N730EV

Service difficulty reports · 221

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 = 'N730EV' 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.

SDR TRAX200701060Megaphone · inoperativeMEGAPHONE INOP.Jul 25, 2007 · N730EV · Cndair CL6002C10 · Emergency EquipmentSDR TRAX200700736Flashlight · inoperativeCAPTAIN`S FLASHLIGHT INOP.May 28, 2007 · N730EV · Cndair CL6002C10 · Emergency EquipmentSDR TRAX200700042Seat Track · corrodedFOUND RT SIDE I/B ( FLOOR) SEAT TRACK FWD END CORRODED.Jan 7, 2007 · N730EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR TRAX200700026Seat Track · corrodedLIGHT SURFACE CORROSION DETECTED THROUGHOUT LEFT FLOOR SEAT RAIL BETWEEN FS 400 TO FS 700.Dec 31, 2006 · N730EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR TRAX200700009Seat Track · corrodedLIGHT SURFACE CORROSION DETECTED THROUGHOUT LEFT SIDE WALL SEAT RAIL BETWEEN FS 400 TO FS 953. REMOVED SURFACE CORROSION AND TREATED AS REQUIRED IAW CRJ 700 SRM 53-31-49 AT FS 400 THRU FS 953 SM17032 JOB COMPLETE.Dec 31, 2006 · N730EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR TRAX200700010Seat Track · corrodedLITE SURFACE CORROSION DETECTED THROUGHOUT RIGHT SIDE WALL SEAT RAIL BETWEEN FS 400 TO FS 953. REMOVED LITE SURFACE CORROSION ON RT SIDE WALL SEAT RAIL FROM FS 752.50 TO FS 953.00 IAW CRJ 700 SRM 51-21-49. SUPPLEMENTAL - SDR.Dec 31, 2006 · N730EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR TRAX200700012Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED AT AFT MOTOR PULLEY BRACKET. REPAIRED IAW ALL SRMS.Dec 31, 2006 · N730EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR TRAX200700011Seat Track · corrodedLITE SURFACE CORROSION DETECTED THROUGHOUT RIGHT FLOOR SEAT RAIL BETWEEN FS 400 TO FS 700.Dec 31, 2006 · N730EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR TRAX200700014Bulkhead · corrodedRIGHT STA 280 AFT BULKHEAD AFT WEB CORRODED.Dec 29, 2006 · N730EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR TRAX200700006Rib · crackedRIGHT WING TRAILING EDGE SUPPORT RIB CRACKED AT WS 216. REPAIRED IAW SRM.Dec 29, 2006 · N730EV · Cndair CL6002C10 · Wing, Rib/BulkheadSDR TRAX200700005Bulkhead · corrodedLEFT BS 280 BULKHEAD AFT WEB CORRODED. REMOVED AND REPLACED LT 280 WEB SPLICE IAW REO 670-53-11-052.Dec 29, 2006 · N730EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR TRAX200700004Crossbeam · corrodedSTA 280 CROSSBEAM CORRODED BETWEEN RBL 9 AND LBL 9. COMPLIED WITH EC/TC EO700-53-0054 01 AND EO700-53-0061.Dec 29, 2006 · N730EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200700003Bulkhead · corrodedRT STA 280 AFT BULKHEAD AFT WEB CORRODED.Dec 29, 2006 · N730EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR TRAX200700001Attach Angle · crackedPOSSIBLE CRACK AT LEFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE AFT END (MARKED). PERFORMED ET INSPECTION OF LT ATTACH ANGLE IAW CRJ 700 NDT MANUAL PART 1, CHAPTER 51-20-006. ANGLE IS CRACKED IN RADIUS. CUT OUT DAMAGED AREA PER REO 670-55-31-015. ALL WORK DODec 28, 2006 · N730EV · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR TRAX200601071Light · inoperativeLEFT FUSELAGE AFT EMERGENCY LIGHT INOP.Dec 3, 2006 · N730EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200600420Odor · detectedABOUT 10 AFTER TAKE OFF FROM MEN F/A NOTICED A BURNING ODOR, CAPT DID NOT. THEN CAPT NOTICED IT. THE ODOR THEN WENT AWAY, THEN CAME BACK STRONGER THAN BEFORE. CREW DONNED THE SMOKE MASKS. FTL DIV. F/A REPORTED BURNING SMELL CAME AND WENT SEVERAL TIMES ANDJun 25, 2006 · N730EV · Cndair CL6002C10 · Air Distribution SystemSDR TRAX200600138Warning Light · illuminatedAFTER TAKEOFF WHEN SELECTING GEAR UP ALL 3 GEAR REMAINED EXTENDED AND "GEAR DISAGREE" MSG ILLUMINATED. FOLLOWED QRH PROCEEDURES" GEAR UP DISAGREE" GEAR DISAGREE MSG DISAPPEARED. A/C RETURNED TO ATL AFTER T/O, AN EMERGENCY WAS DECLARED.Apr 25, 2006 · N730EV · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR ASOA06068Step · brokenDURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Jan 7, 2006 · N730EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA05668Step · crackedDURING A C-CHECK IN MCN, THE BOTTOM STEP ON PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M)Aug 16, 2005 · N730EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA05589SWire Harness · inoperativeDURING DESCENT, AT APPROX 18,000 FT, THE CREW RECEIVED A BRAKE OVERHEAT WARNING MESSAGE ON EICAS WITH THE LT OB BRAKE INDICATOR GOING TO TWENTY AND FLUCTUATED ERRATICALLY. AFTER COMPLYING WITH THE QRH, ALL INDICATIONS RETURNED TO NORMAL. UPON LOWERING THE GEJul 10, 2005 · N730EV · Cndair CL6002C10 · Landing Gear System WiringSDR ASOA05589Warning Light · false indicationDURING DESCENT FROM SLC-SAT, AT APPROXIMATELY 18,000 FEET THE CREW RECEIVED A BRAKE OVERHEAT WARNING MESSAGE ON EICAS WITH THE LEFT OUTBOARD BRAKE INDICATOR GOING TO TWENTY AND FLUCTUATED ERRATICALLY. AFTER COMPLYING WITH THE QRH ALL INDICATIONS RETURNED TO NJul 10, 2005 · N730EV · Cndair CL6002C10 · Overheat Detection
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