N901EV

Service difficulty reports · 167

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 = 'N901EV' 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 SWIA2018122145379Bracket · bentRETURN TO FIELD AFTER NOSE GEAR WOULD NOT RETRACT. (FLT#5714) FO: 12/21/2018 CLOSED NLG PROX SENSOR BENT. REMOVED AND REPLACE NLG PROX BRACKET IAW CMM AND AMM. PERFORMED SEVERAL GEAR SWINGS IAW AMM. OPS CHECK GOOD.Dec 21, 2018 · N901EV · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA2018060144742Fairing · chafedRIGHT FLAP STUB FAIRING CHAFED. REPLACED THESTUB FARING IAW SRM. NO DEFECTS NOTED.May 6, 2018 · N901EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2018060144741Doubler · dentedDENTS FOUND ON THE DOUBLER ON THE RT AFT FUSELAGE AFT OF LOW PRESSURE AIR SERVICE DOOR. REMOVED AND REPLACED THE DOUBLER IAW REO.May 2, 2018 · N901EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2018060144740Floorbeam · corrodedFLOORBEAM CORRODED ON THE UPPER CAP, RBL 27, BS 559. REMOVED AND REPLACED THE UPPER CAP IAW REO.May 2, 2018 · N901EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2018060144739Floorbeam · corrodedFLOORBEAM CORRODED ON THE UPPER CAP, RBL 9, BS 559. REMOVED AND REPLACED THE CORRODED UPPER CAP IAW REO.May 2, 2018 · N901EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2018060144738Skin · dentedLT AILERON, TOP DENTED. CONTOURED THE AILERON SKIN IAW REO.May 1, 2018 · N901EV · Cndair CL6002B19 · AileronsSDR SWIA2018060144737Skin · dentedMULTIPLE DENTS ON THE UPPER SKIN PANEL OF LT INBD FLIGHT SPOILER. REPAIRED MULTIPLE DENTS ON THE LT INBD FLIGHT SPOILER IAW REO.Apr 28, 2018 · N901EV · Cndair CL6002B19 · SpoilersSDR SWIA201744082Bracket · crushedGEAR DISAGREE WARNING. REPLACED BRACKET ON NOSE GEAR SMASHED BY TOWBAR STRAP. OPS CHECKED GOOD.Dec 21, 2017 · N901EV · Cndair CL6002B19 · Nose/Tail Landing GearSDR SWIA201743651Bracket · bentGEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED THE NLG PROXIMITY SENSOR BRACKET IAW AMM. ALL INDICATIONS NORMAL.Aug 23, 2017 · N901EV · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR SWIA201743238Servo Valve · malfunctionedNOSE WHEEL STEERING INOPERATIVE CAUTION ENROUTE. REMOVED AND REPLACED ELECTRO HYD SERVO VALVE IAW AMM. OK FOR SERVICE.Apr 27, 2017 · N901EV · Cndair CL6002B19 · Landing Gear Steering SystemSDR ASOA2016041914720Battery Pack · dischargedFORWARD EMERGENCY FLOOR LIGHT AND EXIT SIGN ARE INOPERATIVE. R & R ELECTRICAL CONNECTOR IAW ESPM 20-11-00 20-17-10 ON WIRES LY6022 AND LY32A22. R & R EMERGENCY LIGHTS BATTERY NR 2 PACK IAW AMM 33-51-04-400-801, 33-51-04-000-801, IPC 33-51-04, ITEM 17. OPS TApr 19, 2016 · N901EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2016041414719Structure · crackedCENTER LT LOWER CLIP AT 202 PRESSURE BULKHEAD IS CRACKED. REMOVED LT & RT LOWER CENTER POST CLIPS AT 202 PRESSURE BULKHEAD IAW SRM 51-42-21-00. LOCATED, DRILLED AND INSTALLED NEW LT & RT LOWER CENTER POST CLIPS AT 202 PRESSURE BULKHEAD IAW SRM 51-40-11 AND 5Apr 14, 2016 · N901EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2016041114718Skin · damagedWHILE PERFORMING REO 601R-57-21-130, FOUND 1 EA OVERSIZE HOLE ON LT WING PLANK. RECEIVED AND COMPLIED WITH REO 601R-57-21-2436 AND ECTC 601R-57-21-2436.Apr 11, 2016 · N901EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2016040714721Shim · shiftedREFER TO EO 600-53-2650003, LT AND RT MLG SIDE BRACE FITTING BRACKET SHIMS ARE MIGRATED. COMPLIED WITH PERMANENT REPAIR IAW EC/TC REO 601R-53-41-101-01.Apr 7, 2016 · N901EV · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR ASOA2016040614717Floor Support · corrodedCORROSION ON LBL 42.5 FLOOR SILL AT FS 559+32. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526, REV, DATED 5/22/2013 AS WRITTEN.Apr 6, 2016 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2016040614710Floor Support · corrodedCORROSION AROUND 2 NUTPLATES ON RT FLOOR SILL. RBL 42.5 AND BETWEEN FS 559+32 TO 559+48. CORROSION AROUND 2 NUTPLATES ON RT FLOOR SILL. RBL 42.5 AND BETWEEN FS 559+32 TO 559+48. COMPLIED WITH EC/TC REO 601R-53-00-526 01 AND GREO 601R-53-00-526, REV. DATED Apr 6, 2016 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2016040414716Battery Pack · dischargedNR 2 BATTERY PACK INSIDE CABIN FOR EMERGENCY LIGHTS INOPERATIVE. R & R NR 2 EMERGENCY LIGHTS BATTER PACK IAW AMM 33-51-04-000-801/33-51-04-400-801, IPC 33-51-04, FIG 1, ITEM 17. R & R NR 2 EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51-04-000-801/33-51-04-400-801Apr 4, 2016 · N901EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2016040414709Floorbeam · corrodedCORROSION AROUND FLOORBOARD SCREW HOLE ON RBL9 AND AT FS 409+40. REMOVED CORROSION AT FS 409+40, RBL 9 INBD SIDE IAW SRM 51-21-06, AND FOUND TO HAVE COMPLETE MATERIAL LOSS. REPAIR FLOORBEAM SUPPORT STRUCTURE IAW SRM 53-00-43. REPAIRED FLOORBEAM AT 409+40 IAWApr 4, 2016 · N901EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2016040414708Seat Track · corrodedSEAT RAIL SEGMENT ON RBL 9 AND BETWEEN FS 394 TO FS 409+112 CORRODED OUT OF LIMITS. FABRCIATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. REMOVED SEAT RAIL AT FS 394 TO FS 409+112, RBL9 IAW AMM 53-01-11-000-802. INSTALLED NEW FABRCIATED SEAT RAIL AT RBL 9 FApr 4, 2016 · N901EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016040414707Bracket · corrodedBOTTOM CORNER OF SERVICE DOOR CUTOUT AT FS 319.70, STR 17R AND RBL42 CORRODED. LOWER FRAME BRACKET AT FS 319.70 CORRODED OUT OF LIMITS IAW SRM 53-00-00. R & R BRACKET AT FS 319.70 IAW SRM 51-40-11 AND 51-42-21.Apr 4, 2016 · N901EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2016040414706Placard · crackedSERVICE DOOR INNER OPEN/CLOSE HANDLE PHOTOLUMINESCENT "EXIT" PLASTIC PLACARD CRACKED. REMOVED SERVICE DOOR INNER PHOTOLUMINCENT "EXIT" PLACARD BY REMOVING 2 SCREWS WITH A SCREW DRIVER. INSTALLED A SERVICABLE EXIT PLACARD IAW AMM 20-21-00-910-801.Apr 4, 2016 · N901EV · Cndair CL6002B19 · Placards and MarkingsSDR ASOA2016033114715Skin · dentedDENT ON LT FLAP LOWER SKIN OTBD OF OTBD HINGE. REPAIRED IAW SRM 57-52-00 TO LT FLAP LWR SKIN OTBD OF OTBD HINGE AREA. RECEIVED AND COMPLIED WITH EC/TC EO 600-57-0476.Mar 31, 2016 · N901EV · Cndair CL6002B19 · Trailing Edge FlapsSDR ASOA2016033114714Skin · crackedFWD FUSELAGE SKIN CRACKED AT LT FWD HYDRAULIC BAY DOOR SURROUND JUST BELOW LT AFT LATCH. REMOVED CRACKED SKIN AT LT FORWARD HYD BAY DOOR SURROUND IAW SRM 51-42-06 & 51-42-13. INSTALLED NEW SKIN AT LT FWD HYDRAULIC BAY IAW SRM 51-42-06 & 51-42-13 & DWG 600-370Mar 31, 2016 · N901EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2016033114690Angle · crackedBS 625 ANGLE CRACKE. R & R THE ANGLE IAW SRM 51-42-21-00.Mar 31, 2016 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2016033114689Handle · lack of lubeRT OVERWING EMERGENCY EXIT HANDLE FAILS OPS FORCE CHECK. PERFORMED LUBRICATION OF THE RT OVERWING EMERGENCY EXIT HANDLE IAW AMM 12-20-52-640-802, FUNCTIONAL TEST OF HANDLE GOOD REF AMM 52-21-00-720-801.Mar 31, 2016 · N901EV · Cndair CL6002B19 · Emergency ExitsSDR ASOA2016012414390Skin · crackedCRACK FOUND AT RT LOWER WING PLANK, WS 148.019. COMPLIED WITH ECTC REO 601R-57-21-130 01 AND REO 601R-57-21-131. REMOVED UPPER PIE PANEL IAW SRM 51-42-06 & 51-42-13. INSTALLED UPPER PIE PANEL IAW CRJ 200 SRM 51-42-06, 51-42-13. COMPLIED WITH ECTC REO 601R-5Jan 24, 2016 · N901EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2016012414389Skin · crackedCRACK FOUND AT LT LOWER WING PLANK WS 148.019 CRACK LENGTH IS .7170. COMPLIED WITH ECTC REO 601R-57-21-130 AND REO 601R-57-21-131. REMOVED UPPER AND LOWER PIE SKIN PANELS IAW SRM 51-42-06 AND 51-42-15 AND 511-42-21. INSTALLED PIE PANELS IAW SRM 51-41-02 ANDJan 24, 2016 · N901EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015050812775Lens · missingWARDROBE LOWER EMERGENCY LIGHT COVER MISSING. REPLACED WARDROBE LOWER EMERGENCY LIGHT LENS COVER IAW AMM 33-51-19.May 5, 2015 · N901EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2014101711436Unknown · odorPAX DOOR WILL NOT OPEN AND ELECTRICAL ODOR. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-08. OPS CHECK IS GOOD. PERFORMED INSPECTION OF DOOR ASSIST MOTOR IAW AMM 52-11-08. NO DEFECTS ARE NOTED AT THIS TIME, DOOR OPERATES CORRECTLY. ACFT IS OK FOR SERVIOct 13, 2014 · N901EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2014090511182Fuel Sys · malfunctioned400 LB IMBALANCE DURING CLIMBOUT, LT TANK, DURING FLIGHT, LEFT TANK IMBALANCE INCREASED TO AROUND 900 LBS WITH PUMPS WORKING, FOLLOWED QRH, DIVERTED. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. PERFORMED OPS CHECK OF FUEL TRANSFER EJECTOR PUMP IAW AMM 28Sep 2, 2014 · N901EV · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR ASOA2014042910439Connector · corrodedCONNECTOR FOR LT FWD FUSELAGE EMERGENCY LIGHT IS CORRODED. R & R CONNECTOR IAW ESPM 20-17-10 AND WIRING DIAGRAM MANUAL 33-52-00. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.Apr 4, 2014 · N901EV · Cndair CL6002B19 · Light System WiringSDR ASOA2014042910438Access Panel · crackedFUEL ACCESS PANEL 650EB HAS 2 INDICATIONS ON THE OTBD FWD & AFT SIDES 50 PERCENT FCH FAILED NDT. PERFORMED ROTOPEEN IAW SRM 51-24-11 IAW REO 601R-57-21-030, REV L.Apr 2, 2014 · N901EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014042910437Access Panel · crackedFUEL ACCESS PANEL 550DB HAS 1 INDICATIION ON THE FWD, INBD SIDE 50 PERCENT FCH FAILED NDT. PERFORMED ROTOPEEN IAW SRM 51-24-11 REO 601R-57-21-030, REV L.Apr 2, 2014 · N901EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014042910436Access Panel · crackedLEFT FUEL ACCESS PANEL 540DB HAS ONE INDICATION ON THE INBD SIDE 60 PERCENT FCH FAILED NDT. COMPLIED WITH REO 601R-57-21-030. PERFORMED ROTOPEEN IAW SRM 51-24-11 IAW REO 601R-57-21-030, REV L.Apr 2, 2014 · N901EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014042910435Vertical Beam · crackedFS 409+128, VERTICAL BEAM IS CRACKED AT RBL 27 INBD SIDE BOTTOM FASTENER HOLE. COMPLIED WITH EC/TC REO 601R-53-41-056 IAW REO 601R-53-41-056, REV F.Apr 2, 2014 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014042910434Vertical Beam · crackedFS 409+128, VERTICAL BEAM IS CRACKED AT RBL 36 INBD SIDE BOTTOM FASTENER HOLE. C/W REO 601R-53-41-189 AT INBD SIDE OF RBL 36, VERTICAL POST AT FS 409+128. C/W REO 601R-53-41-189 AT INBD SIDE OF RBL 36 VERTICAL POST AT FS 409+128. C/W EC/TC REO 601R-53-41-18Apr 2, 2014 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014042910433Skin · crackedFOUND LT AFT DRAIN VALVE HOLE INBD SIDE AFT LOWER PLANK BETWEEN STR 7 AND 5 MULTIPLE INDICATIONS APPROX .5" IN LENGTH 70 PERCENT FSH. FAILED NDT INSPECTION. COMPLIED WITH EA 25-2014-113. EA 25-2014-113 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTEApr 2, 2014 · N901EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014042910432Bulkhead · damagedFS 621 BULKHEAD EXCEEDS LIMITATIONS OF REO 601R-53-61-1285, LBL 9.50 REQUIRES REPAIR. LOCATED AND DRILLED REPAIR ITEMS IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS & FINAL REAMED ALL HOLES FOR REPAIR TO LBL 9.50 IAW REO 601R-53-61-5250 & REO 601R-53-6Apr 2, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014042910431Bulkhead · damagedFS 621.00 BULKHEAD EXCEEDS LIMITATIONS OF REO 601R-53-61-1285, LBL 36.20. REQUIRES REPAIR. LOCATED AND DRILLED REPAIR ITEMS IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS & FINAL REAMED ALL HOLES FOR REPAIR TO LBL 36.2 IAW REO 601R-53-61-5250 & REO 601Apr 2, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014042910430Bulkhead · unknownFS 621.00, BULKHEAD EXCEEDS LIMITATIONS OF REO 601R-53-61-1285, RBL 27.50. REQUIRES REPAIR. C/W REO 601R-53-61-5250, P1 AT RBL 27.5. ADDED WEIGHT OF REPAIR PARTS & FIELD FASTENERS IS 4.10 LBS. C/W REO 601R-53-61-5250, REV. RECEIVED AND VERIFIED FINAL REO 6Apr 2, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014042910429Bulkhead · unknownFS 621.00, BULKHEAD EXCEEDS LIMITATIONS OF REO 601R-53-61-1285, LBL 27.50 REQUIRES REPAIR. REMOVED ANGLE 601R36008-39, FS 621, BULKHEAD AFT SIDE LBL 27.50 IAW SRM 51-42-06 AND 51-42-21. INSTALLED ANGLE 601R36008-39 AFT SIDE OF FS 621, BULKHEAD LBL 27.50 IAWApr 2, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014042910428Bulkhead · unknownFS 621.00 BULKHEAD EXCEEDS LIMITATIONS OF REO 601R-53-61-1285, LBL 18.00. LOCATED AND DRILLED REPAIR ITEMS IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS AND FINAL REAMED ALL HOLES FOR REPAIR TO LBL 18 IAW REO:601R-53-61-5250. PERFORMED CUT ON BULKHEADApr 2, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014042910427Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROXIMATELY .5" IN LENGTH, 100 PERCENT FSH, FAILED NDT INSPECTION. REMOVED CARGO COMPARTMENT DOOR FOR ACCESS IAW AMM 52-31-00-000-801. REMOVED AFT CARGO BALANCE SPRING BOX IAW AMM 5Apr 1, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014042910426Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0, WL 112-WL 107.5 APPROX 4.5" IN LENGTH, 50 PERCENT FSH, FAILED NDT INSPECTION. REMOVED STIFFENER ANGLE FROM FS 621.00, BULKHEAD AT WL 120.43 IAW SRM 51-42-06. INSTALLED STIFFENER ANGLE IAW CJR Apr 1, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014042910425Bulkhead Web · corrodedFOUND REAR PRESSURE BULKHEAD WEB, RBL 9.50, WL 103 HAS INDICATION NOTED APPROX 1.0" IN LENGTH, 50 PERCENT FSH, FAILED NDT INSPECTION. LOCATED AND DRILLED IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS & FINAL REAMED ALL HOLES FOR REPAIR TO RBL 9.5 IAW RApr 1, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014042910424Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB RBL 18.00, WL 107 HAS INDICATION NOTED APPROX 1.0" IN LENGTH, 50 PERCENT FSH, FAILED NDT INSPECTION. PERFORMED CUTOUT OF BULKHEAD WEB IAW REO: 601R-53-61-5250. COMPLIED WITH REO:601R-53-61-5250 IAW NDTM PT 1 51-20-06. C/W REApr 1, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014042910423Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB, RBL 36.20, WL 82-WL 85 HAS INDICATIONS NOTED APPROX 3.0" IN LENGTH, 70 PERCENT FSH, FAILED NDT INSPECTION. LOCATED AND DRILLED REPAIR IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS & FINAL REAMED ALL HOLES FOR REPAIR TOApr 1, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014042910422Floorbeam · corrodedCORROSION ON FLOORBEAM CAP AT FS 589.00, RBL 27. REMOVED DAMAGED CAP IAW SRM 51-42-06. INSTALLED CAP IAW SRM 51-40-11, 51-42-06 AND 51-42-15.Mar 31, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014042910421Attach Angle · crackedSTRINGER 3L FWD UPPER AND LOWER ATTACH ANGLES CRACKED JUST AFT OF FS 280 BULKHEAD. REMOVED 2 ATTACH ANGLES AT FS 280 STGR 3L IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW ATTACH ANGLES AT FS 280, STGR 3L IAW SRM 51-42-06 AND 51-42-02.Mar 30, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2014042910420Isolator · crackedFS 621 PRESSURE BULKHEAD ISOLATOR LOCATED SECOND UP FROM BOTTOM AT RBL 9 IS CRACKED. REMOVED CRACKED ISOLATOR IAW SRM 51-42-13. INSTALLED NEW ISOLATOR IAW SRM 51-42-13.Mar 30, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
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