# Service difficulty reports: N748EV

A list on [N748EV](https://openairdocs.org/aircraft/N748EV.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 · 277 reports

- [SDR SWIA2025080600528](https://openairdocs.org/sdr/SWIA2025080600528.md): Structure · cracked · May 28, 2025 · N748EV · Cndair CL6002C10 · Fuselage Main, Structure
  > SUSPECTED CRACK ON LT LOWER TR BAY LAND. LOWER AFT CORNER OF ACCESS PANEL 211BL. REMOVED AND REPLACED LT LOWER TRU/HYDRAULIC BAY SKIN AS REQ'D PER BOMBARDIER DRWG'S CC670-33040 REV-G. CC670-32010 REV-F AND REO 670-53-11-2159 REV-- DATED: 2025-07-09, SEE ATTA
- [SDR SWIA2025080600506](https://openairdocs.org/sdr/SWIA2025080600506.md): Frame · cracked · May 6, 2025 · N748EV · Cndair CL6002C10 · Fuselage Main, Frame
  > MAIN CABIN, FRAME AT F.S 333 IS CRACKED JUST OUTBD OF STR 1R. PERFORMED REPAIR ON FRAME AT MAIN CABIN FS 333, JUST OTBD OF STR #1. SEE CONTINUATION CARD TO DETAILS. IAW REO 670-53-21-2625 REV - -.
- [SDR SWIA2025080061066](https://openairdocs.org/sdr/SWIA2025080061066.md): Slat Track · worn · May 5, 2025 · N748EV · Cndair CL6002C10 · Leading Edge Devices
  > SLAT TRACK 1-2 AFT IB & OB WORN OUT OF LIMITS. REMOVED AND REPLACED SLAT TRACK 1-2 AFT IB & OB PER CRJ 700 AMM 27-81-44-801-A01
- [SDR SWIA2025080601065](https://openairdocs.org/sdr/SWIA2025080601065.md): Roller · worn · May 5, 2025 · N748EV · Cndair CL6002C10 · Leading Edge Slat Control System
  > SLAT TRACK 1-2 OB AFT ROLLER WORN OUT OF LIMITS. REMOVEDAND REPLACED SLAT TRACK 1-2 OB AFT ROLLER PER AMM 27-81-44-400-801
- [SDR SWIA2025080600502](https://openairdocs.org/sdr/SWIA2025080600502.md): Doubler · worn · May 2, 2025 · N748EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > ON BELLY UNDER FAIRING FS-969, BL -0, DEEP WEAR MARK ON DOUBLER. REMOVED AND REPLACED DOUBLER UNDER BELLY FAIRING FS969 BL 0 IAW REO 670-53-00-290 REV. -F DATED: 2019-04-26
- [SDR SWIA202265435](https://openairdocs.org/sdr/SWIA202265435.md): None · cracked · Apr 23, 2022 · N748EV · Cndair CL6002C10 · Window/Windshield System
  > CAPTAINS LEFT WINDSHIELD CRACKED INFLIGHT FOLLOWED IMMEDIATELY BY L WSHLD CAUTION MESSAGE. QRH COMPLETED. (FLIGHT 6248 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24711696 WITH THE FOLLOWING CORRECTIVE ACTION: "VERIFIED COMPLETION OF TASK
- [SDR SWIA202265163](https://openairdocs.org/sdr/SWIA202265163.md): None · cracked · Mar 25, 2022 · N748EV · Cndair CL6002C10 · Engine Cowl Flaps
  > DURING A4 INSPECTION OF THE LH ENGINE INLET, FOUND 2 DENTS WITH CRACKS AT THE 3 AND 5 O' CLOCK POSITIONS, BOTH ARE OUT OF LIMITS. (FILED - CLOSED) REMOVED AND REPLACED LH ENGINE INLET IN REFERENCE TO AMM 71-61-01
- [SDR SWIA2020062651252](https://openairdocs.org/sdr/SWIA2020062651252.md): Stringer · damaged · Jun 23, 2020 · N748EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > COMPLY WITH SERVICE BULLETIN TO INCORPORATE PERMANENT REPAIR OF STR3L AT FS 280. (C-CHECK) RO 6/24/2020 SERVICE BULLETIN, FUSELAGE CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00. INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGE
- [SDR SWIA2020062651251](https://openairdocs.org/sdr/SWIA2020062651251.md): Angle · corroded · Jun 13, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > REINFORCEMENT ANGLE SH670-33119-1 IS CORRODED. (C-CHECK) RO 6/24/2020 REPLACED REINFORCMENT ANGLE WITH NEW REF SRM AND DWG. COMPLIED WITH TASK CARD AND FORM M-337.
- [SDR SWIA2020062651249](https://openairdocs.org/sdr/SWIA2020062651249.md): Frame · corroded · Jun 2, 2020 · N748EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME FS364.00 IS CORRODED AT STR 27. (C-CHECK) RO 6/24/2020 REPAIRED LOWER FRAME SECTOR, FS364 PER REO. SEE CONTINAUATION CARD FOR DETAILS, COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651248](https://openairdocs.org/sdr/SWIA2020062651248.md): Stringer Splice · corroded · Jun 2, 2020 · N748EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STRINGER SPLICE STR25L AT FS333.00. (C-CHECK) RO 6/24/2020 REPLACED SPLICE AT STR 25L REF SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651247](https://openairdocs.org/sdr/SWIA2020062651247.md): Cleat · corroded · May 28, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON CLEAT AT FS349.00 STR20R. (C-CHECK) RO 6/24/2020 INSTALLED NEW CLEAT AT FS349.00 STR 20R IAW DWG, SRM. COMPLIED WITH TASK CARD AND FORM M-337.
- [SDR SWIA2020062651246](https://openairdocs.org/sdr/SWIA2020062651246.md): Cleat · corroded · May 27, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON CLEAT AT FS333.00 STR20R. (C-CHECK) RO 6/24/2020 INSTALLED NEW CLEAT AT FS333 STR 20R IAW DWG SH670-32014 REV NC, SRM. COMPLIED WITH TASK CARD AND FORM M-337.
- [SDR SWIA2020062651255](https://openairdocs.org/sdr/SWIA2020062651255.md): Angle · cracked · May 26, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ANGLE FOUND CRACKED ON LOWER SIDE OF RT FS280 CROSSBEAM. (C-CHECK) RO 6/24/2020 INSTALLED NEW ANGLE TO LOWER SIDE OF RT FS280 CROSSBEAM REF SRM.
- [SDR SWIA2020062651245](https://openairdocs.org/sdr/SWIA2020062651245.md): Stiffener · cracked · May 26, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUND STIFFENER CRACKED AT FWD SIDE OF FS280 BULKHEAD AT LBL26 AT LOWER FASTENER HOLE. (C-CHECK) RO 6/24/2020 REMOVED AND REPLACED DAMAGED STIFFENER WITH NEW PN CC670-34117-5. REF SRM AND DWG.
- [SDR SWIA2020062651244](https://openairdocs.org/sdr/SWIA2020062651244.md): Angle · corroded · May 23, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ANGLE ATTACHMENT BRACKET CORRODED ON INTERCOSTAL AT FS 349.00 STR 26L. (C-CHECK) RO 6/24/2020 REMOVED CORROSION FROM ANGLE AT FORWARD SIDE OF INTERCOSTAL AT FS349, STR 26L AND FOUND REWORKED AREA TO BE OUT OF LIMITS. REPLACED ANGLE REF SRM AND DWG. COMPLIED
- [SDR SWIA2020062651243](https://openairdocs.org/sdr/SWIA2020062651243.md): Crossbeam · corroded · May 22, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SUSPECTED CORROSION ON FS280 CROSSBEAM UNDER CENTER SPLICE TOP STRAP. (C-CHECK) RO 6/24/2020 REMOVED CORROSION ON FS280 CROSSBEAM. FOUND TO BE OUT OF LIMITS. REPLACED FS280 CROSSBEAM REF SRM, DWG.
- [SDR SWIA2020062651242](https://openairdocs.org/sdr/SWIA2020062651242.md): Gusset · corroded · May 21, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 1015 STR 23L CORNER GUSSET CORRODED ON LWR FWD SIDE. (C-CHECK) RO 6/24/2020 INSTALLED NEW GUSSET CLIP PN MM670-36482-003 AT FS 1015 STR 23L REF SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651241](https://openairdocs.org/sdr/SWIA2020062651241.md): Gusset · corroded · May 21, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 1015 STR 24L CORNER GUSSET CORRODED ON LWR FWD SIDE. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 24L FS 1015 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-003 REF SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651240](https://openairdocs.org/sdr/SWIA2020062651240.md): Gusset · corroded · May 21, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 1015 STR 22L CORNER GUSSET CORRODED ON BOTH THE LOWER FWD SIDE AND THE INBD SIDE. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 22L FS 1015 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-003 REF SRM AND DWG. COMPLIED WITH T
- [SDR SWIA2020062651273](https://openairdocs.org/sdr/SWIA2020062651273.md): Seat Track · corroded · May 20, 2020 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT MARKED WITH RED GREASE PEN RAIL AT APPROX 669+40 TO FS740 2ND FWD OF EMER EXIT HAS MULTI AREAS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED RT SIDE SEAT TRACK AT FS 675 TO FS 713 REF AMM. FABRICATED NEW SEAT TRACK FROM P/N N126-2075 PO T-52211
- [SDR SWIA2020062651254](https://openairdocs.org/sdr/SWIA2020062651254.md): Floorboard · cracked · May 20, 2020 · N748EV · Cndair CL6002C10 · Fuselage Floor Panel
  > CABIN FLOORBOARD 271GLF CRACKED. (PN: SH670-32593-11) (C-CHECK) RO 6/24/2020 ORDERED/RECEIVED NEW CABIN FLOOR PANEL 271GLF PN SH670-32593-13. SEE TRANS 20927305 FOR INSTALLATION.
- [SDR SWIA2020062651253](https://openairdocs.org/sdr/SWIA2020062651253.md): Housing · cracked · May 20, 2020 · N748EV · Cndair CL6002C10 · Leading Edge Devices
  > SLAT TRACK HOUSING CRACKED IN FUEL TANK OF RIGHT WING UNDER PANEL LOCATION 651BB. (C-CHECK) RO 6/24/2020 REPAIRED CRACK AT THE SLAT TRACK HOUSING ON THE RT WING UNDER PANEL 651BB REF REO.
- [SDR SWIA2020062651239](https://openairdocs.org/sdr/SWIA2020062651239.md): Floorbeam · cracked · May 20, 2020 · N748EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT FLOOR STRUCTURE RT FLOORBEAM AT RBL 12.00, SUSPECT CRACK AT APPROX FS280 (C-CHECK) RO 6/24/2020 CUT AWAY DAMAGED SECTION OF FLOORBEAM AND INSTALLED NEW FLOORBEAM SECTION AND REPAIR PARTS PER SRM. COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651238](https://openairdocs.org/sdr/SWIA2020062651238.md): Floorbeam · cracked · May 20, 2020 · N748EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT FLOOR STRUCTURE LT FLOORBEAM AT LBL 12.00, SUSPECT CRACK AT APPROX FS280. (C-CHECK) RO 6/24/2020 CUT AWAY DAMAGED SECTION OF FLOORBEAM AND INSTALLED REPAIR PER SRM. COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651237](https://openairdocs.org/sdr/SWIA2020062651237.md): Intercostal · corroded · May 20, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AVIONICS BAY DOOR SURROUND INTERCOSTAL TO THE RIGHT SIDE OF STR 27 BETWEEN FS349 AND FS364 HAS CORROSION. (C-CHECK) RO 6/24/2020 REPLACED RT INTERCOSTAL AT AVIONICS BAY DOOR CUTOUT PER SRM & DRAWING. SEE CONTINUATION CARD FOR SETAILS. COMPLIED WITH TASK
- [SDR SWIA2020062651272](https://openairdocs.org/sdr/SWIA2020062651272.md): Seat Track · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT RAIL AT APROX FS740 TO 773 (1ST FWD OF EMER EXIT) HAS CORROSION. (C-CHECK) RO 6/24/2020 REPLACED RT SIDE SEAT RAIL FROM FS 740 TO FS 773 REF AMM. FABRICATED SEAT TRACK WITH P/N N126-2075 PO R52211 REF SRM.
- [SDR SWIA2020062651271](https://openairdocs.org/sdr/SWIA2020062651271.md): Seat Track · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT RAIL AT APROX FS 865 TO FS 953 (2ND-FWD. OF CARGO DOOR) HAS AREAS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED LT SIDE SEAT RAIL FROM FS 865 TO FS 953 REF AMM. FABRICATED SEAT TRACK FROM P/N N126-2075 PO T-52211 REF SRM.
- [SDR SWIA2020062651270](https://openairdocs.org/sdr/SWIA2020062651270.md): Seat Track · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT RAIL AT APROX FS 785.15 TO FS 865 HAS AREAS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED LT SIDE SEAT RAIL BETWEEN FS 785.15 TO FS 865.00 REF AMM. FABRICATED FROM N126-2075 PO T52211 REF SRM.
- [SDR SWIA2020062651269](https://openairdocs.org/sdr/SWIA2020062651269.md): Seat Track · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT RAIL JUST FWD OF EMER EXIT HAS MULT AREAS OF CORROSION. (C-CHECK) RO 6/24/2020 REMOVED AND REPLACED LT SIDE SEAT RAIL FORWARD OF EMER EXIT REF AMM.
- [SDR SWIA2020062651268](https://openairdocs.org/sdr/SWIA2020062651268.md): Seat Track · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT RAIL AT APPROX FS 669+40 TO FS 740 ( 2ND FWD OF EMER EXIT) HAS MULT AREAS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED LT SIDE SEAT RAIL AT FS 675 TO FS 713 REF AMM. FABRICATED NEW SEAT TRACK FROM P/N N126-2075 PO T-52211 REF SRM.
- [SDR SWIA2020062651267](https://openairdocs.org/sdr/SWIA2020062651267.md): Gusset · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STR 23L FS 1031 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 23L FS 1031 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-007 REF SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651266](https://openairdocs.org/sdr/SWIA2020062651266.md): Seat Track · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE WALL SEAT RAIL FROM APROX FS 575 -FS 674, CORRODED AT APROX FS 581 AND GOUGED AT APROX FS 665. (C-CHECK) RO 6/24/2020 REMOVED AND REPLACED RT SEAT RAIL FROM APPROX FS 575 TO FS 674, REF AMM.
- [SDR SWIA2020062651265](https://openairdocs.org/sdr/SWIA2020062651265.md): Seat Track · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 SEAT TRACK FROM FS 280 TO FS 477 CORRODED AT APROX FS 409 -FS 421. (C-CHECK) RO 6/24/2020 REPLACED SEAT TRACK AT RBL 9 FROM FS 350 TO FS 485 REF AMM. FABRICATED SEAT TRACK FROM P/N N126-2075 PO T52211 REF SRM.
- [SDR SWIA2020062651264](https://openairdocs.org/sdr/SWIA2020062651264.md): Seat Track · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT TRACK SECTION AT LBL27.00 FROM FS485.00 TO APPROX FS501.00 HAS CORROSION. (C-CHECK) RO 6/24/2020 REMOVED AND REPLACED SEAT TRACK SECTION AT LBL 27 FROM FS 485 TO APPROX FS501, REF AMM.
- [SDR SWIA2020062651263](https://openairdocs.org/sdr/SWIA2020062651263.md): Seat Track · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT TRACK SECTION AT RBL9.00 FROM FS581.00 TO APPROX FS693.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED SEAT TRACK AT RBL 9 BETWEEN FS 581 TO FS 693 REF AMM. FABRICATED SEAT TRACK FROM P/N N126-2075 PO T-52211 REF SRM.
- [SDR SWIA2020062651262](https://openairdocs.org/sdr/SWIA2020062651262.md): Seat Track · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT TRACK SECTION AT LBL9.00 FROM FS581.00 TO APPROX FS693.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED SEAT TRACK AT LBL 9 BETWEEN FS 581.00 TO FS 693.00 REF AMM. FABRICATED NEW SEAT FROM P/N N126-2075 PO T-52211 REF SRM.
- [SDR SWIA2020062651261](https://openairdocs.org/sdr/SWIA2020062651261.md): Seat Track · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT TRACK AT LBL9.00 FROM FS485.00 TO FS581.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED SEAT TRACK AT RBL 9 FROM FS 485 TO FS 581 REF AMM. FABRICATED SEAT FROM P/N N126-2075 PO T-52211 REF SRM.
- [SDR SWIA2020062651260](https://openairdocs.org/sdr/SWIA2020062651260.md): Seat Track · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT TRACK AT RBL9.00 FROM FS485.00 TO FS581.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 6/24/2020 REPLACED SEAT TRACK AT RBL 9 BETWEEN FS 485.00 TO FS 581.00 REF AMM. FABRICATED SEAT TRACK FROM P/N N126-2075 PO T-52211 REF SRM.
- [SDR SWIA2020062651236](https://openairdocs.org/sdr/SWIA2020062651236.md): Fitting · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CLIP AT STR 27 ON THE FORWARD SIDE OF THE FS265.00 FRAME IS CORRODED. (C-CHECK) RO 6/24/2020 REMOVED AND REPLACED CLIP AT STR 27 FORWARD SIDE OF FS265.00 REFERENCING APPLICABLE STEPS OF SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651235](https://openairdocs.org/sdr/SWIA2020062651235.md): Gusset · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STR 20L FS 1047 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 REPLACED ST 20L FS1047 STRINGER CLEAT WITH NEW REF REO. COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651234](https://openairdocs.org/sdr/SWIA2020062651234.md): Gusset · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STR 19L FS 1047 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 REPLACED STR 19L FS1047 STRINGER CLEAT WITH NEW REF REO. COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651233](https://openairdocs.org/sdr/SWIA2020062651233.md): Gusset · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STR 19L FS 1051 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 REPLACED STR 19L FS1051 STRINGER CLEAT WITH NEW REF REO.
- [SDR SWIA2020062651232](https://openairdocs.org/sdr/SWIA2020062651232.md): Gusset · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STR 20L FS 1031 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 20L FS 1031 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-005 REF SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651231](https://openairdocs.org/sdr/SWIA2020062651231.md): Gusset · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STR 21L FS 1031 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 21L FS 1031 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-007 REF SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651230](https://openairdocs.org/sdr/SWIA2020062651230.md): Gusset · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STR 22 FS 1031 CORNER BRACKET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 22L FS 1031 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-007 REF SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651229](https://openairdocs.org/sdr/SWIA2020062651229.md): Gusset · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STR 24L FS 1031 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 24L FS 1031 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-007 REF SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651228](https://openairdocs.org/sdr/SWIA2020062651228.md): Gusset · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STR 25L FS 1031 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 25L FS 1031 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-008 REF SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651227](https://openairdocs.org/sdr/SWIA2020062651227.md): Gusset · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STR 21L FS 1015 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 21L FS 1015 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-003 REF SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA2020062651226](https://openairdocs.org/sdr/SWIA2020062651226.md): Gusset · corroded · May 19, 2020 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STR 20L FS 1015 CORNER GUSSET CORRODED. (C-CHECK) RO 6/24/2020 CORNER GUSSET/ CLIP AT STR 20L FS 1015 IS CORRODED OUT OF LIMITS AND REPLACED WITH NEW GUSSET CLIP PN MM670-36482-003 REF SRM AND DWG. COMPLIED WITH TASK CARD.

Next page: https://openairdocs.org/aircraft/N748EV/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 = 'N748EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N748EV/reports

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