# Service difficulty reports: N708EV

A list on [N708EV](https://openairdocs.org/aircraft/N708EV.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 7 · 333 reports

- [SDR SWIA20231120](https://openairdocs.org/sdr/SWIA20231120.md): Unknown · warning message · Nov 20, 2023 · N708EV · Cndair CL6002C10 · Master Cylinder/Brake Valve
  > MLG OVERHEAT WARNING MESSAGE DURING DESCENT. EVERY TIME WE RESET THE MASTER WARNING, IT WOULD GO OFF AGAIN. FOLLOWED QRH PROCEDURE. WITH GEAR FULLY DOWN, ALL BRAKE TEMPS SHOWED ZERO BUT THE WARNING MESSAGE PERSISTED. WARNING WENT AWAY ONCE WE WERE FULLY CONFIG
- [SDR SWIA202266225](https://openairdocs.org/sdr/SWIA202266225.md): None · failed · Aug 15, 2022 · N708EV · Cndair CL6002C10 · Pneumatic System
  > L BLEED DUCT WARNING MSG CLIMBING THROUGH F240 RAN AND COMPLIED WITH QRH PROCEDURE AND RETURNED TO DFW (FLIGHT #3079 FILED CLOSED) UPON ARRIVAL FOUND B1-349536 AND B1-349537 IN HISTORY AND TROUBLESHOOT PER CRJ 700 FIM 36-21-01. UPON PERFORMING EVENT LOCATI
- [SDR SWIA202266146](https://openairdocs.org/sdr/SWIA202266146.md): None · failed · Jul 24, 2022 · N708EV · Cndair CL6002C10 · Pneumatic System
  > L BLEED AIR DUCT WARNING (FLIGHT 3027 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25215068 WITH THE FOLLOWING CORRECTIVE ACTION: "THE AILC EVENT LOCATION HISTORY RECORDED THE LEAK AT LOOPS MT137 76% AND MT138 80%, WHICH WAS ALSO THE SAM
- [SDR SWIA202265373](https://openairdocs.org/sdr/SWIA202265373.md): None · damaged · Feb 15, 2022 · N708EV · Cndair CL6002C10 · Fuselage Structure (General)
  > PASSENGER DOOR PIANO HINGE HALF REQUIRES REPLACEMENT. (FILED CLOSED) REMOVED AND REPLACED PASSENGER DOOR PIANO HINGE HALF WITH REFERENCE TO SRM 52-11-01. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMPLETED M-337.
- [SDR SWIA202265374](https://openairdocs.org/sdr/SWIA202265374.md): None · defective · Feb 8, 2022 · N708EV · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings
  > D: MCD DIFFICULT TO OPEN AT GATE / C: 52-21-1A / CAT "A" DUE 3 FLT DAYS, 2/11/22 / ORD MX VERIFIED ALL REMARKS, EXCEPTIONS AND OPERATIONAL PROCEDURES WERE MET (FILED - CLOSED) REMOVED AND REPLACED PASSENGER DOOR HINGE (AIRCRAFT SIDE) IN REFERENCE TO SRM 53
- [SDR SWIA2021110862314](https://openairdocs.org/sdr/SWIA2021110862314.md): Terminal · loose · Nov 7, 2021 · N708EV · Cndair CL6002C10 · Window System Wiring
  > DURING CRUISE FLIGHT PILOT NOTICED A STRANGE ODER SEEMED TO BE COMING FROM FO SIDE OF FLT DECK. DECLARED EMERGENCY AND DIVERTED (FLIGHT 3018 - FILED CLOSED) UPON ARRIVAL TO THE AIRCRAFT FOUND HARDWARE FOR RH WINDOW HEATER POWER TERMINAL LEADS TO BE LOOS
- [SDR SWIA202161462](https://openairdocs.org/sdr/SWIA202161462.md): None · missing · Aug 14, 2021 · N708EV · Cndair CL6002C10 · Pneumatic System
  > LH ENGINE UPPER C-DUCT ASSY RECEIVED WITHOUT ATTACHING HARDWARE IN THE NYLON INSERTS. (C-CHECK RO 9/27/2021) TRANSFERRED FROM CO: 10060821 JOB 71006085 OP 189 / REMOVED AND REPLACED L/H UPPER C-DUCT NYLON INSERT (REF CRJ-700 AMM 78-33-05-960-801-A02), AN
- [SDR SWIA202161461](https://openairdocs.org/sdr/SWIA202161461.md): None · bent · Aug 7, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CUT-OUT FOR NOSE LANDING GEAR AT AFT EDGE HAS INTERNAL ANGLES THAT ARE BENT. (C-CHECK RO 9/27/2021) PERFORMED DOUBLER REPAIR TO LOWER FUSELAGE SKIN BETWEEN FS220-280, STGRS 25L - 25R REF MHIRJ REO 670-53-11-1720 REV -- DATED 2021-08-24 AND
- [SDR SWIA202161499](https://openairdocs.org/sdr/SWIA202161499.md): None · worn · Aug 1, 2021 · N708EV · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > MULTIPLE SLAT TRACK SIDE ROLLERS WORN ON THE R/H WING (C-CHECK RO 9/27/2021) RH SLAT TRACK 1-2 SIDE ROLLERS REMOVED AND REPLACED WITH NEW, REF CRJ 700 AMM 27-81-44-000-801-A01 AND CRJ 700 AMM 27-81-44-400-801-A01. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202161459](https://openairdocs.org/sdr/SWIA202161459.md): None · corroded · Jul 26, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Keel
  > UPON REMOVAL TO FOM, BRACKET WAS FOUND TO BE CORRODED COMMON TO STGR21R AMD FS310 (C-CHECK RO 9/27/2021) REMOVED AND REPLACED BRACKET STGR21R FS310, REF CRJ 700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG SH670-32600 REV AJ, COMPLIED WITH
- [SDR SWIA202161458](https://openairdocs.org/sdr/SWIA202161458.md): None · damaged · Jul 26, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME SPLICE AT FS 485.00 TO STGR 26R TO FOM FOR STGR 21R REPAIR JOB71006084 OP 179 MX#23186251 (C-CHECK RO 9/27/2021) INSTALLED SPLICE AT FS 485 TO STRINGER 26R THAT WAS REMOVED FOR ACCESS ON JOB 71006084 OP 179 MX NUMBER 23186251 IAW CRJ-700 SRM 51-
- [SDR SWIA202161454](https://openairdocs.org/sdr/SWIA202161454.md): None · corroded · Jul 26, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Keel
  > EVIDENCE OF CORROSION ON STGR 19R APPROXIMATELY FROM FS 437.00 - FS 533.00 DAMAGE IS AT 100% MATERIAL LOSS (C-CHECK RO 9/27/2021) REPAIRED DAMAGED STRINGER 19R BETWEEN FS437-533 IAW CRJ-700 SRM 53-00-03-201-001-A01 LEAK CHECK GOOD. COMPLIED WITH TASK C
- [SDR SWIA2021100161451](https://openairdocs.org/sdr/SWIA2021100161451.md): Stringer Splice · corroded · Jul 26, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > EVIDENCE OF CORROSION AND EXCESSIVE EXFOLIATION AT STGR 21R AND SPLICE ANGLE AREA BETWEEN / FS 453.00 - FS 485.00 DAMAGE IS 100% MATERIAL LOSS (C-CHECK RO 9/27/2021) REPLACED OUT OF LIMITS STGR 21R, AT 2 SECTION FROM FS445.00 - FS477.00 AND FS477.00 -
- [SDR SWIA202161449](https://openairdocs.org/sdr/SWIA202161449.md): None · corroded · Jul 25, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Keel
  > INTERCOSTAL ON STGR 21L FS310.00 - FS333.00 IS CORRODED, (C-CHECK RO 9/27/2021) INTERCOSTAL STGR21L FS310 - FS333 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL STGR21L FS310 - FS333 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG SH670-318
- [SDR SWIA202161446](https://openairdocs.org/sdr/SWIA202161446.md): None · corroded · Jul 23, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Keel
  > FOUND MULTIPLE AREAS OF CORROSION ON STGR23R STRINGER SPLICE ON FS333. (C-CHECK RO 9/27/2021) REPLACED STRINGER SPLICE 23R AT FS333.00 WITH NEW. REF CRJ700 SRM 51-42-06-001-001-A01,DWG SH670-31630 REV F. LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202161444](https://openairdocs.org/sdr/SWIA202161444.md): None · corroded · Jul 21, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Keel
  > FOUND MULTIPLE AREAS OF CORROSION ON STGR20R BETWEEN APPROX. FS280 - FS319. (C-CHECK RO 9/27/2021) STRG20R BETWEEN FS280 AND FS319 WAS OUT OF LIMITS OF CRJ700 SRM 53-21-03-101-002-A01, REPLACED STRG20R LOCATED BETWEEN FS280 & FS319 IAW CRJ700 SRM 51-42-0
- [SDR SWIA202161440](https://openairdocs.org/sdr/SWIA202161440.md): None · corroded · Jul 21, 2021 · N708EV · Cndair CL6002C10 · Fuselage Structure (General)
  > UPON REMOVAL TO FOM, BRACKET WAS FOUND TO BE CORRODED COMMON TO STGR21R AMD FS333 (C-CHECK RO 9/27/2021) REMOVED AND INSTALLED NEW BRACKET COMMON TO STGR21R AND FS333 PER DWG# SH670-32600 REV AJ AND CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A
- [SDR SWIA202161438](https://openairdocs.org/sdr/SWIA202161438.md): None · damaged · Jul 19, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME SPLICE AT FS 421.00 TO STGR 16R TO FOM FOR STGR 19R REPAIR JOB 71006084 OP 173 MX# 23148650 (C-CHECK RO 9/27/2021) REMOVED AND REINSTALLED FRAME SPLICE STGR 20R AT FS 421.00 TO FOM REF. CRJ-700 SRM 51-42-06-001-001-A01 AND REO 670-53-21-2091 REV
- [SDR SWIA2021100161435](https://openairdocs.org/sdr/SWIA2021100161435.md): Stringer · corroded · Jul 19, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION AND EXCESSIVE EXFOLIATION AT STGR 19R BETWEEN FS 437.00 - FS 453.00 MATERIAL LOSS AT 100% (C-CHECK RO 9/27/2021) REMOVED AND REPLACED STGR 19R AT FS349 - FS477.00 REF. CRJ 700 SRM 51-42-06-001-001-A01 AND REO 670-53-21-2099 REV -- DATE
- [SDR SWIA202161432](https://openairdocs.org/sdr/SWIA202161432.md): None · cracked · Jul 17, 2021 · N708EV · Cndair CL6002C10 · Nacelle/Pylon Structure
  > HOLE #3 ON UPPER R/H PYLON CRACKED (C-CHECK RO 9/27/2021) PERFORMED REPAIR FOR CRACKED FASTENER HOLE # 3 TO RH UPPER PYLON SKIN IAW REO 670-54-51-059 REV - - DATE 2021-08-02. REAMED HOLE TO INTERFERENCE FIT.307 /.310 DIAMETER INSTALLED HST11AG10 + HS
- [SDR SWIA202161430](https://openairdocs.org/sdr/SWIA202161430.md): None · corroded · Jul 15, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > PAX DOOR AFT DD5 INTERCOSTAL FOUND TO HAVE CORROSION (C-CHECK RO 9/27/2021) REMOVED AND REPLACED PAX DOOR AFT DD5 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N. LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202161428](https://openairdocs.org/sdr/SWIA202161428.md): None · corroded · Jul 15, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Keel
  > CORROSION ON MULTIPLE AREAS OF STGR19R, FS364.00 €“ FS394.00. (C-CHECK RO 9/27/2021) REPLACED STRINGER 19R FROM FS347.00-FS477.00 REF REO 670-53-21-2099 REV. -- DATE 2021-07-27, DWG SH670-31103 REV. A, CRJ 700 SRM 53-00-03-201-001-A01 REV. 38 DATE JUL 2
- [SDR SWIA202161426](https://openairdocs.org/sdr/SWIA202161426.md): None · corroded · Jul 14, 2021 · N708EV · Cndair CL6002C10 · Doors
  > FOUND CORROSION AT AFT CARGO LOWER DOOR SILL BETWEEN FS1000 - FS1047REMOVED AND REPLACED AFT CARGO LOWER DOOR SILL BETWEEN FS1000 - FS1047 REF DWG NO. MM670-35085 REV L, CRJ700 SRM51-42-06-001-001-A01 REV 38 JUL 25/2020, SRM51-42-21-001-001-A01 REV 38 JUL 25/2
- [SDR SWIA202161484](https://openairdocs.org/sdr/SWIA202161484.md): None · corroded · Jul 13, 2021 · N708EV · Cndair CL6002C10 · Passenger/Crew Doors
  > FWD CARGO DOOR SURROUND STRUCTURE, AFT HINGE IS CORRODED (C-CHECK RO 9/27/2021) REMOVED AND REPLACED CORRODED FWD CARGO DOOR SURROUND STRUCTURE AFT HINGE WITH NEW UNIT. REF CRJ700 SRM 51-41-02-001-001-A01. SEE CONTINUE CARD FOR DETAILS. / TRANSFERRE
- [SDR SWIA202161423](https://openairdocs.org/sdr/SWIA202161423.md): None · damaged · Jul 13, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME SPLICE AT FS409.00 STGR 16R TO FOM STGR 20R REF JOB 71006084 OP 23 (C-CHECK RO 9/27/2021) REPAIR FRAME SPLICE AT FS409.00 STGR 16R COMPLIED WITH REO 670-53-21-2083 REV -- DATED 2021-07-16. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2021100161420](https://openairdocs.org/sdr/SWIA2021100161420.md): Intercostal · corroded · Jul 10, 2021 · N708EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID DD4 INTERCOSTAL FOUND TO HAVE CORROSION (C-CHECK RO 9/27/2021) REMOVED AND REPLACED PAX DOOR MID DD4 INTERCOSTAL, REF CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DWG 601R31702 REV N. LEAK CHECK GOOD / COMPLIED WITH SKYWEST TAS
- [SDR SWIA202161417](https://openairdocs.org/sdr/SWIA202161417.md): None · corroded · Jul 10, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Keel
  > FOUND CORROSION ON STRINGER SPLICE ON STGR22R AND FS333. (C-CHECK RO 9/27/2021) REMOVED AND REPLACD STRINGER SPLICE REF CRJ 700 SRM 51-42-06-001-001-A01, AND DWG SH670-32420 REV E, STGR22R FS333. LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202161414](https://openairdocs.org/sdr/SWIA202161414.md): None · corroded · Jul 10, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FOUND CORROSION ON SKIN ON THE INSIDE BETWEEN STGR21R - STGR22R AND BETWEEN FS333 AND FS319. (C-CHECK RO 9/27/2021) REPAIRED SKIN BETWEEN STGR21R - STGR22R AND FS333 AND FS319 PER REO 670-53-21-2081 REV -- DATE: 2021-08-09 ALL STEPS COMPLIED WITH. LEAK C
- [SDR SWIA2021102861409](https://openairdocs.org/sdr/SWIA2021102861409.md): Bracket · corroded · Jul 8, 2021 · N708EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD DD5 INTERCOSTAL BRACKET PN: 601R31902-461 FOUND TO HAVE CORROSION (C-CHECK RO 9/27/2021) REMOVED AND REPLACED PAX DOOR DD5 INTERCOSTAL BRACKET P/N 601R31902-461, REF CRJ 900 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N. LEAK CHECK GOOD
- [SDR SWIA202161412](https://openairdocs.org/sdr/SWIA202161412.md): None · corroded · Jul 8, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR21L INTERCOSTAL BETWEEN FS349 AND FS333 HAS CORROSION (MARKED) (C-CHECK RO 9/27/2021) REMOVED AND REPLACED INTERCOSTAL STGR21L FS333-FS349 REF CRJ 700 SRM 51-42-06-001-001-A01, DWG SH670-31810 REV AE, COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2021100161409](https://openairdocs.org/sdr/SWIA2021100161409.md): Intercostal · corroded · Jul 8, 2021 · N708EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD DD5 INTERCOSTAL BRACKET PN: 601R31902-461 FOUND TO HAVE CORROSION (C-CHECK RO 9/27/2021) REMOVED AND REPLACED PAX DOOR DD5 INTERCOSTAL BRACKET P/N 601R31902-461, REF CRJ 900 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N. LEAK CHECK GOOD
- [SDR SWIA202161407](https://openairdocs.org/sdr/SWIA202161407.md): None · corroded · Jul 8, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > PAX DOOR FWD DD5 INTERCOSTAL FOUND TO HAVE CORROSION (C-CHECK RO 9/27/2021) REPLACED PAX DOOR INTERCOSTAL DD5 WITH NEW. REF CRJ 700 SRM 51-42-06-001-001-A01 DWG 601R31702 REV N. LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202161488](https://openairdocs.org/sdr/SWIA202161488.md): None · cracked · Jul 7, 2021 · N708EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR AFT WEB IS CRACKED ON STAIR RISER FLANGE (C-CHECK RO 9/27/2021) REMOVED PAX DOOR AFT WEB ASSY ATTACHING PARTS AND REASSEMBLED ONTO NEW AFT WEB PN: 601R317071-7 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R317071 REV E. PAX DOOR A
- [SDR SWIA202161487](https://openairdocs.org/sdr/SWIA202161487.md): None · cracked · Jul 7, 2021 · N708EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR AFT WEB DRAG ANGLE IS CRACKED (C-CHECK RO 9/27/2021) REMOVED AND REPLACED PAX DOOR AFT WEB DRAG ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01
- [SDR SWIA202161482](https://openairdocs.org/sdr/SWIA202161482.md): None · corroded · Jul 7, 2021 · N708EV · Cndair CL6002C10 · Wing Structure
  > R/H AILERON PCU OUTPUT LINKS HAVE WORN SPHERICAL BUSHINGS (C-CHECK RO 9/27/2021) REMOVED AND REPLACED R/H AILERON PCU OUTPUT LINK SPHERICAL BUSHINGS REF GOODRICH CMM 27-14-01. / OPS TEST GOOD. COMPLIED WITH 27-900-1008-SKY
- [SDR SWIA202161404](https://openairdocs.org/sdr/SWIA202161404.md): None · damaged · Jul 7, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Frame
  > REPAIR FOR # 2 DAMAGE IN FLOOR BEAM LBL9 INBOARD FLANGE BETWEEN FS909.00 - FS923.00 (C-CHECK RO 9/27/2021) REPAIRED DAMAGE AT LBL9 INBOARD FLANGE BETWEEN FS909.00-FS923.00 REF.CRJ700 SRM 53-00-41-201-001-A01 TASK CARD 51-900-1002-SKY
- [SDR SWIA202161402](https://openairdocs.org/sdr/SWIA202161402.md): None · corroded · Jul 7, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > PAX DOOR FWD DD1A INTERCOSTAL FOUND TO BE CORRODED (C-CHECK RO 9/27/2021) EVALUATED REMOVAL OF CORROSION WITH ORIGINAL THICKNESS.050, REMIANING.049, REMOVED.001. FOUND TO BE WITHIN LIMITS NOT EXCEEDING 10% MAXIMUM PER CRJ 200 SRM 52-00-00-01 WITH BOMB
- [SDR SWIA202161401](https://openairdocs.org/sdr/SWIA202161401.md): None · corroded · Jul 7, 2021 · N708EV · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > PAX DOOR FWD DD6 CLIP FOUND TO BE CORRODED ON BOTH FACES (C-CHECK RO 9/27/2021) REMOVED AND REPLACED PAX DOOR FWD DD6 CLIP IAW CRJ 700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV N TASK CARD 51-900-1002-SKY
- [SDR SWIA202161481](https://openairdocs.org/sdr/SWIA202161481.md): None · worn · Jul 6, 2021 · N708EV · Cndair CL6002C10 · Wing Structure
  > L/H AILERON PCU OUTPUT LINK HAS WORN SPHERICAL BUSHINGS (C-CHECK RO 9/27/2021) REMOVED AND REPLACED L/H AILERON PCU OUTPUT LINK SPHERICAL BUSHINGS. REF GOODRICH CMM 27-14-01. / OPS TEST GOOD. COMPLIED WITH 27-900-1008-SKY
- [SDR SWIA202161400](https://openairdocs.org/sdr/SWIA202161400.md): None · corroded · Jul 6, 2021 · N708EV · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > FWD CARGO DOOR SURROUND STRUCTURE, SILL AT STRG 25L AND APPROXIMATELY FS539 IS CORRODED UNDER FWD CARGO DOOR FWD HINGE (C-CHECK RO 9/27/2021) REMOVED AND REPLACED FWD CARGO DOOR SURROUND STRUCTURE, SILL AT STRG 25L AND APPROXIMATELY FS539 REF CRJ 700 S
- [SDR SWIA2021100161399](https://openairdocs.org/sdr/SWIA2021100161399.md): Channel · corroded · Jul 6, 2021 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF STGR 27, CORROSION FOUND ON TCAS DOUBLER CHANNEL (C-CHECK RO 9/27/2021) REMOVED AND REPLACED LWR TCAS DBLR CHANNEL, REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-13-001-001-A01 AND BOMBARDIER DWG SH670-30023 REV G. LEAK CHECK GO
- [SDR SWIA202161395](https://openairdocs.org/sdr/SWIA202161395.md): None · corroded · Jul 3, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > PAX DOOR FWD DD7 INTERCOSTAL BRACKET PN: 601R318824-1 FOUND TO HAVE CORROSION (C-CHECK RO 9/27/2021) REPLACED PAX DOOR FWD DD7 BRACKET PN: 601R318824-1 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV N / COMPLIED WITH TASK CARD 51-9
- [SDR SWIA2021100161394](https://openairdocs.org/sdr/SWIA2021100161394.md): Intercostal · corroded · Jul 3, 2021 · N708EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD DD7 INTERCOSTAL FOUND TO HAVE CORROSION (C-CHECK RO 9/27/2021) REMOVED AND REPLACE PAX DOOR FWD DD7 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV N. LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900
- [SDR SWIA202161393](https://openairdocs.org/sdr/SWIA202161393.md): None · corroded · Jul 3, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > PAX DOOR FWD DD6 INTERCOSTAL BRACKET PN: 601R318084-1 FOUND TO HAVE CORROSION (C-CHECK RO 9/27/2021) REPLACED PAX DOOR FWD DD6 INTERCOSTAL BRACKET PN: 601R318084-1 IAW BOMBARDIER DWG 601R31702 REV N AND CRJ 700 SRM 51-42-06-001-001-A01 / COMPLIED WITH TA
- [SDR SWIA202161391](https://openairdocs.org/sdr/SWIA202161391.md): Intercostal · corroded · Jul 3, 2021 · N708EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR DD6 INTERCOSTAL FOUND TO HAVE CORROSION (C-CHECK RO 9/27/2021) REMOVED AND REPLACED PAX DOOR FWD DD6 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV N. LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-10
- [SDR SWIA202161388](https://openairdocs.org/sdr/SWIA202161388.md): None · corroded · Jul 3, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Keel
  > MULTIPLE AREAS OF CORROSION FOUND ON STGR19R BETWEEN FS280.00 TO APPROX. FS300.00. (C-CHECK RO 9/27/2021) REPAIRED STRINGER 19R BETWEEN FS280.00-FS300.00 REF REO 670-53-21-2101 REV -- DATED 2021-08-09 ALL STEPS COMPLIED WITH. LEAK CHECK GOOD. COMPLIED WI
- [SDR SWIA202161386](https://openairdocs.org/sdr/SWIA202161386.md): None · none · Jul 3, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Keel
  > MULTIPLE AREAS OF CORROSION ON STGR21R BETWEEN FS280.00 - FS310.00. (C-CHECK RO 9/27/2021) REMOVED AND INSTALLED NEW STGR21R BETWEEN FS280.00 - FS310.00 PER DWG# SH670-32600 REV AJ, SH670-30002 REV A AND SH670-31630 REV K AND CRJ 700 SRM 51-42-06-001-001
- [SDR SWIA202161383](https://openairdocs.org/sdr/SWIA202161383.md): None · corroded · Jul 3, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Keel
  > MULTIPLE AREAS OF CORROSION FOUND ON STGR22R BETWEEN FS280.00 - FS333.00. (C-CHECK RO 9/27/2021) REMOVED AND INSTALLED NEW STGR22R BETWEEN FS280.00 €“ FS333.00 PER DWG# SH670-31630 REV K, DWG# SH670-30002 REV A AND CRJ 700 SRM 51-42-21-001-001-A01 AND C
- [SDR SWIA202161381](https://openairdocs.org/sdr/SWIA202161381.md): None · corroded · Jul 3, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Keel
  > MULTIPLE AREAS OF CORROSION FOUND ON STGR23R BETWEEN FS280.00 - FS333.00. (C-CHECK RO 9/27/2021) TRANSFERRED FROM CO: 10060821 JOB 71006084 OP 136 / REMOVED AND INSTALLED NEW STGR23R BETWEEN FS280.00 - FS333.00 PER BOMBARDIER DWG# SH670-31630 REV K, CRJ
- [SDR SWIA202161380](https://openairdocs.org/sdr/SWIA202161380.md): None · corroded · Jul 3, 2021 · N708EV · Cndair CL6002C10 · Fuselage Main, Keel
  > MULTIPLE AREAS OF CORROSION FOUND ON STGR27 BETWEEN FS280.00 - FS295.00.REPLACED STRINGER 27 FROM FS280-FS295 WITH NEW. REF DRAWING SH670-31630 REV K, CRJ700 SRM 51-42-06-001-001-A01 REV 38 JUL25/2020, CRJ700 SRM 51-42-21-001-001-A01 REV 38 JUL 25/2020. LEAK

Next page: https://openairdocs.org/aircraft/N708EV/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 = 'N708EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N708EV/reports

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