# Service difficulty reports: N463CA, cancelled Sep 6, 2013 A list on [N463CA, cancelled Sep 6, 2013](https://openairdocs.org/deregistered/N463CA-2013-09-06.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 92 reports - [SDR COMA0210027](https://openairdocs.org/sdr/COMA0210027.md): Roller · worn · Jun 17, 2002 · N463CA · Emb EMB120RT · Trailing Edge Flap Control System > FLIGHT 6043 FLAP DISAGREEMENT WARNING AFTER T/O.REPLACED WORN ROLLERS ON R/H OUTBD FLAP. - [SDR COMA0210026](https://openairdocs.org/sdr/COMA0210026.md): Generator · Jun 15, 2002 · N463CA · Emb EMB120RT · DC Generating System > FLIGHT 5067 #1 GENERATOR FAILED AFTER T/O.DEFERRED MAINT ON #1 GENERATOR PER MEL. - [SDR COMA0210022](https://openairdocs.org/sdr/COMA0210022.md): Engine · May 23, 2002 · N463CA · Emb EMB120RT · Turbine Engine Combustion Section > FLIGHT 5067 - DURING CRUISE FLIGHT, DESTINATION EYW THE RIGHT ENGINE WAS SHUT DOWN DUE TO LOSS OF OIL PRESSURE.REPLACED THE RIGHT ENGINE ASSEMBLY DUE TO HOT SECTION FAILURE. - [SDR COMA0210013](https://openairdocs.org/sdr/COMA0210013.md): Valve · malfunctioned · Apr 7, 2002 · N463CA · Emb EMB120RT · Cabin Cooling System > FLIGHT 5069 CABIN VERY HOT A/C SYSTEM NOT WORKING.REPLACED THE L/H TEMP CONTROL VALVE. - [SDR COMA0110159](https://openairdocs.org/sdr/COMA0110159.md): Gyro · Dec 3, 2001 · N463CA · Emb EMB120RT · Autopilot System > FLIGHT #5049 - AFTER T/O, RED FD FLAP ON PILOTS AND COPILOTS EADI.COULD NOT DUPLICATE. SYSTEM TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE. - [SDR COMA0110145](https://openairdocs.org/sdr/COMA0110145.md): Circuit Breaker · Sep 25, 2001 · N463CA · Emb EMB120RT · Battery Overheat Warning System > FLIGHT #5057. DURING PRE-FLIGHT CREW DISCOVERED THE CIRCUIT BREAKER FOR THE FLIGHT IDLE STOP SOLENOID TRIPPED.PERFOMRED RESET AND OPERATIONAL CHECK OF THE FLIGHT IDLE STOP CIRCUIT BREAKER. - [SDR COMA0110143](https://openairdocs.org/sdr/COMA0110143.md): Indicator · faulty · Sep 22, 2001 · N463CA · Emb EMB120RT · Power Indicating System > FLIGHT #5017. DURING TAKE OFF AT MCO THE LEFT ENGINE DIGITAL TORQUE INDICATION WAS INTERMITTENT, TAKE OFF WAS ABORTED AND REUTRNED TO THE GATE.REPLACED THE LEFT ENGINE TORQUE GAUGE. - [SDR COMA0110137](https://openairdocs.org/sdr/COMA0110137.md): Computer · faulty · Aug 29, 2001 · N463CA · Emb EMB120RT · Attitude and Direction Data System > FLIGHT #5005. DURING TAXI OUT RECEIVED A HEADING COMPUTER WARNING, AIRCRAFT RETURNED TO THE GATE.REPLACED THE AHC-85. - [SDR COMA0110130](https://openairdocs.org/sdr/COMA0110130.md): Sill · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 141-01Z, THE AFT LEFT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110129](https://openairdocs.org/sdr/COMA0110129.md): Skin · gouged · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, Plate/Skin > DURING 2 YEAR CORROSION CHECK TASK 5310-132-C01E, THE LOWER RH FUSELAGE SKIN WAS FOUND GOUGED JUST BELOW THE LAV DUMP VALVE DOUBLER. THE SKIN WAS REPAIRED PER EMBRAER SRM STANDARD PRACTICES AND REPAIR FAX GST-0992/01, DATED 3/28/01. - [SDR COMA0110128](https://openairdocs.org/sdr/COMA0110128.md): Stringer · dented · Apr 18, 2001 · N463CA · Emb EMB120RT · Nacelle/Pylon, Longeron/Stringer > DURING 2C-CHECK TASK 5410-442-04I, THE RIGHT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE DENTED BY THE GEAR DOOR TENSIONER. THE STRINGER WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND EMBRAER REPAIR GST-1034/01, DATED 3/30/01. - [SDR COMA0110127](https://openairdocs.org/sdr/COMA0110127.md): Support · cracked · Apr 18, 2001 · N463CA · Emb EMB120RT · Wing Miscellaneous Structure > DURING 2C-CHECK TASK 5710-652-01I, THE RIGHT WING UPPER SKIN SUPPORT ON RIB NR 21, BETWEEN STRINGERS NR 2 AND 3, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110126](https://openairdocs.org/sdr/COMA0110126.md): Skin · cracked · Apr 18, 2001 · N463CA · Emb EMB120RT · Trailing Edge Flaps > DURING 2C-CHECK (NO SPECIFIC TASK APPLIES), THE LEFT NACELLE FLAP LOWER SKIN WAS FOUND TO BE CRACKED AT ACCESS PANEL NR 436AB CUTOUT. THE NACELLE FLAP WAS REMOVED AND REPLACED PER EMB-120 MM 27-50-03. - [SDR COMA0110125](https://openairdocs.org/sdr/COMA0110125.md): Support · cracked · Apr 18, 2001 · N463CA · Emb EMB120RT · Wing Miscellaneous Structure > DURING 2C-CHECK 5720-552-01I, THE LEFT WING UPPER SKIN SUPPORT AT RIB NR 21, BETWEEN FRONT SPAR AND STRINGER NR 2, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REMOVED AND REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110124](https://openairdocs.org/sdr/COMA0110124.md): Support · cracked · Apr 18, 2001 · N463CA · Emb EMB120RT · Wing Miscellaneous Structure > DURING 2C-CHECK 5720-552-01I, THE LEFT WING UPPER SKIN SUPPORT AT RIB 21, BETWEEN STRINGER NR 2 AND 3, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REMOVED AND REPLACED PER EMB-120 SRM STANDRAD PRACTICES. - [SDR COMA0110123](https://openairdocs.org/sdr/COMA0110123.md): Floor Support · cracked · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 5310-121-01I, THE LEFT FUSELAGE FLOOR PROP AT FRAME NR 13 WAS FOUND TO BE CRACKED. THE FLOOR PROP WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3647-1, REV IR, 5-3-00. - [SDR COMA0110122](https://openairdocs.org/sdr/COMA0110122.md): Floor Support · cracked · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 5310-122-01I, THE RIGHT FUSELAGE FLOOR PROP AT FRAME NR 13 WAS FOUND TO BE CRACKED. THE FLOOR PROP WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3647-1, REV IR, 5-3-00. - [SDR COMA0110121](https://openairdocs.org/sdr/COMA0110121.md): Angle · cracked · Apr 18, 2001 · N463CA · Emb EMB120RT · Wing Miscellaneous Structure > DURING 2C-CHECK TASK 5320-243-01I, THE LEFT WING UPPER SKIN ATTACH ANGLE FOR FAIRING NR 193 WAS FOUND TO BE CRACKED. THE ANGLE WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 1126-21, REV IR, 7/6/99. - [SDR COMA0110120](https://openairdocs.org/sdr/COMA0110120.md): Shear Tie · cracked · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, Structure > DURING 2C-CHECK TASK 232-01Z, THE RIGHT FUSELAGE SKIN SUPPORT AT FRAME NR 13A AND STRINGER NR 14R, WAS FOUND TO BE CRACKED. THE SUPPORT WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3653-2, REV IR, 11/7/00. - [SDR COMA0110119](https://openairdocs.org/sdr/COMA0110119.md): Shear Tie · cracked · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, Structure > DURING 2C-CHECK TASK 221-01Z, THE LEFT FUSELAGE SKIN SUPPORT JUST BEHIND CAPTAIN''S DV WINDOW, BETWEEN FRAMES 12A AND 23, WAS FOUND TO BE CRACKED. THE SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110118](https://openairdocs.org/sdr/COMA0110118.md): Bracket · cracked · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 262-01Z, THE AFT CARGO DOOR TRACK UPPER MOUNTING BRACKET WAS FOUND TO BE CRACKED. THE BRACKET WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 1657-3, REV IR, 6/12/00. - [SDR COMA0110117](https://openairdocs.org/sdr/COMA0110117.md): Channel · cracked · Apr 18, 2001 · N463CA · Emb EMB120RT · Passenger/Crew Doors > DURING 2C-CHECK TASK 811-02Z, THE CHANNEL INSIDE THE PASSENGER DOOR WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110116](https://openairdocs.org/sdr/COMA0110116.md): Shear Tie · cracked · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, Structure > DURING 2C-CHECK TASK 221-01Z, THE FUSLEAGE SKIN SUPPORT ON LEFT SIDE OF COCKPIT AT FRAME NR 9 WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2/16/93. - [SDR COMA0110115](https://openairdocs.org/sdr/COMA0110115.md): Shear Tie · cracked · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, Structure > DURING 2C-CHECK TASK 222-01Z, THE FUSELAGE SKIN SUPPORT ON RIGHT SIDE OF COCKPIT AT FRAME NR 9 WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2/16/93. - [SDR COMA0110114](https://openairdocs.org/sdr/COMA0110114.md): Channel · cracked · Apr 18, 2001 · N463CA · Emb EMB120RT · Passenger/Crew Doors > DURING 2C-CHECK TASK 811-02Z, THE U-CHANNEL INSIDE THE PASSENGER DOOR WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110113](https://openairdocs.org/sdr/COMA0110113.md): Sill · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2-C CHECK TASK 164-01Z, THE AFT RIGHT FLOOR SUPPORT SILL INSIDE THE CARGO COMPARTMENT WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3661-1, REV IR, 5/15/00. - [SDR COMA0110112](https://openairdocs.org/sdr/COMA0110112.md): Sill · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 162-01Z, THE FORWARD RIGHT FLOOR SUPPORT SILL INSIDE THE CARGO COMPARTMENT WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110111](https://openairdocs.org/sdr/COMA0110111.md): Strap · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2-C CHECK TASK 152-01Z, THE AFT RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110110](https://openairdocs.org/sdr/COMA0110110.md): Strap · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2-C CHECK TASK 152-01Z, THE AFT RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110109](https://openairdocs.org/sdr/COMA0110109.md): Strap · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 151/152-01Z, THE AFT CENTER FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PACTICES. - [SDR COMA0110108](https://openairdocs.org/sdr/COMA0110108.md): Strap · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 151-01Z, THE AFT LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110107](https://openairdocs.org/sdr/COMA0110107.md): Strap · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 141-01Z, THE LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110106](https://openairdocs.org/sdr/COMA0110106.md): Strap · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 141-01Z, THE LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110105](https://openairdocs.org/sdr/COMA0110105.md): Strap · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110104](https://openairdocs.org/sdr/COMA0110104.md): Strap · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EM-120 SRM STANDARD PRACTICES. - [SDR COMA0110103](https://openairdocs.org/sdr/COMA0110103.md): Sill · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110102](https://openairdocs.org/sdr/COMA0110102.md): Sill · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110101](https://openairdocs.org/sdr/COMA0110101.md): Support · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 243-01Z, THE LEFT SIDEWALL SUPPORT SECTION INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SUPPORTING SECTION WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110100](https://openairdocs.org/sdr/COMA0110100.md): Strap · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 132-01Z, THE RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110099](https://openairdocs.org/sdr/COMA0110099.md): Strap · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 131/132-01Z, THE CENTER FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110098](https://openairdocs.org/sdr/COMA0110098.md): Strap · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 131-01Z, THE LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110097](https://openairdocs.org/sdr/COMA0110097.md): Strap · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 131-01Z, THE FORWARD LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER SRM STANDARD PRACTICES AND AERODESIGN REPORT 1671-2, REV IR 12/4/96. - [SDR COMA0110096](https://openairdocs.org/sdr/COMA0110096.md): Strap · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 131/132-01Z, THE FORWARD CENTER FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICE AND AERODESIGN REPORT 1671-1, REV A, 1/28/97. - [SDR COMA0110095](https://openairdocs.org/sdr/COMA0110095.md): Sill · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 132-01Z, THE FOWARD RIGHT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110094](https://openairdocs.org/sdr/COMA0110094.md): Support · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 232-01Z, THE FORWARD RIGHT SIDEWALL SEAT TRACK SUPPORT INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110093](https://openairdocs.org/sdr/COMA0110093.md): Support · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 242-01Z, THE RIGHT SIDEWALL SEAT TRACK SUPPORT INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110092](https://openairdocs.org/sdr/COMA0110092.md): Floorbeam · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, Floor Beam > DURING 2C-CHECK TASK 131-01Z, THE FORWARD LEFT FLOOR SUPPORT T-SECTION AT FRAME 16 INSIDE THE CABIN,WAS FOUND TO BE CORRODED. THE T-SECTION WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110091](https://openairdocs.org/sdr/COMA0110091.md): Crossbeam · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 151-01Z, THE LEFT FLOOR SUPPORT CROSSBEAM AT FRAME 36, INSIDE THE CABIN, WAS FOUND TO BE CORRODED. THE CROSSBEAM WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110090](https://openairdocs.org/sdr/COMA0110090.md): Door Frame · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Passenger/Crew Doors > DURING 2C-CHECK TASK 811-02Z, THE PASSENGER DOOR LOWER LONGITUDINAL FRAME, WAS FOUND TO BE CORRODED. THE FRAME WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110089](https://openairdocs.org/sdr/COMA0110089.md): Angle · corroded · Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C-CHECK TASK 131/132-01Z, THE FUSELAGE FORWARD FLOOR SUPPORTING Z-SECTION AT FRAME 13 WAS FOUND TO BE CORRODED. THE Z-SECTION WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. Next page: https://openairdocs.org/deregistered/N463CA-2013-09-06/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N463CA' AND deregistration_id = 'N463CA-2013-09-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N463CA-2013-09-06/reports --- 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.