# Service difficulty reports: Bombardier CL-600-2D24

A list on [Bombardier CL-600-2D24](https://openairdocs.org/model/bombardier-cl-600-2d24.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 763 · 38,113 reports

- [SDR VNAA2026102827202](https://openairdocs.org/sdr/VNAA2026102827202.md): Warning Message · false activation · Oct 27, 2026 · N568NN · Cndair CL6002D24 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING FOLLOWED BY QRH FIXED THE DISAGREE / PERFORMED TROUBLESHOOTING OF SELECTOR VALVE IAW FIM 32-51-50-810-801-A01. OPS CHECK GOOD. VERIFIED PROX SENSORS WITHIN RANGE WITH THE MDC IAW AMM 32-61-00-710-801-A01-PSA. COMPLETED 15 FULL EXTENSION/R
- [SDR VNAA2026102827101](https://openairdocs.org/sdr/VNAA2026102827101.md): Arming Switch · defective · Oct 27, 2026 · N566NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP CAUTION MSG IN ROUTE (AFTER GEAR RETRACTION) QRH PROCEDURE UNSUCCESSFUL. FOUND B1 007461. T/S PER FIM 32-51-37-810-A01. REMOVED AND REPLACED STEERING ARMING SWITCH IAW AMM 32-51-37-000/400-8001-A01. OPS TEST GOOD. PERFORMED NLG EXTENSION AND RET
- [SDR VNAA202610260034](https://openairdocs.org/sdr/VNAA202610260034.md): Fitting · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Ailerons
  > AFTER BUSHINGS AND BEARINGS REMOTIONS, CORROSION ON LUGS L2, LH AILERON. LUG L2 AT LH AILERON WAS REPAIRED PER REO 670-57-61-237 REV -.
- [SDR VNAA202610260033](https://openairdocs.org/sdr/VNAA202610260033.md): Fitting · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN AFT ACCESS 109 (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 109 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-96 REV NO. 9.
- [SDR VNAA202610260032](https://openairdocs.org/sdr/VNAA202610260032.md): Fitting · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN AFT ACCESS 107 OUT SIDE (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 107 OUT SIDE (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-96 REV NO. 9.
- [SDR VNAA202610260031](https://openairdocs.org/sdr/VNAA202610260031.md): Fitting · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN AFT ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER CMM 25-33-96 REV NO. 9.
- [SDR VNAA202610260030](https://openairdocs.org/sdr/VNAA202610260030.md): Fitting · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN UNDER WASTE CONTAINER. FLOOR FITTING IN UNDER WASTE CONTAINER (PN: A414252-3) WAS REPLACED PER CMM 25-40-40.
- [SDR VNAA202610260029](https://openairdocs.org/sdr/VNAA202610260029.md): Lug · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Ailerons
  > AFTER BUSHINGS AND BEARINGS REMOVAL, CORROSION WAS FOUND ON LUG R2 AT RH AILERON LUG R2 AT RH AILERON WAS REPAIRED PER REO 670-57-61-237 REV -.
- [SDR VNAA202610260028](https://openairdocs.org/sdr/VNAA202610260028.md): Hinge Fitting · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON UPPER HINGE FITTING RH WAS FOUND. NLG DOOR HINGE FITTING ASSEMBLY (RH) WAS EVALUATED OUT LIMITS PER SRM 53-00-00-101-001-A01 AND REPLACED PER SRM 51-41-02-001-001-A01.
- [SDR VNAA202610260027](https://openairdocs.org/sdr/VNAA202610260027.md): Skin · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Wing, Plate/Skin
  > CORROSION ON SKIN OF FUEL ACCESS PANEL 611BB. SUMMARY: SKIN OF FUEL ACCESS PANEL 611BB WAS REPAIRED PER EA 2811-2026-1159 REV. - - SECTION III PERMANENT REPAIR"
- [SDR VNAA202610260026](https://openairdocs.org/sdr/VNAA202610260026.md): Stringer · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 26LH AND SPACER NUT BTW FS310 TO FS 319 BELOW FLOOR PANELS AT E/E COMPARTMENT. CORROSION ON STRINGER 26LH AND SPACER NUT BTW FS310 TO FS 319 BELOW FLOOR PANELS AT E/E COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATE
- [SDR VNAA202610260025](https://openairdocs.org/sdr/VNAA202610260025.md): Web · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB FS280 BTW RBL9 TO RBL45 AT CPAX. CORROSION ON WEB FS280 BTW RBL9 TO RBL45 AT CPAX WAS EVALUATED OF LIMITS PER CRJ/900 SRM 53-00-00-101-001-A01 AND REPAIRED PER CRJ/900 SRM 53-11-10-201-004-A01.
- [SDR VNAA202610260024](https://openairdocs.org/sdr/VNAA202610260024.md): Web · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB FS280 BTW LBL9 TO LBL45 AT CPAX. CORROSION ON WEB BS 280 BTW LBL9 TO LBL45 AT CPAX WAS EVALUATED OUT OF LIMITS PER SRM 53-00-00-101-001-A01 AND REPAIRED PER SRM 53-11-10-201-004-A01.
- [SDR VNA2026F00013](https://openairdocs.org/sdr/VNA2026F00013.md): Web · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB FS280 BTW LBL9 TO LBL45 AT CPAX. CORROSION ON WEB FS280 BTW LBL9 TO LBL45 AT CPAX WAS EVALUATED OUT OF LIMITS PER SRM 53-00-00-101-001-A01 AND REPAIRED PER SRM 53-11-10-201-004-A01.
- [SDR VNAA202610260023](https://openairdocs.org/sdr/VNAA202610260023.md): Seat Track · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL LBL27.00 (3 EAS) BTW FS364.00 TO FS581.00 AT PASSENGER CABIN. SEAT RAILS LBL27 BTW FS 364.00- FS 581.00 (3EA) AT PASSENGER CABIN DUE TO EXCESSIVE DAMAGED WERE REPLACED PER CRJ-900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02
- [SDR VNAA202610260022](https://openairdocs.org/sdr/VNAA202610260022.md): Seat Track · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK RBL9.00 (6 EAS) BTW FS349.00 TO FS693.00 AT PASSENGER CABIN. DUE TO EXCESSIVE DAMAGED ON SEAT RAIL RBL9.00 (6 EAS) BTW FS349.00 TO FS693.00 AT PASSENGER CABIN WERE REPLACED PER CRJ-900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-00
- [SDR VNAA202610260021](https://openairdocs.org/sdr/VNAA202610260021.md): Seat Track · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL9.00 (5 EAS) BTW FS364.00 TO FS693.00 AT PASSENGER CABIN. DUE TO EXCESSIVE DAMAGED SEAT RAIL LBL9 BTW FS364.00 TO FS693.00 (5 EAS) WERE REPLACED PER CRJ-900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02 AND PER AMM 53-00-49-
- [SDR VNAA202610260020](https://openairdocs.org/sdr/VNAA202610260020.md): Floorbeam · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > AFTER REMOVE FLOORBEAM BS 280 CORRODED. THE FLOORBEAM WAS EVALUATED OUT LIMITS IAW SRM 53-00-00-101-001-A01, & WAS REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01, & SRM 51-42-21-001-001-A01.
- [SDR VNAA202610260019](https://openairdocs.org/sdr/VNAA202610260019.md): Floorbeam · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > AFTER REMOVAL OF FLOOR PANEL, THE FLOORBEAM AND CLIPS LT/RT BS 280. CORROSION ON LH FLOORBEAM. THE FLOORBEAM WAS EVALUATED OUT LIMITS IAW SRM 53-00-00-101-001-A01, AND WAS REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01, & SRM 51-42-21-001
- [SDR VNAA202610260018](https://openairdocs.org/sdr/VNAA202610260018.md): Hinge Arm · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON HINGE ARMS AND BASE OF ACCESS PANEL 196ER. HINGE ARMS AND HINGE BRACKETS WERE REPLACED IAW AMM 52-45-01-400-801, (CONFIG. A01), & SRM 51-41-02-001-001-A01.
- [SDR VNAA202610260017](https://openairdocs.org/sdr/VNAA202610260017.md): Seat Track · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT TRACK, STR 15R (6EAS) BTWN BS 744.15 - 969 IN THE PASSENGER CABIN. CORROSION ON SIDE SEAT TRACK WAS EVALUATED OUT OF LIMITS IAW SRM 53-41-49-101-001-A01, & REPLACED IAW AMM 53-00-49.
- [SDR VNAA202610260016](https://openairdocs.org/sdr/VNAA202610260016.md): Seat Track · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON THE SIDE SEAT TRACK, STR 15L (6EAS) BTW BS 744.15 - 969 IN THE PASSENGER CABIN. CORROSION ON FITTING GALLEY SUPPORTS ON SEAT TRACK BTW BS 280 TO 295, RBL 39, & BS 310 - 319, RBL 7 WAS REMOVED IAW SRM 51-21-06-001-001-A01, AND IS OUT OFF LIMITS IA
- [SDR VNAA202610260015](https://openairdocs.org/sdr/VNAA202610260015.md): Seat Track · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT TRACK STR 15R (5 EAS) BTWN BS 379 - 720.85. THE SEAT TRACK WAS EVALUATED OUT OF LIMITS IAW SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02, AND SRM 53-41-49-101-001-A02. AND REPLACED IAW AMM 53-00-49.
- [SDR VNAA202610260014](https://openairdocs.org/sdr/VNAA202610260014.md): Fitting · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORRODED FITTING AT BS 349 STR 17L. DUE TO EXCESS DAMAGE, THE FITTING WAS REPLACED IAW SRM 53-21-23-101-001-A02, AND SRM 51-42-21-001-001- A01.
- [SDR VNAA202610260013](https://openairdocs.org/sdr/VNAA202610260013.md): Floor Support · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON GALLEY FLOOR SUPPORTS BTWN BS 280 - 295, RBL 39, & BS 310 - 319, RBL 7. THE GALLEY FLOOR SUPPORTS REMOVED IAW SRM 51-21-06-001-001-A01, AND FOUND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01, AND REPLACED IAW SRM 51-42-21-0.
- [SDR VNAA202610260012](https://openairdocs.org/sdr/VNAA202610260012.md): Seat Track · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT TRACK STR 15L (6 EAS) BTW BS 379 - 720.85. THE SIDE SEAT TRACK BTWN BS 469 - 565 WAS CLEANED IAW SRM 51-26-00-001-001-A01, AND INSPECTED DETAILED VISUAL INSPECTION OF AREA WAS PERFORMED PER IAW NDT MANUAL 51-20-009-210, STEP 1. C. NO D
- [SDR VNAA202610260011](https://openairdocs.org/sdr/VNAA202610260011.md): Door Frame · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON MID CAP OF PASSENGER DOOR SURROUND STRUCTURE. PASSENGER DOOR SURROUND WAS EVALUATED OUT OF LIMITS IAW SRM 53-21-23-101-001-A02, & REPLACED IAW SRM 51-21-06-001-001-A01, AND SRM 51-41-02-001-001-A01.
- [SDR VNAA202610260010](https://openairdocs.org/sdr/VNAA202610260010.md): Drip Tray · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON DRIP TRAY LT & RT OF BS 280. THE DRIP TRAY WAS EVALUATED OUT LIMITS IAW SRM 53-00-00-101-001-A01, & REPLACED IAW SRM 51-42-13-001-001-A01.
- [SDR VNAA202610260009](https://openairdocs.org/sdr/VNAA202610260009.md): Clamp · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON CLAMPS (12EAS) AT 6 LH / 6 RH MAIN WHEEL WELL AREA. CLAMPS (12EAS) AT 6 LT / 6 RT MAIN WHEEL WELL AREA WERE REPLACED IAW ESPM 20-12-00.
- [SDR VNAA202610260008](https://openairdocs.org/sdr/VNAA202610260008.md): Support · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CORROSION ON SUPPORT AND LIGHT (DS151) OF SERVICE WASTE AT AFT INNER FAIRING AREA. CORROSION ON SUPPORT AND LIGHT (DS151) OF SERVICE WASTE AT AFT INNER FAIRING AREA WAS EVALUATED OUT LIMITS IAW SRM 51-10-06-001-001-A01, AND REPLACED IAW SRM 51-41-02-001-001-A
- [SDR VNAA202610260007](https://openairdocs.org/sdr/VNAA202610260007.md): Plate · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Wing Main, Frame Structure
  > CORROSION ON LTWINGLET TIP METALLIC PLATE. THE METALLIC PLATE ON LT WINGLET TIP WAS REPLACED AND WINGLET TIP WAS REPAIRED IAW DOC 701650 REV U. AND EA 5730-2026-1107, REV-, SECTION III PERMANENT REPAIR.
- [SDR VNAA202610260006](https://openairdocs.org/sdr/VNAA202610260006.md): Lug · corroded · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > AFTER BUSHINGS AND BEARINGS REMOVAL, CORROSION ON LUGS L2, LH AILERON. LUG L2 AT LT AILERON WAS REPAIRED IAW REO 670-57-61-237 REV -.
- [SDR VNAA202610260005](https://openairdocs.org/sdr/VNAA202610260005.md): Floor Support · cracked · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50). FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOO
- [SDR VNAA202610260004](https://openairdocs.org/sdr/VNAA202610260004.md): Rib · cracked · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACKED RIB LEADING EDGE SS57.16 AT LT WING, RIB LEADING EDGE SS57.16 AT LH WING WAS REPLACED PER SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-10-001-001-A01.
- [SDR VNAA202610260003](https://openairdocs.org/sdr/VNAA202610260003.md): Web · cracked · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMP. CRACK ON UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMP WAS REPAIRED PER REO 670-53-11-509 REV. - E. AND REO 690-53-11-2259 REV -.
- [SDR VNAA202610260002](https://openairdocs.org/sdr/VNAA202610260002.md): Cowl Door · worn · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > ELONGATED SCREW HOLE ON RH ENG UPPER FAN COWL DOOR ASSY WITHIN 2188 FLIGHT HOURS AFTER SECTION I, ELONGATED SCREW HOLE ON RH ENG UPPER FAN COWL DOOR ASSY WAS REPAIRED PER REO 690-54-14-828 REV.-- AND REO 690-54-22-154 REV--.
- [SDR VNAA202610260001](https://openairdocs.org/sdr/VNAA202610260001.md): Lug · worn · Oct 26, 2026 · N554NN · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > AFTER BUSHINGS AND BEARINGS REMOTIONS, WEAR ON LUGS L4 AT LH AILERON LUGS L4 AT LH AILERON WASR REPAIRED PER REO 690-57-61-562 REV - - AND PAINT REMOVED AND APPLIED PER SRM 51-25-06-001-001-A01.
- [SDR SWIA2026102577794](https://openairdocs.org/sdr/SWIA2026102577794.md): Seal · missing · Oct 25, 2026 · N817SK · Cndair CL6002D24 · Air Intake Anti/De-Ice System
  > D LT COWL AI DUCT WARNING MSG IN FLIGHT RAN THE QRH LEAD TO INFLIGHT ENGINE SHUTDOWN B1 349549 LOOP BC MEL 36-21-6CCAT C DUE 110426. FLIGHT 4684, INTEROGATED MDC, FOUND B1-349549 IN AIRCRAFT HISTORY TROUBLESHOT IAW 36-21-01 INSPECTED LOOP ELEMENT, NO DEF
- [SDR VNAA2026102627001](https://openairdocs.org/sdr/VNAA2026102627001.md): Control Unit · faulted · Oct 25, 2026 · N644NN · Cndair CL6002D24 · Trailing Edge Flap Control System
  > ERRONEOUS INDICATION DURING FLAPS TRAVEL AFTER A FLAPS OVERSPEED CONDITION. PULLED AND RE-RACKED SFECU 1 & 2 IAW AMM 27-51-05-000/400-801-A01. CLEARED INHIBITS IAW AMM 45-45-00-970-821-A01. PERFORMED SELF TEST OF THE SFECU'S IAW AMM 27-51-05-740-801-A01. PER
- [SDR REXA202601998](https://openairdocs.org/sdr/REXA202601998.md): Lamp · inoperative · Oct 22, 2026 · N600LR · Cndair CL6002D24 · Emergency Lighting
  > ENTRANCE EMERGENCY EXIT-LIGHT LAMPS INOP R/R ENTRANCE EMERGENCY EXIT-LIGHT LAMPS IAW AMM 33-51-05 OPS TEST GOOD PN OFF/ON: OL-3071BPE/GPL
- [SDR REXA2026102601999](https://openairdocs.org/sdr/REXA2026102601999.md): Wire Harness · inoperative · Oct 20, 2026 · N131EV · Cndair CL6002D24 · Landing Gear System Wiring
  > SHORTLY AFTER TAKEOFF, RECEIVED A BRAKE OVHT WARNING MESSAGE. COMPLETED QRH,TEMPERATURE SPIKED AGAIN. RECEIVED BRAKE OVHT WARNING AGAIN. COORDINATED WITH MOC AND DISPATCH. AIR RETURN TO RDU. DEFERRED LHIB BTMS (TEMP SENSOR) IAW MEL 32-46-1D. PLACARD INSTALLED
- [SDR REXA2026102001948](https://openairdocs.org/sdr/REXA2026102001948.md): Window Post · cracked · Oct 19, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > RT WINDOW SUPPORT STRAP OF THE WINDOW POST FOUND CRACKED. REPLACED RT WINDOW STRAP SUPPORT POST.
- [SDR VNAA2026102126801](https://openairdocs.org/sdr/VNAA2026102126801.md): Actuator · tripped · Oct 18, 2026 · N547NN · Cndair CL6002D24 · Trailing Edge Flap Actuator
  > FLAPS FAIL MSG DURING CRUISE, RAN QRH AND FLAPS DID NOT EXTEND PAST FLAPS 1 POSITION C/A REPLACED #4 FLAP ACTUATOR.
- [SDR SWIA2026101877759](https://openairdocs.org/sdr/SWIA2026101877759.md): None · none · Oct 18, 2026 · N246LR · Cndair CL6002D24 · Standard Practices/Structures
  > SMELL OF SMOKE IN FWD CABIN, SMOKE ALARM WENT OFF IN FWD LAV FOR 60 SECONDS, RECEIVED SMOKE LAV WARNING MESSAGE. FLIGHT 6355. ON ARRIVAL, INSPECTED FWD LAV FOR ANY SIGNS OF BURNED WIRING, LIGHT BULBS OR ELECT ISSUES, NONE FOUND. OPERATED PACKS AND RAN BOT
- [SDR VNAA2026102026701](https://openairdocs.org/sdr/VNAA2026102026701.md): Fan · failed · Oct 17, 2026 · N574NN · Cndair CL6002D24 · Air Distribution Fan
  > EVACUATION FOR FUMES IN AIRCRAFT. C/W FIM 21-22-00-810-806-A01 AND 21-21-00-810-806-A01. CABIN FUMES APPEAR TO BE FROM ACTIVATION OF O2 GENERATORS. FLIGHT DECK FUMES APPEAR RELATED TO NR 2 DISPLAY FAN FAIL. REMOVED AND REPLACED DISPLAY COOLING FAN NR 2 IAW A
- [SDR VNAA2026101926602](https://openairdocs.org/sdr/VNAA2026101926602.md): Pdu · unserviceable · Oct 17, 2026 · N547NN · Cndair CL6002D24 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MSG DURING CRUISE C/A T/S B1 006551 IAW CRJ 900 FIM 27ˆ’52ˆ’09ˆ’810ˆ’802. REMOVED AND REPLACED FLAP PDU IAW CRJ 900 AMM 27€“52€“37€“000/400€“801. OPS TEST GOOD NO DEFECTS NOTED. NO FLAP HALF SPEED OR FLAP FAIL MSG.
- [SDR SWIA2026101577762](https://openairdocs.org/sdr/SWIA2026101577762.md): Not Reported · not reported · Oct 15, 2026 · N822SK · Cndair CL6002D24 · Standard Practices/Structures
  > COMPLY WITH REO 690-53-41-571 REV --. COMPLIED WITH ALL STEPS OF REO 690-53-41-571 REV -. COMPLETED COMPLIED WITH SKYWEST TASKCARD 51-900-1002-SKY
- [SDR VNAA2026100826402](https://openairdocs.org/sdr/VNAA2026100826402.md): Washer · disconnected · Oct 8, 2026 · N576NN · Cndair CL6002D24 · Emergency Exits
  > OVERHEAD BIN INTERFERES WITH L/H AFT OVERWING EMERGENCY EXIT DOOR OPENING / FOUND OVERHEAD BIN EYELET TO BE DISCONNECTED AT L/H AFT EMERGENCY DOOR. RECONNECTED EYELET IAW AMM 25-23-01-400-801-A50-PSA. OPS CHECKS GOOD AT THIS TIME.
- [SDR VNAA2026100826301](https://openairdocs.org/sdr/VNAA2026100826301.md): Fitting · gouged · Oct 5, 2026 · N643NN · Cndair CL6002D24 · Horizontal Stabilizer Miscellaneous Structure
  > TOOLING DAMAGE TO HSS UPPER FITTING ASSEMBLY, LEFT. PERFORMED ALL WORK USING STEPS AND DRAWINGS LISTED IN REO 690-55-11-235.
- [SDR REXA2026100601884](https://openairdocs.org/sdr/REXA2026100601884.md): Bulb · inoperative · Oct 4, 2026 · N302PQ · Cndair CL6002D24 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT BY PAX DOOR INOP. R & R LIGHT BULB IAW GOODRICH CMM 33-52-07. OPS. CHECK GOOD. P/N ON/OFF: 8GH002473-08

Next page: https://openairdocs.org/model/bombardier-cl-600-2d24/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 = 'CL6002D24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/bombardier-cl-600-2d24/reports

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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.