# Service difficulty reports: N710EV A list on [N710EV](https://openairdocs.org/aircraft/N710EV.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 · 223 reports - [SDR SWIA202265928](https://openairdocs.org/sdr/SWIA202265928.md): None · worn · May 12, 2022 · N710EV · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings > PASSENGER 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. - [SDR SWIA202265927](https://openairdocs.org/sdr/SWIA202265927.md): None · cut · Apr 14, 2022 · N710EV · Cndair CL6002C10 · Doors > COMPLY 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 FS - [SDR SWIA202164817](https://openairdocs.org/sdr/SWIA202164817.md): None · damaged · Dec 13, 2021 · N710EV · Cndair CL6002C10 · Doors > PASSENGER 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 REV - [SDR SWIA202164816](https://openairdocs.org/sdr/SWIA202164816.md): None · corroded · Dec 2, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Keel > DURING 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 C - [SDR SWIA202164815](https://openairdocs.org/sdr/SWIA202164815.md): Extension · corroded · Nov 28, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Frame > FS 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 51-900-1002 - [SDR SWIA202164814](https://openairdocs.org/sdr/SWIA202164814.md): Frame · corroded · Nov 18, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Frame > DURING 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 CRJ - [SDR SWIA202164813](https://openairdocs.org/sdr/SWIA202164813.md): None · corroded · Nov 13, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > CORROSION 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 F - [SDR SWIA202164812](https://openairdocs.org/sdr/SWIA202164812.md): None · corroded · Nov 12, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > INTERCOSTAL 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. CRJ700 - [SDR SWIA202164811](https://openairdocs.org/sdr/SWIA202164811.md): None · corroded · Nov 12, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > INTERCOSTAL 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 P - [SDR SWIA202164810](https://openairdocs.org/sdr/SWIA202164810.md): None · chafed · Nov 9, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Keel > FS 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 - [SDR SWIA202164809](https://openairdocs.org/sdr/SWIA202164809.md): None · corroded · Nov 3, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Keel > CORROSION 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 ACTI - [SDR SWIA202164808](https://openairdocs.org/sdr/SWIA202164808.md): None · corroded · Nov 3, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Keel > CORROSION 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 51-42-21-00 - [SDR SWIA202164807](https://openairdocs.org/sdr/SWIA202164807.md): Nut · dented · Nov 1, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Frame > L/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. P - [SDR SWIA202164806](https://openairdocs.org/sdr/SWIA202164806.md): None · dented · Nov 1, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Frame > L/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 AND - [SDR SWIA202164805](https://openairdocs.org/sdr/SWIA202164805.md): None · cracked · Nov 1, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Frame > ABOVE 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 D - [SDR SWIA202164804](https://openairdocs.org/sdr/SWIA202164804.md): None · cracked · Oct 27, 2021 · N710EV · Cndair CL6002C10 · Fuselage Structure (General) > FORWARD 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, 51-40-11 - [SDR SWIA202164803](https://openairdocs.org/sdr/SWIA202164803.md): None · corroded · Oct 21, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Frame > FS565 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 - [SDR SWIA202164802](https://openairdocs.org/sdr/SWIA202164802.md): None · corroded · Oct 21, 2021 · N710EV · Cndair CL6002C10 · Fuselage Main, Frame > FS549 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-A - [SDR SWIA202164801](https://openairdocs.org/sdr/SWIA202164801.md): None · worn · Oct 16, 2021 · N710EV · Cndair CL6002C10 · Wing, Fuselage Attach Fittings > RIGHT 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- - [SDR ASOA201809057164](https://openairdocs.org/sdr/ASOA201809057164.md): Stringer · damaged · Sep 5, 2018 · N710EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > TYS-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. - [SDR ASOA201809057163](https://openairdocs.org/sdr/ASOA201809057163.md): Stringer · damaged · Sep 5, 2018 · N710EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > DAMAGED 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. - [SDR ASOA201809057162](https://openairdocs.org/sdr/ASOA201809057162.md): Stringer · damaged · Sep 5, 2018 · N710EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > FOUND 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. - [SDR ASOA201801255041](https://openairdocs.org/sdr/ASOA201801255041.md): Connector · damaged · Jan 25, 2018 · N710EV · Cndair CL6002C10 · Emergency Lighting > DURING MX INSPECTION, THE EMERGENCY CEILING LIGHT AT ROW 9 WAS FOUND INOPERATIVE. MX CRIMPED NEW PINS IN THE CONNECTOR. OPS CHECKED GOOD. - [SDR ASOA201712075248](https://openairdocs.org/sdr/ASOA201712075248.md): Strap · damaged · Dec 7, 2017 · N710EV · Cndair CL6002C10 · Wing Miscellaneous Structure > REF: 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 EXPRE - [SDR ASOA201712075247](https://openairdocs.org/sdr/ASOA201712075247.md): Strap · damaged · Dec 7, 2017 · N710EV · Cndair CL6002C10 · Wing Miscellaneous Structure > REF: 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 EXPRE - [SDR ASOA201712075246](https://openairdocs.org/sdr/ASOA201712075246.md): Rib · damaged · Dec 7, 2017 · N710EV · Cndair CL6002C10 · Wing, Rib/Bulkhead > REF: 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. - [SDR ASOA201702081298](https://openairdocs.org/sdr/ASOA201702081298.md): Smoke Detector · failed · Feb 8, 2017 · N710EV · Cndair CL6002C10 · Smoke Detection > FIRE 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. - [SDR ASOA201611076146](https://openairdocs.org/sdr/ASOA201611076146.md): Channel · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > NUT 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. - [SDR ASOA201611076145](https://openairdocs.org/sdr/ASOA201611076145.md): Floorbeam · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Main, Floor Beam > FLOORBEAM 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. - [SDR ASOA201611076144](https://openairdocs.org/sdr/ASOA201611076144.md): Seat Track · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > RT 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. - [SDR ASOA201611076143](https://openairdocs.org/sdr/ASOA201611076143.md): Seat Track · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > RT 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. - [SDR ASOA201611076142](https://openairdocs.org/sdr/ASOA201611076142.md): Seat Track · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > RT 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. - [SDR ASOA201611076141](https://openairdocs.org/sdr/ASOA201611076141.md): Seat Track · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > LT 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. - [SDR ASOA201611076140](https://openairdocs.org/sdr/ASOA201611076140.md): Seat Track · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > LT 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. - [SDR ASOA201611076139](https://openairdocs.org/sdr/ASOA201611076139.md): Seat Track · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > LT 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. - [SDR ASOA201611076138](https://openairdocs.org/sdr/ASOA201611076138.md): Door Sill · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > RT 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. - [SDR ASOA201611076137](https://openairdocs.org/sdr/ASOA201611076137.md): Door Sill · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > AFT 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. - [SDR ASOA201611076136](https://openairdocs.org/sdr/ASOA201611076136.md): Floorbeam · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Main, Floor Beam > FLOORBEAM CORRODED FS 1000-1031. COMPLIED WITH EC/TC 700-53-0356 AND REO 670-53-029. - [SDR ASOA201611076135](https://openairdocs.org/sdr/ASOA201611076135.md): Floor Support · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > LBL 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. - [SDR ASOA201611076134](https://openairdocs.org/sdr/ASOA201611076134.md): Floor Support · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > LEFT FLOOR SUPPORT CORRODED AT BS 547. REPAIRED IAW EC/TC REO 970-53-00-390. AIRCRAFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201611076133](https://openairdocs.org/sdr/ASOA201611076133.md): Floor Support · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > RIGHT FLOOR SUPPORT CORRODED BS 351 RBL 45. REPAIRED IAW EC/TC REO 670-53-00-390. AIRCRAFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201611076132](https://openairdocs.org/sdr/ASOA201611076132.md): Frame · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Main, Frame > FRAME CORRODED AT BS 333 STRINGER 26-27R. REPAIRED THE FRAME IAW EC/TC 25-2016-247. AIRCRAFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201611076131](https://openairdocs.org/sdr/ASOA201611076131.md): Door Frame · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Main, Structure > LEFT 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. - [SDR ASOA201611076130](https://openairdocs.org/sdr/ASOA201611076130.md): Buttstrap · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Main, Structure > BUTTSTRAP 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. - [SDR ASOA201611076129](https://openairdocs.org/sdr/ASOA201611076129.md): Angle · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Main, Floor Beam > AVIONICS 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. - [SDR ASOA201611076128](https://openairdocs.org/sdr/ASOA201611076128.md): Doubler · corroded · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin > TCAS 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. - [SDR ASOA201611076127](https://openairdocs.org/sdr/ASOA201611076127.md): Skin · dented · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Trailing Edge Flaps > RIGHT INBD FLAP DENTED. REPAIRED IAW SRM 57-52-01-201-001-A01 REPAIR IV. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201611076126](https://openairdocs.org/sdr/ASOA201611076126.md): Heat Shield · damaged · Nov 7, 2016 · N710EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame > HOLE 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. - [SDR ASOA201610180595](https://openairdocs.org/sdr/ASOA201610180595.md): Charger · inoperative · Oct 18, 2016 · N710EV · Cndair CL6002C10 · Emergency Lighting > DURING 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. - [SDR ASOA201610120835](https://openairdocs.org/sdr/ASOA201610120835.md): Floor Support · corroded · Oct 12, 2016 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > DURING 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. Next page: https://openairdocs.org/aircraft/N710EV/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 = 'N710EV' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N710EV/reports --- 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.