# N462CA: 1992 Embraer EMB-120QC, registration cancelled 2013-09-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 3, 2013 - Exported to: South Africa - Status when cancelled: Valid registration - Airframe: [Embraer EMB-120QC](https://openairdocs.org/model/embraer-emb-120qc) (registry code 3260205) - 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: 120.264 - Year built: 1992 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: July 3, 1992 - Certificate issued: July 29, 2013 - Last registry action: July 29, 2013 - Mode S code: A5A13C - Owner when cancelled: [Jet Midwest Group LLC](https://openairdocs.org/faa-owner/JET%20MIDWEST%20GROUP%20LLC) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N462CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=462CA - Page: https://openairdocs.org/deregistered/N462CA-2013-09-03 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-120QC: https://openairdocs.org/model/embraer-emb-120qc.md ## Service difficulty reports (88, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FXGA20101214001](https://openairdocs.org/sdr/FXGA20101214001), Dec 14, 2010: SKIN. CHAFED. FUSELAGE SKIN CHAFED BY A FLEX DUCT AT FRAME 30(F/S 10172) AND STRINGER L18. REPAIRED IAW SRM 53-00-01. - [SDR COMA0210024](https://openairdocs.org/sdr/COMA0210024), Jun 4, 2002: BRAKE ASSY. FLIGHT 5064 DURING LANDING ALL 4 MLG TIRES BLEW OUT. REPLACED 4 MLG BRAKE ASSY, 4 MLG WHEEL AND TIRES. REPLACED BOTH BRAKE CONTROL VALVES FOR PREVENTIVE MAINT. - [SDR COMA0210014](https://openairdocs.org/sdr/COMA0210014), Apr 13, 2002: BRACKET. CRACKED. DUIRNG A 2,000 FLIGHT CYCLE INSPECTION, THE FUEL SHUT-OFF SUPPORT BRACKET (P/N 120-24373-002) ON THE RIGHT WING BOX FORWARD SIDE AFT OF FRAME 10 WAS FOUND TO BE - [SDR COMA0110161](https://openairdocs.org/sdr/COMA0110161), Dec 11, 2001: GAUGE. MALFUNCTIONED. FLIGHT 5070 R/H ENGINE TORQUE GAUGE FAILED DURING T/O.REPLACED THE TORQUE INDICATOR. - [SDR COMA0110132](https://openairdocs.org/sdr/COMA0110132), Aug 1, 2001: LIGHT. BROKEN. EMERGENCY LIGHT AT ROW 5 IS BROKEN.REPLACED LIGHT ASSY. - [SDR COMA0110081](https://openairdocs.org/sdr/COMA0110081), Mar 12, 2001: FLOOR SUPPORT. CRACKED. DURING 2C CHECK TASK 121-01Z, THE FUSELAGE LT FLOOR PROP AT FRAME 13 WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES - [SDR COMA0110080](https://openairdocs.org/sdr/COMA0110080), Mar 12, 2001: STRAP. CORRODED. DURING 2C CHECK TASK 141-01Z, THE FUSELAGE LT FLOORBEAM BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES A - [SDR COMA0110079](https://openairdocs.org/sdr/COMA0110079), Mar 12, 2001: CROSSBEAM. CORRODED. DURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FLOOR CROSSBEAM AT FRAME 15 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRAC - [SDR COMA0110078](https://openairdocs.org/sdr/COMA0110078), Mar 12, 2001: FLOORBEAM. CORRODED. DURING 2C CHECK TASK 152-01Z, THE FUSELAGE RT FLOOR T-SECTION AT FRAME 36 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRAC - [SDR COMA0110077](https://openairdocs.org/sdr/COMA0110077), Mar 12, 2001: SUPPORT. CRACKED. DURING 2C CHECK TASK 5720-552-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 21, BETWEEN FR ON SPAR AND STRINGERS 2A, WAS FOUND CRACKED. THE PART WAS REPLACED IN AC - [SDR COMA0110076](https://openairdocs.org/sdr/COMA0110076), Mar 12, 2001: SUPPORT. CRACKED. DURING 2C CHECK TASK 5720-552-01I, THE LT WING SUPPER SKIN SUPPORT AT RIB 20, BETWEEN STRINGERS 2A AND 3A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANC - [SDR COMA0110075](https://openairdocs.org/sdr/COMA0110075), Mar 12, 2001: SUPPORT. CRACKED. DURING 2C CHECK TASK 5720-552-01I, THE LT WING UPPER SUPPORT AT RIB 20, BETWEEN STRINGERS 3A AND 4A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH - [SDR COMA0110074](https://openairdocs.org/sdr/COMA0110074), Mar 12, 2001: SUPPORT. CRACKED. DURING 2C CHECK TASK 232-01Z, THE FUSELAGE RT SKIN SUPPORT AT FRAME 13A, STRINGER 14R WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM ST - [SDR COMA0110073](https://openairdocs.org/sdr/COMA0110073), Mar 12, 2001: SUPPORT. CRACKED. DURING 2C CHECK TASK 5310-221-05I, THE FUSELAGE LT SKIN SUPPORT BEHIND THE CAPTAIN''S DV WINDOW, BETWEEN FRAMES 12A AND 13, WAS FOUND CRCKED. THE PART WAS REPLA - [SDR COMA0110072](https://openairdocs.org/sdr/COMA0110072), Mar 12, 2001: SUPPORT. CRACKED. DURING 2C CHECK TASK 5310-221-05I, THE FUSELAGE LT SKIN SUPPORT BEHIND AND ABOVE THE CAPTAIN''S DV WINDOW, BETWEEN FRAMES 12A AND 13, WAS FOUND CRACKED. THE PAR - [SDR COMA0110071](https://openairdocs.org/sdr/COMA0110071), Mar 12, 2001: SUPPORT. CRACKED. DURING 2C CHECK TASK 261-01Z, THE FUSELAGE LT SKIN SUPPORT AT FRAME 40, BETWEEN STRINGERS 3L AND 4L, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH - [SDR COMA0110070](https://openairdocs.org/sdr/COMA0110070), Mar 12, 2001: FRAME. GOUGED. DURING 2C CHECK TASK 163-01Z, THE FUSELAGE FRAME 46A WAS FOUND TO BE GOUGED BY AN INTERIOR LINING SCREW AT FLOOR LEVEL ON THE LEFT SIDE. THE FRAME WAS REPAIRED - [SDR COMA0110069](https://openairdocs.org/sdr/COMA0110069), Mar 12, 2001: STRAP. CORRODED. DURING 2C CHECK TASK 162-01Z, THE FORWARD RT FLOORBEAM BUTTSTRAP IN THE CARGO COMPARTMENT, WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 - [SDR COMA0110068](https://openairdocs.org/sdr/COMA0110068), Mar 12, 2001: STRINGER. CRACKED. DURING 2C CHECK TASK 5410-432-04I, THE LEFT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE CRACKED JUST AFT OF NACELLE FRAME 10. THE STRINGER WAS REPLACED IN AC - [SDR COMA0110067](https://openairdocs.org/sdr/COMA0110067), Mar 12, 2001: STRAP. CORRODED. DURING 2C CHECK TASK 142-01Z, THE RT FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODES - [SDR COMA0110066](https://openairdocs.org/sdr/COMA0110066), Mar 12, 2001: FLOORBEAM. CORRODED. DURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FLOORBEAM T-SECTION AT FRAME 16 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD - [SDR COMA0110065](https://openairdocs.org/sdr/COMA0110065), Mar 12, 2001: SKIN. GOUGED. DURING 2 YEAR CORROSION CHECK TASK 5310-132-CO1E, THE FUSELAGE LOWER SKIN WAS FOUND TO BE GOUGED JUST BELOW THE LAV DUMP VALVE DOUBLER. THE SKIN WAS REPAIRED IN - [SDR COMA0110064](https://openairdocs.org/sdr/COMA0110064), Mar 12, 2001: SUPPORT. CRACKED. DURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SUPPORT AT RIB 23, BETWEEN STRINGERS 2A AND 3A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH - [SDR COMA0110063](https://openairdocs.org/sdr/COMA0110063), Mar 12, 2001: SUPPORT. CRACKED. DURING 2C CHECK TASK 5310-221-05I, THE LT FUSELAGE SKIN SUPPORT AT FRAME 9, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRA - [SDR COMA0110062](https://openairdocs.org/sdr/COMA0110062), Mar 12, 2001: STIFFENER. CRACKED. DURING 2C CHECK TASK 5410-442-04I, THE RT NACELLE FRAME 10 STIFFENER ANGLE, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRA - [SDR COMA0110061](https://openairdocs.org/sdr/COMA0110061), Mar 12, 2001: SHEAR TIE. CRACKED. DURING 2C CHECK TASK 5310-222-05I, THE RT FUSELAGE SKIN SUPPORT AT FRAME 9, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRA - [SDR COMA0110060](https://openairdocs.org/sdr/COMA0110060), Mar 12, 2001: SUPPORT. CRACKED. DURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 23, BETWEEN STRINGERS 3A AND 4A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE - [SDR COMA0110059](https://openairdocs.org/sdr/COMA0110059), Mar 12, 2001: FLOOR SUPPORT. CRACKED. DURING 2C CHECK TASK 122-01Z, THE FUSELAGE RT FLOOR PROP AT FRAME 13 WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES - [SDR COMA0110058](https://openairdocs.org/sdr/COMA0110058), Mar 12, 2001: SUPPORT. CRACKED. DURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 23, BETWEEN STRINGER 5A AND REAR SPAR, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCO - [SDR COMA0110057](https://openairdocs.org/sdr/COMA0110057), Mar 12, 2001: SUPPORT. CRACKED. DURING 2C CHECK TASK 5720-522-011, THE LT WING LOWER SKIN SUPPORT AT RIB 8, AND STRINGER 10, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 - [SDR COMA0110056](https://openairdocs.org/sdr/COMA0110056), Mar 12, 2001: CROSSBEAM. CORRODED. DURING 2C CHECK TASK 132-01Z, THE FUSELAGE RT FLOOR CROSSBEAM AT FRAME 16 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRAC - [SDR COMA0110055](https://openairdocs.org/sdr/COMA0110055), Mar 12, 2001: BEAM. CRACKED. DURING 2C CHECK TASK 811-02Z, THE PAX DOOR AFT LATERAL BEAM WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM 52-10-02, FIGURE 201. - [SDR COMA0110054](https://openairdocs.org/sdr/COMA0110054), Mar 12, 2001: FLOORBEAM. CORRODED. DURING 2C CHECK TASK 131/132-01Z, THE FUSELAGE CENTER FORWARD FLOOR OMEGA BEAM WAS FOUND CORRODED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 STANDARD PRA - [SDR COMA0110053](https://openairdocs.org/sdr/COMA0110053), Mar 12, 2001: STRAP. CORRODED. DURING 2C CHECK TASK 132-01Z, THE FUSELAGE RT FORWARD FLOOR BEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRA - [SDR COMA0110052](https://openairdocs.org/sdr/COMA0110052), Mar 12, 2001: SILL. CORRODED. DURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FORWARD FLOOR BEAM SILL WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICE - [SDR COMA0110051](https://openairdocs.org/sdr/COMA0110051), Mar 12, 2001: SILL. CORRODED. DURING 2C CHECK TASK 132-01Z, THE FUSELAGE RT FORWARD FLOORBEAM SILL WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES - [SDR COMA0110050](https://openairdocs.org/sdr/COMA0110050), Mar 12, 2001: STRAP. CORRODED. DURING 2C CHECK TASK 131/132-01Z, THE FUSELAGE CENTER FORWARD FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STAND - [SDR COMA0110048](https://openairdocs.org/sdr/COMA0110048), Mar 12, 2001: STRAP. CORRODED. DURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FORWARD FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRAC - [SDR COMA0110047](https://openairdocs.org/sdr/COMA0110047), Mar 12, 2001: STRAP. CORRODED. DURING 2C CHECK TASK 131/132-01Z, THE FUSELAGE CENTER FORWARD FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STAND - [SDR COMA0110046](https://openairdocs.org/sdr/COMA0110046), Mar 12, 2001: CHANNEL. CRACKED. DURING 2C CHECK TASK 811-02Z, THE PAX DOOR 3RD U-CHANNEL WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110045](https://openairdocs.org/sdr/COMA0110045), Mar 12, 2001: CHANNEL. CRACKED. DURING 2C CHECK TASK 811-02Z, THE PAX DOOR AFT U-CHANNEL WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110044](https://openairdocs.org/sdr/COMA0110044), Mar 12, 2001: CHANNEL. CRACKED. DURING 2C CHECK TASK 811-02Z, THE PAX DOOR 1ST U-CHANNEL WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110003](https://openairdocs.org/sdr/COMA0110003), Dec 31, 2000: RELAY. MALFUNCTIONED. LANDING GEAR WILL NOT RETRACT. REPLACED THE LANDING GEAR RELAY BOX. - [SDR COMA0010005](https://openairdocs.org/sdr/COMA0010005), Jan 7, 2000: RELAY. INOPERATIVE. EMERGENCY LIGHTS WILL NOT ARM. REPLACED RELAY KO201. - [SDR COMA9910100](https://openairdocs.org/sdr/COMA9910100), Jun 24, 1999: SIGN. MISSING. EMERGENCY EXIT SIGN ON BULKHEAD AT CABIN DOOR WAS MISSING. REPLACED EXIT SIGN ASSY. - [SDR COMA9910057](https://openairdocs.org/sdr/COMA9910057), Apr 6, 1999: WINDSHIELD. SHATTERED. PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. - [SDR COMA9810181](https://openairdocs.org/sdr/COMA9810181), Aug 27, 1998: FUEL LINE. CRACKED. WHILE REPLACING LEAKING RIVET IN RIGHT OUTBOARD WING, FOUND RE-FUEL LINE (P/N 120-08728-009) CRACKED AT BEND RADIUS. REPLACED CRACKED FUEL LINE. - [SDR COMA0810177](https://openairdocs.org/sdr/COMA0810177), Aug 15, 1998: BATTERY. DISCHARGED. EMERGENCY LIGHTS INOPERABLE. REPLACED BATTERY. - [SDR COMA9810154](https://openairdocs.org/sdr/COMA9810154), Jul 12, 1998: LAMP. FAILED. THREE EMERGENCY LIGHTS ARE INOP ROW 6 AND 7. REPLACED INOP LAMPS. - [SDR COMA9810135](https://openairdocs.org/sdr/COMA9810135), Jun 8, 1998: BATTERY. DISCHARGED. EMERGENCY LIGHTS AFT OF ROW 6 ARE INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERY. All 88: https://openairdocs.org/deregistered/N462CA-2013-09-03/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 20020604019629I](https://openairdocs.org/incident/20020604019629I), Jun 4, 2002: Emb EMB120RT (N462CA), Orlando, FL, Minor damage. (-23) On landing the aircraft blew 4 main landing gear tires on runway 17 at Orlando airport. Precautionary measure passengers deplaned on runway via entrance… - [Incident 19941026038819I](https://openairdocs.org/incident/19941026038819I), Oct 26, 1994: Emb EMB120RT (N462CA), Asheville, NC, Minor damage. Struck a deer on takeoff. Aborted takeoff safely. ## Other aircraft with N462CA - [Registered now](https://openairdocs.org/aircraft/N462CA): Cirrus Design SR22T, S/N 2462, built 2021 --- 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.