# Service difficulty reports: N751EV

A list on [N751EV](https://openairdocs.org/aircraft/N751EV.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 6 · 281 reports

- [SDR SWIA2026061576242](https://openairdocs.org/sdr/SWIA2026061576242.md): Tru · faulted · Jun 15, 2026 · N751EV · Cndair CL6002C11 · DC Power Distribution System
  > DC BUSS 2 CAUTION MESSAGE. SMELLED A BURNING ODOR FOR ABOUT A MINUTE BEFORE GOING AWAY. MULTIPLE ASSOCIATED FAILURES INCLUDING CAUTION MESSAGES AS WELL AS MANY STATUS MESSAGES. MEL 24-31-1CAT B. SMOD APPROVEL REQUIRED FOR RTS DUE TO ODI EVENT (FLIGHT 468
- [SDR SWIA2026040375667](https://openairdocs.org/sdr/SWIA2026040375667.md): Control Unit · faulted · Apr 3, 2026 · N751EV · Cndair CL6002C11 · Landing Gear Steering System
  > STEERING INOPERATIVE CAUTION AFTER PUSHBACK. RAN QRH MESSAGE CLEARED. (FLIGHT 4710) INTERROGATED MDC AND FOUND FAULT CODE B-007456 FOR NWS ECU FAILED DUE TO INTERNAL FAULT. REMOVED AND REPLACED NWS STEERING ECU REFERENCING APPLICABLE STEPS OF AMM 32-51-10.
- [SDR SWIA20250317120](https://openairdocs.org/sdr/SWIA20250317120.md): Plate · gouged · Jan 20, 2025 · N751EV · Cndair CL6002C10 · Fuselage Main, Structure
  > UPON REMOVAL OF CARGO NET MOUNTING PLATE INTERCOSTAL FOUND DEEP GOUGES IN RADIUS. (C-CHECK RO 3/14/2025) REMOVED AND REPLACED INTERCOSTAL WITH NEW ONE. REF: CRJ-700 S.R.M. 51-42-06-001--001-A01,51-42-21-001-001-A01, 51-45-00-001--001-A01, DWG-SH670-335
- [SDR SWIA202503170118](https://openairdocs.org/sdr/SWIA202503170118.md): Frame · corroded · Jan 18, 2025 · N751EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FOUND CORROSION ON FWD WEB FACE AND LOWER FLANGE OF FRAME AT FUSELAGE BELOW FLOOR FS 295 STR24L ( MX# 29494459 JOB OP: HN00214212) (C-CHECK RO 3/14/2025) REPAIRED FWD. WEB FACE AND LOWER FLANGE OF FRAME AT FUSELAGE BELOW FLOOR FS295 STR24L IAW REO 670
- [SDR SWIA202503170114](https://openairdocs.org/sdr/SWIA202503170114.md): Floor Support · corroded · Jan 14, 2025 · N751EV · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > CORROSION ON UPPER SURFACE OF FLOOR SUPPORT STRUCTURE, RH SIDE AT APPROXIMATELY FS 1088. SEE ATTACHED PIC. (C-CHECK RO 3/14/2025) REMOVED CORROSION ON UPPER SURFACE OF FLOOR SUPPORT STRUCTURE (SILL) REF-CRJ-700 SRM 51-21-06-001-001 A01 AND FOUND AREA RE
- [SDR SWIA202503170110](https://openairdocs.org/sdr/SWIA202503170110.md): Landing · cracked · Jan 10, 2025 · N751EV · Cndair CL6002C10 · Fuselage Main, Structure
  > RH SIDE TRU BAY DOOR LOWER LANDING HAS A CRACK ON AFT LATCH CUT OUT (C-CHECK RO 3/14/2025) REMOVED AND REPLACED TRU LOWER LANDING WITH NEW ONE. REF: CRJ-700 S.R.M.51-42-06-001-001-A01, 51-42-22-001-001-A01, REO- 670-53-11-2086 REV -- DATE 2025-01-16. (
- [SDR SWI2025F00333](https://openairdocs.org/sdr/SWI2025F00333.md): Bayonet · cracked · Jan 8, 2025 · N751EV · Cndair CL6002C10 · Emergency Exits
  > RIGHT OVERWING EXIT DOOR AFT PROXIMITY SWITCH BAYONET IS CRACKED. 29442720 (C-CHECK RO 3/14/2025) REPAIRED RIGHT OVERWING EXIT DOOR AFT PROXIMITY SWITCH BAYONET BY COMPLYING WITH ALL STEPS OF REO# 670-52-21-106 REV:-- DATE: 2025-02-03. COMPLIED WITH SKY
- [SDR SWIA202503170108](https://openairdocs.org/sdr/SWIA202503170108.md): Bayonet · cracked · Jan 8, 2025 · N751EV · Cndair CL6002C10 · Emergency Exits
  > LEFT OVERWING EXIT DOOR FORWARD & AFT PROXIMITY SWITCH BAYONETS ARE CRACKED. 29442703 (C-CHECK RO 3/14/2025) REPAIRED LEFT OVERWING EXIT DOOR FORWARD & AFT PROXIMITY SWITCH BAYONETS REF GREO PL 670-52-21-103 REV:--:DATE:2024-11-06
- [SDR SWIA202503170103](https://openairdocs.org/sdr/SWIA202503170103.md): Bracket · cracked · Jan 3, 2025 · N751EV · Cndair CL6002C10 · Wing, Attach Fittings
  > S/N 0440LH WING, SLAT TRAK CANISTER BRACKET 1-3 IS CRACKED. FLAGGED (C-CHECK RO 3/14/2025) REPAIRED THE LH WING SLAT TRACK CANNISTER BRACKET AT SLAT TRACK 1-3 REF REO 670-57-42-577 REV -- 2016-12-02. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECKS
- [SDR SWIA2025031701231](https://openairdocs.org/sdr/SWIA2025031701231.md): Pitot Tube · scratched · Dec 31, 2024 · N751EV · Cndair CL6002C10 · Pitot/Static System
  > R/H PITOT STATIC PROBE CUTOUT ON THE UPPER SKIN AT FS210.00 BETWEEN STGR 14 AND STGR 15 LOWER AFT HOLE HAS MULTIPLE SCRATCHES AS MARKED (C-CHECK RO 3/14/2025) WET INSTALLED NEW REPLACEMENT R/H PITOT STATIC MOUNTING PLATE AT FUSELAGE SKIN FS.210 BETWEEN
- [SDR SWIA202503171229](https://openairdocs.org/sdr/SWIA202503171229.md): Drag Angle · cracked · Dec 29, 2024 · N751EV · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
  > RH FWD VERTICAL STAB. DRAG ANGLE HAS SUSPECTED CRACK. (C-CHECK RO 3/14/2025) REPAIRED RH FWD VERTICAL STAB DRAG ANGLE IAW MHI RJ R.E.O. 670-55-31-187 REV. -- DATED 2025-02-18 AND COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWI2025F00334](https://openairdocs.org/sdr/SWI2025F00334.md): Drag Angle · cracked · Dec 29, 2024 · N751EV · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
  > LH AFT VERTICAL STAB. DRAG ANGLE HAS SUSPECTED CRACK. (C-CHECK RO 3/14/2025) REPAIRED IAW REO 670-55-31-018 REV-A DATE 2016-11-10 AND COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWI2025F00335](https://openairdocs.org/sdr/SWI2025F00335.md): Panel · corroded · Dec 27, 2024 · N751EV · Cndair CL6002C10 · Fuselage Main, Structure
  > THE RH MLG WHEEL WELL PANEL 642AZ ATTACHMENT ANGLE IS CORRODED. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED NEW ATTACHMENT ANGLE, BELOW PANEL 642AZ IN RH MLG WHEEL WELL AREA REF: CRJ 700 SRM 51-42-20-001-001-A01 AND DWG: CC670-10320 REV E. COMPLIED WI
- [SDR SWIA2025031701227](https://openairdocs.org/sdr/SWIA2025031701227.md): Panel · corroded · Dec 27, 2024 · N751EV · Cndair CL6002C10 · Fuselage Main, Structure
  > THE LH MLG WHEEL WELL PANEL 542AZ ATTACHMENT ANGLE IS CORRODED. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED NEW ATTACHMENT ANGLE, BELOW PANEL 542AZ IN LH MLG WHEEL WELL AREA REF: CRJ 700 SRM 51-42-20-001-001-A01 AND DWG: CC670-10320 REVE. COMPLIED WIT
- [SDR SWIA2025031701226](https://openairdocs.org/sdr/SWIA2025031701226.md): Cowling · chafed · Dec 26, 2024 · N751EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/Skin
  > S/N 0368LH ENGINE INTERNAL. LOWER CORE COWL HAS MULTIPLE CHAFES AND GOUGES. FLAGGED (C-CHECK RO 3/14/2025) REPAIRED LH ENGINE INTERNAL, LOWER CORE COWL AT MULTIPLE CHAFES AND GOUGES. SEE CONTINUATION CARD FOR FURTHER DETAILS. ALL STEPS OF REO 670-54-23
- [SDR SWI202503170336](https://openairdocs.org/sdr/SWI202503170336.md): Deck Plate · dented · Dec 21, 2024 · N751EV · Cndair CL6002C10 · Fuselage Main, Structure
  > S/N 0329UNDER PILOTS SEAT, FLOORING HAS A DENT. FLAGGED (C-CHECK RO 3/14/2025) REPAIRED DENT UNDER PILOTS SEAT, FLOORING REF REO 670-53-11-2081 REV -- DATED 2025-01-23, COMPLIED WITH 51-900-1002-SKY
- [SDR SWI2025F00343](https://openairdocs.org/sdr/SWI2025F00343.md): Strap · corroded · Dec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD BAGGAGE BAY, AFT H STRAP CORRODED @ APROX FS 581 BETWEEN LBL STRGS 25-26 MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED "H" STRAP WITH NEW ONE AT F.S.581.REF: CRJ-700 S.R.M.51-42-22-001-001-A01, 51-42-21-001-001-A01 DWG-SH670-33793 REV-A.COMPL
- [SDR SWI2025F00342](https://openairdocs.org/sdr/SWI2025F00342.md): Crossbeam · corroded · Dec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage Main, Structure
  > CROOS BEAM CAP CORRODED AT APROX FS 1051 RBL 40 MARKED (C-CHECK RO 3/14/2025) CORROSION ON CROSSBEAM CAP FS1051 AT APPROX RBL40 FOUND TO BE OUT OF LIMITS, REPAIRED WITH REO 670-53-61-2449 REV -- DATED 2025-01-22, COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA20203171219](https://openairdocs.org/sdr/SWIA20203171219.md): Mount · corroded · Dec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD BAGGAGE BAY, CARGO NET MOUNTING PLATE CORRODED @ APROX FS 581 BETWEEN LBL STRGS 22-23 MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED FWD BAG BAY CARGO NET MOUNTING PLATE WITH NEW ONE. REF: CRJ-700 S.R.M. 51-42-21-001-001-A01, 51-45-00-001-001-A
- [SDR SWI2025F00340](https://openairdocs.org/sdr/SWI2025F00340.md): Strap · corroded · Dec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD BAGGAGE BAY, FWD H STRAP CORRODED @ APROX FS 538 BETWEEN LBL STRGS 25-26 MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED "H" STRAP AT F.S.538.00.REF: CRJ-700 S.R.M.51-42-22-001-001-A01, 51-42-21-001-001-A01.DWG-SH670-33750 REV-Y. COMPLIED WITH 5
- [SDR SWI2025F00339](https://openairdocs.org/sdr/SWI2025F00339.md): Floorbeam · cracked · Dec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280 CLIP ON THE OB SIDE OF LBL12 APPEARS TO BE CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED CLIP P/N CC670-34099-1 AT FS280 ON THE OUTBOARD SIDE OF LBL12. REF. CRJ700 SRM 51-42-21-001-001-A01 AND DWG# KBA670-30026 REV. J.COMPLIED WITH SKYWEST T
- [SDR SWI2025F00338](https://openairdocs.org/sdr/SWI2025F00338.md): Mount · corroded · Dec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage Main, Structure
  > FWD BAGGAGE BAY, CARGO NET MOUNTING PLATE CORRODED @ APROX FS 533 BETWEEN LBL STRGS 22-23 MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED CARGO NET MOUNTING PLATE WITH NEW ONE. REF: CRJ-700 S.R.M. 51-42-21-001-001-A01,51-42-06-001-001-A01,51-45-00-00
- [SDR SWI2025F00341](https://openairdocs.org/sdr/SWI2025F00341.md): Hinge · gouged · Dec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > FWD BAGGAGE BAY DOOR HINGE ON ACFT SIDE GOUGED AND WORN. REMOVED AND REPLACED DOOR HINGE FITTING WITH NEW ONE. REF: CRJ-700 S.R.M.51-41-04-001-001-A01,SRM 51-40-11-001-001 A01, DWG-SH670-33840 REV-C TUC--5659 CAL DUE 31-MAR-2025.COMPLIED WITH 51-900-1002-SKY
- [SDR SWI2025F00337](https://openairdocs.org/sdr/SWI2025F00337.md): Mount · corroded · Dec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage Main, Structure
  > FWD BAGGAGE BAY, CARGO NET MOUNTING PLATE CORRODED @ APROX FS 557 BETWEEN LBL STRG 27-26 MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED CARGO NET MOUNTING PLATE WIRTH NEW ONE. REF: CRJ-700 S.R.M.51-42-06-001-001-A01, DWG-SH670-33574 REV-A. SEE CONTI
- [SDR SWIA202503171214](https://openairdocs.org/sdr/SWIA202503171214.md): Housing · gouged · Dec 14, 2024 · N751EV · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR HANDLE HOUSING IS GOUGED (MARKED) (C-CHECK RO 3/14/2025) REMOVED DAMAGED AFT CARGO DOOR HANDLE HOUSING. REF. CRJ700 SRM 51-42-21-001-001-A01 INSTALLED NEW AFT CARGO DOOR HANDLE HOUSING. REF. CRJ700 SRM 51-42-21-001-001-A01 AND DWG# CC670
- [SDR SWI2025F00351](https://openairdocs.org/sdr/SWI2025F00351.md): Stand Off · cracked · Dec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED R/H TRANSCOWL I/B "A" BRACKET (CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.
- [SDR SWI2025F00350](https://openairdocs.org/sdr/SWI2025F00350.md): Stand Off · cracked · Dec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED R/H TRANSCOWL O/B "A" BRACKET (CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.
- [SDR SWI2025F00349](https://openairdocs.org/sdr/SWI2025F00349.md): Coaming · chafed · Dec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL INNER COAMING IS CHAFED @ FWD LATCH (C-CHECK RO 3/14/2025) REPAIRED INNER LATCH DOOR COAMING AT FWD. LATCH ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-1028, REV. NC, 2009-06-15 AND REO 670-54-21-1705, REV. --, 2025-01-17. AND OPS TES
- [SDR SWIA202503171211](https://openairdocs.org/sdr/SWIA202503171211.md): Skin · dented · Dec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL INNER PERFORATED SKIN IS DENTED (C-CHECK RO 3/14/2025) REPAIRED R/H UPPER TRANSCOWL INNER PERFORATED SKIN AT DENTED LOCATION, REF. CRJ700 SRM 54-10-00-201-002-A01, REPAIR SRS704 AND REO 670-54-21-1703, REV. --, 2025-01-14. COMPLIED
- [SDR SWI2025F00348](https://openairdocs.org/sdr/SWI2025F00348.md): Rivet · loose · Dec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL Z STIFFENER RIVETS PULLED LOOSE (C-CHECK RO 3/14/2025) REPAIRED L/H UPPER TRANSCOWL AT LOOSE / PULLED RIVETS ON INNER SKIN COMMON TO ZED STIFFENER, REF. REO 670-54-21-1709, REV. --, 2025-01-24. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWI2025F00347](https://openairdocs.org/sdr/SWI2025F00347.md): Stand Off · cracked · Dec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CAR
- [SDR SWI2025F00346](https://openairdocs.org/sdr/SWI2025F00346.md): Stand Off · cracked · Dec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CAR
- [SDR SWI2025F00345](https://openairdocs.org/sdr/SWI2025F00345.md): Stand Off · cracked · Dec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED INBD STANDOFF P/N CN624-2082-201 ON L/H UPPER TRANSCOWL REF. REO 670-54-21-971 REV. B, 2023-11-28. COMPLIED WITH SKY CARD 51-900-1002-SKY.
- [SDR SWI2025F00344](https://openairdocs.org/sdr/SWI2025F00344.md): Stand Off · cracked · Dec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD
- [SDR SWIA202303171016](https://openairdocs.org/sdr/SWIA202303171016.md): Hinge · gouged · Oct 16, 2024 · N751EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA59692-670-53-21-582 N751EV MXCODEID52126-DTI - PAX DOOR HINGE FUSELAGE SIDE HAS NEW GOUGE ON AFT LUG LANDING. REMOVED GOUGE FROM PAX DOOR HINGE (FUSE SIDE) AFT LUG LANDING, MATERIAL LOSS FOUND TO BE WITHIN ALLOWABLE
- [SDR SWIA202266348](https://openairdocs.org/sdr/SWIA202266348.md): None · odor · Aug 22, 2022 · N751EV · Cndair CL6002C10 · Air Conditioning System
  > CREW GETTING SMELLS OF BURNING RUBBER. MOSTLY NEAR ROWS 10 AND 16. SEEMS TO BE MORE PROMINENT DURING TAXI. AND EVEN STRONGER DURING BLEED TRANSFERS FROM BOTH ENGINES TO APU AND APU TO ENGINES. (FLIGHT #4959 FILED CLOSED) COMPLIED WITH ADJUSTMENT AND TEST O
- [SDR SWIA2020080751693](https://openairdocs.org/sdr/SWIA2020080751693.md): Stringer · corroded · Jul 23, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R BETWEEN BS 349 - 364 WAS CORRODED. REPLACED THE STRINGER IAW SRM, AND DWG.
- [SDR SWIA2020080751692](https://openairdocs.org/sdr/SWIA2020080751692.md): Floor Support · corroded · Jul 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT, RBL 9, BS 641- 693 FOUND OUT OF LIMITS CORROSION. REPLACED THE FLOOR SUPPORT IAW SRM AND REO.
- [SDR SWIA2020080751691](https://openairdocs.org/sdr/SWIA2020080751691.md): Floor Support · damaged · Jun 22, 2020 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WHILE PERFORMING A MAJOR REPAIR ON THE FLOOR SUPPORT BETWEEN BS 477 TO 624 AT LBL 9, DAMAGE WAS FOUND AT BS 653, LBL 9. REPAIRED IAW SRM.
- [SDR SWIA2020080751690](https://openairdocs.org/sdr/SWIA2020080751690.md): Stringer · corroded · Jun 20, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STRINGER 27, BS 333 TO 355 HAD DEEP PITTING CORROSION AROUND RIVETS. REPLACED THE STRINGER IAW DWG, AND SRM.
- [SDR SWIA2020080751687](https://openairdocs.org/sdr/SWIA2020080751687.md): Stringer · corroded · Jun 18, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STRINGER 23R CORRODED BETWEEN FS280.00 AND FS333. REPLACED THE STRINGER IAW DWG, AND SRM.
- [SDR SWIA2020080751686](https://openairdocs.org/sdr/SWIA2020080751686.md): Stringer · corroded · Jun 18, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 22R CORRODED BETWEEN BS 280 AND 333. REPLACED THE STRINGER IAW DWG, AND SRM.
- [SDR SWIA2020080751685](https://openairdocs.org/sdr/SWIA2020080751685.md): Doubler · corroded · Jun 18, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TCAS ANTENNA DOUBLER, BS 295 TO 310 HAD SIGNS OF CORROSION. REPLACED THE TCAS ANTENNA DOUBLER IAW DWG, AND SRM.
- [SDR SWIA2020080751684](https://openairdocs.org/sdr/SWIA2020080751684.md): Stringer · corroded · Jun 18, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R, BETWEEN BS 333 AND 349 HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE STRINGER IAW DWG, AND SRM.
- [SDR SWIA2020080751683](https://openairdocs.org/sdr/SWIA2020080751683.md): Frame · corroded · Jun 18, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Frame
  > BB 295 FRAME, BETWEEN STRINGERS 26L & 26R HAD SIGNS OF CORROSION. SPLICED IN A NEW FRAME SECTION IAW SRM.
- [SDR SWIA2020080751682](https://openairdocs.org/sdr/SWIA2020080751682.md): Intercostal · corroded · Jun 12, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID DD3 INTERCOSTAL WAS CORRODED. REPLACED THE INDERCOSTAL IAW SRM AND DWG.
- [SDR SWIA2020080751679](https://openairdocs.org/sdr/SWIA2020080751679.md): Skin · corroded · Jun 9, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EVALUATE EVIDENCE OF CORROSION ON EXTERIOR FUSELAGE BETWEEN FS 980 AND FS 988 AND BETWEEN STGR 26L AND STGR 26R. REPAIRED FUSELAGE SKIN BETWEEB FS 977 - 985 BETWEEN STGRS 26L - 26R, BY RERPLACING THE EXISTING DOUBLERS WITH NEW IAW REO. ALL CHECKED GOOD.
- [SDR SWIA2020080751678](https://openairdocs.org/sdr/SWIA2020080751678.md): Support · corroded · Jun 7, 2020 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON SILL BACKUP AT STRINGER 21L, BETWEEN BS 310 TO 333. REMOVED AND REPLACED THE SILL BACKUP DUE TO FOUND TO BE OUT OF LIMITS IAW SRM, DWG AND REO.
- [SDR SWIA2020080751677](https://openairdocs.org/sdr/SWIA2020080751677.md): Stringer · corroded · Jun 5, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R, BETWEEN BS 310 AND 319 WAS CORRODED. REPLACED THE STRINGER IAW DWG, SRM, AND DWG.
- [SDR SWIA2020080751676](https://openairdocs.org/sdr/SWIA2020080751676.md): Intercostal · corroded · Jun 5, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR DD2 MID INTERCOSTAL CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM AND DWG.

Next page: https://openairdocs.org/aircraft/N751EV/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 = 'N751EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N751EV/reports

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