# Service difficulty reports: N914EV

A list on [N914EV](https://openairdocs.org/aircraft/N914EV.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 4 · 200 reports

- [SDR SWIA2025060900003](https://openairdocs.org/sdr/SWIA2025060900003.md): Skin · dented · Jun 3, 2025 · N914EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND 1 INWARD DENT/GOUGE ON THE OUTER FUSELAGE SKIN APPROX. FS 785.00 IN BETWEEN STR 5R & STR 6R. (FILED CLOSED)COMPLIED WITH REO 601R-53-71-235 DATED: 2025-06-07 REV:-- REPAIR TO FUSELAGE SKIN BETWEEN V-STAB 43.75% - 55.625%(FS 780.00- FS 785.00) & BETWEEN
- [SDR SWI202405200415](https://openairdocs.org/sdr/SWI202405200415.md): Apu · overtemp · May 17, 2024 · N914EV · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) System
  > D: APU OVERTEMP WARNING IN FLIGHT. RAN QRH AND MESSAGE CLEARED.C: MEL 49-10-1ACAT C DUE 5/27/24APU OVERTEMP WARNING IN FLIGHT. RAN QRH AND MESSAGE CLEARED.MAY 17, 2024 STATION: FAR--DEFERRED APU PER CRJ 200 MEL 49-10-1A. MX ACTION COMPLIED WITH AND PLACARD IN
- [SDR SWIA202310250024](https://openairdocs.org/sdr/SWIA202310250024.md): Unknown · warning message · Oct 24, 2023 · N914EV · Cndair CL6002B19 · Air Conditioning System
  > L 10TH DUCT WARNING MESSAGE ON CLIMB AT 15000FT. DID THE QRH PROCEDURE, DIRECTED TO GET LEFT ENGINE TO IDLE. DECLARED EMERGENCY AND DID A SINGLE ENGINE LANDING WITH RIGHT ENGINE. (FLIGHT 5541 FILED OPEN)FOUND LEAK COMING FROM LH 10TH STAGE PRSOV FLANGE CRACK F
- [SDR SWIA20231023](https://openairdocs.org/sdr/SWIA20231023.md): Unknown · warning message · Oct 23, 2023 · N914EV · Cndair CL6002B19 · Pneumatic Indicating System
  > REPEAT L 10TH DUCT WARNING MESSAGE ON CLIMB OUT. PLEASE REVIEW HISTORY AND T/S NEXT OVERNIGHTMCI TYPE: TROUBLESHOOTING PRIORITY 1 (FLIGHT 5452 FILED CLOSED)OCT 24, 2023 STATION: RDD--REMOVED AND REPLACED HEATING ELEMENT SENSOR AT A17WK PER CRJ-200 AMM 36-21
- [SDR SWIA202305220017](https://openairdocs.org/sdr/SWIA202305220017.md): Landing Gear · warning message · May 17, 2023 · N914EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING MESSAGE WHILE SELECTING GEAR DOWN. NOSE GEAR SHOWED DOWN POSITION WHILE MAIN GEAR REMAINED IN UP POSITION. MESSAGE CLEARED DURING GO AROUND. ALL THREE SHOWED DOWN. COMPLIED WITH QRH. (FLT 5135, FILED CLOSED)UPON ARRIVAL TO A/C FOUND PSEU
- [SDR SWIA2023051800017](https://openairdocs.org/sdr/SWIA2023051800017.md): Landing Gear · warning message · May 17, 2023 · N914EV · Cndair CL6002B19 · Landing Gear System
  > GEAR DISAGREE WARNING MESSAGE WHILE SELECTING GEAR DOWN. NOSE GEAR SHOWED DOWN POSITION WHILE MAIN GEAR REMAINED IN UP POSITION. MESSAGE CLEARED DURING GO AROUND. ALL THREE SHOWED DOWN. COMPLIED WITH QRH. (FLT 5135, FILED OPEN)THIS IS CURRENTLY A WORK IN PROG
- [SDR SWIA20230117](https://openairdocs.org/sdr/SWIA20230117.md): None · corroded · Jan 17, 2023 · N914EV · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > DURING CORRODED FASTENERS REMOVAL FOUND CORROSION ON RBL 9.0 SEAT RAIL SECTION FS 409.0 TO FS 409+16. (C-CHECK RO 2/18/2023) SEAT RAIL AT RBL 9.0 FROM FS409.0 TO FS409+128 WAS REMOVED,FABRICATED AND INSTALLED NEW REF REO 601R-53-00-485 REV. D 2018-01-2
- [SDR SWIA202301107](https://openairdocs.org/sdr/SWIA202301107.md): None · corroded · Jan 17, 2023 · N914EV · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *LH CABIN PRESSURE FLOOR SILL CORROSION AROUND SCREW HOLES (2EA) BETWEEN FS529.00 & FS540.25 (C-CHECK RO 2/18/2023) REMOVED CORROSION ON THE LEFT-HAND CABIN PRESSURE FLOOR SILL PANEL AROUND 2 EA. SCREW HOLES BETWEEN FS529.00 AND FS540.25, AND EVALUATED
- [SDR SWIA2023011007](https://openairdocs.org/sdr/SWIA2023011007.md): None · corroded · Jan 17, 2023 · N914EV · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME FS 589.00, BETWEEN STGR 19R - 20R. MARKED. (C-CHECK RO 2/18/2023) REMOVED CORROSION ON FRAME FS589.00, BETWEEN STGR 19R-20R REF. CRJ-200 SRM, 51-21-06. PARTS FABBED AND INSTALLED REPAIR PARTS FRAME SECTION -1 AND FRAME SPLICE -2 ON FR
- [SDR SWIA20230116](https://openairdocs.org/sdr/SWIA20230116.md): None · cracked · Jan 16, 2023 · N914EV · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > PRESSURE FLOOR SUPPORT BEAM AT FS 460.0 RBL 9.0 CASTING HAS CRACK AT UPPER RADIUS. (C-CHECK RO 2/18/2023) REMOVED CRACKED FITTING AT FS460.00, RBL 9.0, AND INSTALLED NEW FITTING, PN: 600-31068-19. REF. DWG 601R31146 REV. J, DWG 601R31118 REV. L, CRJ200
- [SDR SWIA2023011006](https://openairdocs.org/sdr/SWIA2023011006.md): None · cracked · Jan 16, 2023 · N914EV · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FS 280. BOTH AT LBL 9.0 AND RBL 9.0 (2 EA) INBOARD CLIPS HAS SUSPECT CRACKS AT UPPER RADIUS. (C-CHECK RO 2/18/2023) REMOVED AND INSTALLED 1 EA NEW INBOARD ATTACH CLIP AT LBL 9.0 AT FS 280.0 P/N 601R31113-57 AND 1 EA ATTACH CLIP AT RBL 9.0 P/N 601R31113-
- [SDR SWIA202301106](https://openairdocs.org/sdr/SWIA202301106.md): None · damaged · Jan 16, 2023 · N914EV · Cndair CL6002B19 · Passenger/Crew Doors
  > EXISTING PASSENGER DOOR SEAL STRIKER DAMAGE JUST ABOVE FORWARD UPPER PIN STOP FITTING ON FORWARD SIDE OF DOOR CUTOUT (C-CHECK RO 2/18/2023) REMOVED AND REPLACED PASSENGER DOOR SEAL STRIKER JUST ABOVE FORWARD UPPER PIN STOP FITTING ON FORWARD SIDE OF DOO
- [SDR SWIA20230114](https://openairdocs.org/sdr/SWIA20230114.md): None · dented · Jan 14, 2023 · N914EV · Cndair CL6002B19 · Air Conditioning Doors
  > GROUND AIR CONDITIONING DOOR SURROUND (LANDING PLATE) IS PUSHED IN (DENTED) AND DAMAGED. (C-CHECK RO 2/18/2023) REMOVED AND REPLACED FWD ANGLE AT GROUND AIR CONDITIONING DOOR SURROUND REF. CRJ-200 SRM, 51-42-06 AND DWG 601R35226 REV-P. COMPLIED WITH TAS
- [SDR SWIA202301007](https://openairdocs.org/sdr/SWIA202301007.md): None · dented · Jan 7, 2023 · N914EV · Cndair CL6002B19 · Fuselage Main, Frame
  > DENT NEAR FS409+16 STGR 26L (C-CHECK RO 2/18/2023) PERFORMED PERMANENT REPAIR TO DENT AREA OF FUSELAGE STATION FS409.00 AT STGR26L. REF. MHIRJ REO 601R-53-31-1258 REV -- DATED 2023-01-26. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY STRUCTURAL MAJOR
- [SDR SWIA202301006](https://openairdocs.org/sdr/SWIA202301006.md): None · dented · Jan 6, 2023 · N914EV · Cndair CL6002B19 · Wing Structure
  > *MULTIPLE DENTS NOTED ON L/H FLIGHT SPOILER UPPER SURFACE (MARKED) (C-CHECK RO 2/18/2023) REMOVED THE PAINT & EVALUATED THE MULTIPLE DENTS ON THE LH FLIGHT SPOILER REF CRJ-200 SRM 57-73-00 AND COMPLIED WITH ALL THE STEPS OF THE REO 601R-57-73-401 REV--
- [SDR SWIA202301004](https://openairdocs.org/sdr/SWIA202301004.md): None · chafed · Jan 4, 2023 · N914EV · Cndair CL6002B19 · Wing Structure
  > *CHAFFING NOTED AT R/H AILERON L/E LOWER SKIN (MARKED) (C-CHECK RO 2/18/2023) BLENDED OUT DAMAGE ON SKIN PANEL @ AIL STA.370.664 FOUND TO BE WITHIN LIMITS REF REO 670-57-61-194 REV -C DATED 2019-01-07. REMOVED AND REPLACED SKIN PANEL @ AIL STA.324.459
- [SDR SWIA202301002](https://openairdocs.org/sdr/SWIA202301002.md): None · chafed · Jan 2, 2023 · N914EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > * AFT CARGO DOOR, EXTERIOR SKIN REPAIR DOUBLER ( PREVIOUS REPAIR) HAS CHAFFED AREAS ( 2 EACH). (C-CHECK RO 2/18/2023) REMOVED & INSTALLED NEW REPAIR DOUBLER (-1) P/N 2024T-3 0.080 PO: T-58292 REF REO NO. 601R-52-31-310 REV -B DATED 2019-06-13, CRJ200
- [SDR SWIA202212300](https://openairdocs.org/sdr/SWIA202212300.md): None · dented · Dec 30, 2022 · N914EV · Cndair CL6002B19 · Wing Structure
  > THE UPPER SURFACE OF THE LH AILERON HAS MULTIPLE DENTS. PLEASE PLOT, MAP AND EVALUATED THE DAMAGE/AREA. IF THE DAMAGE IS FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICES/PROCEDURES. (C-CHECK RO 2/18/2023) DENTS ON
- [SDR SWIA20221209](https://openairdocs.org/sdr/SWIA20221209.md): None · dented · Dec 9, 2022 · N914EV · Cndair CL6002B19 · Passenger/Crew Doors
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA67724-601R-52-11-2861 N914EV MXCODEID55300-PR - DUE TO DENT IN MCD ABOUT 3/4 WAY UP DENT MEASURES 1 1/4 WIDE BY 1 3/4 LONG AND 1/32 DEPTH, COMPLIED WITH TEMPORARY DISPOSITION PER REO 601R-52-11-2861 STEPS 1 -4. PERMANE
- [SDR SWIA202265390](https://openairdocs.org/sdr/SWIA202265390.md): Unknown · odor · Apr 18, 2022 · N914EV · Cndair CL6002B19 · Fuselage Floor Panel
  > STRONG SMELL OF FUEL IN CABIN (FLIGHT 5682 - FILED CLOSED) UPON FURTHER INSPECTION, FUEL LEAK FOUND INSIDE THE APU BOX AT THE FUEL SHUTOFF SOLENOID VALVE FITTING GOING INTO FUEL CONTROL. REMOVED AND REPLACED THE PACKING ON THE FUEL SHUTOFF SOLENOID VALVE
- [SDR SWIA2019120946855](https://openairdocs.org/sdr/SWIA2019120946855.md): Support Angle · cracked · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * SUPPORT ANGLE CRACKED ON AFT SIDE OF FS 621 LEFT SIDE AT APROX STRG14L MARKED (C-CHECK) RO 12/6/2019 REMOVED AND REPLACED CRACKED SUPPORT ANGLE WITH NEW ANGLE ON AFT SIDE OF FS 621 LEFT SIDE AT APROX STRG14L IAW SRM.
- [SDR SWIA2019120946854](https://openairdocs.org/sdr/SWIA2019120946854.md): Support Angle · cracked · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * SUPPORT ANGLE CRACKED ON FS 621 RIGHT SIDE AT APROX STRG14R MARKED (C-CHECK) RO 12/6/2019 REPLACED ANGLE AT AFT SIDE OF FS621 RHS AT APPROX STGR14R IAW SRM. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**)
- [SDR SWIA2019120946853](https://openairdocs.org/sdr/SWIA2019120946853.md): Floor Support · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * L/H PRESSURE FLOOR SILL PANEL HAS SEVERAL AREAS OF CORROSION FROM FS 409+128 TO FS 559.0 (C-CHECK) RO 12/6/2019 LH PRESSURE FLOOR SILL PANEL BLENDED FROM FS 409+128 TO FS 559.0, FOUND TO BE WITHIN LIMITS AND RESTORED TO ORIGINAL IAW REO. COMPLIED WITH SKY
- [SDR SWIA2019120946852](https://openairdocs.org/sdr/SWIA2019120946852.md): Floor Support · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * L/H PRESSURE FLOOR SILL ANGLE HAS SEVERAL AREAS OF CORROSION FROM FS 409+128 TO FS 559.0 (C-CHECK) RO 12/6/2019 LH PRESSURE FLOOR SILL ANGLE IS BLENDED, FOUND TO BE WITHIN LIMITS AND RESTORED TO ORIGINAL IAW REO.
- [SDR SWIA2019120946851](https://openairdocs.org/sdr/SWIA2019120946851.md): Floor Support · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * R/H PRESURE FLOOR SILL PANEL HAS SEVERAL AREAS OF CORROSION FS 409+128 TO FS 559.0 (C-CHECK) RO 12/6/2019 REMOVED CORROSION AND EVALUATED REPAIRS AT 9 LOCATION ON R/H PRESSURE FLOOR SILL PANEL. REPAIRS FOUND TO BE WITHIN LIMITS. IAW REO. NO FASTENERS REMOV
- [SDR SWIA2019120946850](https://openairdocs.org/sdr/SWIA2019120946850.md): Floor Support · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * R/H PRESSURE FLOOR SILL ANGLE HAS SEVERAL AREAS OF CORROSION FROM FS 409+128 TO FS 559.0 (C-CHECK) RO 12/6/2019 BLENDED DAMAGE ON RH FLOOR SILL AT ALL LOCATIONS FS409.128 - FS559.0. IAW SRM. ALL WITHIN LIMITS IAW REO. RESTORED THE CIC AND TOP COAT FINISH.
- [SDR SWIA2019120946849](https://openairdocs.org/sdr/SWIA2019120946849.md): Floor Support · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * FLOOR BEAM CAP @ FS 559+16 TO FS 559+80 RBL 9 HAS CORROSION (C-CHECK) RO 12/6/2019 FABRICATED AND INSTALLED NEW FLOOR BEAM CAP IAW REO. SEE CONTINUE CARD FOR ALL DETAILS.
- [SDR SWIA2019120946848](https://openairdocs.org/sdr/SWIA2019120946848.md): Floor Support · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * L/H SILL FROM FS 559.0 TO FS 559+80 HAS CORROSION SEVERAL AREAS (C-CHECK) RO 12/6/2019 REMOVED CORROSION ON L/H FLOOR SILL FROM FS559.00 TO FS559.00+80 AND EVALUATED REPAIR. REPAIR FOUND TO BE WITHIN LIMITS AND RESTORED SILL TO ORIG. CONFIGURATION. IAW REO
- [SDR SWIA2019120946847](https://openairdocs.org/sdr/SWIA2019120946847.md): Floor Support · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * R/H SILL FROM FS 559.0 TO FS 559+80 HAS CORROSION SEVERAL AREAS (C-CHECK) RO 12/6/2019 COMPLIED WITH ALL THE STEPS IAW REO. REMOVED CORROSION ON R/H FLOOR SILL BETWEEN FS559.0 AND FS559.+80. REPLACED BLIND FASTENERS. SILL ORIGINAL THICKNESS IS 0.063 IAW SRM
- [SDR SWIA2019120946846](https://openairdocs.org/sdr/SWIA2019120946846.md): Seat Track · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * SEAT TRACK FS 559+112 TO JUST AFT OF FS 574.0 LBL 9 HAS CORROSION (C-CHECK) RO 12/6/2019 BLENDED OUT CORROSION IS OUT OF LIMITS, REMOVED, REPLACED AND INSTALLED NEW CARGO TIE-DOWN TRACK P/N 601R38779-5 AT FS559+112 TO FS568 LBL9.IAW AMM.
- [SDR SWIA2019120946845](https://openairdocs.org/sdr/SWIA2019120946845.md): Seat Track · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * SEAT TRACK FS 559+112 TO JUST AFT OF FS 574.0 RBL 9 HAS CORROSION (C-CHECK) RO 12/6/2019 REPLACED CARGO SEAT TRACK BETWEEN FS559+112 AND FS574.00 RBL 9 IAW AMM. SEE CONTINUE CARD FOR DETAILS
- [SDR SWIA2019120946844](https://openairdocs.org/sdr/SWIA2019120946844.md): Seat Track · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * SMALL SECTION OF SEAT TRACK JUST AFT OF FS 559+80 TO FS 559+96 LBL 27 HAS CORROSION (C-CHECK) RO 12/6/2019 REMOVED CORROSION ON THE AFFECTED SEAT TRACK. REF CRJ200 SRM 51-21-06. SEE CONTINUATION CARD FOR ADDITIONAL DETAILS
- [SDR SWIA2019120946843](https://openairdocs.org/sdr/SWIA2019120946843.md): Seat Track · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * SMALL SECTION OF SEAT TRACK JUST AFT OF FS 559+80 TO FS 559+96 LBL 9 HAS CORROSION (C-CHECK) RO 12/6/2019 REMOVED AND BLENDED OUT CORROSION IS WITHIN LIMITS ON SEAT TRACK AT FS559+80 TO FS559+96 LBL9. IAW SRM.
- [SDR SWIA2019120946842](https://openairdocs.org/sdr/SWIA2019120946842.md): Seat Track · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * SMALL SECTION OF SEAT TRACK JUST AFT OF FS 559+80 TO FS 559+96 RBL 27 HAS CORROSION (C-CHECK) RO 12/6/2019 REMOVED CORROSION ON THE AFFECTED SEAT TRACK. IAW SRM. REFER TO CONTINUE CARD FOR ADDITIONAL DETAILS.
- [SDR SWIA2019120946841](https://openairdocs.org/sdr/SWIA2019120946841.md): Seat Track · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * SMALL SECTION OF SEAT TRACK JUST AFT OF FS 559+80 TO FS 559+96 RBL 9 HAS CORROSION (C-CHECK) RO 12/6/2019 BLENDED OUT DAMAGE AND RESTORED FINISH TO SEAT TRACK AFT OF FS559+80 TO FS559+96. IAW SRM.
- [SDR SWIA2019120946840](https://openairdocs.org/sdr/SWIA2019120946840.md): Floorbeam · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > * CROSS BEAM TOP CAP FS 559+112 LBL 27 TO SILL HAS CORROSION (C-CHECK) RO 12/6/2019 REMOVED CORROSION AND EVALUATED REPAIRS. REPAIRS FOUND TO BE WITHIN LIMITS AND RESTORED REPAIR TO ORIG. FINISH. IAW SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
- [SDR SWIA2019120946839](https://openairdocs.org/sdr/SWIA2019120946839.md): Floorbeam · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > * CROSS BEAM TOP CAP FS 559+80 RBL 27 TO THE SILL HAS CORROSION (C-CHECK) RO 12/6/2019 BLENDED CORROSION FROM CROSS BEAM TOP CAP FS 559+80 RBL 27 TO THE SILL. THE AREA IS FOUND TO BE WITHIN LIMITS AND RESTORED TO ORIGINAL IAW SRM.
- [SDR SWIA2019120946838](https://openairdocs.org/sdr/SWIA2019120946838.md): Floorbeam · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > * CROSS BEAM TOP CAP FS 559+80 RBL 9 TO RBL 27 HAS CORROSION (C-CHECK) RO 12/6/2019 CROSS BEAM TOP CAP FS 559+80 RBL 9 TO RBL 27 IS BLENDED, FOUND TO BE WITHIN LIMITS AND RESTORED TO ORIGINAL FINISH IAW SRM.
- [SDR SWIA2019120946837](https://openairdocs.org/sdr/SWIA2019120946837.md): Floor Support · corroded · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * RH SILL FROM FS 559+80 TO FS 621.0 HAS SEVERAL AREAS OF CORROSION (C-CHECK) RO 12/6/2019 REMOVED CORROSION ON R/H FLOOR SILL FROM FS559.00+90 TO FS621.00 AND EVALUATED REPAIR. REPAIR WAS FOUND WITHIN LIMITS AND RESTORED TO ORIG. CONDITION. AIW REO. SEE CO
- [SDR SWIA2019120946836](https://openairdocs.org/sdr/SWIA2019120946836.md): Bulkhead · cracked · Dec 9, 2019 · N914EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH
- [SDR SWIA2019091746314](https://openairdocs.org/sdr/SWIA2019091746314.md): Warning System · activated · Sep 17, 2019 · N914EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE ON TAKE OFF. C/W QRH PROCEDURE ALL THREE GEAR CAME DOWN AND LOCKED. FLT DIVERTED TO MBS. (FLT#4303) CLOSED DEFERRED MLG RETRACTION SYSTEM PER.
- [SDR SWIA2019082246196](https://openairdocs.org/sdr/SWIA2019082246196.md): Engine · overtemp · Aug 22, 2019 · N914EV · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE HIGH TEMP, PEAKED 169; FOLLOWING QRH PROCEDURE ENGINE SHUTDOWN IN FLIGHT. EMERGENCY DECLARED. REMOVED AND REPLACED ENGINE OIL LEVEL SIGNAL CONDITIONER, ENGINE REPLENISHMENT SIGNAL CONDITIONER, RH ENGINE LOW-OIL LEVEL PROBE, RH ENGINE VIOLET HARN
- [SDR SWIA2019080146107](https://openairdocs.org/sdr/SWIA2019080146107.md): Sensor · out of adjust · Aug 1, 2019 · N914EV · Cndair CL6002B19 · Landing Gear Steering System
  > RECEIVED NWS STEERING INOP CAUTION MESSAGE FOLLOWED BY WOW INPUT CAUTION MESSAGE FOLLOWED BY WOW OUTPUT FAIL. NORMAL LANDING AND STEERING OPERATION. FLT 3959. COMPLIED WITH RE-RIG OF SENSOR-TO-TARGET GAP FOR NLG WOFFW PS13GA AND PS4GA IAW AMM, COMPLETED FULL
- [SDR SWIA2019080246115](https://openairdocs.org/sdr/SWIA2019080246115.md): Seal · failed · Jul 31, 2019 · N914EV · Cndair CL6002B19 · Nose/Tail Landing Gear
  > AFTER TAKEOFF NOSE GEAR DISAGREE ACCOMPANIED BY NOSE DOOR OPEN AND STEERING INOP. PERFORMED QRH PROCEDURE AND LANDED WITHOUT INCIDENT. FLT 3742. REMOVED AND REPACKED BACKUP NLG SEALS AND INSTALLED NEW GUIDE PINS IAW AMM. PERFORMED MLG EXTENSION AND RETRACTIO
- [SDR SWIA2018073044880](https://openairdocs.org/sdr/SWIA2018073044880.md): Pump · failed · Jul 15, 2018 · N914EV · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > HYD 3 LO PRESS CAUTION MESSAGE AFTER TAKE OFF. (FLT 3623) FO: 7/16/2018 CLOSED / REMOVED AND REPLACED ACMP 3A IAW AMM. SERVICED HYD SYSTEM 3, OPS CHECK GOOD.
- [SDR SWIA201743729](https://openairdocs.org/sdr/SWIA201743729.md): Bracket · broken · Sep 8, 2017 · N914EV · Cndair CL6002B19 · Nose/Tail Landing Gear
  > RECEIVED A GEAR DISAGREE WARNING MESSAGE. CREW COMPLIED WITH QRH & RETURNED TO FIELD. REPLACED THE NOSE GEAR UPLOCK BRACKET. SYSTEM OPS CHECKED GOOD.
- [SDR SWIA201743519](https://openairdocs.org/sdr/SWIA201743519.md): Skin · cracked · Jun 6, 2017 · N914EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LOWER WING PLANK HAS MULTIPLE INDICATIONS NOTED ON THE LANDING FOR ACCESS PANEL 550BB ON THE OTBD SIDE AND FWD SIDE. REPAIRED IAW REO.
- [SDR SWIA201743518](https://openairdocs.org/sdr/SWIA201743518.md): Skin · cracked · Jun 6, 2017 · N914EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LOWER WING PLANK HAS MULTIPLE INDICATIONS NOTED ON THE LANDING FOR ACCESS PANEL 540DB ON THE OTBD SIDE, BOTH.200 INCH. REPAIRED IAW REO.
- [SDR SWIA201743515](https://openairdocs.org/sdr/SWIA201743515.md): Skin · cracked · Jun 6, 2017 · N914EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LOWER RT WING PLANK HAS ONE INDICATION NOTED ON THE LANDING FOR ACCESS PANEL 650GB ON THE AFT SIDE. REPAIRED IAW REO.
- [SDR SWIA201743517](https://openairdocs.org/sdr/SWIA201743517.md): Skin · cracked · Jun 5, 2017 · N914EV · Cndair CL6002B19 · Wing, Plate/Skin
  > MULTIPLE INDICATIONS NOTED IN LOWER WING PLANK AT RT BOOST PUMP ACCESS PANEL LANDING 610CB AROUND ENTIRE CIRCUMFERENCE HORIZONTAL AND VERTICAL SURFACES. REPAIRED IAW REO.

Next page: https://openairdocs.org/aircraft/N914EV/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 = 'N914EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N914EV/reports

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