# Service difficulty reports: N718EV

A list on [N718EV](https://openairdocs.org/aircraft/N718EV.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 · 238 reports

- [SDR SWIA2025111200009](https://openairdocs.org/sdr/SWIA2025111200009.md): Sensor · faulted · Nov 9, 2025 · N718EV · Cndair CL6002C11 · Landing Gear Position and Warning
  > GEAR DISAGREE ON TAKEOFF. NOSE GEAR INDICATOR WAS RED. RAN QRH AND GEAR LOCKED DOWN WITH THREE GREEN DN INDICATORS. (FLIGHT 5998) REF. CP 31173584 FOR TROUBLESHOOTING OF GEAR DISAGREE & HEALTH MONITORING CHK OF LANDING GEAR PROXIMITY SENSORS & ADJUSTMENT OF
- [SDR SWIA202157595](https://openairdocs.org/sdr/SWIA202157595.md): Floor Support · corroded · Mar 31, 2021 · N718EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LBL 9 T-CAP CORRODED NEEDS TO BE REPLACED FROM FS565.00 THRU FS693.00. (C-CHECK RO 4/20/2021) REMOVED AND REPLACED LBL 9 FLOOR BEAM T-CAP FROM FS-565.00 THRU FS-693.00 IAW CRJ-700 REO-670-53-31-631,SRM53-00-41-201-001-A01,NDTM-51-20-006-250,AMM-26-17-0
- [SDR SWIA202157594](https://openairdocs.org/sdr/SWIA202157594.md): Fairing · cracked · Feb 22, 2021 · N718EV · Cndair CL6002C10 · Aerodynamic Fairings
  > SUPPORT STRUCTURE FOR FAIRING 196AR CRACKED AFT OF FS909.00 LOWER SECTION. REFERENCE STGR24RH. (C-CHECK RO 4/20/2021) COMPLIED WITH MHIRJ REPAIR ENGINEERING ORDER 670-53-82-575. FORM M-337 COMPLETED.
- [SDR SWIA202157593](https://openairdocs.org/sdr/SWIA202157593.md): Fairing · cracked · Feb 22, 2021 · N718EV · Cndair CL6002C10 · Aerodynamic Fairings
  > SUPPORT STRUCTURE FOR FAIRING 195AL CRACKED AFT OF FS909.00 LOWER SECTION. REFERENCE STGR24LH. (C-CHECK RO 4/20/2021) COMPLIED WITH MHIRJ REPAIR ENGINEERING ORDER 670-53-82-575. FORM M-337 COMPLETED.
- [SDR SWIA202157592](https://openairdocs.org/sdr/SWIA202157592.md): Frame · cracked · Feb 10, 2021 · N718EV · Cndair CL6002C10 · Fuselage Main, Frame
  > POSSIBLE CRACK AT FRAME FS333 BETWEEN STR0 AND STR1 R/H. (C-CHECK RO 4/20/2021) PERFORMED REPAIR IAW REO 670-53-21-1954, SEE ATTACHED FORM M-337.
- [SDR SWIA202157591](https://openairdocs.org/sdr/SWIA202157591.md): Channel · corroded · Feb 6, 2021 · N718EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 1035 TO1045 DOUBLER AND DOME NUTS BETWEEN STR. 27R AND 26R NEEDS CLEANED AND EVALUATED (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED INNER NUT PLATE CHANNEL AT FS1035 TO FS1045, STR27R AND STR26R AT AFT DRAIN MAST IAW CRJ700 SRM 51-40-11, 51-4
- [SDR SWIA202157590](https://openairdocs.org/sdr/SWIA202157590.md): Skin · dented · Feb 4, 2021 · N718EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > RIGHT FUSELAGE DENT INSIDE RVSM AREA, LOWER FORWARD BELOW RIGHT TRU DOOR CUT OUT (C-CHECK RO 4/20/2021) COMPLIED WITH REWORK ON DENT ON ADG SKIN PANEL BETWEEN FS185.00 AND FS 193.00 AND STRINGER 16R AND 17R IAW MHIRJ REPAIR ENGINEERING ORDER 670-53-11-
- [SDR SWIA202157589](https://openairdocs.org/sdr/SWIA202157589.md): Anchor Fitting · corroded · Jan 29, 2021 · N718EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TOP SURFACE OF FORWARD CARGO NETTING ANCHOR HOLD DOWNS FS533.00 AND FS581.00. BOTH BETWEEN STRINGERS 23LH AND 22LH. (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED FWD CARGO FWD ANCHOR FITTING P/N SH670-33390-1 IAW CRJ700 SRM 51-42-21
- [SDR SWIA202157588](https://openairdocs.org/sdr/SWIA202157588.md): Doubler · corroded · Jan 28, 2021 · N718EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON EXTERNAL DOUBLER @ FS 985.00 STGR 26R TO 26L (C-CHECK RO 4/20/2021) REMOVED CORRODED DOUBLER AND TRIPLER FROM F.S. 985.00 STR 26R TO STR26L IAW CRJ700 SRM 51-42-21. FABRICATED NEW DOUBLER AND TRIPLER FROM.063 2024-T3 P.O.# 7992 IAW
- [SDR SWIA202157587](https://openairdocs.org/sdr/SWIA202157587.md): Stringer · corroded · Jan 27, 2021 · N718EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STGR 20R @ FS 316.00 (C-CHECK RO 4/20/2021) REMOVED AND REPLACED STR20R/H FROM FS280 TO FS 319 IAW CRJ700 SRM 51-42-06 AND 51-42-21.
- [SDR SWIA202157586](https://openairdocs.org/sdr/SWIA202157586.md): Stringer · corroded · Jan 27, 2021 · N718EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STGR 21R AND SPLICE ANGLES @ FS 310.00 TO FS 349.00 (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED SRT 21R/H P/N SH670-31383-1S FROM FS310- FS349 IAW CRJ700 SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-06 AND 51-25-16.
- [SDR SWIA202157585](https://openairdocs.org/sdr/SWIA202157585.md): Stringer · corroded · Jan 27, 2021 · N718EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STGR 22R AND SPLICE ANGLES @ FS 319.00 TO FS 349.00 (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED STR22R FROM FS319 TO FS349 IAW CRJ700 SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-06 AND 51-25-16.
- [SDR SWIA202157584](https://openairdocs.org/sdr/SWIA202157584.md): Box Beam · corroded · Jan 26, 2021 · N718EV · Cndair CL6002C10 · Fuselage Main, Structure
  > CORRISION INSIDE OF BOX FRAME ABOVE FWD CARGO DOOR, BETWEEN STR 18 AND 19, F/S 533.00 AND 549.00 (C-CHECK RO 4/20/2021) REPAIRED FWD CARGO DOOR LINTEL DAMAGE AT L/H FS533 TO FS549 BETWEEN STR18L TO STR19L IAW MHIRJ REO # SH670-53-31-604.
- [SDR SWIA202157583](https://openairdocs.org/sdr/SWIA202157583.md): Frame · corroded · Jan 26, 2021 · N718EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 379.00 FRAME CORRODED BETWEEN STRINGER 22RH AND 20RH. FORWARD OF LAVATORY DRAIN. (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED FRAME FS379 FROM STR26R TO STR20R P/N SH670-32118-1 PO# 00013534R IAW CRJ700 SRM 51-40-11, 51-42-06 AND 51-42-20.
- [SDR SWIA202157582](https://openairdocs.org/sdr/SWIA202157582.md): Stringer · corroded · Jan 26, 2021 · N718EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 21 LEFT CORREDED BETWEEN FS 310.00 TO FS 319.00. GROUNDING POINTS ON FRAME GS 405 AND GS 445 ARE ALSO CORRODED. (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED INTERCOSTAL AT STR21L FROM FS 310 TO FS333 IAW CRJ700 SRM 53-21-23, 51-42-06,51
- [SDR SWIA202157581](https://openairdocs.org/sdr/SWIA202157581.md): Frame · corroded · Jan 26, 2021 · N718EV · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION AT FS 517.00 LOWER FRAME BETWEEN STRINGERS 26LH AND 24RH. (C-CHECK RO 4/20/2021) REMOVED CORRODED LOWER FRAMES AT FS517 L/H AND R/H, FABRICATED AND INSTALLED NEW LOWER FRAMES FOR FS517, L/H P/N SH670-33261-7 AND R/H P/N SH670-33210-5 IAW BOMB
- [SDR SWIA202157600](https://openairdocs.org/sdr/SWIA202157600.md): Seat Track · damaged · Jan 25, 2021 · N718EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT RAIL FS810 NEEDS CLEANING AND EVALUATIONING ( FLAGGED DOT 402) (C-CHECK RO 4/20/2021) REMOVED AND REPLACED RH SEAT RAIL AT FS 785.15 THRU FS853.00 UTILIZING PN 20276 PO# 00013626 IAW CRJ700 SRM 51-40-11, 51-42-02 AND AMM 53-00-49
- [SDR SWIA202157598](https://openairdocs.org/sdr/SWIA202157598.md): Seat Track · damaged · Jan 25, 2021 · N718EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT RAIL FS 785.15 NEED TO BE CLEANED AND EVALUATED ALSO MISSING 2EA FASTENERS ( FLAGGED DOT 401) (C-CHECK RO 4/20/2021) REMOVED DAMAGED RH SIDE SEAT TRACK AND INSTALLED NEW SEAT TRACK P.O. 00013626 PER CRJ700 AMM 53-00-49
- [SDR SWIA202157596](https://openairdocs.org/sdr/SWIA202157596.md): Stringer · corroded · Jan 25, 2021 · N718EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > WING TO BODY FUSELAGE STRINGER @ FS 942.0 HAS CORROSION (C-CHECK RO 4/20/2021) REMOVED DAMAGED ANGLES AND INSTALLED NEW L/H, R/H AND CENTER ANGLES AT WING TO BODY FUSELAGE STRINGER F.S 942.00 IAW CRJ 700 SRM 51-42-O6
- [SDR SWIA202157580](https://openairdocs.org/sdr/SWIA202157580.md): Door Sill · corroded · Jan 25, 2021 · N718EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FILIFORM CORROSION AND ALUMINUM OXIDE ON THE UPPER SURFACE OF THE INBOARD FLANGE OF THE LOWER SILL OF THE AFT BAGGAGE DOOR FRAME WHERE THE FLOORBOARD OUTBOARD EDGE ATTACHES, BETWEEN FS1000 AND FS1047. (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED
- [SDR SWIA202157599](https://openairdocs.org/sdr/SWIA202157599.md): Vane · worn · Jan 15, 2021 · N718EV · Cndair CL6002C10 · Trailing Edge Flaps
  > RIGHT HAND FLAP VANE STOPPER IN THE WING TRAILING EDGE- CENTER AND I/B STOPPER PADS MISSING O/B PAD WORN. (C-CHECK RO 4/20/2021) REMOVED AND REPLACED RIGHT WING INBD FLAP VANE STOPS CENTER, INBD, OUTBD IAW CRJ 700 SRM 57-51-02
- [SDR SWIA202157597](https://openairdocs.org/sdr/SWIA202157597.md): Vane · worn · Jan 14, 2021 · N718EV · Cndair CL6002C10 · Trailing Edge Flaps
  > LH I/B FLAP VANE STOPPERS IN THE WING TRAILING EDGE- O/B STOPPER PAD WORN AND CENTER AND I/B STOPPER PAD MISSING. (C-CHECK RO 4/20/2021) LH FLAP - REPLACED CENTER & OUTBOARD STOPPERS (CC670-16073). REPLACED INBOARD STOPPER (CC670-16022). I.A.W. 57-51-0
- [SDR SWIA202157579](https://openairdocs.org/sdr/SWIA202157579.md): Intercostal · corroded · Jan 13, 2021 · N718EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON INTERCOSTALS FROM FS 295 TO FS 349 ON STRINGER # STGR 19RH BELOW WL 72.00 UNDER THE SERVICE DOOR AREA (C-CHECK RO 4/20/2021) AFTER FURTHER INVESTIGATION DAMAGE FOUND TO BE ON STR20R NOT STR19R. REMOVED AND REPLACED CORRODED INTERCOSTA
- [SDR ASOA201801135034](https://openairdocs.org/sdr/ASOA201801135034.md): Doubler · chafed · Jan 13, 2018 · N718EV · Cndair CL6002C10 · Fuselage Structure (General)
  > PREVIOUS REPAIR AT F.S. 977.00 STRINGER 27 IS CHAFED. C/A:REO 670-53-00-528 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. ALL RII'S HAVE BEEN ACCOMPLISHED BY A TRAINED, QUALIFIED AND AUTHORIZED RII INSPECTO
- [SDR ASOA201801135033](https://openairdocs.org/sdr/ASOA201801135033.md): Hinge · gouged · Jan 13, 2018 · N718EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE DOOR SIDE LUGS 2,5,6, AND 12 FROM FRONT ARE GOUGED. REPAIRED THE DOOR HINGE LUGS IAW REO 670-52-11-511, 670-52-11-995, EC/TC REO670-52-11-511, AND 670-52-11-995.
- [SDR ASOA201801115029](https://openairdocs.org/sdr/ASOA201801115029.md): Floor Support · corroded · Jan 11, 2018 · N718EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT BETWEEN BS 533 TO 581 IS CORRODED. REPAIRED THE FLOOR SUPPORT IAW REO 670-53-21-1483, AND REO 670-53-21-1483.
- [SDR ASOA201801105028](https://openairdocs.org/sdr/ASOA201801105028.md): Frame · corroded · Jan 10, 2018 · N718EV · Cndair CL6002C10 · Fuselage Main, Frame
  > BS 364 FRAME IS CORRODED BETWEEN STRINGERS 25L AND 26R. REMOVED AND REPLACED THE FRAME IAW REO 670-53-21-687, REV, 670-53-21-1481, REV --, REO 670-53-21-687, AND REO 670-53-21-1481.
- [SDR ASOA201801105027](https://openairdocs.org/sdr/ASOA201801105027.md): Frame · corroded · Jan 10, 2018 · N718EV · Cndair CL6002C10 · Fuselage Main, Frame
  > BS 280 FRAME WAS CORRODED BETWEEN STRINGERS 26L AND 26R. REPAIRED THE FRAME IAW REO 670-53-21-1478 AND REO 670-53-21-1478.
- [SDR ASOA201801095026](https://openairdocs.org/sdr/ASOA201801095026.md): Intercostal · corroded · Jan 9, 2018 · N718EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STRINGER 27L WAS CORRODED BETWEEN BS 349 AND 364. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR ASOA201801095025](https://openairdocs.org/sdr/ASOA201801095025.md): Intercostal · corroded · Jan 9, 2018 · N718EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STRINGER 27R IS CORRODED BETWEEN BS 349, AND 364. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR ASOA201801095024](https://openairdocs.org/sdr/ASOA201801095024.md): Intercostal · corroded · Jan 9, 2018 · N718EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LEFT INTERCOSTAL AT STRINGER 26L IS CORRODED BETWEEN BS 349 AND 364. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR ASOA201801095023](https://openairdocs.org/sdr/ASOA201801095023.md): Stringer Splice · corroded · Jan 9, 2018 · N718EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE 25R IS CORRODED BETWEEN BS 333 AND 349. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR ASOA201801065019](https://openairdocs.org/sdr/ASOA201801065019.md): Frame · corroded · Jan 6, 2018 · N718EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME BS333 IS CORRODED BETWEEN STRINGERS 26L AND 26R. REPAIRED THE FRAME IAW REO 670-53-21-799, REV A, AND REO 670-53-21-799 03.
- [SDR ASOA201801065018](https://openairdocs.org/sdr/ASOA201801065018.md): Frame · corroded · Jan 6, 2018 · N718EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME BS 310 IS CORRODED BETWEEN STRINGERS 26L AND 25R. REPAIRED THE FRAME IAW REO 670-53-21-799, REV A, AND EO 670-53-21-799 01, REV D.
- [SDR ASOA201801055016](https://openairdocs.org/sdr/ASOA201801055016.md): Frame · corroded · Jan 5, 2018 · N718EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME BS 319.7 IS CORRODED BETWEEN STRINGERS 27 AND 25R. REPAIRED THE FRAME IAW REO 670-53-21-799, AND EC/TC REO 670-53-21-799 02.
- [SDR ASOA201801055015](https://openairdocs.org/sdr/ASOA201801055015.md): Frame · corroded · Jan 5, 2018 · N718EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME BS 295 IS CORRODED BETWEEN STRINGERS 26L AND 25R. REPAIRED THE FRAME IAW REO 670-53-21-799, AND EC/TC REO 670-53-21-799.
- [SDR ASOA201801045014](https://openairdocs.org/sdr/ASOA201801045014.md): Buttstrap · corroded · Jan 4, 2018 · N718EV · Cndair CL6002C10 · Fuselage Main, Structure
  > CIRCUMFERENTIAL BUTTSTRAP IS CORRODED AT BS 333 BETWEEN STRINGERS 25L AND 25R. REPAIRED THE CIRCUMFERENTIAL BUTTSTRAP IAW REO 670-53-21-1479, AND EC/TC REO670-53-21-1479.
- [SDR ASOA201801035013](https://openairdocs.org/sdr/ASOA201801035013.md): Stringer · corroded · Jan 3, 2018 · N718EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 25R CORRODED BETWEEN BS 333 AND 364. REMOVED AND REPLACED THE STRINGER 25R IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR ASOA201801035012](https://openairdocs.org/sdr/ASOA201801035012.md): Stringer · corroded · Jan 3, 2018 · N718EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 25L IS CORRODED BETWEEN BS 280 AND 333. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR ASOA201801035011](https://openairdocs.org/sdr/ASOA201801035011.md): Stringer · corroded · Jan 3, 2018 · N718EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R IS CORRODED BETWEEN BS 333 AND 364. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR ASOA201801035010](https://openairdocs.org/sdr/ASOA201801035010.md): Stringer · corroded · Jan 3, 2018 · N718EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 25R IS CORRODED BETWEEN BS 295 AND 310. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR ASOA201801035009](https://openairdocs.org/sdr/ASOA201801035009.md): Stringer · corroded · Jan 3, 2018 · N718EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R IS CORRODED BETWEEN BS 295 AND 310. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR ASOA201812305006](https://openairdocs.org/sdr/ASOA201812305006.md): Intercostal · corroded · Dec 30, 2017 · N718EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RT INTERCOSTAL AT STRINGER 26R IS CORRODED BETWEEN FS 349.00 AND FS 364.00. REMOVED AND REPLACED INTERCOSTAL P/N SH670-32077-4 IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR ASOA201812295005](https://openairdocs.org/sdr/ASOA201812295005.md): Stringer · corroded · Dec 29, 2017 · N718EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 27 FWD SEGMENT FS 310.00-333.00, AFT SEGMENT FS. 333.00-349.00 AND STRINGER SPLICE AT FS 333.00 ARE CORRODED. REMOVED AND REPLACED STRINGER 27 FWD SEGMENT PN SH670-31635-3, JOINT PN SH670-32429-3, AND AFT SEGMENT PN SH670-31371-3S IAW SRM 51-40-11-001
- [SDR ASOA201812295004](https://openairdocs.org/sdr/ASOA201812295004.md): Doubler · cracked · Dec 29, 2017 · N718EV · Cndair CL6002C10 · Fuselage Floor Panel
  > RT FORWARD EQUIPMENT COMPARTMENT FLOOR PREVIOUS REPAIR IS CRACKED AT BS 193. REMOVED AND REPLACED THE REPAIR DOUBLER IAW REOS 670-53-11-509, 670-53-11-1355, AND EC/TC REO 670-53-11-1355.
- [SDR ASOA201812285003](https://openairdocs.org/sdr/ASOA201812285003.md): Door Frame · cracked · Dec 28, 2017 · N718EV · Cndair CL6002C10 · Fuselage Main, Structure
  > RIGHT FORWARD EQUIPMENT COMPARTMENT DOOR LANDING IS CRACKED IN TWO LOCATIONS NEAR FWD AND AFT DOOR LATCHES. REMOVED AND REPLACED THE DOOR LANDING IAW SRM 51-40-11-001-001-A01, 51-42-22-001-001-A01, 51-42-06-001-001-A01, REO 670-53-11-1356, AND EC/TC REO 670-5
- [SDR ASOA201812285002](https://openairdocs.org/sdr/ASOA201812285002.md): Door Frame · cracked · Dec 28, 2017 · N718EV · Cndair CL6002C10 · Fuselage Main, Structure
  > LEFT FORWARD EQUIPMENT BAY DOOR LANDING IS CRACKED NEAR AFT DOOR LATCH. REMOVED AND REPLACED THE DOOR LANDING IAW SRM 51-40-11-001-001-A01, 51-42-22-001-001-A01, 51-42-06-001-001-A01 REO 670-53-11-1356, AND EC/TC REO 670-53-11-1356.
- [SDR ASOA201812205001](https://openairdocs.org/sdr/ASOA201812205001.md): Bracket · corroded · Dec 20, 2017 · N718EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WEB PROTECTOR BRACKETS ON GALLEY SERVICE DOOR FLOOR SUPPORT ARE CORRODED. REMOVED AND REPLACED THE BRACKETS IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR ASOA201712205254](https://openairdocs.org/sdr/ASOA201712205254.md): Angle · corroded · Dec 20, 2017 · N718EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > BS 280 J ANGLE IS CORRODED ON UPPER FLANGE BETWEEN LBL 11 AND RBL 11. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR ASOA201812165020](https://openairdocs.org/sdr/ASOA201812165020.md): Floor Support · corroded · Dec 16, 2017 · N718EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RIGHT SIDE FLOOR SUPPORT IS CORRODED BETWEEN BS 280 BULKHEAD TO BS 319. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRMS 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-13-001-001-A01, SH670-32170-S01, AND SH670-32170-S01.

Next page: https://openairdocs.org/aircraft/N718EV/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 = 'N718EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N718EV/reports

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