N665BC
Service difficulty reports · 148
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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 = 'N665BC' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = 'N665BC' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SIMA20141215002Frame · chafedFRAME 15 IS CHAFED AT STRINGER 2R. COMPLIED WITH REPAIR TO FRAME 15 AT STRINGER 2R IAW ERS-EM-53MR-944.SDR SIMA20141213005Bushing · corrodedRUDDER 2 UPPER HINGE FITTING HAS CORRODED HAT BUSHINGS, FOUND BORE DAMAGED. INSTALLED NEW RUDDER 2 UPPER HINGE FITTING ASSEMBLY IAW SRM 55-40-02 & ETN EM-55-070. REPLACED BOTH SLEEVE BUSHINGS & BOLT WITH NEW IAW IPC 27-21-02.SDR SIMA20141211005Skin · crackedLEFT REAR FUSELAGE SKIN NR 2 HAS CRACKS BY THE RIVET AT FRAME 78 BETWEEN STRINGERS 3L - 4L. REPAIRED DAMAGE AT FRAME 78, STRINGER 3L - 4L IAW ERS-EM-5300-960.SDR SIMA20141211006Skin · crackedRIGHT REAR FUSELAGE SKIN NR 2 HAS CRACK BY THE RIVET AT FRAME 79 JUST BELOW STRINGER 6R. COMPLETED DOUBLER REPAIR TO SKIN AT FRAME 79 RT IAW ERS-EM-5300-959.SDR SIMA20141210012Support Fitting · crackedFRAME 80 LT STRINGER 8L SUPPORT CLIP IS CRACKED. R & R SHEAR CLIP IAW SRM 51-40-02.SDR SIMA20141210016Profile · crackedREAR ELECTRONICS COMPARTMENT DOOR UPPER PROFILE CRACKED UNDER DOOR SUPPORT BRACKET. REPAIRED REAR ELECTRONICS COMPARTMENT DOOR UPPER PROFILE UNDER DOOR SUPPORT BRACKET IAW ERS-EM-5200-262.SDR SIMA20141210015Attach Angle · crackedRIGHT OVERWING FUSELAGE PANEL UPPER ATTACH ANGLE AFT END HAS SHEARED RIVETS & IS CRACKED. REPAIRED RT OVERWING FUSELAGE PANEL UPPER ATTACH ANGLE IAW SRM 53-23-12 ITEM 3 TYPE 1 REPAIR.SDR SIMA20141210014Support Bracket · crackedCARGO DOOR ASSIST CABLE ROD SUPPORT BRACKET IS CRACKED ON THE FRONT END AT FRAME 61 RT. R & R CARGO DOOR ASSIST CABLE ROD SUPPORT BRACKET AT FRAME 61 RT IAW SRM 51-40-02.SDR SIMA20141210013Support Fitting · corrodedFRAME 80 RT STRINGER 8R SUPPORT CLIP IS CRACKED. INSTALLED A NEW SUPPORT CLIP IAW SRM 51-40-02.SDR SIMA20141124004Wire Harness · chafedIN FLIGHT AFTER EXITING ICING CONDITION E2 ANTI-ICE FAIL WITH VLV IN OPEN POS, SHOULD HAVE CLOSED. RESET IAW AOM VOL 1 PROC TESTED ANTI-ICE IN ALL E2 ANTI-ICE FAIL MSG. VLV WOULD NOT OPEN. LATER IN FLT E2 ANTI-ICE VLV OPENED UNCOMMANDED WITH ELECTOR IN AUTOSDR SIMA20141122001Anti-Ice Valve · malfunctionedON TAKEOFF ROLL HAD EICAS CAUTION MSGS E2 ANTI-ICE FAIL, PACK 2 OVERHEAT THEN AS ABORT WAS CALLED, EICAS WARNING OF SPS 1-2 INOPERATIVE. BEFORE ABORT WAS COMPLETE WE HAD COME PAST 80KTS THRESHOLD. ALL MSGS CLEARED AS ACFT CLEARED RUNWAY. TRANSFERRED TO NRWCSDR SIMA20141011006Light · inoperativeLEFT EXTERNAL OVERWING EMER LAMP INOPERATIVE. R & R IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.SDR SIMA20140726002Packing · leakingSMOKE & HYD FLUID ON ON LT MAIN GEAR. R & R BLEEDER VLV PACKING IAW CMM 32-49-03. OPERATIONS CHECKED GOOD IAW AMM 32-49-07. LEAK CHECKED GOOD.SDR SIMA20140726003Brake Assy · damagedNUMBER 1 MLG SMOKING AT GATE. REPLACED NR 1 MLG BRAKE ASSEMBLY IAW WC 32-600-14.SDR SIMA20140605008Adc · malfunctionedAT FL 360 CAPTAIN`S AIRSPEED INDICATED 244, FIRST OFFICER`S 248 & STANDBY 248. BRIEFLY SPS ADV ON EICAS. AT FL 350 CAPTAIN`S AIRSPEED 231 FIRST OFFICER`S 248 & STANDBY 244. SOMEWHERE BETWEEN FL 350 & 310 CAPTAIN`S AIRSPEED & ALTITUDE DROPPED ABNORMALLY LOW.SDR SIMA20140531004Flashlight · inoperativeCAPTAIN`S FLASHLIGHT RED LIGHT WILL NOT ILLUMINATE. R & R CAPTAIN`S FLASHLIGHT IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.SDR SIMA20140409006Battery · dischargedEMERGENCY LIGHTS COME ON TWO ROWS 8 - 11 WHEN POWER TURNED OFF. R & R NR 3 BACK UP EMERGENCY BATTERY & CHARGER ASSEMBLY IAW AMM 33--50-04. OPERATIONS CHECKED GOOD IAW WC 33-700-17 IAW EMB WC 32-700-19.SDR SIMA20140328008Lamp · inoperativePAX MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R PAX MAIN DOOR EMERGENCY LIGHT IAW AMM 33-50-09. OPS CHECKED GOOD.SDR SIMA20140318006Pressure Switch · corrodedTAKEOFF CONFIG CHECK GETS YOU AURAL WARNING, BRAKES, EVEN THOUGH THE PARKING BRAKES ARE OFF WITH THE BRAKES ON LIGHT EXTINGUISHED. FOUND CONNECTOR CONNECTION TO PRESS SWITCH TO BE CORRODED, BRAKE. R & R PRESS SWITCH IAW AMM 32-44-07. CLEANED PLUG END IAW WMSDR SIMA20140117004Light · inoperativeMAIN CABIN DOOR EMERGENCY LAMP INOPERATIVE. R & R LAMP IN MAIN CABIN DOOR EXTERNAL EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A, OPERATIONS CHECKED GOOD.SDR SIMA20131222011Light · inoperativeMAIN DOOR HINGE EMERGENCY LAMP INOPERATIVE. R & R MAIN ENTRY DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A, OPERATIONS CHECKED GOOD.SDR SIMA20131115007Lamp · inoperativeRIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RT EXTERIOR OVERWING EMERGENCY LAMP IAW AMM TASK 33-50-10-000-801/33-50-10-400-801, OPS GOOD.SDR SIMA20130425010Door Frame · corrodedDURING MAINTENANCE INSPECTION FOUND FRAME 65 CORRODED AROUND CARGO DOOR FORWARD LOWER STRIKER PLATE NUT PLATE HOLES. THE AIRCRAFT WAS REMOVED FROM SERVICE. BLENDED OUT CORROSION AND INSTALLED REINFORCEMENT DOUBLER IAW AE EO EM-53MR-2123. THE LEVEL OF CORROSSDR SIMA20130411018Shear Tie · corrodedFRAME 65 SHEAR TIE CORRODED AT FWD LOWER CORNER OF CARGO DOOR CUTOUT. REPAIRED SHEAR TIE IAW AE EO EM-53MR-1129.SDR SIMA20130411013Wire · brokenDURING B INSPECTION FOUND THE NR 4 EMERGENCY LIGHT STRIP HAD A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SESDR SIMA20130411012Light · brokenDURING MAINTENANCE INSPECTION FOUND THE RIGHT EMERGENCY LIGHT STRIP PROFILE NR 1 AND 2 BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 & 2 RIGHT EMERGENCY FLOOR SIDEWALL ASSEMBLY IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WSDR SIMA20130411011Wire · brokenDURING B INSPECTION FOUND THE NR 2, 3, 5, 7 EMERGENCY LIGHT STRIPS HAVE BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2, 3, 5, 7 EMERGENCY LIGHT STRIPS IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFSDR SIMA20130409003Light · inoperativeON FLIGHT 3339 THE CREW REPORTED THE COCKPIT FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RELAMPED EMERGENCY COCKPIT FLASHLIGHT IAW EMB-145 MM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130122006Inverter · inoperativeDURING B INSPECTION FOUND THE CABIN FORWARD OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 DC/ AC INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICESDR SIMA20121211002Skin · damagedDURING MAINTENANCE INSPECTION FOUND THE RIGHT ELEVATOR UPPER AND LOWER SKINS CREASE/PUNCTURED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED ELEVATOR IAW AEA EO EM-55MR-377. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120929002Sign · inoperativeDURING B INSPECTION FOUND THE FORWARD AISLE CEILING EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD AISLE CEILING EMERGENCY EXIT SIGN IAW EMB 145 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCSDR SIMA20120417002Bracket · brokenON FLIGHT 2761 THE FLIGHT ATTENDANT FORWARD FLASHLIGHT HOLDER WAS FOUND TO BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT BRACKET IAW EMB-145 AMM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RESDR SIMA20120323002Inverter · inoperativeDURING B-INSPECTION FOUND THE RIGHT SEAT 3B FORWARD EXIT SIGN EMERGENCY INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 INVERTER FOR EXIT SIGN AT SEAT 3B IAW EMB- AMM 33-50-11 IAW EMB AMM 33-50-00. THE OPERATIONAL CHECK WAS SDR SIMA2012052007Light · malfunctionedDURING B-INSPECTION, FOUND THE WALL EXIT LIGHT OUT AT SEAT 3BC. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYSTEM. OPS CHECKED GOOD IAW W/C 33-700-17. AIRCRAFT RETURNED TO SERVICE.SDR SIMA2012047003Holder · crackedON FLIGHT 3286 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT HOLDER WAS CRACKED, IT DID NOT SECURE THE FLASHLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT BASE BRACKET HOLDER IAW EMB 145 AMM CHAP 33-50-16SDR SIMA2012017011Flashlight · brokenON FLIGHT 3441 THE CREW REPORTED THE FLASHLIGHT OVER THE CAPTAINS SEAT SWITCH IS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN'S FLASHLIGHT IAW EMB 145 AMM 33-50-16 P/T. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RSDR SIMA201120606Light · inoperativeDURIING MAINTENANCE BASE VISIT FOUND THE EXTERIOR FUSELAGE AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IAW EMB 145 AMM 33-50-07. THE OPERATIONAL GOOD WAS GOOD.SDR SIMA201101202Brake · contaminatedON FLIGHT 3325 UPON LANDING THE TOWER REPORTED SMOKE COMING FROM THE LEFT MAIN WHEEL. AN EMERGENCY WAS DECLARED ON THE GROUND. THE AIRCRAFT ROLLED SAFELY TO A STOP. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED DE-ICING FLUID FROM BOTH BRAKES. PERFORMED SDR SIMA201030801Thermostat · inoperativeON FLIGHT 4080 THE CREW REPORTED THAT DURING THE CLIMB AT APPROXIMATELY FLIGHT LEVEL 160, RECEIVED A BLEED 2 OVER TEMPERATURE MESSAGE IN ICING CONDITIONS. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO RETURN TO ORD. THE AIRCRAFT LANDED AND RETURNED TO THESDR SIMA201021101Controller · inoperativeON FLIGHT 4149 CREW REPORTED BURNING SMELL IN COCKPIT ON CLIMB. RETURNED TO ORD. NO SMOKE WAS DETECTED. THE AIRCRACFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS WINDSHIELD TEMPERATURE CONTROLLER IAW EMB 145 AMM 30-42-01. THE AIRCRAFT WAS SDR SIMA201011301Transducer · failedFLT 2788 AFTER LANDING, DURING THE TAXI IN THE CREW REPORTED THE LEFT SIDE INBOARD-OUTBOARD BRAKE TEMP CLIMBED INTO THE HIGH AMBER RANGE WITH RIGHT SIDE BRAKES SIDE COOL (BELOW MIDDLE GREEN TEMP ANGLE). WITH THE AIRCRAFT STOPPED ON THE TAXI WAY AN AIRPORT VEHSDR SIMA201009503Nut Plate · brokenFOR FLIGHT 3588 THE CREW REPORTED THAT THE MAIN CABIN DOOR WAS HARD TO CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED PERMANENT REPAIR IAW EO-EM-5300-1510. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200934104Electronic Unit · inoperativeON FLIGHT 3854 DURING TAKEOFF THE CREW REPORTED THAT THE TAKEOFF AND GEAR RETRACTION DID NOT HAVE IN TRANSIT INDICATION. ALSO DURING EXTENSION NO IN TRANSIT AND NO 1 THRUST SETTING. THE CREW MANUALLY DEPLOYED THE LANDING GEAR. THE CREW DECLARED AN EMERGENCYSDR SIMA200929902Torque Box · damagedDURING INSPECTION 2 ELONGATED HOLES WERE FOUND IN THE RIGHT INBOARD TORQUE BOX. THE AIRCRAFT HAS BEEN REMOVED FROM SERVICE. PERFORMED AN EDDY CURRENT INSPECTION OF THE RIB, TORQUE BOX 57-28-00-250-806 AND 57-28-00-250-807 A1519. INSTALLED TWO FASTENERS ONSDR SIMA200704402Starter · seizedACID SMELL IN CABIN AND FLIGHT DECK FOLLOWED BY INTERMITTENT APU GENERATOR OFF BUSS MESSAGE ON EICAS. COULD NOT DUPLICATE SMELL IN CABIN OR FLIGHT DECK. PERFORMED ELECTRICAL SYSTEM INSPECTION ON WINDSHIELD CONTROLLER TERMINALS WITH NO DEFECTS. FOUND APU STASDR SIMA200616702Engine · failedCREW REPORTED DURING CRUISE FLIGHT E2 SHUT DOWN WITH NO OTHER IND, ATTEMPTED 1 RESTART PER THE AOM WITH NO SUCCESS, DECIDED TO DIVERT TO YYZ. RAI NR 2 ENGINE. OPS CHECKS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA200534705Floor Support · corrodedTHE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUT OUT. PREPARED A DOUBLER, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 31, CHAPTER 53-00-10. (M)SDR SIMA200507511Skin · damagedABI - DURING A DROP IN REPAIR, AIRCRAFT ARRIVED FOR REPAIR OF ACCIDENTAL DAMAGE ON THE RT AFT FUSELAGE BETWEEN FRAMES 71 AND 73 AND BETWEEN STRINGERS 15R AND 17R. PERFORMED A CUTOUT OF THE SKIN TO REMOVE THE DAMAGE. FABRICATED A FILLER, DOUBLER, FAIL/SAFE ST
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