# Service difficulty reports: Bombardier CL-600-2C10

A list on [Bombardier CL-600-2C10](https://openairdocs.org/model/bombardier-cl-600-2c10.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 934 · 46,660 reports

- [SDR SWIA2026102677798](https://openairdocs.org/sdr/SWIA2026102677798.md): Steering Sys · faulted · Oct 26, 2026 · N760SK · Cndair CL6002C10 · Landing Gear Steering System
  > LOUD SCREECHING ON GEAR RETRACTION FOLLOWED BY STEERING INOP MSG. COMPLIED WITH QRH. FLT 4920. AFTER INTERROGATING MDC, FOUND B1 - 007466 & 007464, FOUND NSW INOP MSG ACTIVE WHEN ENTERING ACFT. AFTER TALKING WITH CREW, FOUND SCREECHING SOUND TO BE COMING F
- [SDR VNAA202610230048](https://openairdocs.org/sdr/VNAA202610230048.md): Flex Hose · worn · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Extinguishing System
  > CHAFING BTW FIRE EXTINGUISHER DISCHARGE LINE (DISCONNECTED FLEX HOSE) AND AGB HOUSING AT LH ENGINE. CHAFING BTW FIRE EXTINGUISHER DISCHARGE LINE (DISCONNECTED FLEX HOSE) AND AGB HOUSING AT LH ENGINE WAS REPAIRED PER EA NO: 7264-2026-1055, REV --, SECTION II
- [SDR VNAA202610230047](https://openairdocs.org/sdr/VNAA202610230047.md): Skin · worn · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Leading Edge Devices
  > WEAR ON INBOARD EDGE OF SLAT 1 SS 57.16 AT RH WING. WEAR ON INBOARD EDGE OF SLAT 1 SS 57.16 AT RH WING WAS REPAIRED PER REO 670-57-42-2560 REV -.
- [SDR VNAA202610230046](https://openairdocs.org/sdr/VNAA202610230046.md): Skin · worn · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Wing, Plate/Skin
  > WEAR ON SLAT LOWER SKIN (WEDGE) BTW SS 57.16 TO SS 337.66 AT RH WING. WEAR ON SLAT LOWER SKIN (WEDGE) BTW SS 57.16 TO SS 337.66 AT RH WING WAS REPAIRED PER PER REO 670-57-42-2574 REV-.
- [SDR VNAA202610230045](https://openairdocs.org/sdr/VNAA202610230045.md): Skin · damaged · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TEMPORARY REPAIR FOR MULTIPLE LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN PANELS BETWEE FS409.00 - FS985.00 AND STR4R - STR9R THE REPORTED CONDITION IS STRUCTURALLY ACCEPTABLE FOR A MAXIMUM OF 1450 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS MULTIPLE LIGH
- [SDR VNAA202610230044](https://openairdocs.org/sdr/VNAA202610230044.md): Skin · damaged · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TEMPORARY DISPOSITION FOR LIGHTNING STRIKE DAMAGE TO UPPER FUSELAGE SKIN PANEL AT FS830.40 AND STR7R THE SUBJECT CONDITION IS ACCEPTABLE FOR A MAXIMUM OF 1500 FLIGHT HOURS FROM THE INCORPORATION OF THIS REO. LIGHTNING STRIKE DAMAGE TO UPPER FUSELAGE SKIN PANE
- [SDR VNAA202610230043](https://openairdocs.org/sdr/VNAA202610230043.md): Skin · damaged · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE TO FUSELAGE SKINS AT FS855.40 AND AT STR7R. DAMAGE TO FUSELAGE SKINS AT FS855.40 AND AT STR7R WAS REPAIRED PER REO 670-53-00-836 REV -.
- [SDR VNAA202610230042](https://openairdocs.org/sdr/VNAA202610230042.md): Skin · damaged · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE - FUSELAGE SKIN PANEL FS169-FS193 PERM REPAIR WITHIN 8000 FH. REPLACE PANEL OR SUBMIT RFTS. LIGHTNING STRIKE DAMAGE - FUSELAGE SKIN PANEL FS169-FS193 WERE REPAIRED PER REO: 670-53-11-2369. REV: - -."
- [SDR VNAA202610230041](https://openairdocs.org/sdr/VNAA202610230041.md): Skin · damaged · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN FS 661+16 AND BTW STGR 8RH TO STGR 9RH AT FUSELAGE. LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN FS 661+16 AND BTW STGR 8RH TO STGR 9RH AT FUSELAGE WAS REPAIRED PER CRJ 900 SRM 53-00-00-201-003-A03.
- [SDR VNAA202610230040](https://openairdocs.org/sdr/VNAA202610230040.md): Angle · gouged · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Service Doors
  > GOUGE ON FWD INTERCOSTAL ANGLE STGR15 RH FS 319.70.00 AT INTERNAL SURROUND STRUCTURE OF GALLEY SERVICE DOOR. GOUGE ON FWD INTERCOSTAL ANGLE STGR15 RH FS 319.70.00 AT INTERNAL SURROUND STRUCTURE OF GALLEY SERVICE DOOR WAS REPAIRED PER REO: 670-53-21-2962 REV-
- [SDR VNAA202610230039](https://openairdocs.org/sdr/VNAA202610230039.md): Stiffener · bent · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Horizontal Stabilizer Miscellaneous Structure
  > BENT ON STABILIZER STIFFENER BTW FS 295.00 TO FS 333.00 RBL 27.0 AT CAB8N PAX FLOOR STRUCTURE. STABILIZER STIFFENER BTW FS 295.00 TO FS 333.00 RBL 27.0 AT CAB8N PAX FLOOR STRUCTURE WAS REPLACED PER SRM 51-42-10-001-001-A01.
- [SDR VNAA202610230038](https://openairdocs.org/sdr/VNAA202610230038.md): Stop Pad · broken · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Structure
  > BROKEN STOP PAD OF AFT LOWER FITTING AT LH EMERGENCY EXIT DOOR EXTERNAL SURROUND STRUCTURE. STOP PAD OF AFT LOWER FITTING AT LH EMERGENCY EXIT DOOR EXTERNAL SURROUND STRUCTURE. WAS REPLACED PER CRJ-700 AMM 53-41-23-000-801 (CONFIG A01) AND CRJ-700 AMM 53-41-
- [SDR VNAA202610230037](https://openairdocs.org/sdr/VNAA202610230037.md): Skin · dented · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TEMPORARY DISPOSITION FOR MULTIPLE DENTS TO MULTIPLE FUSELAGE SKINS DUE TO HAIL BETWEEN FS169.00 - FS235.00 THIS TEMPORARY DISPOSITION IS VALID FOR MAXIMUM 5200 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO. WITHIN 5200 FLIGHT HOURS REPAIR OR REPLACE
- [SDR VNAA202610230036](https://openairdocs.org/sdr/VNAA202610230036.md): Door · dented · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > DENT ON LH ENGINE LOWER FAN-COWL DOOR. DENT ON LH ENGINE LOWER FAN-COWL DOOR WAS REPAIRED PER REO 670-54-14-1012 REV B AND REO 670-54-14-1355, REV-.
- [SDR VNAA202610230035](https://openairdocs.org/sdr/VNAA202610230035.md): Skin · dented · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DENT ON LOWER EXTERNAL FUSELAGE AT APPROXIMATELY FS 270.00 BETWEEN STGR 24R - 25R. DENT ON LOWER EXTERNAL FUSELAGE AT APPROXIMATELY BS 270 BTWN STR 24R AND STR 25R WAS REPAIRED IAW REO 670-51-00-085 REV -B AND REO 670-53-11-2376. REV-.
- [SDR VNAA202610230034](https://openairdocs.org/sdr/VNAA202610230034.md): Fan Cowl · dented · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Nacelle/Pylon, Plate/Skin
  > DENT IN THE LOWER FAN COWL, ENGINE 1. REPAIRED PER REO 670-54-14-1012. REV B.
- [SDR VNAA202610230033](https://openairdocs.org/sdr/VNAA202610230033.md): Skin · dented · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DENT TO ADG SKIN PANEL BELOW THE ADG DOOR BETWEEN FS177.00 AND FS185. DENT TO ADG SKIN PANEL BELOW THE ADG DOOR BETWEEN FS177.00 AND FS185.00 WAS REPAIRED PER REO 670-53-11-2365 REV -- "
- [SDR VNAA202610230032](https://openairdocs.org/sdr/VNAA202610230032.md): Exhaust Duct · damaged · Oct 23, 2026 · N546FF · Cndair CL6002C10 · APU Exhaust System
  > AFTER THE REMOVAL OF THE SEAL ON AFT EXHAUST APU,ENLOGATED RIVET HOLES (4EA) WERE FOUND BTW THE 6 O'CLOCK AND 12 O' CLOCK POSITION APROXIMATELLY AND AN ADITIONAL RIVET HOLE WAS FOUND AT THE 9 O' CLOCK POSITION APROXIMATELLY. ENLOGATED RIVET HOLES (4EA) WERE
- [SDR VNAA202610230031](https://openairdocs.org/sdr/VNAA202610230031.md): Skin Panel · damaged · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Wing, Plate/Skin
  > GOUGES AT LEADING EDGE SKIN PANEL (SS337.66 TO SS446.86), LH WING. GOUGES AT LEADING EDGE SKIN PANEL (SS337.66 TO SS446.86), LH WING WERE REPAIRED PER EA NO. 5741-2026-1071. REV A AND EA 5741-2026-1096 REV A.
- [SDR VNAA202610230030](https://openairdocs.org/sdr/VNAA202610230030.md): Winglet · damaged · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Wing Main, Frame Structure
  > PERM REPAIR BEFORE 34,331.08 FH - WEDGE, WINGLET T/E (LH) WITHIN 7,220.45 FLIGHT HOURS (34,331.08 FH), REPAIR OR REPLACE OF THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. WINGLET T/E (LH TIP FAIRING) WAS REPAIRED PER REO 670-57-30-082 REV -"
- [SDR VNAA202610230029](https://openairdocs.org/sdr/VNAA202610230029.md): Rivet · damaged · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DAMAGED ALIGNMENT RIVETS AT CAPT & FO'S SEAT TRACKS. SEAT TRACKS WAS REPAIRED PER REO: 670-53-11-210, REV D.
- [SDR VNAA202610230028](https://openairdocs.org/sdr/VNAA202610230028.md): Floorbeam · cracked · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > "CRACK ON FLOORBEAM BS 280 AND RBL 12 AT FLOOR STRUCTURE. CRACK ON FLOORBEAM FSTA 280 AND RBL 12 AT FLOOR STRUCTURE WAS REPAIRED PER SRM 53-11-43-201-003-A01.
- [SDR VNAA202610230027](https://openairdocs.org/sdr/VNAA202610230027.md): Floorbeam · cracked · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CRACK ON FLOORBEAM BS 280, LBL 12.0 AT FLOOR STRUCTURE. CRACK ON FLOORBEAM BS 280, LBL 12.0 AT FLOOR STRUCTURE WAS REPAIRED IAW SRM 53-11-43-201-003-A01.
- [SDR VNAA202610230026](https://openairdocs.org/sdr/VNAA202610230026.md): Drag Angle · cracked · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATU
- [SDR VNAA202610230025](https://openairdocs.org/sdr/VNAA202610230025.md): Web · cracked · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK ON WEB BTWN BS 195 - 205, WL 79.50. ON LEFT INTERNAL STRUCTURE IN THE FWD EQUIPMENT BAY. THE WEB BTWN BS 195 TO BS 205, WL 79.50 WAS REPAIRED IAW REO 670-53-11-509, REV E.
- [SDR VNAA202610230024](https://openairdocs.org/sdr/VNAA202610230024.md): Fitting · cracked · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Engine Thrust Reverser
  > CRACK ON UPPER CASCADE ANGLE FITTING ON INNER BORDER AT 3 O'CLOCK, LT ENGINE. CRACK ON UPPER CASCADE ANGLE FITTING ON INNER BORDER AT 3 O'CLOCK, LT ENGINE WAS REPAIRED PER REO: 670-54-22-181 REV- A.
- [SDR VNAA202610230023](https://openairdocs.org/sdr/VNAA202610230023.md): Hinge · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > IN REF TRFKE00AXBML: AFTER REMOVAL OF BUSHING AND BEARING, CORROSION AND WEAR IN THE INNER AREA OF THE LUGS OF FITTING INBD, L1, L2, L3, L4, L5 & L6 ON CENTER FITTING AND FITTING OUTBD ( UPPER / LOWER)AT LH AILERON LUGS L5 & L6 WERE CLEANED PER CRJ -700 SRM
- [SDR VNAA202610230022](https://openairdocs.org/sdr/VNAA202610230022.md): Seat Track · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT TRACK OF LBL 9 BTWN BS 677 TO BS 977 AT PAX CABIN. SEAT TRACK OF LBL 9 BTWN BS 677 TO 977 AT PAX CABIN WERE REPLACED IAW AMM 53-00-49.
- [SDR VNAA202610230021](https://openairdocs.org/sdr/VNAA202610230021.md): Seat Track · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT TRACK OF RBL 9 BTWN BS 677 TO 977 AT PAX CABIN. SEAT TRACK OF RBL 9 BETWEEN FS 677.00 TO FS 977.00 AT PAX CABIN WERE REPLACED PER AMM 53-00-49.
- [SDR VNAA202610230020](https://openairdocs.org/sdr/VNAA202610230020.md): Fitting · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN AFT ACCESS 109 (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 109 (1EA) ON GALLEY1 WAS REPLACED IAW CMM 25-33-44, REV 3.
- [SDR VNAA202610230019](https://openairdocs.org/sdr/VNAA202610230019.md): Fitting · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER CMM 25-33-44 REV 3.
- [SDR VNAA202610230018](https://openairdocs.org/sdr/VNAA202610230018.md): Skin · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION ON STR 26R, BTW BS 969 - 985 AT INTERNAL FUSELAGE SKIN. CORROSION ON STR 26R BTWN BS 969 - 985 AT INTERNAL FUSELAGE SKIN WAS REMOVED AND EVALUATED WHITIN LIMITS IAW REO 670-53-61-2762, REV -.
- [SDR VNAA202610230017](https://openairdocs.org/sdr/VNAA202610230017.md): Skin · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION ON BOTH FACES OF FRAME FS=909 BTW SGTR 25L TO SGTR 25R AT INTERNAL FUSELAGE SKIN. FRAME FS=909 BTW SGTR 25L TO SGTR 25R AT INTERNAL FUSELAGE SKIN WAS REPAIRED PER REO 670-53-51-407 REV -, AND REO: 670-53-31-1251 REV-.
- [SDR VNAA202610230016](https://openairdocs.org/sdr/VNAA202610230016.md): Skin · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > "CORROSION ON SGTR 26R BTW FS=847 TO FS=863 AT INTERNAL FUSELAGE SKIN. SGTR 26R BTW FS=847 TO FS=863 AT INTERNAL FUSELAGE SKIN WAS REPAIRED PER EA 5351-2026-1079 REV -.
- [SDR VNAA202610230015](https://openairdocs.org/sdr/VNAA202610230015.md): Bracket · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "CORROSION ON BRACKET MACHINED 5EA BTW FS517.00-FS597.00, STGR 22L-24R AT FWD BAGGAGE COMPARTMENT. BRACKET MACHINED 5EA BTW FS517.00-FS597.00, STGR 22L-24R AT FWD BAGGAGE COMPARTMENT WERE BLENDED OUT AND FOUND WITHIN LIMITS PER REO NO: 5332-2026-1041. REV.--
- [SDR VNAA202610230014](https://openairdocs.org/sdr/VNAA202610230014.md): Strap · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION ON SETTLEMENT AREA OF HORIZONTAL STABILIZER TIP LH. LOWER STRAP WAS REPLACED ON SETTLEMENT AREA OF HORIZONTAL STABILIZER TIP FAIRING LH PER CRJ-700 SRM 51-42-10-001-001-A01"
- [SDR VNAA202610230013](https://openairdocs.org/sdr/VNAA202610230013.md): Support · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION INSIDE HOLE (8EAS) ON GALLEY SUPPORT FS 285.00 RBL17.0, FS 296.00 RBL 4.0, FS 310.00 RBL 4.0, FS 288.00 LBL 20, FS 310.00 LBL 20, FS 333.00 LBL 38.0, FS 333.00LBL 32.0 AND FS 349.00 LBL 17.0 AT CABIN PAX FLOOR STRUCTURE. CORROSION INSIDE HOLE (8EAS)
- [SDR VNAA202610230012](https://openairdocs.org/sdr/VNAA202610230012.md): Seat Track · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS ALONG PASSENGER CABIN 8 (E/AS) RH SIDE (BTW FS364 TO FS977 STGR 15R). SEAT RAILS ALONG PASSENGER CABIN 8 (E/AS) RH SIDE (BTW FS364 TO FS977 STGR 15R) WERE REPLACED PER CRJ-700 AMM 53-00-49"
- [SDR VNAA202610230011](https://openairdocs.org/sdr/VNAA202610230011.md): Seat Track · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK ALONG PASSENGER CABIN 7EA LH SIDE (BTW FS364 TO FS977 STGR 15L). SEAT TRACK ALONG PASSENGER CABIN 7EA LH SIDE (BTW FS364 TO FS977 STGR 15L) WERE REPLACED PER AMM 53-00-49.
- [SDR VNAA202610230010](https://openairdocs.org/sdr/VNAA202610230010.md): Seat Track · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT TRACK OF LBL9 BETWEEN FS 373.00 TO FS 677.00 AT PAX CABIN. CORROSION AT SEAT TRACK OF LBL9 BETWEEN FS 373.00 TO FS 677.00 AT PAX CABIN WERE REMOVED PER SRM 51-21-06-001-001-A01, WAS EVALUATED, DUE TO EXCESSIVE CORROSION DAMAGE PER CRJ 700
- [SDR VNAA202610230009](https://openairdocs.org/sdr/VNAA202610230009.md): Seat Track · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL OF RBL9 BETWEEN FS 349.00 TO FS 677.00 AT PAX CABIN. CORROSION AT SEAT RAIL OF RBL9 BETWEEN FS 349.00 TO FS 677.00 AT PAX CABIN WERE REMOVED IAW SRM 51-21-06-001-001-A01, WAS EVALUATED, DUE TO EXCESSIVE CORROSION DAMAGE AT SEAT TRACK O
- [SDR VNAA202610230008](https://openairdocs.org/sdr/VNAA202610230008.md): Seat Track · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL OF LBL27 BETWEEN FS 364.00 TO FS 485.00, FS 485 TO FS 581.00 AT PAX CABIN. CORROSION ON SEAT RAIL OF LBL27 BETWEEN FS 364.00 TO FS 485.00, FS 485 TO FS 581.00 AT PAX CABIN WERE REMOVED PER SRM 51-21-06-001-001-A01, WAS EVALUATED, DUE TO
- [SDR VNA2026F00012](https://openairdocs.org/sdr/VNA2026F00012.md): Retainer · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION RETAINER SEAL ON DOOR E/E COMPARTMENT (AVIONICS). RETAINERS SEAL (4EA) ON DOOR E/E COMPARTMENT (AVIONICS) WERE REPLACE PER SRM 51-42-06-001-001-A01.
- [SDR VNAA202610230005](https://openairdocs.org/sdr/VNAA202610230005.md): Skin · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION ON STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT WAS REPAIRED PER REO: 670-53-21-242 REV: - C.
- [SDR VNA2026F00010](https://openairdocs.org/sdr/VNA2026F00010.md): Skin · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION ON STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT WAS REPAIRED PER REO: 670-53-21-242 REV: - C.
- [SDR VNAA202610230004](https://openairdocs.org/sdr/VNAA202610230004.md): Strap · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON STRUCTURE WHERE ACCESS PANEL 195AB SEAT CORROSION ON STRUCTURE WHERE ACCESS PANEL 195AB SEAT WAS REMOVED PER CRJ 700 SRM 51-21-06-001-001-A01 AND EVALUATED (SEAT BTW FS 847) WITHIN OF LIMIT AND SEAT BTW FS 849 TO FS 879 WAS EVALUATED OUT OF LIMITS
- [SDR VNAA202610230003](https://openairdocs.org/sdr/VNAA202610230003.md): Support · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Aerodynamic Fairings
  > CORROSION ON FAIRING SUPPORT (FRAMES) 2 EAS STA BS 629 AND 661 AND DIAFRAGMA 1EA BTW FS 629-FS 661 (SEATLEMENT AREA, UNDER ACCESS PANELS 191 AB, 191BB AND 192BB) SUMMARY:CORROSION WAS REMOVED PER 51-42-06-001-001-A01 AREA WAS EVALUATE PER SRM 53-82-55-101-0
- [SDR VNAA202610230002](https://openairdocs.org/sdr/VNAA202610230002.md): Bracket · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Main Landing Gear
  > CORROSION ON ANTI-ROTATION BEAM ASSY ON LT FWD DOOR HINGE AT NLG W/W. CORROSION ON ANTI-ROTATION BEAM ASSY WAS REMOVED IAW SRM 51-21-06-001-001-A01. AND AREA IT IS OUT LIMITS PER SRM 53-00-00-101-001-A01 AND ANTI-ROTATION BEAM ASSY ON LT FWD DOOR HINGE AT NLG
- [SDR VNAA202610230001](https://openairdocs.org/sdr/VNAA202610230001.md): Hinge · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > "IN REF TASK TRFKE00AXBMU: AFTER REMOVAL OF BUSHINGS THE MOUNTING HOLES FOR HINGES ASSY # 3 (2EA) ON RH AILERON REAR SPAR WERE OVERSIZED AND AFTER REMOVAL OF BUSHINGS THE MOUNTING HOLES FOR HINGE ASSY 2# S (1EA) ON LH AILERON REAR SPAR WAS OVERSIZED ON HOLES
- [SDR SWIA2026102277793](https://openairdocs.org/sdr/SWIA2026102277793.md): Cartridge · warning message · Oct 22, 2026 · N752SK · Cndair CL6002C10 · Fuel Transfer Valve
  > IN IAD, DURING FLIGHT, NOTICED L AUTO XFLOW STAY ON FOR LONGER THAN NORMAL. FUEL IMBALANCE CONTINUED TO DEVELOP WITH THE LEFT SIDE LOW AND XFLOW RUNNING, TOTAL FUEL WAS NOT BELOW EXPECTED. DECLARED AN EMERGENCY AND LANDED WITH 600LB IMBALANCE. NO MESSAGES PO

Next page: https://openairdocs.org/model/bombardier-cl-600-2c10/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 aircraft_model_key = 'CL6002C10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/bombardier-cl-600-2c10/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.