N907EV

Service difficulty reports · 161

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 = 'N907EV' 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 SWIA201904125761Pump · failedON TAKEOFF AT 1000 FEET. THE LEFT ENGINE HAD A FLAMEOUT. CREW HEARD A BANG AND THE ENGINE ROLLED BACK. ITT SPIKED TO 973 FOR 11 SECONDS. NO RELIGHT WAS ATTEMPTED. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. LANDED WITHOUT INCIDENT. (FLT#5313) REMOVEApr 11, 2019 · N907EV · Cndair CL6002B19 · Engine Fuel PumpSDR SWIA2018052144688Sensor · out of adjustGEAR DISAGREE AND NOSE GEAR DOOR WARNING MESSAGES. ADJUSTED THE SENSOR IAW AMM 32-61-00. NO OTHER DEFECTS NOTED. ACFT OK FOR SERVICE.May 19, 2018 · N907EV · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA201844129Bracket · failedGEAR DISAGREE MESSAGE. RETURN TO FIELD. INSTALLED NLG CENTERING SENSOR BRACKET IAW AMM ANC FMM. RETRACTION & EXTENSION CYCLE OF MLG GOOD. OPS CHECKED GOOD.Jan 5, 2018 · N907EV · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA201743642Switch · failedMACH AND STAB TRIM CAUTION MESSAGES DURING CLIMB OUT, WOULD NOT REENGAGE, AUTOPILOT PITCH WOULD NOT ENGAGE. DECLARED EMERGENCY. REPLACED CA YOKE TRIM DISCONNECT SWITCH IAW AMM. OPS CHECKED GOOD. MACH & STAB TRIM & AUTO PILOT PITCH TRIM OPERATE NORMALLY.Aug 15, 2017 · N907EV · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA201743532Skin · chafedLOWER RT WING PLANK IS CHAFED AT RBL 45 AND T/E 1.000" X 4.000" X APPROXIMATELY .040" DEEP. REPAIRED THE WING PLANK IAW REO.Jun 20, 2017 · N907EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201743533Structure · crackedINDICATION NOTED AT RT WING BL5 WATER DRAIN FWD SCREW HOLE. REPAIRED IAW REO.Jun 14, 2017 · N907EV · Cndair CL6002B19 · Wing Main, Frame StructureSDR SWIA201743526Skin · dentedLEFT VERTICAL STAB HAS ONE DENT 10 INCHES FROM T/E AND JUST ABOVE THE NR 2 RIB. REPAIRED VERTICAL STAB IAW REO.Jun 14, 2017 · N907EV · Cndair CL6002B19 · Vertical Stabilizer, Plate/SkinSDR SWIA201743529Angle · corrodedPAX DOOR LOWER MOUNTING ANGLE CORRODED IN MULTIPLE LOCATIONS. REMOVED AND REPLACED THE ANGLE IAW SRM.Jun 9, 2017 · N907EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201743528Floor Support · corrodedLEFT FLOOR SUPPORT CORRODED AT BS 310, LBL 36. REMOVED CORROSION IAW SRM.Jun 9, 2017 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201743534Bulkhead Web · crackedREAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED 1) LBL9.5 WL 134 APPROX 3 INCHES LONG 60%FSH 2) RBL9.5 WL 134 APPROX 2 INCHES LONG 50%FSH 3) RBL18 WL 134 4 INCHES LONG 90%FSH 4) RBL27.50 WL 134 APPROX 1 INCH 50% FSH 5) RBL27.50 WL111 APPROX 5 INCHES Jun 6, 2017 · N907EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201743531Skin · dentedEXTERNAL FUSELAGE SKIN DENTED, BS 656 BETWEEN STRINGERS 26 AND 27R. REPAIRED THE SKIN IAW REO.Jun 4, 2017 · N907EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201743530Skin · gougedTHE SKIN HAD SEVERAL SMALL NICKS AND GOUGES FROM BS 589 TO 605 BETWEEN STRINGER 21R & 23R. REPAIRED THE SKIN IAW SRM.Jun 4, 2017 · N907EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201743527Skin · dentedRT INBOARD FLAP HAS A DENT ON THE LOWER SKIN INBOARD SIDE. REPAIRED THE FLAP SKIN IAW REO.Jun 4, 2017 · N907EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201743525Panel · damagedTWO OVERSIZED HOLES IN PANEL 131AL. REPAIRED TWO OVERSIZED HOLES IN PANEL 131AL AT 10 O'CLOCK AND 9 O'CLOCK POSITIONS IAW REO.May 19, 2017 · N907EV · Cndair CL6002B19 · Standard Practices/StructuresSDR ASOA20161112155AFloor Support · corrodedDURING C CHECK, FOUND RT FLOOR SUPPORT CORRODED BETWEEN BS 409+32 - 409+96. REPAIRED IAW EC/TC REO 601R53-00-530.Nov 12, 2016 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA20161112154AFloor Support · corrodedDURING C CHECK, FOUND RBL 46 FLOOR SUPPORT CORRODED AT BS 559+80. REPAIRED IAW EC/TC REO 601R-53-00-526.Nov 12, 2016 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA20161112153Floor Support · corrodedDURING C CHECK, FOUND LBL 46 FLOOR SUPPORT CORRODED BETWEEN BS 559+16 - 559+48. REPAIRED IAW EC/TC REO 601R-53-00-526.Nov 12, 2016 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA20161112152AFloor Support · corrodedDURING C CHECK, FOUND RBL 46 FLOOR SUPPORT CORRODED BETWEEN BS 582-621. REPAIRED IAW EC/TC REO 601R-53-00-526.Nov 12, 2016 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA20161108148Stiffener · crackedDURING C CHECK, FOUND PAX DOOR ASSIST MOTOR AFT SIDE PANEL STIFFENER CRACKED AT LOWER SECTION. C/W EC/TC REO 601R-52-11-1376 REV A.Nov 8, 2016 · N907EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA20161108099Skin · damagedDURING C CHECK, FOUND FASTENER HOLE DAMAGED ON FUSELAGE SKIN DURING INSTALLATION OF PANEL 132AL. REPAIRED THE SKIN IAW REO 601R-53-11-162 & EC/TC REO 601R-53-11-162. MAJOR REPAIR.Nov 8, 2016 · N907EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2016081715279Wire · misinstalledNUMBERS 1, 2, AND 7 EXTERNAL EMERGENCY LIGHTS INOPERTIVE. ACFT NOT OPERATED AT NIGHT. FOUND WIRES TO FORWARD NR 1 SERVICE DOOR EMERGENCY LIGHT INCORRECTLY INSTALLED. R & R NR 1 LT AND RT EMERGENCY LIGHT SOCKETS AND REPLACED FUSE TO NR 1 BATTERY PACK. R & RAug 17, 2016 · N907EV · Cndair CL6002B19 · Light System WiringSDR ASOA2016080515193Lamp · burned outNR 2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.Aug 5, 2016 · N907EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2016080515192Lamp · burned outNR 2 CABIN EMERGENCY CEILING FLOOD LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 3-51-16. OPS CHECKED GOOD.Aug 5, 2016 · N907EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2016061914945Light · inoperativeRIGHT NR 3 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R RT NR 3 EXTERIOR EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECK GOOD.Jun 19, 2016 · N907EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2015122114236Sign · damagedLIGHTED FLOOR-LEVEL EXIT SIGN AT SERVICE DOOR DAMAGED. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.Dec 21, 2015 · N907EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2015110213995Inverter · failedLIGHTED FLOOR-LEVEL EXIT SIGN AT RT OVERWING EMERGENCY EXIT INOPERATIVE. R & R AFFECTED INVERTER IAW 33-51-07. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.Nov 2, 2015 · N907EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2014121111861Sign · inoperativeRT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. OPS CHECKED EMERGENCY LIGHT IAW AMM 33-51-00. OPS CHECKED GOOD.Dec 7, 2014 · N907EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2014111211636Frame · corrodedBS 364, FRAME IS CORRODED BETWEEN STR 26L AND 26R. REPAIRED.Oct 29, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2014111211635Post · crackedFS 409+128, RBL 18 INBD VERT POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROX .5" LONG X 50 PERCENT FSH. FAILED NDT INSP. REMOVED LT AND RT VERTICAL POSTS AT FS 409+128, RBL 18 IAW SRM 51-42-06 AND 51-42-22. C/W ECTC REO: 601R-53-41-889Oct 27, 2014 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014111011625Stiffener · crackedFS 409+128, BL 0 VERT POST RT SIDE HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69, APPROX .250" LONG BY 50 PERCNET FSH. FAILED NDT. R & R RT VERT POST AT BL 0 PN 601R32208-132 IAW CRJ 200 51-42-22, 51-42-06. COMPLIED WITH EC/TC REO 601R-53-41-889Oct 27, 2014 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014111211634Pin · corrodedLT AND RT LATCH IN INTERCOSTALS ARE CORRODED BETWEEN FS 349 AND FS 364. REMOVED LT AND RT LATCH PIN INTERCOSTALS IAW SRM 51-42-06 AND 51-42-21. INSTALLED LT LATCH PIN INTERCOSTAL 601R31049-9 AND RT LATCH PIN INTERCOSTAL 601R31049-10 IAW SRM 51-42-06, 51-42-2Oct 25, 2014 · N907EV · Cndair CL6002B19 · Standard Practices/StructuresSDR ASOA2014111011624Isolator · crackedREAR PRESSURE BULKHEAD FWD FACE OF WEB HAS A MISSING ISOLATOR AND A BENT AND CRACKED ISOLATOR AT RBL 27.50 AND WL 75.00. R & R ISOLATOR BRACKET AND INSTALLED NEW ISOLATOR IAW SRM 51-42-06.Oct 23, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014111011623Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0, WL 108-112, 3.5" L, 70 PERCNET FSH. FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND GREO 601R-53-61-1285, REV D.Oct 23, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014111011622Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0, WL 131-134, 2.5" L, 50 PERCENT FSH. FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND REO 601R-53-61-1285, REV D.Oct 23, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014111211633Floor Support · corrodedCORROSION ON LT UPPER SURFACE OF PRESSURE FLOOR SUPPORT BS 409+128 - 559.00. BLENDED CORROSION IAW REO 601R-53-41-666 2.2 DISP A AND B. PERFORMED EDDY CURRENT REWORKED AREAS IAW REO 601R-53-41-666, REV C 1.2, STEP C. NO INDICATIONS NOTED AT THIS TIME.Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014110711621Cargo Track · corrodedCARGO TRACK AT RBL 9 BS 559+110 - 568 CORRODED. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014110711620Seat Track · corrodedCARGO TRACK AT RBL 9, BS 559+87-559+96 CORRODED. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014110711619Cargo Track · corrodedCARGO TRACK AT RBL 27 BS 559+79 - 559+95 HAS CORROSION. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014110611610Cargo Track · corrodedCARGO TRACK AT LBL 27, BS 559 HAS CORROSION AT ATTACHMENT HOLES. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014110611609Cargo Track · corrodedCARGO TRACK AT LBL 9, BS 612-617 HAS CORROSION AT ATTACHMENT HOLES. R & R THE CARGO TRACK SEGMENT IAW SRM 51-42-02-00, 51-41-04-00.Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014110611608Cargo Track · corrodedCARGO TRACK AT LBL 9 BS 559+110 - 568 HAS CORROSION. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014110611607Cargo Track · corrodedCARGO TRACK AT LBL 9 BS 559+87- 559-96 HAS CORROSION AT ATTACHMENT HOLES. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014110611606Floor Support · corrodedRT CARGO FLOOR SILL FROM FS 559.00+112 TO FS 621.00 HAS FILIFORM CORROSION AT FLOORBOARD SCREW HOLES. REMOVED NUTPLATES FROM RT CARGO FLOOR SILL FROM FS 559.00+112 TO FS 621.00 IAW SRM 51-54-10. INSTALLED 13 NEW SERVICEABLE NUTPLATES, PN MS21059L3 IAW SRM 5Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014110611605Frame · corrodedCORROSION ON FRAME AT FS 333.00 BETWEEN LBL STGR 24 AND RBL STGR 24. REMOVED POSTS AT FS 333 RBL 20 AND LBL 20 IAW SRM 51-42-06 & 51-42-21. UPON FURTHER INVESTIGATION, FOUND TO BE BETWEEN STR 24 & 23L AND STR 24 & 23R, INSTALLED SAME SERVICEABLE VERTICAL POSOct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2014110611604Frame · corrodedCORROSION ON FRAME AT FS 349.00 BETWEEN LBL STR 24 AND RBL STGR 24. REMOVED CORRODED FRAME SECTOR AT FS 349.00 BETWEEN STR 23L-23R IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE FS 349.00 FRAME SECTOR IAW SRM 51-40-11. INSTALLED IAW SNIEOct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2014110611603Bracket · crackedPILOTS SIDE WINDOWS AFT BRACKET IS CRACKED APPROX .250"L AT BOTTOM OF POST. REMOVED AFT, PILOT SIDE WINDSCREEN FITTING IAW SRM 51-42-21. INSTALLED NEW FITTING IAW SRM 51-42-21. LOCATED AND DRILLED NEW BRACKET IAW SRM 51-40-11. COMPLIED WITH SNIEO 601R33007Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2014110511601Floorbeam · corrodedRBL 9 - 27 FLOORBEAM CAP BS 559+96 CORRODED . REPAIRED IAW REO 601R-53-00-005.Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014110511600Floorbeam · corrodedRBL 9 - 27 FLOORBEAM TEE AT BS 559+112 HAS CORROSION. REPAIRED IAW REO 601R-53-090-005.Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014110511599Floor Support · corrodedLT CARGO FLOOR SUPPORT FROM BS 574 - 621 HAS CORROSION AT FLOORBOARD SCREW HOLES. REPAIRED IAW REO 601R-53-00-526 AND GREO 601R-53-00-526 REV.Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014110511598Floor Support · corrodedCORROSION ON LT FLOOR SUPPORT AT BS 349 JUST AFT OF PAX DOOR. REPAIRED IAW REO 601R-53-00-530.Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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