug 8, 1995: SKIN SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 3 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED F
- [SDR C2XA95IA171](https://openairdocs.org/sdr/C2XA95IA171), Aug 8, 1995: SKIN SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 2, AND NR 4 SKIN SUPPORTS CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT
- [SDR C2XA95IA170](https://openairdocs.org/sdr/C2XA95IA170), Aug 8, 1995: SKIN SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 1 UPPER SKIN SUPPORT CRACKED AT RIB NR 21. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR
- [SDR C2XA95IA169](https://openairdocs.org/sdr/C2XA95IA169), Aug 8, 1995: SKIN SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND RT WING LOWER NR 2 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR
- [SDR C2XA95IA168](https://openairdocs.org/sdr/C2XA95IA168), Aug 8, 1995: SKIN SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 4 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR
- [SDR C2XA95IA167](https://openairdocs.org/sdr/C2XA95IA167), Aug 8, 1995: SKIN SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 3 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR
- [SDR C2XA95IA166](https://openairdocs.org/sdr/C2XA95IA166), Aug 8, 1995: SKIN SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND RT WING LOWER SKIN SUPPORT NR 2 CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR
- [SDR C2XA5IA176](https://openairdocs.org/sdr/C2XA5IA176), Aug 8, 1995: SKIN SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 3 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED F

All 54: https://openairdocs.org/deregistered/N47722-2012-03-07/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 19960125003339I](https://openairdocs.org/incident/19960125003339I), Jan 25, 1996: Emb EMB120RT (N47722), Rochester, NY. Narrative: on January 25, 1996 at 0905, an Embraer Emb-120RT aircraft operated by Continental express airlines, experienced a flap asymmetry problem while on…

## Other aircraft with N47722

- [Cancelled 1971-09-25](https://openairdocs.org/deregistered/N47722-1971-09-25): Taylorcraft DCO-65, S/N 4819. Owner: [Arnold L Petersen](https://openairdocs.org/faa-owner/ARNOLD%20L%20PETERSEN), [Lynwood, CA](https://openairdocs.org/faa-place/CA/Lynwood)

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