N710EV

Service difficulty reports · 223

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 = 'N710EV' 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 SWIA202265928None · wornPASSENGER DOOR HINGE (AIRFRAME SIDE) PIN HOLES ARE WORN. (FILED CLOSED)REMOVED AND REPLACED PASSENGER DOOR HINGE (AIRFRAME SIDE) IN REF TO SRM 53-21-23 AND REO 670-53-21-2255, REV --, DATED 2022-05-13. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMPLETED M-337.May 12, 2022 · N710EV · Cndair CL6002C10 · Fuselage, Equipment Attach FittingsSDR SWIA202265927None · cutCOMPLY WITH REPAIR AUTHORIZATION: RA75921-670-53-21-2206 N710EV MXCODEID60842-PR - PASSENGER DOOR F.S. 310, BETWEEN STRINGER 17 LH AND STRINGER 18LH, REQUIRE FURTHER EVALUATION DUE TO DAMAGE. REPAIRED DAMAGED PAX DOOR CUT OUT ON FUSELAGE FWD,LWR CORNER AT FSApr 14, 2022 · N710EV · Cndair CL6002C10 · DoorsSDR SWIA202164817None · damagedPASSENGER DOOR F.S. 310, BETWEEN STRINGER 17 LH AND STRINGER 18LH, REQUIRE FURTHER EVALUATION DUE TO DAMAGE. (C-CHECK RO 3/10/2022) REPAIRED DAMAGED PAX DOOR CUT OUT ON FUSELAGE FWD,LWR CORNER AT FS310 FROM STGR 17L TO STGR18L PER REO 670-53-21-2206 REVDec 13, 2021 · N710EV · Cndair CL6002C10 · DoorsSDR SWIA202164816None · corrodedDURING INSPECTION WAS FOUND CORROSION ON STRINGER 20L AT FS. 310.00 TO FS. 349.00 REQUIRES CLEANING AND EVALUATION. (C-CHECK RO 3/10/2022) REMOVED CORRODED STRINGER STGR20L FROM FUSELAGE STATION FS310-FS349 / INSTALLED WITH NEWSTRINGER STGR20L PER CDec 2, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, KeelSDR SWIA202164815Extension · corrodedFS 863 TO FS 954, LBL 9 FLOOR BEAM UNDER SEAT TRACK SEVERAL SPOTS OF CORROSION. (C-CHECK RO 3/10/2022) REMOVED CORRODED FLOOR BEAM SUPPORT AND REPLACED WITH NEW FLOOR BEAM SUPPORT, FILLERS AND CLIPS AT LBL9 FROM FS863 TO FS954 PER TASK CARD 51-900-1002Nov 28, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202164814Frame · corrodedDURING INSPECTION WAS FOUND CORROSION ON FRAME LOCATION FS 319.00 BETWEEN STGR 21L TO STGR 18L NEED TOBE EVALUATED. (C-CHECK RO 3/10/2022) REMOVED AND REPLACED CORRODED FRAME SECTION AT FS319 FROM SGTR18L TO SGTR20L PER TASK CARD 51-900-1002 SKY AND CRJNov 18, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202164813None · corrodedCORROSION ON STRINGER STRG20R BETWEEN FUSELAGE FS879 THRU FS893 (C-CHECK RO 3/10/2022) REMOVED CORRODED STGR20R FROM FS879-FS893 AND REPLACED WITH NEW STGR SECTION PER NHIRJ REO 670-53-51-241 REV. -- DATED:2021-12-27. PLEASE REFER TO CONTINUATION CARD FNov 13, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202164812None · corrodedINTERCOSTAL ON STRG20R FROM FS319 TO FS349, UNDER SERVICE DOOR, CORRODED. FOUND OUT OF LIMITS ON CAMP#23764037, REQUIRES TO BE REPLACED. (C-CHECK RO 3/10/2022) REMOVED AND REPLACED CORRODED INTERCOSTAL ON STGR 20R AT FS 319.00 TO FS 349.00. REF. CRJ700Nov 12, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202164811None · corrodedINTERCOSTAL AT STRG20R FROM FS310 TO FS319, UNDER SERVICE DOOR, CORRODED AND OUT OF LIMITS, REF CAMP #23764037. REQUIRES TO BE REPLACED. (C-CHECK RO 3/10/2022) REMOVED CORRODED INTERCOSTAL AT STGR20R FROM FS310-FS319 AND REPLACED WITH NEW INTERCOSTAL PNov 12, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202164810None · chafedFS 975 - FS 981, STR 27 EXT SKIN DOUBLER CHAFED/GOUGED BY WING TO BODY FAIRINGS 196DL/DR SPLICE STIFFENER. (C-CHECK RO 3/10/2022) REMOVED GOUGED DOUBLER AND TOP DOUBLER AND REPLACED WITH NEW DOUBLER AND TOP DOUBLER PER TASK CARD 51-900-1002-SKY AND REO Nov 9, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, KeelSDR SWIA202164809None · corrodedCORROSION FOUND ON STRINGER STR19 BETWEEN FS333 AND FS349 UNDER SERVICE DOOR. (C-CHECK RO 3/10/2022) REMOVED AND REPLACED SGTR19R FROM FS333-FS349 PER CRJ700 SRM 51-42-06--01-001-A01. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTINov 3, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, KeelSDR SWIA202164808None · corrodedCORROSION AT FS310 TO FS349 & L/H STRINGER 21LH (C-CHECK RO 3/10/2022) REMOVED AND REPLACED CORRODED BACK UP SILL AT FS 310.00 TO FS 349.00 STGR 21L WITH NEW BACK UP SILL. REF. CRJ700 SRM 51-40-11-001-001-A01, SRM 51-42-06-001-001-A01, SRM 51-42-21-00Nov 3, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, KeelSDR SWIA202164807Nut · dentedL/H SIDE FUSELAGE FS533, BETWEEN STR16L & 17L DENT; MEASURE AT 7"X 4" ; .012" IN DEPTH; NO ALLOWABLE DAMAGE IN AREA. (C-CHECK RO 3/10/2022) PERFORMED REPAIR ON DENTED SKIN AT FS535, SGTR16L TO SGTR18L PER REO 670-53-31-761 REV. -- DATED: 2021-12-28. PNov 1, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202164806None · dentedL/H SIDE FUSELAGE FS453, BETWEEN STR14L & 15L DENT; MEASURE AT 3"X 4" .010" DEPTH; NO ALLOWABLE DAMAGE IN AREA. (C-CHECK RO 3/10/2022) PERFORMED REPAIR ON FRAME AT FS453 BETWEEN STGR14L & 15L PER MHIRJ REO 670-53-21-2198 REV. -- DATED: 2021-12-21 ANDNov 1, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202164805None · crackedABOVE FLOOR FS333.00 FRAME CRACKED BEBOW STGR 1RH (C-CHECK RO 3/10/2022) REMOVED AND REPLACED CRACKED FRAME AT FS333 FROM STGR0 TO STGR9R WITH NEW FRAME SECTION PER CRJ700 SRM 51-42-06-001-001-A01. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND DNov 1, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202164804None · crackedFORWARD FUSELAGE LEFT WINDSHIELD SUPPORT POST BETWEEN PILOT'S SIDE WINDSLIELD AND FORWARD WINDSHIELD IS CRACKED. (C-CHECK RO 3/10/2022) REMOVED CRACKED PILOT SIDE WINDOW SUPPORT POST AND REPLACED WITH NEW SUPPORT POST. REF. CRJ700 SRM 53-11-35, 51-40-11Oct 27, 2021 · N710EV · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202164803None · corrodedFS565 AND STGR18L FRAME CORROSION /BARE METAL (C-CHECK RO 3/10/2022) REMOVED AND REPLACED CORRODED FRAME AT FS565, STGR18L TO STGR8L REF CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND Oct 21, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202164802None · corrodedFS549 AND STGR18L FRAME CORROSION /BARE METAL (C-CHECK RO 3/10/2022) REMOVED CORRODED FRAME SECTOR AT FS549 FROM STGR9L TO STGR18L AND REPLACED WITH NEW FRAME SECTOR PER TASK CARD 51-900-1002-SKY, CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-AOct 21, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202164801None · wornRIGHT HAND SLAT NO.# 3 AT SLAT SATATION SS337.66 INBOARD CONNER RUBBING ON TOP OF THE WING LEADING EDGED AREA (C-CHECK RO 3/10/2022) PERFORMED REPAIR TO RIGHT HAND #3 SLAT AT SS337.66 INBOARD CORNER PER TASK CARD 51-900-1002- SKY AND MHIRJ REO 670-57-Oct 16, 2021 · N710EV · Cndair CL6002C10 · Wing, Fuselage Attach FittingsSDR ASOA201809057164Stringer · damagedTYS-DAMAGED FOUND AT STRINGER 6L, BETWEEN FR 1144.00 AND FR 1162. MAINTENANCE BLENDED THE DAMAGED TO STR 6L AT STA 1144.00 TO 1162.00. PERFORMED A NDT INSPECTION AND NO DEFECTS FOUND. INSTALLED THE REPAIR, RETURNED TO ORIGINAL FINISH IAW STS EA 32-2018-161.Sep 5, 2018 · N710EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201809057163Stringer · damagedDAMAGED FOUND AT STR 7L BETWEED FS 1144-1162. BLENDED DAMAGE TO STR 7L BETWEEN FS 1144-1162. PERFORMED NDI NO DEFECTS FOUND. INSTALLED REPAIR AND RETURNED TO ORIGINAL FINISH IAW STS EA 32-2018-162.Sep 5, 2018 · N710EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201809057162Stringer · damagedFOUND DAMAGE AT STR 7R BETWEEN FS 1144-1162. BLENDED DAMAGE TO 7R FS 1144-1162. PERFORMED NDI NO DEFECTS FOUND. INSTALLED REPAIR AND RESTORED TO ORIGINL FINISH IAW REO 670-53-61-292.Sep 5, 2018 · N710EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201801255041Connector · damagedDURING MX INSPECTION, THE EMERGENCY CEILING LIGHT AT ROW 9 WAS FOUND INOPERATIVE. MX CRIMPED NEW PINS IN THE CONNECTOR. OPS CHECKED GOOD.Jan 25, 2018 · N710EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201712075248Strap · damagedREF: CO# EJA150D JOB# EJA050D OP# 51: STRAP LANDING FIXED LEADING EDGE PN CC670-12107-3 REQUIRES FABRICATION DUE TO PART AVAILABILITY.C/A: FABRICATED STRAP LANDING FIXED LEADING EDGE PN CC670-12107-3 IAW BOMBARDIER SNIEO CC670-12107-S01 AND COMPLIED WITH EXPREDec 7, 2017 · N710EV · Cndair CL6002C10 · Wing Miscellaneous StructureSDR ASOA201712075247Strap · damagedREF: CO# EJA150D JOB# EJA050D OP# 49: STRAP LANDING FIXED LEADING EDGE PN CC670-12106-3 REQUIRES FABRICATION DUE TO PART AVAILABILITY.C/A: FABRICATED STRAP LANDING FIXED LEADING EDGE PN CC670-12106-3 IAW BOMBARDIER SNIEO CC670-12106-S01 AND COMPLIED WITH EXPREDec 7, 2017 · N710EV · Cndair CL6002C10 · Wing Miscellaneous StructureSDR ASOA201712075246Rib · damagedREF: CO# EJA150D JOB# EJA050D OP# 14: LEFT WING STATION 15.5 RIB IS DAMAGED. C/A: REMOVED AND REPLACED LEFT WING STATION 15.5 RIB IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01, AND 51-42-06-001-001-A01.Dec 7, 2017 · N710EV · Cndair CL6002C10 · Wing, Rib/BulkheadSDR ASOA201702081298Smoke Detector · failedFIRE SYS FAULT STATUS MSG. REMOVED AND REPLACED FWD CARGO SMOKE DET 2 (A227 ) IAW AMM 26-17-01, IPC REF 26-17-01 ITEM 5, OPS CHECK GOOD DEFER CLEARED, PLACARD REMOVED.Feb 8, 2017 · N710EV · Cndair CL6002C10 · Smoke DetectionSDR ASOA201611076146Channel · corrodedNUT PLATE CHANNEL CORRODED BETWEEN 193AB AND 194AB. COMPLIED WITH EC/TC EA 32-2016-202 AND EA 32-2016-202. A/C WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201611076145Floorbeam · corrodedFLOORBEAM CORRODED FS 797-813. COMPLIED WITH EC/TC REO 670-53-41-289 AND REO 670-53-41-289. A/C WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201611076144Seat Track · corrodedRT SEAT RAIL CORRODED FS 785-863. REMOVED RAIL. COMPLIED WITH EC/TC REO 670-53-00-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201611076143Seat Track · corrodedRT SEAT RAIL CORRODED FS 677-708. REMOVED RAIL. C/W EC/TC REO 670-53-00-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201611076142Seat Track · corrodedRT SEAT RAIL CORRODED FS 581-677. REMOVED RAIL. C/W EC/TC REO 670-53-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201611076141Seat Track · corrodedLT SEAT RAIL CORRODED FS 785-863. REMOVED RAIL. C/W EC/TC REO 670-53-00-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201611076140Seat Track · corrodedLT SEAT RAIL CORRODED FS 708-761. REMOVED RAIL. COMPLIED WITH EC/TC REO 670-53-00-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201611076139Seat Track · corrodedLT SEAT RAIL CORRODED FS 677-708. REMOVED RAIL AND C/W EC/TC REO 670-53-00-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201611076138Door Sill · corrodedRT FLOOR SILL CORRODED FS 1000-1080. C/W EC/TC REO 970-53-00-390 AND REO 670 53-00-390. A/C APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201611076137Door Sill · corrodedAFT CARGO FLOOR SILL CORRODED. REMOVED AND REPLACED AFT CARGO FLOOR SILL PER SRM 700 51-42-06-001-001, 51-42-13-001-001. P/N MM670-35655-003 DRAWING MM670-35655. A/C WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201611076136Floorbeam · corrodedFLOORBEAM CORRODED FS 1000-1031. COMPLIED WITH EC/TC 700-53-0356 AND REO 670-53-029.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201611076135Floor Support · corrodedLBL 9 FLOOR SUPPORT CORRODED AT BS 549 - 638. REPAIRED IAW EC/TC EO 700-53-0358 AND EO 700-53-0359. AIRCRAFT APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201611076134Floor Support · corrodedLEFT FLOOR SUPPORT CORRODED AT BS 547. REPAIRED IAW EC/TC REO 970-53-00-390. AIRCRAFT APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201611076133Floor Support · corrodedRIGHT FLOOR SUPPORT CORRODED BS 351 RBL 45. REPAIRED IAW EC/TC REO 670-53-00-390. AIRCRAFT APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201611076132Frame · corrodedFRAME CORRODED AT BS 333 STRINGER 26-27R. REPAIRED THE FRAME IAW EC/TC 25-2016-247. AIRCRAFT APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201611076131Door Frame · corrodedLEFT FLIGHT DECK DOOR POST CORRODED AT BOTTOM, BS 280 LBL 9. REPAIRED IAW EC/TC EA 25-2016-248. AIRCRAFT APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201611076130Buttstrap · corrodedBUTTSTRAP CORRODED FS 280 BETWEEN STRINGERS 26-27L. REPAIRED THE BUTTSTRAP IAW EA 12-2016-146 AND EC/TC EA 12-2016-146. AIRCRAFT APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201611076129Angle · corrodedAVIONICS BAY FLOORBEAM ANGLE ON AFT SIDE OF BS 280 IS CORRODED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06-001-001-A01 AND DRAWING CC670-34010. AIRCRAFT APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201611076128Doubler · corrodedTCAS ANTENNA DOUBLER CORRODED AT STRINGER 27L BETWEEN BS 295-310. REMOVED AND REPLACED DOUBLER IAW SRM 51-40-001-001-A01 AND 51-42-06-001-001-A01. AIRCRAFT APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201611076127Skin · dentedRIGHT INBD FLAP DENTED. REPAIRED IAW SRM 57-52-01-201-001-A01 REPAIR IV. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Trailing Edge FlapsSDR ASOA201611076126Heat Shield · damagedHOLE WORN THROUGH RT ENGINE LOWER CORE COWL INNER HEAT SHIELD. REPAIRED HOLE TO LOWER CORE COWL IAW REO 670-54-23-959 AND ECTC REO 670-54-23-959. AIRCRAFT APPROVED FOR RETURN TO SERVICE.Nov 7, 2016 · N710EV · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR ASOA201610180595Charger · inoperativeDURING MX INSPECTION, THE NR 1 EMERGENCY FLOOD LIGHT WOULD NOT ILLUMINATE. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPS CHECKED GOOD. RETURNED TO SERVICE.Oct 18, 2016 · N710EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201610120835Floor Support · corrodedDURING C CHECK INSPECTION, AFT CARGO FLOOR SUPPORT HAS CORROSION. R & R THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01. ACFT WAS APPROVED FOR RETURN TO SERVICE.Oct 12, 2016 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
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