# Service difficulty reports: N248CA, cancelled Jan 12, 2007 A list on [N248CA, cancelled Jan 12, 2007](https://openairdocs.org/deregistered/N248CA-2007-01-12.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 · 56 reports - [SDR COMA0010370](https://openairdocs.org/sdr/COMA0010370.md): Channel · cracked · Sep 28, 2000 · N248CA · Emb EMB120RT · Passenger/Crew Doors > WHILE PERFORMING A SCHEDULED INSPECTION, IT WAS DISCOVERED THAT THE PAX DOOR CHANNEL NR 4 IS CRACKED (P/N 120-1658-001). REMOVED THE OLD CHANNEL AND INSTALLED A SERVICEABLE CHANNEL. - [SDR COMA0010369](https://openairdocs.org/sdr/COMA0010369.md): Channel · cracked · Sep 28, 2000 · N248CA · Emb EMB120RT · Passenger/Crew Doors > THE PAX DOOR VERTICAL CHANNEL (P/N 120-21057-003) BETWEEN NR 4 AND NR 5 STRINGERS IS CRACKED. REMOVED THE OLD CHANNEL AND INSTALLED A SERVICEABLE CHANNEL. - [SDR COMA0010368](https://openairdocs.org/sdr/COMA0010368.md): Channel · cracked · Sep 28, 2000 · N248CA · Emb EMB120RT · Passenger/Crew Doors > THE PAX DOOR NR 2 STRINGER FROM THE TOP END FWD SIDE IS CRACKED (P/N 120-21158-001). REMOVED THE OLD NR 2 STRINGER CHANNEL AND INSTALLED A SERVICEABLE STRINGER. - [SDR COMA0010367](https://openairdocs.org/sdr/COMA0010367.md): Channel · cracked · Sep 28, 2000 · N248CA · Emb EMB120RT · Passenger/Crew Doors > THE PAX DOOR VERTICAL CHANNEL (P/N 12024577-003) BETWEEN NR 5 AND NR 6 STRINGER IS CRACKED. REMOVED THE OLD CHANNEL AND INSTALLED A SERVICEABLE CHANNEL. - [SDR COMA0010330](https://openairdocs.org/sdr/COMA0010330.md): Battery · discharged · Sep 9, 2000 · N248CA · Emb EMB120RT · Emergency Lighting > FORWARD CABIN EMERGENCY LIGHTS WILL NOT REMAIN ILLUMINATED. REPLACED BATTERY. - [SDR COMA0010126](https://openairdocs.org/sdr/COMA0010126.md): Pump · leaking · May 29, 2000 · N248CA · Emb EMB120RT · Hydraulic Pump (Electric/Engine), Main > GREEN HYDRAULIC SYSTEM LOW PRESSURE AND LOW QUANTITY. REPLACED THE LEFT HAND ENGINE HYDRAULIC PUMP. - [SDR COMA0010058](https://openairdocs.org/sdr/COMA0010058.md): Sign · broken · Apr 25, 2000 · N248CA · Emb EMB120RT · Emergency Lighting > EXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN. - [SDR COMA0010050](https://openairdocs.org/sdr/COMA0010050.md): Warning Light · false indication · Mar 31, 2000 · N248CA · Emb EMB120RT · Central Warning > LOW OIL PRESSURE WARNING LIGHT ON MAP CAME ON. REPLACED THE MAP. - [SDR COMA9910189](https://openairdocs.org/sdr/COMA9910189.md): Battery · discharged · Dec 16, 1999 · N248CA · Emb EMB120RT · Emergency Lighting > EMERGENCY LIGHTS FWD OF ROW 4 WERE INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY. - [SDR COMA9910155](https://openairdocs.org/sdr/COMA9910155.md): Circuit Breaker · tripped · Sep 28, 1999 · N248CA · Emb EMB120RT · Central Warning > DURING TAKEOFF FROM MCO, THE AURAL TRIM WARNING ACTIVATED. FOUND THE AURAL WARNING CIRCUIT BREAKER TRIPPPED, RESET THE AURAL TRIM WARNING CIRCUIT BREAKER. - [SDR COMA9910108](https://openairdocs.org/sdr/COMA9910108.md): Bulb · failed · Jul 8, 1999 · N248CA · Emb EMB120RT · Emergency Lighting > OVERHEAD EMERGENCY LIGHT AT ROW 8 IS INOPERATIVE. REPLACED LIGHT BULB. - [SDR COMA9910065](https://openairdocs.org/sdr/COMA9910065.md): Bellcrank · cracked · Apr 22, 1999 · N248CA · Emb EMB120RT · Flight Compartment Windows > UPON REINSTALLATION OF THE PILOT'S DIRECT VISION WINDOW AFTER REPLACEMENT OF THE SEAL, FOUND AFT LOWER BELL CRANK TO BE CRACKED.25 INCH THROUGH WEB BY ROLLER. REMOVED AND REPLACED LOWER BELL CRANK AND RIGGED IAW EMB-120 MM CH 52-22-01. - [SDR COMA9810276](https://openairdocs.org/sdr/COMA9810276.md): Battery · discharged · Dec 6, 1998 · N248CA · Emb EMB120RT · Emergency Lighting > TWO EMERGENCY LIGHTS ARE INOPERABLE FORWARD CABIN SECTION. REPLACED EMERGENCY LIGHT BATTERY. - [SDR COMA9810249](https://openairdocs.org/sdr/COMA9810249.md): Box Control · malfunction · Nov 8, 1998 · N248CA · Emb EMB120RT · Landing Gear Retraction/Extension System > LANDING GEAR WILL NOT RETRACT. REPLACED LANDING GEAR CONTROL BOX. - [SDR COMA9810214](https://openairdocs.org/sdr/COMA9810214.md): Buttstrap · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 151-012 REVEALED LEFT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 STANDARD PRACTICES. - [SDR COMA9810213](https://openairdocs.org/sdr/COMA9810213.md): Buttplate · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 5310-131-01I REVEALED CENTER BUTTPLATE TO HAVE SPOTS OF CORROSION THAT WERE BEYOND LIMITS. REMOVED CENTER BUTTPLATE AND INSTALLED SERVICEABLE BUTTPLATE USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810212](https://openairdocs.org/sdr/COMA9810212.md): Buttstrap · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT FORWARD BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810211](https://openairdocs.org/sdr/COMA9810211.md): Buttstrap · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSEPCTION, TASK 151-012 REVEALED RIGHT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 STANDARD PRACTICES. - [SDR COMA9810210](https://openairdocs.org/sdr/COMA9810210.md): Crossbeam · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 5310-131-01I REVEALED RIGHT CENTER CROSSBEAM AT FRAME 16 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810209](https://openairdocs.org/sdr/COMA9810209.md): Crossbeam · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LT CROSSBEAM AT FRAME 14 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810208](https://openairdocs.org/sdr/COMA9810208.md): Crossbeam · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LT CENTER CROSSBEAM TO BE CORRODED AT FRAME 16. REMOVED AND REPLACED CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810207](https://openairdocs.org/sdr/COMA9810207.md): Crossbeam · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 5310-131-01I REVEALED RIGHT CROSSBEAM AT FRAME 16 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810206](https://openairdocs.org/sdr/COMA9810206.md): Crossbeam · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK5310-131-01I REVEALED LT CENTER CROSSBEAM TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810205](https://openairdocs.org/sdr/COMA9810205.md): Crossbeam · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK5310-131-01I REVEALED RT CROSSBEAM AT FRAME 20 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120SRM STANDARD PRACTICES. - [SDR COMA9810204](https://openairdocs.org/sdr/COMA9810204.md): Crossbeam · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK5320-141-03I REVEALED LT CENTER CROSSBEAM AT FRAME 23 TO BE HEAVILY CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810203](https://openairdocs.org/sdr/COMA9810203.md): Sill · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 163-012 REVEALED LEFT CARGO SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810202](https://openairdocs.org/sdr/COMA9810202.md): Sill · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT NR 1 SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810201](https://openairdocs.org/sdr/COMA9810201.md): Sill · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 5310-131-01I REVEALED RIGHT NR 1 SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810200](https://openairdocs.org/sdr/COMA9810200.md): Buttstrap · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 151-012 REVEALED LEFT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE PART USING EMB 120 STANDARD PRACTICES. - [SDR COMA9810199](https://openairdocs.org/sdr/COMA9810199.md): Buttstrap · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 5310-131-01I REVEALED CENTER NR 1 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810198](https://openairdocs.org/sdr/COMA9810198.md): Buttstrap · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 145-012 REVEALED LEFT NR 2 BUTTSTRAP TO BE CORRODED. REMOVED AND REPLACED BUTTSTRAP WITH SERVICEABLE ONE USING EMB 120 STANDARD PRATICES. - [SDR COMA9810197](https://openairdocs.org/sdr/COMA9810197.md): Buttstrap · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 151-012 REVEALED RIGHT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE ONE USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810196](https://openairdocs.org/sdr/COMA9810196.md): Buttstrap · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 151-012 REVEALED RIGHT NR 4 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE PART USING EMB 120SRM STANDARD PRACTICES. - [SDR COMA9810195](https://openairdocs.org/sdr/COMA9810195.md): Buttstrap · corroded · Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 145-012 REVEALED RIGHT NR 3 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED A SERVICEABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810173](https://openairdocs.org/sdr/COMA9810173.md): Indicator · malfunction · Aug 7, 1998 · N248CA · Emb EMB120RT · Cabin Pressure Control System > PRESSURIZATION SYSTEM DOES NOT WORK. REPLACED THE CABIN PRESSURE TRIPLE INDICATOR. - [SDR COMA9810157](https://openairdocs.org/sdr/COMA9810157.md): Current Sensor · failed · Jul 13, 1998 · N248CA · Emb EMB120RT · Airfoil Anti/De-ice System > CREW REPORTED F/O 'S AOA HEAT INOP. AVIONICS REPLACED THE RIGHT CURRENT SENSOR ASSEMBLY. UPON INSPECTION/TEARDOWN IN THE AVIONICS SHOP, THE CURRENT SENSOR FOR THE RIGHT AOA VANE HEAT WAS FOUND TO BE DAMGED BY SEVERE OVERHEATING. THE CURRENT SENSOR WAS REPLA - [SDR COMA9810152](https://openairdocs.org/sdr/COMA9810152.md): Battery · discharged · Jul 5, 1998 · N248CA · Emb EMB120RT · Emergency Lighting > EMERGENCY EXIT LIGHTS INOP AT ROW 4 AND 5. REPLACED EMERGENCY BATTERY. - [SDR COMA9810025](https://openairdocs.org/sdr/COMA9810025.md): Seal · torn · Jan 16, 1998 · N248CA · Emb EMB120RT · Cargo/Baggage Doors > AIRCRAFT WOULD NOT PRESURIZE AFTER TAKEOFF. REPLACED CARGO DOOR SEAL. - [SDR COMA9710479](https://openairdocs.org/sdr/COMA9710479.md): Battery · discharged · Nov 13, 1997 · N248CA · Emb EMB120RT · Emergency Lighting > FORWARD CABIN EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT BATTERY. - [SDR COMA9710418](https://openairdocs.org/sdr/COMA9710418.md): Warning Unit · malfunction · Sep 28, 1997 · N248CA · Emb EMB120RT · Central Warning > TAKEOFF, TRIM AURAL WARNING SOUNDED, TRIM WAS CONFIRMED TO BE IN TAKEOFF RANGE. REPLACED THE AURAL WARNING UNIT. - [SDR COMA9710408](https://openairdocs.org/sdr/COMA9710408.md): Control Module · malfunction · Sep 21, 1997 · N248CA · Emb EMB120RT · Landing Gear Selector > WITH THE LANDING GEAR IN UP POSITION, THE B-SYSTEM DISAGREE LIGHTS ILLUMINATED. CYCLED GEAR CONTROL AND INDICATIONS NORMAL. REPLACED THE LANDING GEAR CONTROL MODULE. - [SDR COMA9710322](https://openairdocs.org/sdr/COMA9710322.md): Engine · failed · Jul 2, 1997 · N248CA · Emb EMB120RT · Engine (Turbine/Turboprop) > LEFT ENGINE CHIP DETECTOR WARNING ON. REPLACED LEFT ENGINE. - [SDR COMA9710266](https://openairdocs.org/sdr/COMA9710266.md): Fuse · blown · May 4, 1997 · N248CA · Emb EMB120RT · Emergency Lighting > RT EXTERNAL OVERWING EMERGENCY LIGHT IS INOP. REPLACED THE NR 2 EMERGENCY BATTERY FUSE. - [SDR COMA9710239](https://openairdocs.org/sdr/COMA9710239.md): Cowl Door · separated · May 4, 1997 · N248CA · Emb EMB120RT · Engine Cowling System > LT ENGINE NACELLE AFT INBOARD COWLING DOOR SEPARATED AIRCRAFT AFTER TAKEOFF. REPLACED COWLING DOOR AND ASSOCIATED INTERMEDIATE COWLING ASSY DUE TO ADDITIONAL DAMAGE. - [SDR COMA9710233](https://openairdocs.org/sdr/COMA9710233.md): Battery · discharged · Apr 29, 1997 · N248CA · Emb EMB120RT · Emergency Lighting > FIVE LIGHTS IN THE EMERGENCY FLOOR PATH LIGHTING ARE INOP. REPLACED THE NR 2 BATTERY PACK. - [SDR COMA9710229](https://openairdocs.org/sdr/COMA9710229.md): Battery · discharged · Apr 29, 1997 · N248CA · Emb EMB120RT · Emergency Lighting > 4 WHITE AND 1 RED FLOOR EMERGENCY LIGHTS FAILED DURING TAXI-OUT. REPLACED NR 2 BATTERY PACK AT SEAT 4C LOCATION. - [SDR COMA9710087](https://openairdocs.org/sdr/COMA9710087.md): Accessory Gb · oil leak · Jan 24, 1997 · N248CA · Emb EMB120RT · Turbine Engine Accessory Drive > RT ENGINE OIL PRESSURE DROPPED TO 50 PERCENT DURING FLIGHT. ENGINE WAS FOUND TO BE 6 QUARTS LOW OIL LEVEL. REPLACED THE AGB BREATHER SEAL AND GEAR SHAFT. - [SDR COMA9610297](https://openairdocs.org/sdr/COMA9610297.md): Valve · defective · Oct 5, 1996 · N248CA · Emb EMB120RT · Aircraft Fuel Distribution System > AFTER TAKEOFF, THERE WAS A 1,500 LB FUEL IMBALANCE. AIRCRAFT RETURNED TO FIELD. REPLACED DEFECTIVE RIGHT WING FUEL PILOT VALVE. - [SDR COMA9610286](https://openairdocs.org/sdr/COMA9610286.md): Transfer Tube · not seated · Sep 23, 1996 · N248CA · Emb EMB120RT · Fuel Injector Nozzle > RT ENGINE LEAKING FUEL AND SMOKING AFTER SHUT DOWN. SECURED LOOSE FUEL TRANSFER TUBES ON THE NR 14 FUEL NOZZLE. - [SDR COMA9610285](https://openairdocs.org/sdr/COMA9610285.md): Tube · leaking · Sep 22, 1996 · N248CA · Emb EMB120RT · Engine Fuel Distribution > RT ENGINE LEAKING FUEL AND SMOKING AFTER SHUT DOWN. REPLACED LEAKING FUEL NOZZLE TRANSFER TUBE. Next page: https://openairdocs.org/deregistered/N248CA-2007-01-12/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 = 'N248CA' AND deregistration_id = 'N248CA-2007-01-12' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N248CA-2007-01-12/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.