# Service difficulty reports: N916EV

A list on [N916EV](https://openairdocs.org/aircraft/N916EV.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 5 · 214 reports

- [SDR SWIA2026090977110](https://openairdocs.org/sdr/SWIA2026090977110.md): Vane · out of limits · Sep 9, 2026 · N916EV · Cndair CL6002B19 · Trailing Edge Flaps
  > REPLACE LEFT INBD FLAP INBD VANE CAP. OPEN
- [SDR SWIA2026030375431](https://openairdocs.org/sdr/SWIA2026030375431.md): Bracket · damaged · Mar 3, 2026 · N916EV · Cndair CL6002B19 · Passenger/Crew Doors
  > DAMAGE TO THE MCD PULLEY MOUNTING BRACKET AND SKIN (FLIGHT 4696) PERFORMED PERMANENT REPAIR TO PAX DOOR INNER SKIN AND FORMER AT FS347.25 AND BTW DATUM #3 AND #5 IAW REO 601R-52-11-3088 REV-- DATE 2026-03-03 STEPS 4-21. SEE CP 31820099 FOR STEPS 1 AND 2 OF R
- [SDR SWIA2025100400024](https://openairdocs.org/sdr/SWIA2025100400024.md): Frame · dented · Oct 24, 2025 · N916EV · Cndair CL6002B19 · Fuselage Main, Frame
  > COMPLY WITH REO 601R-53-11-4030, TEMPORARY REPAIR FOR DENT DAMAGE TO FRAME WEB AT BS 241.60, RBL 5.50 - RBL 11.16. COMPLIED WITH REO 601R-53-11-4030, REV-, TEMPORARY REPAIR FOR DENT DAMAGE TO FRAME WEB AT FS 241.60 AND BETWEEN RBL 5.50 €“ RBL 11.16. ENSURE
- [SDR SWIA2025102700024](https://openairdocs.org/sdr/SWIA2025102700024.md): Frame · dented · Oct 24, 2025 · N916EV · Cndair CL6002B19 · Fuselage Main, Frame
  > COMPLY WITH REO 601R-53-11-4030 (LATEST REVISION) TEMPORARY REPAIR FOR DENT DAMAGE TO FRAME WEB AT FS 241.60 AND BETWEEN RBL 5.50 €“ RBL 11.16. (FILED OPEN)
- [SDR SWIA2025100401](https://openairdocs.org/sdr/SWIA2025100401.md): Skin · dented · Oct 1, 2025 · N916EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ONE DENTED AREA ON RT TOP FUSELAGE SKIN, DWG 601R33010. AND ONE DEFORMED AREA ON BS 241.60 FRAME. BETWEEN BS 233.276 - 241.60 BETWEEN BL 0.0 - RBL11.16. REF REO 601R-53-11-4021. REPAIRED DENTED AREA ON RT TOP FUSELAGE SKIN IAW REO 601R-53-11-4022, REV-. CO
- [SDR SWIA202506301112](https://openairdocs.org/sdr/SWIA202506301112.md): Skin · dented · Nov 12, 2024 · N916EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > THERE IS ONE SMALL PROTRUDING DENT LOCATED IN THE BAY BETWEEN FS 589.00 AND FS 605.00 AND BETWEEN STRINGERS 25L AND 26L. (FILED CLOSED)PERFORMED A PERMANENT REPAIR TO THE AREA OF THE SKIN AND PLATING - REPAIR NO. 1 - EXTERNAL NON-FLUSH PERMANENT REPAIRS - PRE
- [SDR SWIA202506301107](https://openairdocs.org/sdr/SWIA202506301107.md): Nut Plate · corroded · Nov 7, 2024 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CORROSION AROUND NUTPLATE SCREW HOLE AT APPROX. FS531.00 AND RBL42.70. (PRESSURE FLOOR) (FILED CLOSED)BLENDED CORROSION AROUND NUTPLATE SCREW HOLE AT APPROX FS531.00 AND RBL 42.70 (PRESSURE FLOOR) WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICK
- [SDR SWIA202506301029](https://openairdocs.org/sdr/SWIA202506301029.md): Bolt · seized · Oct 29, 2024 · N916EV · Cndair CL6002B19 · Ailerons
  > DURING REMOVAL OF THE LH AILERON FOUND THE ANTI ROTATION TAB BOLT SEIZED INTO THE #3 HINGE FITTING (FILED CLOSED)REMOVED AND REPLACED THE LH FITTIING, AILERON, HINGE NO.3 IN REFERENCE WITH THE CRJ-200 SRM 51-42-21, DWG 601R10003 AND DWG 601R10006. COMPLIED W
- [SDR SWIA202506301025](https://openairdocs.org/sdr/SWIA202506301025.md): Skin · damaged · Oct 25, 2024 · N916EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE BELLY SKIN AND STRUCTURE AT AFT NLG BAY BULKHEAD AT FS 235.00 TO FS 250.00 AND BETWEEN STRINGERS 26L TO 26R DAMAGED DUE TO CONTACT WITH NLG ASSY. (FILED CLOSED)COMPLIED WITH REO 601R-53-11-3953 REV -- DATED: 2024-12-13 AND ISE-STR-24-077 SHORING MEMO
- [SDR SWIA202506301023](https://openairdocs.org/sdr/SWIA202506301023.md): Pump · cracked · Oct 23, 2024 · N916EV · Cndair CL6002B19 · Fuel Boost Pump
  > LH BOOST PUMP SATELLITE HOLE ALMOST MOST FORWARD AND SLIGHTLY TO THE LEFT, HAS EDDY CURRENT CRACK INDICATION (HALF SCREEN) GOING OUTBOARD. (FILED CLOSED)REPAIRED LH BOOST PUMP SATELLITE HOLE ALMOST MOST FORWARD AND SLIGHTLY TO THE LEFT IN REF. TO REO 601R-57-
- [SDR SWIA202410240003](https://openairdocs.org/sdr/SWIA202410240003.md): Pump · cracked · Oct 23, 2024 · N916EV · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > LH BOOST PUMP SATELLITE HOLE ALMOST MOST FORWARD AND SLIGHTLY TO THE LEFT, HAS EDDY CURRENT CRACK INDICATION (HALF SCREEN) GOING OUTBOARD. (FILED OPEN)
- [SDR SWIA2023050400001](https://openairdocs.org/sdr/SWIA2023050400001.md): Unknown · warning message · May 1, 2023 · N916EV · Cndair CL6002B19 · Cabin Pressure Indicator
  > CABIN ALT CAUTION, THEN CABIN ALT WARNING. RAN QRH PRESSURE DIFFERENTIAL WOULD NOT GO ABOVE 1.5. SWAPPED BLEEDS TO APU ON DESCENT DID NOT CHANGE. PASSENGER MASKS DROPPED. (FLT 5286 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26564546 WITH THE FO
- [SDR SWIA2023050200001](https://openairdocs.org/sdr/SWIA2023050200001.md): Unknown · warning message · May 1, 2023 · N916EV · Cndair CL6002B19 · Cabin Pressure Indicator
  > CABIN ALT CAUTION, THEN CABIN ALT WARNING. RAN QRH PRESSURE DIFFERENTIAL WOULD NOT GO ABOVE 1.5. SWAPPED BLEEDS TO APU ON DESCENT DID NOT CHANGE. PASSENGER MASKS DROPPED. (FLT 5286 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202163087](https://openairdocs.org/sdr/SWIA202163087.md): None · worn · Dec 5, 2021 · N916EV · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > PAX DOOR FUSELAGE HALF PIANO HINGE WORN. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, FORM M-337 WILL BE REQUIIRED. REFERENCE CP23945301 ( FILED - CLOSED) NEW PAX DOOR FUSELAGE HALF PIANO HINGE INSTALLED IN REFERENCE TO CRJ200 REO 601R-53-21-656 ALSO IN
- [SDR ICRR202109010001](https://openairdocs.org/sdr/ICRR202109010001.md): Link · cracked · Sep 1, 2021 · N916EV · Cndair CL6002B19 · Engine Mount Section
  > ABNORMAL INDICATION WAS DISCOVERED DURING ULTRASONIC TEST NDT 71-23-103 PART 4. TSN 19209.60 CSN 19729.
- [SDR SWIA2020091652539](https://openairdocs.org/sdr/SWIA2020091652539.md): Bulkhead · cracked · Aug 14, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 202.75 CRACKED WHERE PARKING BRAKE CABLE PASSES THROUGH IT. C-CHECK RO 9/12/2020. REPAIRED THE FS 202.75 BULKHEAD BETWEEN LBL 22 & LBL 30 AT PARKING BRAKE CABLE PASS THRU, REF MHIRJ REO. ALL CHECKS GOOD, SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020091652538](https://openairdocs.org/sdr/SWIA2020091652538.md): Pressure Deck · cracked · Aug 13, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Structure
  > REPAIR CRACK IN THE PRESSURE FLOOR FS 461.00-FS 473.15 BETWEEN BL0-RBL 9, MARKED. C-CHECK RO 9/12/2020. REPAIRED THE PRESSURE FLOOR CRACK FROM FS 461-FS 473.15 LBL 9-RBL 9, REF REO CRJ200 SRM. COMPLIED WITH ST. LEAK CHECKS GOOD.
- [SDR SWIA2020091652559](https://openairdocs.org/sdr/SWIA2020091652559.md): Access Panel · chafed · Aug 11, 2020 · N916EV · Cndair CL6002B19 · Wing, Plate/Skin
  > FRETTING DAMAGE TO ACCESS PANEL LANDS (540AT, 540BT, 540CT) ON LT WING UPPER PLANK. C-CHECK RO 9/12/2020. BLENDED REPAIR AREA, NDT (0.197?). EVALUATED, OUT OF LIMITS, REF CRJ 200 SRM AND BOMBARDIER DRAWING.
- [SDR SWIA2020091652537](https://openairdocs.org/sdr/SWIA2020091652537.md): Access Panel · corroded · Aug 11, 2020 · N916EV · Cndair CL6002B19 · Wing, Plate/Skin
  > FRETTING DAMAGE TO ACCESS PANEL LANDS 640AT, 640BT,640CT ON RT WING UPPER PLANK. C-CHECK RO 9/12/2020. BLENDED REPAIR AREA, NDT ED (0.199?), EVALUATED OUT OF LIMITS. RECEIVED/COMPLIED WITH REO-PART WITHIN LIMITS, RESTORED THE FINISH, REF CRJ 200 SRM, BOMBAR
- [SDR SWIA2020091652549](https://openairdocs.org/sdr/SWIA2020091652549.md): Seat Track · corroded · Aug 10, 2020 · N916EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON SEAT TRACK SECTION AT RBL 9 FS 559+110 TO 559+121. C-CHECK RO 9/12/2020. LOCATED, DRILLED, AND COUNTERSUNK NEW SEAT TRACK SECTION AT RBL 9 FS 559+110 TO 559+121, REF CRJ200 SRM AND BOMBARDIER STANDARDS MANUAL.
- [SDR SWIA2020091652548](https://openairdocs.org/sdr/SWIA2020091652548.md): Seat Track · corroded · Aug 10, 2020 · N916EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON SEAT TRACK SECTION AT RBL 9 FS 559+86 TO 559+95. C-CHECK RO 9/12/2020. LOCATED, DRILLED, AND COUNTERSUNK NEW SEAT TRACK SECTION AT RBL 9 FS 559+86 TO 559+95, REF CRJ200 SRM AND BOMBARDIER STANDARDS MANUAL.
- [SDR SWIA2020091652557](https://openairdocs.org/sdr/SWIA2020091652557.md): Check Valve · inoperative · Aug 9, 2020 · N916EV · Cndair CL6002B19 · Air Conditioning System
  > FS 621.00 PRESSURE BULKHEAD RT FLIGHT COMPARTMENT DISTRIBUTION CHECK VALVE, ONE FLAPPER ON CHECK VALVE WILL NOT CLOSE FULLY. C-CHECK RO 9/12/2020. REMOVED AND REPLACED THE RT PASSENGER COMPARTMENT PRESSURE BULKHEAD CHECK VALVE, REF CRJ200 AMM. LEAK CHECKS G
- [SDR SWIA2020091652556](https://openairdocs.org/sdr/SWIA2020091652556.md): Check Valve · inoperative · Aug 9, 2020 · N916EV · Cndair CL6002B19 · Air Distribution System
  > FS 621.00 PRESSURE BULKHEAD LT FLIGHT COMPARTMENT DISTRIBUTION CHECK VALVE, ONE FLAPPER ON CHECK VALVE WILL NOT CLOSE FULLY. C-CHECK RO 9/12/2020. REMOVED AND REPLACED THE LT PRESSURE BULKHEAD CHECK VALVE, REF CRJ200 AMM. LEAK CHECKS GOOD.
- [SDR SWIA2020091652547](https://openairdocs.org/sdr/SWIA2020091652547.md): Mount · corroded · Aug 9, 2020 · N916EV · Cndair CL6002B19 · Wing, Attach Fittings
  > LEFT WING AILERON POSITION TRANSMITTER HAS CORRODED MOUNT HARDWARE 3 LOCATIONS, MARKED WITH ORANGE FLAG. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW LEFT WING AILERON POSITION TRANSMITTER MOUNT HARDWARE, REF. CRJ 200 AMM. OPS CHECK GOOD.
- [SDR SWIA2020091652536](https://openairdocs.org/sdr/SWIA2020091652536.md): Rib · cracked · Aug 8, 2020 · N916EV · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RT BATT RIB ASSY APPROX 48.3 IS CRACKED, AS MARKED. C-CHECK RO 9/12/2020. REMOVED CRACKED AND INSTALLED NEW RT BATT RIB AT WS 48.3, REF CRJ 200 SRM. FOR FASTENER TYPE AND SIZE REF DRAWINGS. SEE CONTINUATION CARD FOR DETAILS. COMPLETED TASK CARD.
- [SDR SWIA2020091652535](https://openairdocs.org/sdr/SWIA2020091652535.md): Rib · cracked · Aug 8, 2020 · N916EV · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LT BATT RIB ASSY APPROX 48.3 IS CRACKED, AS MARKED. C-CHECK RO 9/12/2020. INSTALLED NEW LT BATT RIB AT WS 48.3 (P/N: 600-10389-1), REF CRJ 200 SRM AND DRAWINGS. COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWIA2020091652534](https://openairdocs.org/sdr/SWIA2020091652534.md): Door Sill · corroded · Aug 6, 2020 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL HAS CORROSION. C-CHECK RO 9/12/2020. EVALUATED, OUT OF LIMITS. REPLACED PART, REF CRJ200 SRM BOMBARDIER DRAWING. COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWIA2020091652533](https://openairdocs.org/sdr/SWIA2020091652533.md): Hinge Fitting · chafed · Aug 6, 2020 · N916EV · Cndair CL6002B19 · Elevator Structure
  > LT CENTER HORIZONTAL STAB ELEVATOR HINGE FITTING HAVE ABRASION DAMAGE, AS MARKED. C-CHECK RO 9/12/2020. BLENDED CHAFED AREA ON THE LT CENTER HORIZONTAL STAB ELEVATOR HINGE FITTING TO A SMOOTH CONTOUR. NDT CHECKED FOR CRACKS WITH NO DEFECTS NOTED. ROTO-PEEN
- [SDR SWIA2020091652532](https://openairdocs.org/sdr/SWIA2020091652532.md): Hinge Fitting · chafed · Aug 6, 2020 · N916EV · Cndair CL6002B19 · Elevator Structure
  > RT OUTBOARD HORIZONTAL STAB ELEVATOR HINGE FITTING HAVE ABRASION DAMAGE, AS MARKED. C-CHECK RO 9/12/2020. BLENDED CHAFED AREA ON THE RT OUTBOARD HORIZONTAL STAB ELEVATOR HINGE FITTING TO A SMOOTH CONTOUR. NDT CHECKED FOR CRACKS WITH NO DEFECTS NOTED. ROTO-
- [SDR SWIA2020091652531](https://openairdocs.org/sdr/SWIA2020091652531.md): Hinge Fitting · chafed · Aug 6, 2020 · N916EV · Cndair CL6002B19 · Elevator Structure
  > RT CENTER HORIZONTAL STAB ELEVATOR HINGE FITTING HAVE ABRASION DAMAGE, AS MARKED. C-CHECK RO 9/12/2020. BLENDED CHAFED AREA ON THE RT CENTER HORIZONTAL STAB ELEVATOR HINGE FITTING TO A SMOOTH CONTOUR. NDT CHECKED FOR CRACKS WITH NO DEFECTS NOTED. ROTO-PEEN
- [SDR SWIA2020091652530](https://openairdocs.org/sdr/SWIA2020091652530.md): Skin · gouged · Aug 6, 2020 · N916EV · Cndair CL6002B19 · Spoilers
  > RT WING TRAILING EDGE RIB AT OUTBOARD END OF RT SPOILERON HAS A GOUGE ON THE UPPER SURFACE. C-CHECK RO 9/12/2020. BLENDED, NDT (NO DEFECTS) AND EVALUATED REPAIR, FOUND TO BE OUT LIMITS. COMPLIED WITH REO, REPAIR IN LIMITS, REF REO. TOOL MACT1463X DUE 31 MA
- [SDR SWIA2020091652546](https://openairdocs.org/sdr/SWIA2020091652546.md): Bracket · cracked · Aug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LT WING-161 PANEL MOUNT BRACKET CRACKED AS MARKED AT APROX FS 468. C-CHECK RO 9/12/2020. REMOVED CRACKED MOUNT BRACKET AND INSTALLED NEW MOUNT BRACKET P/N 601R31037-61, REF CRJ200 SRM.
- [SDR SWIA2020091652545](https://openairdocs.org/sdr/SWIA2020091652545.md): Bracket · cracked · Aug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT WING-162 PANEL MOUNT BRACKET CRACKED AS MARKED AT APROX FS 449. C-CHECK RO 9/12/2020. REPLACED RT WING PANEL 162 MOUNT BRACKET AT FS 461.00, REF CRJ200 SRM.
- [SDR SWIA2020091652544](https://openairdocs.org/sdr/SWIA2020091652544.md): Bracket · cracked · Aug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT WING-162 PANEL MOUNT BRACKET CRACKED AS MARKED AT APROX FS 461. C-CHECK RO 9/12/2020. REPLACED RT WING PANEL 162 MOUNT BRACKET AT FS 461.00, REF CRJ200 SRM.
- [SDR SWIA2020091652543](https://openairdocs.org/sdr/SWIA2020091652543.md): Bracket · cracked · Aug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT WING-162 PANEL MOUNT BRACKET CRACKED AS MARKED AT APROX FS 468. C-CHECK RO 9/12/2020. REPLACED RT WING PANEL 162 MOUNT BRACKET AT FS 468.00, REF CRJ200 SRM.
- [SDR SWIA2020091652542](https://openairdocs.org/sdr/SWIA2020091652542.md): Bracket · cracked · Aug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT WING-162 PANEL MOUNT BRACKET CRACKED AS MARKED AT APROX FS 476. C-CHECK RO 9/12/2020. REPLACED RT WING PANEL 162 MOUNT BRACKET AT FS 476.00, REF CRJ200 SRM.
- [SDR SWIA2020091652529](https://openairdocs.org/sdr/SWIA2020091652529.md): Attach Fitting · nicked · Aug 4, 2020 · N916EV · Cndair CL6002B19 · Wing, Nacelle/Pylon Attach Fittings
  > LT OUTBOARD FLAP WS 220 FWD HINGE BOX ATTACHMENT LUG HAS NICKS/BURRS THAT NEED BLENDING AND TOUCH UP, AS MARKED. C-CHECK RO 9/12/2020. BLENDED LT OUTBOARD FLAP HINGE BOX FWD ATTACHMENT LUG AT WS 220.00 TO A SMOOTH CONTOUR, REF REO. COMPLIED WITH TASK CARD.
- [SDR SWIA2020091652528](https://openairdocs.org/sdr/SWIA2020091652528.md): Attach Fitting · nicked · Aug 4, 2020 · N916EV · Cndair CL6002B19 · Trailing Edge Flaps
  > LT OUTBOARD FLAP WS 220 AFT HINGE BOX ATTACHMENT LUG HAS NICKS/BURRS THAT NEED BLENDING AND TOUCH UP, AS MARKED. C-CHECK RO 9/12/2020. BLENDED LT OUTBOARD FLAP HINGE BOX AFT ATTACHMENT LUG AT WS 220.00 TO A SMOOTH CONTOUR, REF REO. COMPLIED WITH TASK CARD.
- [SDR SWIA2020091652527](https://openairdocs.org/sdr/SWIA2020091652527.md): Attach Fitting · nicked · Aug 4, 2020 · N916EV · Cndair CL6002B19 · Trailing Edge Flaps
  > LT OUTBOARD FLAP WS 178 AFT HINGE BOX ATTACHMENT LUG HAS NICKS/BURRS THAT NEED BLENDING AND TOUCH UP, AS MARKED. C-CHECK RO 9/12/2020. BLENDED LT OUTBOARD FLAP HINGE BOX AFT ATTACHMENT LUG AT WS 178.00 TO A SMOOTH CONTOUR, REF REO. COMPLIED WITH TASK CARD.
- [SDR SWIA2020091652526](https://openairdocs.org/sdr/SWIA2020091652526.md): Bracket · cracked · Aug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CLIP ON FRAME AT APPROX FS 625 ON THE LEFT SIDE OF THE AIRCRAFT IS CRACKED, FLAGGED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED INTERCOSTAL CLIP BETWEEN FS 621-625 ADJACENT TO STRINGER 14 LT, REF CRJ200 SRM AND REO. COMPLIED WITH TASK CARD.
- [SDR SWIA2020091652525](https://openairdocs.org/sdr/SWIA2020091652525.md): Bracket · cracked · Aug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CLIP ON FRAME AT APPROX FS 625 ON THE RIGHT SIDE OF THE AIRCRAFT IS CRACKED, FLAGGED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED INTERCOSTAL CLIP BETWEEN FS 621-625 ADJACENT TO STRINGER 14 RT, REF CRJ200 SRM AND REO. COMPLIED WITH TASK CARD.
- [SDR SWIA2020091652524](https://openairdocs.org/sdr/SWIA2020091652524.md): Floor Support · corroded · Aug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL HAS MULTIPLE AREAS OF CORROSION (X7) FS 280 THRU FS 409.00, CIRCLED WITH GREASE PENCIL. C-CHECK RO 9/12/2020. REPAIRED ALL MARKED AREAS OF CORROSION, BLENDS MARKED NR 1 AND NR 6 WITHIN LIMITS, REF REO ALL STEPS COMPLIED WITH. REMAINING AREAS R
- [SDR SWIA2020091652558](https://openairdocs.org/sdr/SWIA2020091652558.md): Gusset · gouged · Aug 3, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Structure
  > GUSSET FOR FRAME AT APPROX FS 559+48 AND APPROX STGR 6R IS GOUGED, FLAGGED. C-CHECK RO 9/12/2020. FOUND DAMAGES ON OVERHEAD BIN DRAG LINK GUSSET AT FRAME AT APPROX FS 559+48 AND APPROX STGR 6R OUT OF LIMIT WITH 100% MATERIAL LOSS. REPLACED GUSSET WITH NEW F
- [SDR SWIA2020091652523](https://openairdocs.org/sdr/SWIA2020091652523.md): Mount Bracket · corroded · Aug 3, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT FS 310/FS 319.00 STGR 17 RT OUTBOARD GALLEY MOUNT PLATE IS CORRODED, FLAGGED. C-CHECK RO 9/12/2020. REPLACED RT OUTBOARD GALLEY MOUNT PLATE BETWEEN FS 310.00 & FS 319.00 AT STGR 17, REF BOMBARDIER DWG CRJ200 SRM. COMPLIED WITH TASK CARD.
- [SDR SWIA2020091652522](https://openairdocs.org/sdr/SWIA2020091652522.md): Skin · corroded · Aug 3, 2020 · N916EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LOWER PLANK ACCESS HOLE FOR PANEL 510AB HAS PITTING AND SIGNS OF CORROSION ON THE LANDING AREA. C-CHECK RO 9/12/2020. REMOVED PITTING AND EVIDENCE OF CORROSION PART IN LIMITS. RESTORED PEEN/FINISH, COMPLIED WITH ALL STEPS OF REO, REF REO.
- [SDR SWIA2020091652521](https://openairdocs.org/sdr/SWIA2020091652521.md): Skin · corroded · Aug 3, 2020 · N916EV · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER PLANK ACCESS HOLE FOR PANEL 640BB HAS PITTING AND SIGNS OF CORROSION ON THE LANDING AREA. C-CHECK RO 9/12/2020. REMOVED PITTING AND EVIDENCE OF CORROSION PART IN LIMITS. RESTORED PEEN/FINISH, COMPLIED WITH ALL STEPS OF REF REO. LEAK CHECKS
- [SDR SWIA2020091652520](https://openairdocs.org/sdr/SWIA2020091652520.md): Floor Support · corroded · Aug 3, 2020 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FS 409.00+128 TO FS 559.00 UPPER FLOOR SILL PANEL HAVE NUMEROUS AREAS OF CORROSION, AS MARKED. C-CHECK RO 9/12/2020. REMOVED CORROSION FROM 17 LOCATIONS ON LT UPPER FLOOR SILL PANEL BETWEEN FS 409.00+128 AND FS 559.00. ALL 17 BLEND LOCATIONS ARE WITHIN L
- [SDR SWIA2020091652519](https://openairdocs.org/sdr/SWIA2020091652519.md): Floor Support · corroded · Aug 3, 2020 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM FS 409.0+128 TO FS 559.0. C-CHECK RO 9/12/2020. COMPLIED WITH REO FOR REPAIR CORROSION FROM FS 409.0+128 TO FS 559.0 LBL 9.0 FLOOR BEAM CAP INBOARD AND OUTBOARD FLANGES. COMPLIED WITH SKY CARD.
- [SDR SWIA2020091652518](https://openairdocs.org/sdr/SWIA2020091652518.md): Floor Support · corroded · Aug 3, 2020 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM FS 409.0+128 TO FS 559.0. C-CHECK RO 9/12/2020. COMPLIED WITH PERMANENT REPAIR RBL 9 FLOOR SUPPORT CORROSION FROM FS 409+128 TO FS 559, REF REO. VERIFIED ALL STEPS 1-5 COMPLIED WITH, COMPLETED TASK CARD. WEIGHT CH
- [SDR SWIA2020091652517](https://openairdocs.org/sdr/SWIA2020091652517.md): Intercostal · gouged · Aug 3, 2020 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL GOUGED AT APPROX STGR 10R ON THE FWD SIDE OF THE RT EMER DOOR SURROUND STRUCTURE. C-CHECK RO 9/12/2020. REMOVED AND REPLACED THE INTERCOSTAL AT THE EMER SURROUND STRUCTURE STR 10R, REF DRAWING CRJ200 SRM. COMPLIED WITH ST, ALL CHECKS GOOD.

Next page: https://openairdocs.org/aircraft/N916EV/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 = 'N916EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N916EV/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.