# Service difficulty reports: N730EV A list on [N730EV](https://openairdocs.org/aircraft/N730EV.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 · 221 reports - [SDR SWIA2026071276619](https://openairdocs.org/sdr/SWIA2026071276619.md): Unknown · odor · Jul 12, 2026 · N730EV · Cndair CL6002C10 · Air Distribution System > ON SHORT FINAL FAS CALLED ADVISING VERY FAINT SMOKE IN THE CABIN. NO INDICATIONS IN COCKPIT. AFTER LANDING AND SITTING FOR ABOUT 2 MIN, WE RECEIVED RT PACK AUTOFAIL CAUTION MESSAGE. PACK WAS SET TO 23 CABIN TEMP WAS 25 AND PACK TEMP WAS 94. FLIGHT 4920. OP - [SDR SWIA2025072800006](https://openairdocs.org/sdr/SWIA2025072800006.md): Warning Message · false activation · Jul 26, 2025 · N730EV · Cndair CL6002C10 · Central Warning > ANTI ICE DUCT WARNING MESSAGE MOMENTARILY THEN ANTI ICE CAUTION ASSOCIATED WITH L/R WING A/I CCAUTION MESSAGES. PERFORMED EMER CHECKLIST AND ANTI ICE DUCT MESSAGES DISAPPEARED. (FLIGHT 4903 - FILED CLOSED)INTERROGATED MDC FOUND NO CURRENT FAULTS POSTED AT THI - [SDR SWIA202507110002](https://openairdocs.org/sdr/SWIA202507110002.md): Stop Fitting · cracked · Jul 2, 2025 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > UPON TROUBLESHOOTING HARD TO CLOSE PAX DOOR FOUND FORWARD STOP BRACKET CRACKED. (FILED CLOSED)REMOVED AND REPLACED PAX DOOR FORWARD STOP BRACKET WITH REFERENCE TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMPLETED M-337. REFERENCE CHILD CAMP - [SDR SWIA20241006](https://openairdocs.org/sdr/SWIA20241006.md): Mount · unknown · Oct 6, 2024 · N730EV · Cndair CL6002C10 · Engine Mount Section > COMPLY WITH SCHEDULED MAINTENANCE CODE: ENGINE FORWARD FITTING MOUNT, YOKE AND LINK - PART IS DUE SPECIAL DETAILED INSPECTION. REMOVE AND REPLACE WITH SERVICEABLE PART IAW AMM. SEND REMOVED PART TO VENDOR FOR INSPECTION (MRB 71-21-101, REF TASK CARD(S) 71-410- - [SDR SWIA2024090600821](https://openairdocs.org/sdr/SWIA2024090600821.md): Skin · dented · Aug 21, 2024 · N730EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin > TRANSFER FROM EAML 1414568: DENT ON LOWER L/H SIDE OF NOSE FUSELAGE BETWEEN FS210.92 AND FS220.00 AND STGR 23L AND STGR 24L, DENT IS 0.115 INCHES DEEP BY 1.50 INCHES WIDE AND 1.75 INCHES LONG. INSPECTED DENT FOUND TO BE OUT OF LIMITS PER SRM 53-11-01 AND 53- - [SDR SWIA2024051000008](https://openairdocs.org/sdr/SWIA2024051000008.md): Windshield · cracked · May 8, 2024 · N730EV · Cndair CL6002C10 · Flight Compartment Windows > WINDSHIELD CRACKED. (FLIGHT 4955 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28207743 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED RH WINDSHIELD PER CRJ 700 AMM 56-11-01 AND COMPLIED WITH TASK CARD 56-220-1000-SKY. SEE ML 28207742 - [SDR SWI2024080900395](https://openairdocs.org/sdr/SWI2024080900395.md): Windshield · cracked · May 8, 2024 · N730EV · Cndair CL6002C10 · Flight Compartment Windows > WINDSHIELD CRACKED. (FLIGHT 4955 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS. - [SDR SWIA20240508329](https://openairdocs.org/sdr/SWIA20240508329.md): Stringer · corroded · Mar 29, 2024 · N730EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > WHILE APPLYING CIC, CORROSION WAS DISCOVERED ON STRINGER 20R AFT OF FS863.00 (C-CHECK RO 5/6/2024) CORROSION FOUND TO BE OUT OF LIMITS ON STGR 20R AT APPROX FS863 - FS879. PERFORMED SPLICE REPAIR REF REO 670-53-51-280 REV -- 2024-04-15, CRJ-700 SRM 51-42-0 - [SDR SWIA202405080326](https://openairdocs.org/sdr/SWIA202405080326.md): Attach Fitting · cracked · Mar 26, 2024 · N730EV · Cndair CL6002C10 · Wing, Control Surface Attach Fittings > RH SLAT TRACK 1-3, TRACK CANNISTER ATTACH FITTING CRACKED INSIDE FUEL PANEL 651AB (MARKED) (C-CHECK RO 5/6/2024) COMPLIED WITH REO 670-57-42-577 REV-- DATED: 2016-12-02 AND REPAIRED RH SLAT TRACK 1-3 TRACK CANNISTER ATTACH FITTING. SEE CONTINUATION FOR DE - [SDR SWI202405080373](https://openairdocs.org/sdr/SWI202405080373.md): Frame · corroded · Mar 20, 2024 · N730EV · Cndair CL6002C10 · Fuselage Main, Frame > FRAME AT FS250 STGR27-26L HAS AREAS CORROSION (FWD AND AFT) MARKED (C-CHECK RO 5/6/2024) REPAIRED FRAME AT FS250, STGR 25L - 25R REF REO 670-53-11-1936 REV -- 2024-04-10. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECKS GOOD - [SDR SWI202405080372](https://openairdocs.org/sdr/SWI202405080372.md): Plate · corroded · Mar 20, 2024 · N730EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FWD CARGO HOLD DOWN PLATE AFT OF CARGO DOOR CORRODED AT FS 581 MARKED (C-CHECK RO 5/6/2024) REPLACED FWD CARGO HOLD DOWN PLATE (BRACKET) WITH NEW PN SH670-33390-2 AT FS 581 BETWEEN STR 22L -23L REF CRJ 700 SRM 51-42-21-001-001-A01 AND DWG SH670-33600 RE - [SDR SWI202405080371](https://openairdocs.org/sdr/SWI202405080371.md): Frame · corroded · Mar 20, 2024 · N730EV · Cndair CL6002C10 · Fuselage Main, Frame > FRAME AT FS265 STGR27 HAS AREAS CORROSION (C-CHECK RO 5/6/2024) PERFORMED FRAME SPLICE REPAIR AT F.S 265 BETWEEN 26L TO 26R REF. REO 670-53-11-1937 REV. -- DATED 2024-04-29 ALL STEPS COMPLIED WITH.. COMPLIED WITH TAK CARD 51-900-1002-SKY. PRESSURE CHECKS - [SDR SWIA20240508320](https://openairdocs.org/sdr/SWIA20240508320.md): Diaphragm · corroded · Mar 20, 2024 · N730EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > BACKUP DIAPHRAGM HAS CORROSION ON UPPER FLANGE BENEATH NUTPLATE @ APPROX FS581.00 - FS597.00 BETWEEN STGR22L & STGR23L (C-CHECK RO 5/6/2024) REMOVED CORROSION ON BACKUP DIAPHRAGM ON UPPER FLANGE @ FS581.00 - FS597.00 BETWEEN STGR22L & STGR23L WITH NO NOTED - [SDR SWIA20240508317](https://openairdocs.org/sdr/SWIA20240508317.md): Door Sill · corroded · Mar 17, 2024 · N730EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > SERVICE DOOR SILL HAS AREAS OF CORROSION (C-CHECK RO 5/6/2024) PERFORMED REPAIR OF SERVICE DOOR SILL BY COMPLYING WITH ALL STEPS OF REO 670-53-21-2380 REV -- DATED 2024-03-30. SEE CONTINUATION FOR WORK PERFORMED.COMPLIED WITH 51-900-1002-SKY - [SDR SWI202405080353](https://openairdocs.org/sdr/SWI202405080353.md): Striker · dented · Mar 10, 2024 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > FWD LOWER PAX DOOR SEAL STRIKER ON FUSELAGE HAS A DENT. (C-CHECK RO 5/6/2024) COMPLIED WITH REO 670-53-22-001 REV -J DATED 2016-11-10 FOR REPAIR (TYPE 1) TO FWD LOWER PAX DOOR SEAL STRIKER. COMPLIED WITH ALL STEPS OF REO FOR REPAIR (TYPE 1). LEAK TEST GOOD - [SDR SWI202405080352](https://openairdocs.org/sdr/SWI202405080352.md): Skin · chafed · Mar 10, 2024 · N730EV · Cndair CL6002C10 · Ailerons > RH AILERON LOWER LEADING EDGE CHAFED. (C-CHECK RO 5/6/2024) INSTALLED NEW R/H AILERON SKIN LOWER OTBD LEADING EDGE PANEL P/N: CC670-13054-2 REF DRW CC670-13000 REV -D, CRJ 700 SRM 51-42-21-001-001-A01 AND CRJ 700 SRM 51-42-06-001-001-A01. AND INSTALLED NEW - [SDR SWI2024050800351](https://openairdocs.org/sdr/SWI2024050800351.md): Skin · chafed · Mar 10, 2024 · N730EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin > PREVIOUS REPAIR PLATE HAS CHAFING FS985.00 STGR26L - STGR26R. (MARKED) (C-CHECK RO 5/6/2024) REMOVED EXISTING REPAIR PER REO 670-53-00-290 REV -F DATE 2019/04/26 AND INSTALLED NEW REPAIR PER REO 670-53-00-290 REV -F DATE 2019/04/26 SOLUTION #1, PRESSURE - [SDR SWI202405080350](https://openairdocs.org/sdr/SWI202405080350.md): Skin · chafed · Mar 10, 2024 · N730EV · Cndair CL6002C10 · Ailerons > LH AILERON LOWER LEADING EDGE CHAFED (C-CHECK RO 5/6/2024) REMOVED AND REPLACED LH AILERON LOWER LEADING EDGE SKIN (PN CC670-13054-1) PER CRJ700 SRMS 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND COMPLIED WITH TASK CARD 51-900-1002-SKY. - [SDR SWI202405080349](https://openairdocs.org/sdr/SWI202405080349.md): Retainer · dented · Mar 10, 2024 · N730EV · Cndair CL6002C10 · Fuselage Main, Structure > AFT UPPER PAX DOOR SEAL RETAINER ON FUSELAGE HAS A DENT (C-CHECK RO 5/6/2024) COMPLIED WITH REO 670-53-22-001 REV -J DATED 2016-11-10 REPAIR (TYPE 1) FOR AFT UPPER PAX DOOR SEAL STRIKER REPAIR. COMPLIED WITH ALL STEPS OF REO REPAIR (TYPE 1). LEAK TEST GOO - [SDR SWIA2024050800310](https://openairdocs.org/sdr/SWIA2024050800310.md): Skin · chafed · Mar 10, 2024 · N730EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/Skin > LEFT ENGINE UPPER FAN COWL INNER SKIN IS CHAFED AT THE OUTBOARD SIDE. (C-CHECK RO 5/6/2024) REMOVED DAMAGED OUTBOARD GUSSET P/N CN622-0333-203 FROM L/H UPPER FAN COWL, REF. CRJ700 SRM 51-42-13-001-001-A01 AND INSTALLED NEW OUTBOARD GUSSET P/N CN622-0333-20 - [SDR SWI202405080370](https://openairdocs.org/sdr/SWI202405080370.md): Intercostal · corroded · Mar 6, 2024 · N730EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > PAX DOOR INTERCOSTAL DD4 FS320.00 - FS338.00 IS CORRODED (C-CHECK RO 5/6/2024) REMOVED AND DISCARDED EXISTING PAX DOOR INTERCOSTAL DD4 FS320.00 - FS338.00. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01 AND INSTALLED NEW PAX DO - [SDR SWI202405080369](https://openairdocs.org/sdr/SWI202405080369.md): Intercostal · corroded · Mar 6, 2024 · N730EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > PAX DOOR INTERCOSTAL DD7 FS320.00 - FS327.763 IS CORRODED (C-CHECK RO 5/6/2024) REMOVED AND DISCARDED EXISTING PAX DOOR INTERCOSTAL DD7 FS320.00 - FS327.763. RE F: CRJ-700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW PAX DOOR INTERCOSTAL DD7 FS320.00 - FS327 - [SDR SWI202405080368](https://openairdocs.org/sdr/SWI202405080368.md): Intercostal · corroded · Mar 6, 2024 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD1A FS338.00 - FS347.25 IS CORRODED (C-CHECK RO 5/6/2024) REMOVED AND DISCARDED EXISTING PAX DOOR INTERCOSTAL DD1A FS338.00 - FS347.25. RE F: CRJ-700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW PAX DOOR INTERCOSTAL DD1A FS338.00 - FS34 - [SDR SWIA20240508306](https://openairdocs.org/sdr/SWIA20240508306.md): Intercostal · corroded · Mar 6, 2024 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD6 FS338.00 - FS347.25 IS CORRODED (C-CHECK RO 5/6/2024) REMOVED AND DISCARDED EXISTING PAX DOOR INTERCOSTAL DD6 FS338.00 - FS347.25. RE F: CRJ-700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW PAX DOOR INTERCOSTAL DD6 FS338.00 - FS347. - [SDR SWIA20240508305](https://openairdocs.org/sdr/SWIA20240508305.md): Skin · cracked · Mar 5, 2024 · N730EV · Cndair CL6002C10 · Engine Thrust Reverser > L/H UPPER TRANSCOWL PERFORATED SKIN UNDER Z STIFFENER IS CRACKED (C-CHECK RO 5/6/2024) L/H ENGINE UPPER TRANSCOWL INNER SKIN HAS BEEN REPAIRED REF REO# 670-54-21-1626, REV --, DATED 3/29/24. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED FULLY W/SKYCARD 51- - [SDR SWI202405080359](https://openairdocs.org/sdr/SWI202405080359.md): Hinge · chafed · Mar 4, 2024 · N730EV · Cndair CL6002C10 · Fuselage, Door Hinge > PAX DOOR HINGE (DOOR SIDE) HAS CHAFE DAMAGE TO LUGS 1, 3, 5, 11, 16, 18, 19, 25, 26, AND 27 (C-CHECK RO 5/6/2024) BLENDED OUT CHAFFNG AND RESTORED FINISH TO REWORKED AREA ON PAX DOOR HINGE (DOOR SIDE) LUGS 1, 3, 5, 11, 16, 18, 19, 25, 26, AND 27.REF: CRJ- - [SDR SWI202405080358](https://openairdocs.org/sdr/SWI202405080358.md): Hinge · gouged · Mar 4, 2024 · N730EV · Cndair CL6002C10 · Fuselage, Door Hinge > FOUND GOUGE ON PAX DOOR HINGE (FUSELAGE SIDE) LAND #27 (C-CHECK RO 5/6/2024) REPLACED PAX. DOOR HINGE WITH A NEW ONE (FUSELAGE SIDE). REF: CRJ-700 SRM 53-21-13-201-007-A01 REV 38 DATED JULY 25/2020 AND DWG SH670-31810 REV AE. LEAK CHECK GOOD WITH NO LEAKS - [SDR SWI202405080357](https://openairdocs.org/sdr/SWI202405080357.md): Floorbeam · cracked · Mar 4, 2024 · N730EV · Cndair CL6002C10 · Fuselage Main, Floor Beam > CRACK FOUND AT RBL12 COCKPIT FLOOR BEAM FS280 (C-CHECK RO 5/6/2024) PERFORMED REPAIR TO THE RH CENTER COCKPIT FLOOR BEAM AT RBL12.00 REF CRJ-700 SRM 53-11-43-201-003-A01 TYPE IV. COMPLIED WITH TASK CARD 51-900-1002-SKY - [SDR SWI202405080356](https://openairdocs.org/sdr/SWI202405080356.md): Skin · corroded · Mar 4, 2024 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR OUTER SKIN IS CORRODED BETWEEN TOP OF DOOR CENTER AND DD1 NEAR STANDOFF (C-CHECK RO 5/6/2024) REPAIRED PAX DOOR OUTER SKIN BETWEEN FS320.163 - FS338.963 AND UPPER DOOR BEAM - DOOR DATUM 1 PER REO 670-51-11-1378 REV -- DATED: 2024-03-25. COMPLIED W - [SDR SWI202405080355](https://openairdocs.org/sdr/SWI202405080355.md): Intercostal · corroded · Mar 4, 2024 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD1A FS323.00 - FS336.00 IS CORRODED (C-CHECK RO 5/6/2024) REMOVED AND DISCARDED EXISTING PAX DOOR INTERCOSTAL DD1A FS323.00 - FS336.00. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01 AND INSTALLED NEW PAX D - [SDR SWIA202405080304](https://openairdocs.org/sdr/SWIA202405080304.md): Floorbeam · cracked · Mar 4, 2024 · N730EV · Cndair CL6002C10 · Fuselage Main, Floor Beam > CRACK FOUND AT LBL12 COCKPIT FLOOR BEAM FS280 (C-CHECK RO 5/6/2024) PERFORMED CENTER COCKPIT FLOOR BEAM AT BL12.00 TYPE 4 REPAIR IAW CRJ 700 SRM 53-11-43-201-003-A01, SEE CONTINUATION CARD FOR FURTHER DETAILS.COMPLIED WITH 51-900-1002-SKY - [SDR SWI202405080361](https://openairdocs.org/sdr/SWI202405080361.md): Drag Angle · cracked · Mar 2, 2024 · N730EV · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings > R/H VERTICAL STAB TO FUSELAGE ATTACHMENT DRAG ANGLE AFT POSSIBLE CRACK. (MARKED) (C-CHECK RO 5/6/2024) COMPLIED WITH ALL STEPS OF REPAIR TO RH VERTICAL TO FUSELAGE AFT DRAG ANGLE AND INSTALLED ALL FABRICATED REPAIR PARTS -6 R/H AFT ANGLE DOUBLER AND -8 R/H - [SDR SWI202405080360](https://openairdocs.org/sdr/SWI202405080360.md): Vane · chafed · Mar 2, 2024 · N730EV · Cndair CL6002C10 · Trailing Edge Flaps > RIGHT INBOARD FLAP, FLAP VANE. LEADING EDGE AT FLS72 IS CHAFED. (MARKED) (C-CHECK RO 5/6/2024) REMOVED AND INSTALLED 1EA NEW R/H INBD FLAP VANE CAP AT FLS72 PER CRJ700SRM 51-42-13-001-001-A01 AND CRJ700SRM 51-23-00-001-001-A01 AND DWG CC670-14010 REV -F. S - [SDR SWIA202405080302](https://openairdocs.org/sdr/SWIA202405080302.md): Skin · damaged · Mar 2, 2024 · N730EV · Cndair CL6002C10 · Trailing Edge Flaps > LEFT INBOARD FLAP LOWER SKIN HAS A CREASE FLS 41 AND 5.5 INCHES FROM THE TRAILING EDGE. (MARKED) (C-CHECK RO 5/6/2024) L/H I/B FLAP LOWER SKIN HAS BEEN REPAIRED REF CRJ SRM 57-52-01-201-002-A01, TYPE 4, PERMANENT NON FLUSH REPAIR.. COMPLIED FULLY W/SKYCA - [SDR SWIA202266680](https://openairdocs.org/sdr/SWIA202266680.md): None · none · Oct 30, 2022 · N730EV · Cndair CL6002C10 · Window/Windshield System > DURING DECENT PASSING THROUGH 24000 L WSHLD HEAT CAUTION MESSAGE APPEARED. WHILE FOLLOWING QRH ARCING ON WINDSHIELD WAS NOTED. PASSING 20000 WINDSHIELD PLY SHATTERED. (FLIGHT #3027 FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25727129 WITH T - [SDR SWIA202081951821](https://openairdocs.org/sdr/SWIA202081951821.md): Selector Valve · inoperative · Aug 19, 2020 · N730EV · Cndair CL6002C10 · Landing Gear Retraction/Extension System > GEAR DISAGREE WARNING MESSAGE WHILE ON FINAL EXTENDING THE LANDING GEAR. ON 6 MILE FINAL MOVED THE LANDING GEAR LEVER TO DOWN AND THE GEAR DID NOT MOVE. COMPLIED WITH THE QRH FOR A GEAR DOWN DISAGREE. CYCLED THE GEAR SEVERAL TIMES ACCORDING TO THE QRH. COMPLET - [SDR SWIA2019122747165](https://openairdocs.org/sdr/SWIA2019122747165.md): Angle · corroded · Dec 2, 2019 · N730EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > PAX DOOR LOWER SILL ANGLE MID CAP ANGLE HAD CORROSION. REMOVED AND REPLACED THE ANGLE IAW DWG. - [SDR SWIA2019122747164](https://openairdocs.org/sdr/SWIA2019122747164.md): Angle · corroded · Dec 2, 2019 · N730EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > PAX DOOR LOWER SILL ANGLE FWD CAP ANGLE HAD CORROSION. REMOVED AND REPLACED THE ANGLE IAW DWG SH670-31810, REV AE, AND SRM. - [SDR SWIA2019122747153](https://openairdocs.org/sdr/SWIA2019122747153.md): Intercostal · corroded · Nov 26, 2019 · N730EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > INTERCOSTAL, BS 310 TO 333, STRINGER 21L HAD CORROSION. BLENDED AND FOUND TO BE OUT OF LIMITS. REMOVED & INSTALLED A NEW INTERCOSTAL IAW DWG SH670-31810, REV Y, AND SRMS. - [SDR SWIA2019122747163](https://openairdocs.org/sdr/SWIA2019122747163.md): Cleat · corroded · Nov 24, 2019 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR CENTER INTERCOSTAL, FWD CLEAT HAD CORROSION. INSTALLED A NEW CLEAT IAW SRM. - [SDR SWIA2019122747162](https://openairdocs.org/sdr/SWIA2019122747162.md): Cleat · corroded · Nov 24, 2019 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR FWD INTERCOSTAL AFT CLEAT HAD CORROSION. INSTALLED A NEW CLEAT IAW SRM. - [SDR SWIA2019122747161](https://openairdocs.org/sdr/SWIA2019122747161.md): Cleat · corroded · Nov 24, 2019 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR FWD INTERCOSTAL, FWD CLEAT HAD CORROSION. INSTALLED A NEW CLEAT IAW SRM. - [SDR SWIA2019122747160](https://openairdocs.org/sdr/SWIA2019122747160.md): Cleat · corroded · Nov 24, 2019 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR AFT CLEAT ON INTERCOSTAL WAS CORRODED. REMOVED AND INSTALLED THE CLEAT ON INTERCOSTAL IAW SRM. - [SDR SWIA2019122747159](https://openairdocs.org/sdr/SWIA2019122747159.md): Intercostal · corroded · Nov 24, 2019 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR AFT INTERCOSTAL WAS CORROED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM. - [SDR SWIA2019122747158](https://openairdocs.org/sdr/SWIA2019122747158.md): Intercostal · corroded · Nov 24, 2019 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR FWD INTERCOSTAL WAS CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM AND DWG. - [SDR SWIA2019122747157](https://openairdocs.org/sdr/SWIA2019122747157.md): Intercostal · corroded · Nov 23, 2019 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL WAS CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM AND DWG. - [SDR SWIA2019122747156](https://openairdocs.org/sdr/SWIA2019122747156.md): Intercostal · corroded · Nov 23, 2019 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL WAS CORRODED. INSTALLED A NEW INTERCOSTAL AND CLEATS IAW SRM. - [SDR SWIA2019122747155](https://openairdocs.org/sdr/SWIA2019122747155.md): Intercostal · corroded · Nov 23, 2019 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL WAS CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM. - [SDR SWIA2019122747154](https://openairdocs.org/sdr/SWIA2019122747154.md): Former · corroded · Nov 23, 2019 · N730EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR FWD FORMER WAS CORRODED. INSTALLED A NEW FORMER IAW SRM. - [SDR SWIA2019122747166](https://openairdocs.org/sdr/SWIA2019122747166.md): Seat Track · corroded · Nov 21, 2019 · N730EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK AT LBL9, BS 693 TO 830 CORRODED. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM. Next page: https://openairdocs.org/aircraft/N730EV/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 = 'N730EV' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N730EV/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.