# Service difficulty reports: N247CA, cancelled Aug 13, 2025 A list on [N247CA, cancelled Aug 13, 2025](https://openairdocs.org/deregistered/N247CA-2025-08-13.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 · 60 reports - [SDR COMA0010314](https://openairdocs.org/sdr/COMA0010314.md): Channel · cracked · Aug 3, 2000 · N247CA · Emb EMB120RT · Passenger/Crew Doors > UPON COMPLIANCE OF 1C-CHECK TASK 52-14, THE PASSENGER DOOR INNER CHANNEL WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACCORDANCE WITH EMB-120 STUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010313](https://openairdocs.org/sdr/COMA0010313.md): Bulkhead · cracked · Aug 3, 2000 · N247CA · Emb EMB120RT · Nacelle/Pylon, Bulkhead/Firewall > UPON COMPLIANCE OF 1C-CHECK TASK 433-01Z, THE LEFT NACELLE FRAME 14 EXHAUST PAN SUPPORT BULKHEAD WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACCORDANCE WITH EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 33712-1, IR-7-2 - [SDR COMA0010312](https://openairdocs.org/sdr/COMA0010312.md): Skin · gouged · Aug 3, 2000 · N247CA · Emb EMB120RT · Fuselage Main, Plate/Skin > UPON COMPLIANCE OF 1C-CHECK TASK 100-01Z, THE FUSELGE FWD LOWER RT SKIN JUST BELOW LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR NR SST-18 - [SDR COMA0010311](https://openairdocs.org/sdr/COMA0010311.md): Skin · dented · Aug 3, 2000 · N247CA · Emb EMB120RT · Fuselage Main, Plate/Skin > UPON COMPLIANCE OF 1C-CHECK TASK 5310-122-01E, THE FUSELAGE RT FWD LOWER SKIN WAS FOUND TO BE DENTED. THE DAMAGED PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMB120 SRM 53-00-01, FIGURE 201. - [SDR COMA0010310](https://openairdocs.org/sdr/COMA0010310.md): Shear Tie · cracked · Aug 3, 2000 · N247CA · Emb EMB120RT · Fuselage Main, Structure > WHILE PERFORMING OTHER MAINTENANCE, THE FUSELAGE LEFT HAND SKIN SUPPORT AT FRAME 9, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1, IR, 2-16-93. - [SDR COMA0010309](https://openairdocs.org/sdr/COMA0010309.md): Skin · gouged · Aug 3, 2000 · N247CA · Emb EMB120RT · Cargo/Baggage Doors > UPON COMPLIANCE OF 1C-CHECK TASK 813-01Z THE CARGO DOOR SKIN WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMB-120 SRM 52-30-01, FIGURE 201. - [SDR COMA0010308](https://openairdocs.org/sdr/COMA0010308.md): Angle · cracked · Aug 3, 2000 · N247CA · Emb EMB120RT · Wing Miscellaneous Structure > UPON COMPLIANCE OF 1C-CHECK TASK 194-01Z THE RIGHT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 194 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, IR, - [SDR COMA0010307](https://openairdocs.org/sdr/COMA0010307.md): Angle · cracked · Aug 3, 2000 · N247CA · Emb EMB120RT · Wing Miscellaneous Structure > UPON COMPLIANCE OF 1C-CHECK TASK 193-01Z, THE LEFT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, IR, - [SDR COMA0010306](https://openairdocs.org/sdr/COMA0010306.md): Skin · damaged · Aug 3, 2000 · N247CA · Emb EMB120RT · Wing, Plate/Skin > UPON COMPLIANCE OF 1C-CHECK TASK 5720-622-02E, THE RIGHT WING LOWER SKIN RIVET HOLE AT RIB 6, STRINGER 10 WAS FOUND TO BE IMPROPERLY COUNTERSUNK. THE DAMAGED SKIN WAS REPAIRED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESI - [SDR COMA0010305](https://openairdocs.org/sdr/COMA0010305.md): Strap · corroded · Aug 3, 2000 · N247CA · Emb EMB120RT · Fuselage Miscellaneous Structure > WHILE PERFORMING OTHER MAINTENANCE, THE FUSELAGE FORWARD CENTER CABIN FLOOR BEAM BUTT-STRAP WAS FOUND TO BE CORRODED. THE BUTT-STRAP WAS REPLACED IN ACCORDANCE WITH THE EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010202](https://openairdocs.org/sdr/COMA0010202.md): Battery · discharged · Jun 17, 2000 · N247CA · Emb EMB120RT · Emergency Lighting > EMERGENCY FLOOR PATH LIGHTING IS INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY. - [SDR COMA0060258](https://openairdocs.org/sdr/COMA0060258.md): Boot · leaking · Mar 11, 2000 · N247CA · Cndair CL6002B19 · Airfoil Anti/De-ice System > WING DE-ICE FAIL WARNING. REPLACED THE RIGHT WING INBOARD DE-ICE BOOT. - [SDR COMA0010028](https://openairdocs.org/sdr/COMA0010028.md): Battery · discharged · Feb 20, 2000 · N247CA · Emb EMB120RT · Emergency Lighting > CABIN EMERGENCY LIGHT SYSTEM WAS PARTIALLY INOP. REPLACED EMERGENCY BATTERY. - [SDR COMA0010026](https://openairdocs.org/sdr/COMA0010026.md): Battery · discharged · Feb 16, 2000 · N247CA · Emb EMB120RT · Emergency Lighting > 5 EXIT LIGHTS ON FLOOR AND 1 ON OVERHEAD ARE INOPERABLE. REPLACED THE NR 1 AND NR 2 EMERGENCY BATTERIES. - [SDR COMA9910198](https://openairdocs.org/sdr/COMA9910198.md): Sign · inoperative · Dec 25, 1999 · N247CA · Emb EMB120RT · Emergency Lighting > EMERGENCY EXIT SIGN AT ROW 8 IS INOPERABLE. REPAIRED DAMAGED WIRES AT EXIT SIGN. - [SDR COMA9910190](https://openairdocs.org/sdr/COMA9910190.md): Controller · malfunctioned · Dec 15, 1999 · N247CA · Emb EMB120RT · Propeller Controlling System > RT PROPELLER RPM WAS 99.2 TO 99.6 AFTER TAKEOFF. GROUND RUNS SHOWED PROPELLER RPM TO BE IN LIMITATIONS. - [SDR COMA9910184](https://openairdocs.org/sdr/COMA9910184.md): Rccb · failed · Dec 14, 1999 · N247CA · Emb EMB120RT · Propeller/Rotor Anti-Ice/De-Ice System > RIGHT HAND PROPELLER DEICE FAIL WARNING. REPLACED RCCB (CB0226). - [SDR COMA9910169](https://openairdocs.org/sdr/COMA9910169.md): Light · inop · Oct 29, 1999 · N247CA · Emb EMB120RT · Emergency Lighting > FWD EMERGENCY FLOOR LIGHT WAS INOP. REPLACED LIGHT ASSY. - [SDR COMA9910149](https://openairdocs.org/sdr/COMA9910149.md): Warning · activated · Sep 19, 1999 · N247CA · Emb EMB120RT · Door Warning System > SERVICE DOOR WARNING DURING TAKEOFF. DOOR WARNING SYSTEM PREVIOUSLY DEFERRED PER MEL. - [SDR COMA9910150](https://openairdocs.org/sdr/COMA9910150.md): Warning · activated · Sep 18, 1999 · N247CA · Emb EMB120RT · Door Warning System > SERVICE DOOR WARNING DURING TAKEOFF. DEFERRED DOOR WARNING SYSTEM PER MEL. - [SDR COMA9910084](https://openairdocs.org/sdr/COMA9910084.md): Sensor · failed · May 25, 1999 · N247CA · Emb EMB120RT · Landing Gear Position and Warning > LEFT MLG DOWN INDICATOR ON WITH GEAR RETRACTED. LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. FREE FALL SYSTEM USED TO EXTEND GEAR. REPLACED DOWN LOCK PROXIMITY SENSOR. (M) - [SDR COMA9910034](https://openairdocs.org/sdr/COMA9910034.md): Deice · inop · Feb 16, 1999 · N247CA · Emb EMB120RT · Propeller Deice Boot Section > RIGHT HAND PROPELLER DEICE IS INOPERABLE. REPLACED THE NR 3 BLADE ON RIGHT HAND PROPELLER. - [SDR COMA9910026](https://openairdocs.org/sdr/COMA9910026.md): Frame · cracked · Feb 2, 1999 · N247CA · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/Rib > LEFT NACELLE, FRAME WEB NR 10 CRACKED AT INBOARD RADIUS OF THE FLANGE. REPAIRED BY SPLICING IN A NEW FLANGE PER AERODESIGN REPORT NR 1076-2 AND EMB120 SRM 51-40-02. - [SDR COMA9910025](https://openairdocs.org/sdr/COMA9910025.md): Battery Pack · discharged · Jan 27, 1999 · N247CA · Emb EMB120RT · Emergency Lighting > FORWARD SECTION OF CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK FOR THE FORWARD EMERGENCY LIGHTING. - [SDR COMA9910005](https://openairdocs.org/sdr/COMA9910005.md): Contactor · failed · Jan 3, 1999 · N247CA · Emb EMB120RT · External Power System > EXTERNAL POWER CONTACTOR BURNT/OVERHEATED AT TERMINAL ENDS. REPLACED CONTACTOR AND POSITIVE CABLE. - [SDR COMA9810277](https://openairdocs.org/sdr/COMA9810277.md): Fastener · broken · Dec 2, 1998 · N247CA · Emb EMB120RT · Fluid Service Doors > SERVICE DOOR WARNING DURING TAKEOFF. REPLACED BROKEN CAM LOCK FASTENER ON SINGLE POINT FUEL SERVICE DOOR. - [SDR COMA9810274](https://openairdocs.org/sdr/COMA9810274.md): Sensor · malfunctioned · Dec 1, 1998 · N247CA · Emb EMB120RT · Landing Gear Position and Warning > AFTER LANDING GEAR RETRACTED, RIGHT HAND MLG DOWN INDICATOR REMAINED ON. REPLACED DEFECTIVE DOWNLOCK PROXIMITY SENSOR. - [SDR COMA9810270](https://openairdocs.org/sdr/COMA9810270.md): Latch · not secured · Nov 18, 1998 · N247CA · Emb EMB120RT · Service Doors > SERVICE DOOR WARNING DURING CLIMBOUT. AIRCRAFT RETURNED TO THE FIELD. CLOSED DOOR AND SECURED LATCH. - [SDR COMA9810238](https://openairdocs.org/sdr/COMA9810238.md): Pin · not removed · Oct 19, 1998 · N247CA · Emb EMB120RT · Landing Gear Retraction/Extension System > NOSE LANDING GEAR WOULD NOT RETRACT. REMOVED NLG PIN. GEAR SWINGS GOOD. - [SDR COMA9810235](https://openairdocs.org/sdr/COMA9810235.md): Crossbeam · corroded · Oct 8, 1998 · N247CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT CENTER CROSSBEAM TO BE CORRODED AT FRAME 16. REMOVED AND REPLACED CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810233](https://openairdocs.org/sdr/COMA9810233.md): Sill · corroded · Oct 8, 1998 · N247CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT NR 1 STILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810232](https://openairdocs.org/sdr/COMA9810232.md): Sill · corroded · Oct 8, 1998 · N247CA · 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 COMA9810231](https://openairdocs.org/sdr/COMA9810231.md): Buttstrap · corroded · Oct 8, 1998 · N247CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 151-01Z REVEALED LEFT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 STANDARD PRACTICES. - [SDR COMA9810230](https://openairdocs.org/sdr/COMA9810230.md): Buttstrap · corroded · Oct 8, 1998 · N247CA · 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 COMA9810229](https://openairdocs.org/sdr/COMA9810229.md): Wire Harness · out of position · Oct 7, 1998 · N247CA · Emb EMB120RT · Fuel System Wiring > DURING 2C INSPECTION, TASK 5720-622-01I, REVEALED THE WIRE HARNESS FOR THE RIGHT WING FORWARD FUEL BOOST PUMP TO BE CHAFFING ON THE METAL BRAIDED FUEL LINE. PUMP WIRE INSULATION WAS NOT DAMAGED ONLY WIRE HARNESS PROTECTIVE COVERING. REMOVED PUMP AND HARNESS - [SDR COMA9810236](https://openairdocs.org/sdr/COMA9810236.md): Buttplate · corroded · Oct 6, 1998 · N247CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131-O1I REVEALED CENTER BUTTPLATE TO HAVE SPOTS OF CORROSION THAT WERE BEYOND LIMITS. REMOVED CENTER BUTTPLATE AND INSTALLED SERVICEABLE BUTTPLATE USING EMB120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 1671-1. - [SDR COMA9810172](https://openairdocs.org/sdr/COMA9810172.md): Wheel · cracked · Aug 10, 1998 · N247CA · Emb EMB120RT · Wheel/Ski/Float > DURING TEARDOWN VISUAL INSPECTION FOR TIRE CHANGE, THE INNER HALF OF THE MAIN WHEEL ASSY WAS FOUND TO HAVE A CRACK APPROXIMATELY 2 INCHES IN LENGTH RUNNING INWARD IN THE WEB AREA, STARTING FROM UNDER THE BEARING CUP. THE WHEEL WAS REMOVED FROM SERVICE AT THIS - [SDR COMA9810123](https://openairdocs.org/sdr/COMA9810123.md): Battery · discharged · May 17, 1998 · N247CA · Emb EMB120RT · Emergency Lighting > SOME OF THE CABIN EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY. - [SDR COMA9710506](https://openairdocs.org/sdr/COMA9710506.md): Wire · broken · Dec 23, 1997 · N247CA · Emb EMB120RT · Light System Wiring > SOME OF THE CABIN FLOOR PATH EMERGENCY LIGHTS ARE INOP. REPAIRED BROKEN WIRE. - [SDR COMA9710316](https://openairdocs.org/sdr/COMA9710316.md): Fuel Door · not latched · Jun 17, 1997 · N247CA · Emb EMB120RT · Fluid Service Doors > SERVICE DOOR WARNING CAME ON AFTER TAKEOFF. SINGLE POINT FUEL SERVICE DOOR NOT LATCHED. SECURED DOOR AND AIRCRAFT RETURNED TO SERVICE. - [SDR COMA9710089](https://openairdocs.org/sdr/COMA9710089.md): Roller · dirty · Jan 26, 1997 · N247CA · Emb EMB120RT · Trailing Edge Flaps > FLAP DISAGREEMENT AFTER FLAPS SELECTED TO 0 DEGREES. REPLACED FLAP ROLLERS ON LEFT AND RIGHT OUTBOARD FLAPS. - [SDR COMA9710013](https://openairdocs.org/sdr/COMA9710013.md): Relay · failed · Dec 30, 1996 · N247CA · Emb EMB120RT · Emergency Lighting > EMERGENCY LIGHTING NOT ARMED WARNING ON MAP, CIRCUIT BREAKER TRIPPED. COULD NOT DUPLCIATE DISCREPANCY. REPLACED RELAY K201 FOR TROUBLESHOOTING. - [SDR COMA9610401](https://openairdocs.org/sdr/COMA9610401.md): Tubing · chafed · Dec 15, 1996 · N247CA · Emb EMB120RT · Hydraulic System, Main > HYDRAULIC FLUID LEAKING FROM LT ENGINE NACELLE. REPLACED DAMAGED SECTION OF GREEN SYSTEM HYDRAULIC PRESSURE TUBING BETWEEN NACELLE 13 AND 14. - [SDR COMA9610334](https://openairdocs.org/sdr/COMA9610334.md): Potentiometer · malfunction · Nov 20, 1996 · N247CA · Emb EMB120RT · Landing Gear Steering System > CLUNKING SOUND AND UNCOMMANDED MOVEMENT FROM NOSE WHEEL STEERING SYSTEM. REPLACED THE NWS FEEDBACK POTENTIOMETER. - [SDR COMA9610288](https://openairdocs.org/sdr/COMA9610288.md): Switch · out of adjust · Sep 26, 1996 · N247CA · Emb EMB120RT · Door Warning System > CARGO DOOR WARNING SOUNDED DURING TAKEOFF. ADJUSTED CARGO DOOR MICROSWITCH. AIRCRAFT CONTINUED SERVICE. - [SDR COMA9610223](https://openairdocs.org/sdr/COMA9610223.md): Controller · failed · Jul 12, 1996 · N247CA · Emb EMB120RT · ATC Transponder System > TRANSPONDER NR 1 AND NR 2 REPORTED INOPERATIVE BY AIR TRAFFIC CONTROL. REPLACED CTL-92. - [SDR COMA9610225](https://openairdocs.org/sdr/COMA9610225.md): Fuel Nozzle · leaking · Jul 11, 1996 · N247CA · Emb EMB120RT · Fuel Injector Nozzle > FUEL LEAKING FROM RT ENGINE NACELLE. REPLACED THE RT ENGINE FUEL NOZZLES. - [SDR COMA9610166](https://openairdocs.org/sdr/COMA9610166.md): Sensor · defective · Jun 4, 1996 · N247CA · Emb EMB120RT · Landing Gear Retraction/Extension System > WHEN LANDING GEAR SELECTED DOWN, GEAR DID NOT EXTEND. INDICATION WAS 5 RED INTRANSIT AND ONE GREEN DOWNLOCK. EMERGENCY SYSTEM USED TO EXTEND GEAR. REPLACED DEFECTIVE DOWNLOCK PROXIMITY SENSOR ON LEFT MLG. - [SDR COMA9610154](https://openairdocs.org/sdr/COMA9610154.md): Latch · broken · May 27, 1996 · N247CA · Emb EMB120RT · Landing Gear Door Retract Section > RIGHT MLG OUTBOARD GEAR DOOR WILL NOT CLOSE. REPLACED BROKEN DOOR LATCH ASSY. - [SDR COMA9610145](https://openairdocs.org/sdr/COMA9610145.md): Prop Contl Unit · malfunction · May 14, 1996 · N247CA · Emb EMB120RT · Propeller Controlling System > LEFT PROPELLER TAKES 30 SECONDS TO TRANSITION FROM FEATHER TO BETA RANGE. REPLACED THE PROPELLER CONTROL UNIT. Next page: https://openairdocs.org/deregistered/N247CA-2025-08-13/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 = 'N247CA' AND deregistration_id = 'N247CA-2025-08-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N247CA-2025-08-13/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.