Bombardier CL-600-2D24

Service difficulty reports · 38,082

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duckdb -csv -c "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"

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SDR VNAA202610260034Fitting · corrodedAFTER BUSHINGS AND BEARINGS REMOTIONS, CORROSION ON LUGS L2, LH AILERON. LUG L2 AT LH AILERON WAS REPAIRED PER REO 670-57-61-237 REV -.Oct 26, 2026 · N554NN · Cndair CL6002D24 · AileronsSDR VNAA202610260033Fitting · corrodedCORROSION 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR VNAA202610260032Fitting · corrodedCORROSION 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR VNAA202610260031Fitting · corrodedCORROSION 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR VNAA202610260030Fitting · corrodedCORROSION FLOOR FITTING IN UNDER WASTE CONTAINER. FLOOR FITTING IN UNDER WASTE CONTAINER (PN: A414252-3) WAS REPLACED PER CMM 25-40-40.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR VNAA202610260029Lug · corrodedAFTER 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 -.Oct 26, 2026 · N554NN · Cndair CL6002D24 · AileronsSDR VNAA202610260028Hinge Fitting · corrodedCORROSION 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Door HingeSDR VNAA202610260027Skin · corrodedCORROSION 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"Oct 26, 2026 · N554NN · Cndair CL6002D24 · Wing, Plate/SkinSDR VNAA202610260026Stringer · corrodedCORROSION 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, EVALUATEOct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNAA202610260025Web · corrodedCORROSION 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202610260024Web · corrodedCORROSION 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNA2026F00013Web · corrodedCORROSION 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202610260023Seat Track · corrodedCORROSION 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 Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202610260022Seat Track · corrodedCORROSION 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 53-31-49-101-00Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202610260021Seat Track · corrodedCORROSION 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-Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202610260020Floorbeam · corrodedAFTER 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA202610260019Floorbeam · corrodedAFTER 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 51-42-21-001Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA202610260018Hinge Arm · corrodedCORROSION 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Door HingeSDR VNAA202610260017Seat Track · corrodedCORROSION 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202610260016Seat Track · corrodedCORROSION 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 IAOct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202610260015Seat Track · corrodedCORROSION 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202610260014Fitting · corrodedCORRODED 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202610260013Floor Support · corrodedCORROSION 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202610260012Seat Track · corrodedCORROSION 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 DOct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202610260011Door Frame · corrodedCORROSION 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA202610260010Drip Tray · corrodedCORROSION 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202610260009Clamp · corrodedCORROSION 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202610260008Support · corrodedCORROSION 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-AOct 26, 2026 · N554NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR VNAA202610260007Plate · corrodedCORROSION 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Wing Main, Frame StructureSDR VNAA202610260006Lug · corrodedAFTER BUSHINGS AND BEARINGS REMOVAL, CORROSION ON LUGS L2, LH AILERON. LUG L2 AT LT AILERON WAS REPAIRED IAW REO 670-57-61-237 REV -.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR VNAA202610260005Floor Support · crackedCRACKED 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 FLOOOct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202610260004Rib · crackedCRACKED 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR VNAA202610260003Web · crackedCRACK 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 -.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202610260002Cowl Door · wornELONGATED 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--.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR VNAA202610260001Lug · wornAFTER 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.Oct 26, 2026 · N554NN · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR SWIA2026102577794Seal · missingD 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 DEFOct 25, 2026 · N817SK · Cndair CL6002D24 · Air Intake Anti/De-Ice SystemSDR VNAA2026102627001Control Unit · faultedERRONEOUS 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. PEROct 25, 2026 · N644NN · Cndair CL6002D24 · Trailing Edge Flap Control SystemSDR REXA202601998Lamp · inoperativeENTRANCE 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/GPLOct 22, 2026 · N600LR · Cndair CL6002D24 · Emergency LightingSDR REXA2026102601999Wire Harness · inoperativeSHORTLY 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 INSTALLEDOct 20, 2026 · N131EV · Cndair CL6002D24 · Landing Gear System WiringSDR REXA2026102001948Window Post · crackedRT WINDOW SUPPORT STRAP OF THE WINDOW POST FOUND CRACKED. REPLACED RT WINDOW STRAP SUPPORT POST.Oct 19, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA2026102126801Actuator · trippedFLAPS FAIL MSG DURING CRUISE, RAN QRH AND FLAPS DID NOT EXTEND PAST FLAPS 1 POSITION C/A REPLACED #4 FLAP ACTUATOR.Oct 18, 2026 · N547NN · Cndair CL6002D24 · Trailing Edge Flap ActuatorSDR SWIA2026101877759None · noneSMELL 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 BOTOct 18, 2026 · N246LR · Cndair CL6002D24 · Standard Practices/StructuresSDR VNAA2026102026701Fan · failedEVACUATION 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 AOct 17, 2026 · N574NN · Cndair CL6002D24 · Air Distribution FanSDR VNAA2026101926602Pdu · unserviceableFLAPS 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.Oct 17, 2026 · N547NN · Cndair CL6002D24 · Trailing Edge Flap Control SystemSDR SWIA2026101577762Not Reported · not reportedCOMPLY 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-SKYOct 15, 2026 · N822SK · Cndair CL6002D24 · Standard Practices/StructuresSDR VNAA2026100826402Washer · disconnectedOVERHEAD 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.Oct 8, 2026 · N576NN · Cndair CL6002D24 · Emergency ExitsSDR VNAA2026100826301Fitting · gougedTOOLING DAMAGE TO HSS UPPER FITTING ASSEMBLY, LEFT. PERFORMED ALL WORK USING STEPS AND DRAWINGS LISTED IN REO 690-55-11-235.Oct 5, 2026 · N643NN · Cndair CL6002D24 · Horizontal Stabilizer Miscellaneous StructureSDR REXA2026100601884Bulb · inoperativeEXTERIOR EMERGENCY LIGHT BY PAX DOOR INOP. R & R LIGHT BULB IAW GOODRICH CMM 33-52-07. OPS. CHECK GOOD. P/N ON/OFF: 8GH002473-08Oct 4, 2026 · N302PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2026101601934Frame · corrodedAFTER CORROSION REMOVAL ON FRAME BS 794 FOUND OUT OF LIMITS. REPLACED THE FRAME IAW SRM 51-42-21-001-001-A01.Oct 3, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA2026100526201Target · missingGEAR DISAGREE ON CLIMB OUT C/A FOUND NLG PROX SENSOR TARGET MISSING. INSTALLED RH NLG CTR PROX SENSOR TARGET.Oct 3, 2026 · N635NN · Cndair CL6002D24 · Landing Gear Position and Warning
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