# Service difficulty reports: N919EV

A list on [N919EV](https://openairdocs.org/aircraft/N919EV.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 6 · 253 reports

- [SDR SWIA2026100877554](https://openairdocs.org/sdr/SWIA2026100877554.md): Hydraulic Line · failed · Oct 8, 2026 · N919EV · Cndair CL6002B19 · Hydraulic System, Main
  > HYD 1 LO PRESS ON CLIMB OUT, RAN QRH DID NOT FIX ISSUE, HAD TO TURN PUMP OFF, SHOWED 600 PSI & ZERO FLUID QTY. FLIGHT 5133. REF AML 202066 FOR ED1 R & R, REF AML 2011651 FOR ENGINE DRIVEN PUMP EDP AFTER DRY OPS DUE TO HYDRAULIC FLUID LOSS COMPLIANCE, REF
- [SDR SWIA2026032075564](https://openairdocs.org/sdr/SWIA2026032075564.md): Warning Message · false activation · Mar 20, 2026 · N919EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > NOSE DOOR OPEN MASTER WARNING ON CLIMB OUT AND CRUISE TWICE. WENT OUT THE FIRST TIME, CAME BACK ON A FEW MINUTES LATER. (FLIGHT 5197) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31924622 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CAMP 31925918 FOR MX A
- [SDR SWIA2026031975551](https://openairdocs.org/sdr/SWIA2026031975551.md): Door · warning message · Mar 19, 2026 · N919EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER TAKEOFF NOSE DOOR OPEN WARNING MESSAGE RECEIVED. RAN QRH AND RETURNED TO NEAREST SUITABLE AIRPORT. (FLIGHT 5025) PERFORMED DETAILED VISUAL INSPECTION OF NLG DOORS PER AMM 32-20-00. NO DEFECTS NOTED, VERIFIED NLG DOORS OPERATE NORMALLY. FOUND NLG DOORS
- [SDR SWIA2026010500002](https://openairdocs.org/sdr/SWIA2026010500002.md): Landing Gear · warning message · Jan 2, 2026 · N919EV · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > MLG DISAGREE, ONLY NOSE GEAR INDICATING DOWN, RAN QRH PROCEDURE, PULLED LANDING GEAR MANUAL RELEASE HANDLE TO DEPLOY GEAR, GEAR DEPLOYED WITH MANUAL RELEASE HANDLE. (FLIGHT 4674 - FILED CLOSED)ARRIVED AT AIRCRAFT AND INTERROGATED PSCU PLEASE SEE ATTACHED FILE
- [SDR SWIA202507090008](https://openairdocs.org/sdr/SWIA202507090008.md): Connector · shorted · Jul 8, 2025 · N919EV · Cndair CL6002B19 · Fire Protection System Wiring
  > ANTI ICE DUCT WARNING AT CRUISE. QRH COMPLETED. MESSAGE CLEARED. (FLIGHT 5135 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30455056 WITH THE FOLLOWING CORRECTIVE ACTION: "TORUBLESHOT THE A/I DUCT WARNING IN REFERENCE TO WM 36-21-00. CHECKED PI
- [SDR SWIA202506240328](https://openairdocs.org/sdr/SWIA202506240328.md): Structure · damaged · Mar 28, 2025 · N919EV · Cndair CL6002B19 · Wing Main, Frame Structure
  > TEMPORARY REPAIR OF THE RH & LH LOWER WING PLANK AT BL45.00 BETWEEN R/SPAR & STR 6 (C-CHECK RO 06/23/2025)PERFORMED TEMPORARY REPAIR OF THE RH AND LH LOWER WING PLANK AT BL45.00 BETWEEN R/SPAR AND STR 6. REF K- REO 601R-21-3893 REV -- DATED 2025-03-08. COMPLI
- [SDR SWIA2025062400318](https://openairdocs.org/sdr/SWIA2025062400318.md): Panel · cracked · Mar 18, 2025 · N919EV · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > R/H ENGINE NACELLE & PYLON LANDING FOR PNL 422AB (BENT/CRACKED) LOC. FWD INBD (MARKED) (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED NEW RIB, PYLON STRUCT P/N 601-37004-86,REF. CRJ-200 SRM 51-42-06, REF. CRJ-200 SRM 51-42-21, REF.CRJ-200 SRM 51-45-00 AND DR
- [SDR SWI2025F00763](https://openairdocs.org/sdr/SWI2025F00763.md): Fitting · cracked · Mar 6, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CO-PILOT SIDE WINDOW POST LOWER FITTING P/N: 601R33235-2 CRACKED. #29747104 (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED 1EA NEW R/H LWR SIDE POST FITTING (P/N 601R33235-2) PER CRJ200SRM 51-42-21 AND DWG 601R33007 REV -U. COMPLIED WITH SKYWEST TASK CARD 51-90
- [SDR SWIA2025062400306](https://openairdocs.org/sdr/SWIA2025062400306.md): Window Frame · cracked · Mar 6, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CO-PILOT SIDE WINDOW POST LOWER FITTING P/N: 601R33235-4 CRACKED. #29747105 (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED 1EA NEW R/H COCKPIT SIDE POST LWR FITTING (P/N 601R33235-4) PER CRJ200SRM 51-42-21 AND DWG 601R33007 REV -U. COMPLIED WITH SKYWEST TASK CA
- [SDR SWIA202506240301](https://openairdocs.org/sdr/SWIA202506240301.md): Skin · dented · Mar 1, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT ON EXTERIOR SKIN AT FASTENER AT FS559.00 BETWEEN STGR3R - STGR4R AS MARKED (C-CHECK RO 06/23/2025) SUSPECTED DENTED AREA AT FS559.00 STGR3R-STGR4R FOUND TO BE A PREVIOUSLY BLENDED AREA. REPAIRED BLEND AREA AT FS544.00-FS559.00+16 STGR2R-STGR5R PER REO 6
- [SDR SWI2025F00738](https://openairdocs.org/sdr/SWI2025F00738.md): Window Frame · cracked · Feb 26, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CO-PILOT SIDE POST LWR OTBD HOLE CRACKED (C-CHECK RO 06/23/2025) INSTALLED NEW CO-PILOT SIDE WINDOW POST REF CRJ200 SRM 51-42-21 AND DWG# 601R33007 REV-U. CAL TOOL TORQUE SCREWDRIVER TUC9692 DUE 31-MAR-25 C/W 51-900-1003-SKY
- [SDR SWIA2025062400226](https://openairdocs.org/sdr/SWIA2025062400226.md): Intercostal · corroded · Feb 26, 2025 · N919EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR MID DD2 INTERCOSTAL IS CORRODED (C-CHECK RO 06/23/2025)INSTALLED NEW REMOVED PAX DOOR MID DD2 INTERCOSTAL IAW. CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21 AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY
- [SDR SWI2025F00756](https://openairdocs.org/sdr/SWI2025F00756.md): Intercostal · corroded · Feb 22, 2025 · N919EV · Cndair CL6002B19 · Passenger/Crew Doors
  > (MX 29683591) PAX DOOR AFT DD4 INTERCOSTAL IS CORRODED (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED NEW PAX DOOR AFT DD4 INTERCOSTAL. REF. CRJ200 SRM 51-42-06. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWI2025F00755](https://openairdocs.org/sdr/SWI2025F00755.md): Intercostal · corroded · Feb 22, 2025 · N919EV · Cndair CL6002B19 · Passenger/Crew Doors
  > ( MX 29683654) PAX DOOR MID DD4 INTERCOSTAL IS CORRODED (C-CHECK RO 06/23/2025) INSTALLED NEW PAX DOOR MID DD4 INTERCOSTAL IAW. CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21 AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY
- [SDR SWI2025F00754](https://openairdocs.org/sdr/SWI2025F00754.md): Intercostal · corroded · Feb 22, 2025 · N919EV · Cndair CL6002B19 · Passenger/Crew Doors
  > ( MX 29683706) PAX DOOR MID DD3 INTERCOSTAL IS CORRODED (C-CHECK RO 06/23/2025)INSTALLED NEW PAX DOOR MID DD3 INTERCOSTAL IAW. CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21 AND DWG 601R31702 REV. N COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY
- [SDR SWI2025F00753](https://openairdocs.org/sdr/SWI2025F00753.md): Intercostal · corroded · Feb 22, 2025 · N919EV · Cndair CL6002B19 · Passenger/Crew Doors
  > (MX 29683552) UPON REMOVAL OF PAX DOOR INNER SKIN FOUND AFT DD5 INTERCOSTAL CORRODED ON 2 ELEMENT. (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED NEW PASSENGER DOOR AFT DD5 INTERCOSTAL AND CLEAT. REF. CRJ200 SRM 51-42-06. AND DWG 601R31702 REV. -N. COMPLIED WIT
- [SDR SWI2025F00752](https://openairdocs.org/sdr/SWI2025F00752.md): Intercostal · corroded · Feb 22, 2025 · N919EV · Cndair CL6002B19 · Passenger/Crew Doors
  > (MX 29683525) UPON REMOVAL OF PAX DOOR INNER SKIN FOUND AFT DD2 INTERCOSTAL CORRODED ON 2 ELEMENT. (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED NEW PASSENGER DOOR AFT DD2 INTERCOSTAL. REF. CRJ200 SRM 51-42-06 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD
- [SDR SWIA2025062400222](https://openairdocs.org/sdr/SWIA2025062400222.md): Intercostal · corroded · Feb 22, 2025 · N919EV · Cndair CL6002B19 · Passenger/Crew Doors
  > (MX 29683568) PAX DOOR AFT DD3 INTERCOSTAL IS CORRODED (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED NEW PAX DOOR AFT DD3 INTERCOSTAL. REF. CRJ200 SRM 51-42-06.AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWI2025F00750](https://openairdocs.org/sdr/SWI2025F00750.md): Retainer · corroded · Feb 20, 2025 · N919EV · Cndair CL6002B19 · Passenger/Crew Doors
  > (MX 29672880) UPON REMOVAL OF PAX DOOR UPPER SEAL RETAINER FOUND EXFOLIATED CORROSION ON 2 ELEMENT AFT ANGLE SUPPORT. (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED NEW PAX DOOR AFT SUPPORT ANGLE IAW CRJ 200 SRM 51-42-06 AND IAW DWG 601R31702 REV. N.. COMPLIED
- [SDR SWIA2025062400220](https://openairdocs.org/sdr/SWIA2025062400220.md): Former · corroded · Feb 20, 2025 · N919EV · Cndair CL6002B19 · Passenger/Crew Doors
  > ( MX 29673788) UPON REMOVAL OF PAX DOOR INNER SKIN FOUND FWD FORMER CORRODED (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED NEW PAX DOOR FWD FORMER IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV. N.. COMPLIED WITH TASK CARD 51-900-100
- [SDR SWIA2025062400219](https://openairdocs.org/sdr/SWIA2025062400219.md): Doubler · cracked · Feb 19, 2025 · N919EV · Cndair CL6002B19 · Passenger/Crew Doors
  > MX 29666702) PAX DOOR DOUBLER, PULL IN CAM SUSPECTED CRACK (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED NEW PAX DOOR FWD PULL CAM DOUBLER IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV. N COMPLIED WITH TASK CARD 51-900-1003-SKY
- [SDR SWIA202506240218](https://openairdocs.org/sdr/SWIA202506240218.md): Stringer Clip · gouged · Feb 18, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > R/H INTERIOR FRAME AND STRINGER GUSSET GOUGED AT FS 559.00+48 STGR6 (MARKED) (C-CHECK RO 06/23/2025)REMOVED AND FABRICATED AND INSTALLED 1EA NEW GUSSET (P/N 601R38522-19) AT FS559.00+48 STGR6R PER CRJ200SRM 51-42-06-00 AND DWG 601R38522 REV A. SEE CONTINUATIO
- [SDR SWI2025F00760](https://openairdocs.org/sdr/SWI2025F00760.md): Floorbeam · cracked · Feb 15, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FOUND FLOOR SUPPORT CLIP AT FS 280 & RBL 9.0 INBOARD CRACKED. MX 29646977. (C-CHECK RO 06/23/2025)REMOVED CRACKED FLOOR SUPPORT CLIP AND REPLACED WITH NEW AT FS 280 & RBL 9.0 INBOARD IAW CRJ200 SRM 51-42-21-00 & DWG NO 601R31113 REV AD. SEE CONTINUATION CARD
- [SDR SWI2025F00759](https://openairdocs.org/sdr/SWI2025F00759.md): Floorbeam · cracked · Feb 15, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FOUND FLOOR SUPPORT CLIP AT FS 280 & LBL 9.0 OUTBOARD CRACKED. MX 29647003 (C-CHECK RO 06/23/2025)REMOVED CRACKED CLIP AND INSTALLED FABRICATED FLOOR SUPPORT CLIP AT FS 280 & LBL 9.0 OUTBOARD IAW CRJ200 SRM 51-42-21-00 & REO 601R-53-11-926 REV -B, 2006/05/10.
- [SDR SWIA2025062400215](https://openairdocs.org/sdr/SWIA2025062400215.md): Floorbeam · cracked · Feb 15, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FOUND FLOOR SUPPORT CLIP AT FS 280 & LBL 9.0 INBOARD CRACKED. MX 29646990. (C-CHECK RO 06/23/2025)REMOVED CRACKED CLIP AND REPLACED WITH FABRICATED FLOOR SUPPORT CLIP AT FS 280 & LBL 9.0 INBOARD IAW CRJ200 SRM 51-42-21-00 & REO 601R-53-11-926 REV -B, 2006/05/
- [SDR SWIA2025062400214](https://openairdocs.org/sdr/SWIA2025062400214.md): Hinge Fitting · corroded · Feb 14, 2025 · N919EV · Cndair CL6002B19 · Elevator Structure
  > UPON REMOVAL AND INSPECTION ON JOB HN00219316 CAMP #29599374, FOUND R/H ELEVATOR #1 L/E HINGE FITTING ASSY P/N 600-24043-1 @ ES16.52 TO HAVE PITTING CORROSION IN BEARING BORES OF BOTH HINGE HALVES. REPLACE HINGE FITTING ASSY. (C-CHECK RO 06/23/2025)INSTALLED
- [SDR SWI2025F00761](https://openairdocs.org/sdr/SWI2025F00761.md): Lug · gouged · Feb 13, 2025 · N919EV · Cndair CL6002B19 · Trailing Edge Flaps
  > LH O/B FLAP HINGE BOX(WS178.00) FWD MOUNT LUG GOUGED. CAMP # 29632585. (C-CHECK RO 06/23/2025)REMOVED GOUGE ON LH O/B FLAP HINGE BOX(WS178.00) FWD MOUNT LUG PER REF.CRJ/200 SRM.51-12-00-00 AND COMPLIED WITH ALL THE STEPS OF THE REO 601R-57-21-3903 REV -- DATE
- [SDR SWIA2025062400213](https://openairdocs.org/sdr/SWIA2025062400213.md): Hinge Fitting · corroded · Feb 13, 2025 · N919EV · Cndair CL6002B19 · Elevator Structure
  > UPON REMOVAL AND INSPECTION ON JOB HN00219315 CAMP #29599361, FOUND L/H ELEVATOR #1 L/E HINGE FITTING ASSY P/N 600-24043-1 @ ES16.52 TO HAVE PITTING CORROSION IN BEARING BORES OF BOTH HINGE HALVES. REPLACE HINGE FITTING ASSY. (C-CHECK RO 06/23/2025)REMOVED EX
- [SDR SWI2025F00762](https://openairdocs.org/sdr/SWI2025F00762.md): Window Frame · cracked · Feb 12, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CRACK NOTED AT L/H WINDSHIELD SIDE SUPPORT POST CHANNEL BELOW WL110 (MARKED) (C-CHECK RO 06/23/2025)INSTALLED NEW LH WINDSHIELD SUPPORT ANGLE P/N 601R34032-21 REF CRJ 200 SRM 51-42-06-00 REV 39 DATE MAR10/21 DRWG 601R34032 REV -V AND DRWG 601R33010 REV -J COM
- [SDR SWIA2025062400212](https://openairdocs.org/sdr/SWIA2025062400212.md): Skin · gouged · Feb 12, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN GOUGED FS559.00+112.00 AT STGR20R (C-CHECK RO 06/23/2025)PERFORMED BLEND REPAIR OF EXTERIOR SKIN GOUGE AT F.S 559+112 STGR 20R REF. REO 601R-53-51-705 REV. -- DATED 2025-02-28 ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWI2025F00758](https://openairdocs.org/sdr/SWI2025F00758.md): Cleat · corroded · Feb 11, 2025 · N919EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR CLEAT COMMON TO FORWARD INTERCOSTAL DD6 CORROSION (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED NEW CLEAT COMMON TO FWD DD6 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWI2025F00757](https://openairdocs.org/sdr/SWI2025F00757.md): Former · corroded · Feb 11, 2025 · N919EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT FORMER CORROSION INSIDE BEHIND PANEL 832GR (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED NEW PAX DOOR AFT FORMER IAW CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025062400211](https://openairdocs.org/sdr/SWIA2025062400211.md): Intercostal · corroded · Feb 11, 2025 · N919EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL DD6 CORROSION (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED NEW PASSENGER DOOR INTERCOSTAL DD6. REF. CRJ200 SRM 51-42-06, CRJ SRM 51-42-21 AND DWG 601R318057 REV. -N. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025062400208](https://openairdocs.org/sdr/SWIA2025062400208.md): Rib · cracked · Feb 8, 2025 · N919EV · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > S/N 0498LEFT WING, BATT RIB IS CRACKED X2 PLACES. FLAGGED (C-CHECK RO 06/23/2025)REMOVED DAMAGED BATT RIB CAP AND INSTALLED NEW BATT RIB CAP REF CRJ200 SRM 51-42-21 DRAWING # 600-10204 REV -M. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWI2025F00751](https://openairdocs.org/sdr/SWI2025F00751.md): Pressure Deck · corroded · Feb 6, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Structure
  > RH PRESSURE FLOOR SILL PANEL HAS CORROSION AT FS424 (C-CHECK RO 06/23/2025)REMOVED CORROSION RH PRESSURE FLOOR SILL PANEL AT FS424. REF. CRJ-200 SRM 51-21-06 AND PERFORMED EVALUATION WITH -IN LIMITS REF. CRJ-200 SRM 53-41-45 AND COMPLIED WITH ALL THE STEPS O
- [SDR SWIA2025062400206](https://openairdocs.org/sdr/SWIA2025062400206.md): Pressure Deck · corroded · Feb 6, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Structure
  > LH PRESSURE FLOOR SILL PANEL HAS CORROSION AT FS501 (C-CHECK RO 06/23/2025)REMOVED CORROSION FROM LH PRESSURE FLOOR SILL PANEL AT FS501 REF. CRJ-200 SRM 51-21-06, PERFORMED EVALUATION WITH-IN REF. CRJ-200 SRM 53-41-45 AND COMPLIED WITH ALL THE STEPS OF THE
- [SDR SWI2025F00764](https://openairdocs.org/sdr/SWI2025F00764.md): Hinge Box · damaged · Feb 4, 2025 · N919EV · Cndair CL6002B19 · Trailing Edge Flaps
  > FOUND (NICK(S)/GOUGE) DAMAGE AT FWD INBD SIDE OF L/H FLAP HINGE BOX AT WS 220.00 (MARKED) (C-CHECK RO 06/23/2025)REMOVED AND REPLACED THE L/H FWD INBD BUSHING ON THE L/H OUTBD FLAP HINGE BOX WS220.00 PER REO 601R-57-21-3901 REV -- DATE 2025-02-18 STEP 1. & CR
- [SDR SWIA2025062400204](https://openairdocs.org/sdr/SWIA2025062400204.md): Floor Support · cracked · Feb 4, 2025 · N919EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING AUDIT OF 48MO TASK CARD 53-140-505(DETAILED INSPECTION OF THE CABIN FLOOR SUPPORT STRUCTURE FROM FS280.0 TO FS409.0 (CPCP)) FOUND CRACKED CLIP ON AFT SIDE OF 280 AT RBL9. (C-CHECK RO 06/23/2025)REPLACED CRACKED FLOOR SUPPORT CLIP AT FS 280 & RBL 9.0 A
- [SDR SWI2025F00765](https://openairdocs.org/sdr/SWI2025F00765.md): Floor Support · corroded · Jan 31, 2025 · N919EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR HAND RAIL NUTPLATE FLOOR SUPPORTS COMMON TO SILL ARE CORRODED BETWEEN FS310-FS349 (MARKED) (C-CHECK RO 06/23/2025)REMOVED & REPLACED 601R31527-217 - BRACKET ASSYS & 601R31527-137 - CLEATS WITH NEW BETWEEN FS310-FS349 IAW CRJ200 SRM 51-42-06-00 & DWG
- [SDR SWIA202506240131](https://openairdocs.org/sdr/SWIA202506240131.md): Door Sill · corroded · Jan 31, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Structure
  > PASSENGER DOOR LOWER SILL HAS CORROSION FORWARD OF FS349.00 AS MARKED (C-CHECK RO 06/23/2025)INSTALLED NEW SILLL, AFT LOWER CORNER 600-31535-70 FWD OF FS349.00. REF CRJ 200 SRM 51-42-06-00 REV 39 DATE MAR 10/21CRJ 200 SRM51-42-21-00 REV 39 DATE MAR 10/21 DRWG
- [SDR SWIA2025062400130](https://openairdocs.org/sdr/SWIA2025062400130.md): Skin · dented · Jan 30, 2025 · N919EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > DENT NOTED ON CARGO DOOR SILL (MARKED) (C-CHECK RO 06/23/2025)INSTALLED NEW CARGO DOOR SILL REF CRJ200 SRM 51-42-06, REF CRJ200 SRM 51-42-21, AND DWG 601R35011-R AND COMPLIED WITH REO 601R-53-61-1574 REV-B DATED 2012-04-15. COMPLIED WITH SKYWEST TASK CARD 51
- [SDR SWI2025F00746](https://openairdocs.org/sdr/SWI2025F00746.md): Frame · corroded · Jan 30, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Frame
  > MULTIPLE SPOTS OF CORROSION NOTED ON FRAME 589 BETWEEN STRG19R-20R ON FWD FACE AND FLANGE AND BETWEEN STRG24R-25L ON TOP FLANG AND AFT FACE (MARKED) (C-CHECK RO 06/23/2025)REMOVED MULTIPLE SPOTS OF CORROSION NOTED ON FRAME 589 BETWEEN STRG19R-20R ON FWD FACE
- [SDR SWI2025F00745](https://openairdocs.org/sdr/SWI2025F00745.md): Floor Support · cracked · Jan 30, 2025 · N919EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING AUDIT OF 48MO TASK CARD 53-160-502 (DETAILED INSPECTION OF THE PRESSURE FLOOR-SUPPORT BEAMS, FS409.0+128 TO FS559.0 (CPCP)) FOUND THE INBOARD CLIP FOR THE INTERCOSTAL, AT APPROX FS484.00 BETWEEN LBL27.00 AND THE LH FLOOR SILL, APPEARS TO HAVE A CRACK AT
- [SDR SWI2025F00744](https://openairdocs.org/sdr/SWI2025F00744.md): Frame · corroded · Jan 30, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Frame
  > MULTIPLE SPOTS OF CORROSION NOTED ON FRAME 574 BETWEEN STRG19R-20R ON FWD AND AFT FACE AND BETWEEN STRG25-STRG27 (MARKED) (C-CHECK RO 06/23/2025)REPAIRED AND COMPLIED WITH REO 601R-53-61-8297 REV--DATED 2025-03-07 SHEET 4 STEPS 1-14 ALL STEPS HAVE BEEN COMPL
- [SDR SWI2025F00743](https://openairdocs.org/sdr/SWI2025F00743.md): Stringer · cracked · Jan 30, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STGR3L IS CRACKED AT THE ATTACH POINT OF THE PASSENGER DOOR UPPER SILL FS379.00 (MARKED) (C-CHECK RO 06/23/2025)INSTALLED STGR3L FS379.00-FS394.00 SPLICE REPAIR PER CRJ200SRM 53-00-03-02 STEP 5.A.(14)-(15) AND FIG 202 SH 2, AND DWG 601R31016 REV D. SPLICE REP
- [SDR SWI2025F00739](https://openairdocs.org/sdr/SWI2025F00739.md): Frame · corroded · Jan 30, 2025 · N919EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS621.00 LOWER FLANGE CORRODED BETWEEN STGR22L - STGR25L AS MARKED (C-CHECK RO 06/23/2025)CUT AND REMOVED CAP ANGLE SECTOR BETWEEN APROX BL13.00 - BL24.00 REF REO 601R-53-61-8291 REV --(P1) DATE 2025-02-25 AND INSTALLED NEW CAP ANGLE SECTOR BETWEEN APPROX. B
- [SDR SWIA20250624129](https://openairdocs.org/sdr/SWIA20250624129.md): Housing · damaged · Jan 29, 2025 · N919EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR HANDLE HOUSING HAS STRIKE DAMAGE FROM THE HANDLE IN SEVERAL AREAS (MARKED) (C-CHECK RO 06/23/2025)INSTALLED NEW AFT CARGO DOOR HOUSING REF CRJ200 SRM 51-42-21 AND DWG 601R35027 REV-AY, PRESSURE LEAK WAS GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY
- [SDR SWIA202412010005](https://openairdocs.org/sdr/SWIA202412010005.md): Striker · dented · Dec 5, 2024 · N919EV · Cndair CL6002B19 · Passenger/Crew Doors
  > MCD STRIKER AS SMALL DENT FROM PAX DOOR SUPPORT WHEEL (FILED CLOSED) PERFORMED RERPAIR TO PASSENGER DOOR SEAL STRIKER IAW REO 601R-53-22-033 REV-D DATED 2014/02/27 REPAIR TYPE 1. COMPLIED WITH TASK CARD 51-900-1003-SKY FOR STRUCTURAL MAJOR REPAIR. COMPLE
- [SDR SWIA2025062401125](https://openairdocs.org/sdr/SWIA2025062401125.md): Skin · cracked · Nov 25, 2024 · N919EV · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA74167-601R-53-11-238 919EV-PR1 - PERFORMED VISUAL INSPECTION OF LH TRU DOOR AFT LATCH CUTOUT CRACK IN REFERENCE TO REO 601R-53-11-2381 REV A DATED 2019-07-15 STEPS 1-3. NO DAMAGE WAS FOUND AROUND FASTENERS OR DAMAGE E
- [SDR SWIA2024060600005](https://openairdocs.org/sdr/SWIA2024060600005.md): Strut · discharged · Jun 5, 2024 · N919EV · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE WARNING MESSAGE ON TAKEOFF WHILE MOVING LEVER INTO UP POSITION. PERFORMED QRH MESSAGE CLEARED AFTER PERFORMING MANUAL EXTENSION. (FLIGHT 4645 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28342242 WITH THE FOLLOWING CORRECTIVE ACTION

Next page: https://openairdocs.org/aircraft/N919EV/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 = 'N919EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N919EV/reports

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