# N16719: Embraer EMB-120ER, registration cancelled 2000-01-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 14, 2000 - Exported to: Brazil - Status when cancelled: Valid registration - Airframe: [Embraer EMB-120ER](https://openairdocs.org/model/embraer-emb-120er) (registry code 3260203) - Data sheets: [TCDS A31SO](https://openairdocs.org/tcds/A31SO) (OpenAirDocs) - Serial number: 120.138 - Type of aircraft: Fixed wing multi engine - Certificate issued: August 18, 1999 - Last registry action: August 18, 1999 - Mode S code: A10E4C - Owner when cancelled: [Rodriguez Elias C Trustee](https://openairdocs.org/faa-owner/RODRIGUEZ%20ELIAS%20C%20TRUSTEE) - Location: [Fairfax, VA](https://openairdocs.org/faa-place/VA/Fairfax) - Owner type: Individual - Owner's area on the map: 38.8595° N, 77.2627° W: Placed by OpenAirDocs at the center of ZIP code 22031, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N16719 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16719 - Page: https://openairdocs.org/deregistered/N16719-2000-01-14 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-120ER: https://openairdocs.org/model/embraer-emb-120er.md ## Service difficulty reports (53, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR C2XA98CL068](https://openairdocs.org/sdr/C2XA98CL068), Sep 22, 1998: ACTUATOR. FAILED. CLE - FLT 3003 - CREW REPORTED THAT DURING CLIMB-OUT THEY RECEIVED A FLAP CONTROL FAULT. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPEC - [SDR C2XA98IA346](https://openairdocs.org/sdr/C2XA98IA346), Sep 3, 1998: ACTUATOR. WORN. IAH - DURING FLIGHT 3778, CREW REPORTED THE LEFT HAND MAIN LANDING GEAR WAS SLOW TO RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOV - [SDR C2XA98IA396](https://openairdocs.org/sdr/C2XA98IA396), Aug 27, 1998: FUSE. FAILED. IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE FORWARD RIGHT FUSELAGE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE FOR T - [SDR C2XA98IA321](https://openairdocs.org/sdr/C2XA98IA321), Aug 24, 1998: ACTUATOR. OUT OF ADJUST. IAH - DURING FLT 3814, THE PILOT REPORTED THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT. MAINTENANCE FOUND THE LEFT MAIN GEAR ACTUATOR TO BE OUT OF ADJUSTMENT. T - [SDR C2XA98IA102](https://openairdocs.org/sdr/C2XA98IA102), Feb 26, 1998: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, THE NR 2 UPPER SKIN SUPPORT ON RIB 19 OF THE LEFT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED S - [SDR C2XA98IA068](https://openairdocs.org/sdr/C2XA98IA068), Feb 26, 1998: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRC - [SDR C2XA98IA067](https://openairdocs.org/sdr/C2XA98IA067), Feb 26, 1998: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAF - [SDR C2XA98IA066](https://openairdocs.org/sdr/C2XA98IA066), Feb 26, 1998: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT - [SDR C2XA98IA065](https://openairdocs.org/sdr/C2XA98IA065), Feb 26, 1998: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCR - [SDR C2XA98IA064](https://openairdocs.org/sdr/C2XA98IA064), Feb 26, 1998: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FORWARD SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE - [SDR C2XA98IA063](https://openairdocs.org/sdr/C2XA98IA063), Feb 26, 1998: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FORWARD FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIR - [SDR C2XA98IA062](https://openairdocs.org/sdr/C2XA98IA062), Feb 26, 1998: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRC - [SDR C2XA98IA061](https://openairdocs.org/sdr/C2XA98IA061), Feb 26, 1998: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE A - [SDR C2XA98IA060](https://openairdocs.org/sdr/C2XA98IA060), Feb 26, 1998: BRACKET. CRACKED. IAH - DURNG C-CHECK INSPECTION, THE NR 2 UPPER SKIN SUPPORT ON RIB 20 OF THE LEFT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SK - [SDR C2XA98IA059](https://openairdocs.org/sdr/C2XA98IA059), Feb 26, 1998: BRACKET. CRACKED. IAH - DURING C-CHECK INSPECTION, THE NR 1 UPPER SKIN SUPPORT ON RIB 20 FO THE LEFT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED S - [SDR C2XA98IA058](https://openairdocs.org/sdr/C2XA98IA058), Feb 26, 1998: T-PROFILE. CORRODED. IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER T-PROFILE AT FRAME 36 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EM - [SDR C2XA98IA057](https://openairdocs.org/sdr/C2XA98IA057), Feb 26, 1998: T-PROFILE. CORRODED. IAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB120 SR - [SDR C2XA98IA056](https://openairdocs.org/sdr/C2XA98IA056), Feb 26, 1998: CREASE BEAM. CORRODED. IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 39 TO 44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION O - [SDR C2XA98IA055](https://openairdocs.org/sdr/C2XA98IA055), Feb 26, 1998: STRAP. CORRODED. IAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 34 AND 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION - [SDR C2XA98IA054](https://openairdocs.org/sdr/C2XA98IA054), Feb 26, 1998: STRAP. CORRODED. IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 39 TO FRAME 40. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION - [SDR C2XA98IA053](https://openairdocs.org/sdr/C2XA98IA053), Feb 26, 1998: STRAP. CORRODED. IAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 39 TO FRAME 40. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION - [SDR C2XA98IA052](https://openairdocs.org/sdr/C2XA98IA052), Feb 26, 1998: STRINGER. CORRODED. IAH - DURING C-CHECK INSPECTION, STRINGER 21 LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 41 AND 42. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF ST - [SDR C2XA98IA051](https://openairdocs.org/sdr/C2XA98IA051), Feb 26, 1998: STRAP. CORRODED. IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 34 TO FRAME 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STR - [SDR C2XA98IA050](https://openairdocs.org/sdr/C2XA98IA050), Feb 26, 1998: T-PROFILE. CORRODED. IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER T-PROFILE AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EM - [SDR C2XA98IA049](https://openairdocs.org/sdr/C2XA98IA049), Feb 26, 1998: T-PROFILE. CORRODED. IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EM - [SDR C2XA98IA048](https://openairdocs.org/sdr/C2XA98IA048), Feb 26, 1998: T-PROFILE. CORRODED. IAH - DURING C-CHECK INSPECTION, THE LEFT T-PROFILE AT FRAME 15 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILER IAW EMB120 SR - [SDR C2XA98IA047](https://openairdocs.org/sdr/C2XA98IA047), Feb 26, 1998: BEAM. CORRODED. IAH - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 39 AND 40. MAINTENANCE REPAIRED THE AFFECTED AREA IAW CONTINENTAL - [SDR C2XA98IA046](https://openairdocs.org/sdr/C2XA98IA046), Feb 26, 1998: RIB. CRACKED. IAH - DURING C-CHECK INSPECTION, THE LEFT WING NOSE RIB NR 21 WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS ENGINEERIN - [SDR C2XA98IA045](https://openairdocs.org/sdr/C2XA98IA045), Feb 26, 1998: T-PROFILE. CORRODED. IAH - DURING C-CHECK INSPECTION, THE CENTER T-PROFILE AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB120 S - [SDR C2XA98IA044](https://openairdocs.org/sdr/C2XA98IA044), Feb 26, 1998: T-PROFILE. CORRODED. IAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB120 SR - [SDR C2XA98IA043](https://openairdocs.org/sdr/C2XA98IA043), Feb 26, 1998: BRACKET. CRACKED. IAH - DURING C-CHECK INSPECTION, THE NR 1 UPPER SKIN SUPPORT ON RIB 21 OF THE LEFT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED S - [SDR C2XA98IA042](https://openairdocs.org/sdr/C2XA98IA042), Feb 26, 1998: BRACKET. CRACKED. IAH - DURING C-CHECK INSPECTION, THE NR 3 UPPER SKIN SUPPORT ON RIB 21 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED - [SDR C2XA98IA041](https://openairdocs.org/sdr/C2XA98IA041), Feb 26, 1998: BRACKET. CRACKED. IAH - DURING C-CHECK INSPECTION, THE NR 2 UPPER SKIN SUPPORT ON RIB 21 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED - [SDR C2XA98IA040](https://openairdocs.org/sdr/C2XA98IA040), Feb 26, 1998: BRACKET. CRACKED. IAH - DURING C-CHECK INSPECTION, THE NR 1 UPPER SKIN SUPPORT ON RIB 21 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED - [SDR C2XA98IA039](https://openairdocs.org/sdr/C2XA98IA039), Feb 26, 1998: BRACKET. CRACKED. IAH - DURING C-CHECK INSPECTION, THE NR 3 UPPER SKIN SUPPORT ON RIB 20 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED - [SDR C2XA98IA038](https://openairdocs.org/sdr/C2XA98IA038), Feb 26, 1998: TRUNNION. CORRODED. IAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR SPRING BOX LOWER TRUNNION WAS FOUND TO BE PITTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TRUNNION - [SDR C2XA98IA037](https://openairdocs.org/sdr/C2XA98IA037), Feb 26, 1998: TRUNNION. CORRODED. IAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR STRUT SPRING BOX UPPER TRUNNION WAS FOUND TO BE PITTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TRU - [SDR C2XA98IA036](https://openairdocs.org/sdr/C2XA98IA036), Feb 26, 1998: PIN. CORRODED. IAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR TORQUE LINK LOWER PIVOT PIN WAS FOUND TO BE CORRODED IN SIDE THE ATTACH PIN HOLE. MAINTENANCE REMOVED AND - [SDR C2XA98IA035](https://openairdocs.org/sdr/C2XA98IA035), Feb 26, 1998: PIN. CORRODED. IAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR TORQUE LINK UPPER PIVOT PIN WAS FOUND TO BE CORRODED INSIDE THE ATTACH PIN HOLE. MAINTENANCE REMOVED AND - [SDR C2XA98IA013](https://openairdocs.org/sdr/C2XA98IA013), Feb 4, 1998: OIL COOLER. CRACKED. BTR - FLT 3865 - PILOT REPORTED AFTER DEPARTURE, THE NR 2 OIL PRESSURE WARNING LIGHT ILLUMINATED, FOLLOWED BY A FLUCTUATING OIL PRESSURE GAUGE WHICH THEN DROPPE - [SDR C2XA97CL080](https://openairdocs.org/sdr/C2XA97CL080), Oct 20, 1997: ENGINE. FAILED. ORF - FLT 3342 - CREW REPORTED THAT THE LEFT PROP RPM WENT TO 115 PERCENT DURING DESCENT, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT T - [SDR C2XA97CL028](https://openairdocs.org/sdr/C2XA97CL028), Mar 20, 1997: RELAY BOX. FAILED. CLE - FLT 3092 - CREW REPORTED, THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE LANDING GEAR SYSTEM - [SDR C2XA96CL003](https://openairdocs.org/sdr/C2XA96CL003), Jan 19, 1996: RELAY BOX. FAILED. CLE - FLT NR 3388 - THE CREW REPORTED THAT UPON GEAR RETRACTION THE MAIN LANDING GEAR FORWARD DOORS REMAINED OPEN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVE - [SDR C2XA96CL002](https://openairdocs.org/sdr/C2XA96CL002), Jan 18, 1996: UPLOCK ACTUATOR. OUT OF ADJUST. ABE - FLT NR 3321 - AFTER TAKEOFF AND GEAR RETRACTION, THE CREW REPORTED THAT THE GEAR DOOR REMAINED OPEN. MAINTENANCE INSPECTED AIRCRAFT AND ADJUSTED THE NOSE - [SDR C2XA95IA082](https://openairdocs.org/sdr/C2XA95IA082), May 18, 1995: RED GEARBOX. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND NR 1 ENGINE PROPELLER SHAFT FACE PITTED AND HEAVY RUST ON INSIDE OF PROPELLER SHAFT. MAINTENANCE REMOVED AND REPLACED THE - [SDR C2XA95IA081](https://openairdocs.org/sdr/C2XA95IA081), May 18, 1995: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERV - [SDR C2XA95IA079](https://openairdocs.org/sdr/C2XA95IA079), May 11, 1995: ANGLE. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN TO FRAME ATTACH ANGLE CRACKED AT BOTH ENDS, FRAME 44 BETWEEN STRINGERS NR 1 LEFT AND NR 1 RIGHT. MAINTENACN - [SDR C2XA95IA078](https://openairdocs.org/sdr/C2XA95IA078), May 11, 1995: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING RIB 15 3RD LOWER SKIN SUPPORT BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPR - [SDR C2XA95IA077](https://openairdocs.org/sdr/C2XA95IA077), May 11, 1995: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING RIB 15 4TH LOWER SKIN SUPPORT BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT AIRCRAFT APPRO - [SDR C2XA95IA076](https://openairdocs.org/sdr/C2XA95IA076), May 11, 1995: SUPPORT. CRACKED. IAH- DURING C-CHECK INSPECTION, FOUND LT WING RIB NR 16, 4TH LOWER SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT, AIRCRAFT APPROVED FOR RE All 53: https://openairdocs.org/deregistered/N16719-2000-01-14/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 19970607021819I](https://openairdocs.org/incident/19970607021819I), Jun 7, 1997: Emb EMB120ER (N16719), Cleveland, OH. Narrative: aircraft returned to Cleveland due to flight crew report of smoke in the cabin. Maintenance removed and replaced R-2 temp sensor and resistor (ref… - [Incident 19891203048719I](https://openairdocs.org/incident/19891203048719I), Dec 3, 1989: Emb EMB120RT (N16719), Houston, TX. Wake turbulence caused flight attendant to hit ceiling on approach. Briefly hospitalized with concussion. ## Other aircraft with N16719 - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N16719-undated): Piper J-2, S/N 727, built 1936. Owner: [Tuominen Eino L](https://openairdocs.org/faa-owner/TUOMINEN%20EINO%20L), [Floodwood, MN](https://openairdocs.org/faa-place/MN/Floodwood) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.