# Service difficulty reports: Bombardier CL-600-2B16

A list on [Bombardier CL-600-2B16](https://openairdocs.org/model/bombardier-cl-600-2b16.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 21 · 1,014 reports

- [SDR 2026FA0000908](https://openairdocs.org/sdr/2026FA0000908.md): Controller · faulted · Oct 19, 2026 · N548BA · Cndair CL6002B16 · Trailing Edge Flap Control System
  > IN AIR ON FINAL APPROACH TO LAND, THE AUTO THROTTLES DISENGAGED AFTER SELECTING FLAPS 30. WHEN SELECTING FLAPS 30, THE FLAP DETENT FELT LIKE IT HAD SOME PLAY TO IT (ALMOST LIKE THERE WERE MULTIPLE DETENTS FOR FLAPS 30.) FLAPS DID NOT MOVE BEYOND PREVIOUS SETTI
- [SDR DXTA2026101910188](https://openairdocs.org/sdr/DXTA2026101910188.md): Handle · false indication · Oct 15, 2026 · N217QS · Cndair CL6002B16 · Passenger/Crew Doors
  > PAX DOOR OUT HANDLE ILLUMINATED DURING FLIGHT MOMENTARILY, THIS WAS ASSOCIATED WITH A FAILURE OF THE AUTOMATIC PRESSURIZATION. THE CAS MESSAGE DID EXTINGUISH, BUT RETURNED AFTER LANDING WHILE IN THE GROUND. PERFORMED AN OPERATIONAL TEST OF THE PASSENGER DOOR
- [SDR DXTA2026101510168](https://openairdocs.org/sdr/DXTA2026101510168.md): O-Ring · defective · Oct 13, 2026 · N268QS · Cndair CL6002B16 · Hydraulic System, Main
  > IN CRUISE FLIGHT AT FL310 HYD 3 LO PRESS CAS ILLUMINATED. SYSTEM SHOWED 2% QUANITY AND 0 PSI. EMERGENCY DECLARED AND DIVERTED TO DJT. ACCOMPLISHED HYD 3 LO PRESS QRH AND MANUAL GEAR EXTENSION QRH PROCEDURES. AFTER MANUAL GEAR EXTENSION, A GEAR DISAGREE MESSAGE
- [SDR DXTA2026101410128](https://openairdocs.org/sdr/DXTA2026101410128.md): Door Seal · leaking · Oct 10, 2026 · N204QS · Cndair CL6002B16 · Passenger/Crew Doors
  > DESCENDING THROUGH 3500 FEET, LOUD CABIN, HISSING SOUND STARTED FROM MAIN CABIN DOOR. FLIGHT ATTENDANT SAID NOISE WAS VERY VERY LOUD NO INITIAL INDICATIONS ON RATES OR ALTITUDE OSCILLATIONS ON BASE LEG AT 2000 FT, NOTICED RATE WAS DESCENDING AT 700 FPM APP
- [SDR DXTA2026100910068](https://openairdocs.org/sdr/DXTA2026100910068.md): Seal · leaking · Oct 6, 2026 · N246QS · Cndair CL6002B16 · Passenger/Crew Doors
  > FROM COCKPIT THERE IS A LOUD RUSHING AIR NOISE COMING FROM MAIN CABIN DOOR. THE FAS, WHEN ASKED, STATED THAT ALONG WITH THE AIR NOISE THEY ALSO HEARD IT AS A HIGH PITCHED SQUEAL. NOISE BECAME EVIDENT CLIMBING THROUGH APPROX 4000-5000' AND CONTINUED THROUGHOUT
- [SDR DXTA2026092209794](https://openairdocs.org/sdr/DXTA2026092209794.md): Adc · defective · Sep 19, 2026 · N268QS · Cndair CL6002B16 · Air Data Computer
  > TWICE DURING FLIGHT (ONCE ON CLIMB OUT AND ONCE ON DESCENT), LEFT PILOT LOST ALL AIRSPEED, ALTITUDE AND VERTICAL SPEED INDICATIONS, WITH ASSOCIATED RED FLAGS, LOSS OF AUTOPILOT, LOSS OF AUTO THROTTLE, AND MACH TRIM FAIL. DURING THE SECOND EVENT (ON DESCENT AT
- [SDR DXTA2026091509704](https://openairdocs.org/sdr/DXTA2026091509704.md): Door · worn · Sep 14, 2026 · N248QS · Cndair CL6002B16 · Passenger/Crew Doors
  > MAIN CABIN DOOR -UNABLE TO OPEN MAIN CABIN DOOR. FO ENTERED THROUGH CARGO DOOR TO ATTEMPT OPENING FROM INSIDE. MCC, TECHS WERE ABLE TO GET THE PAX DOOR OPEN. PERFORMED MULTIPLE OPS CHKS & UNABLE TO DUPLICATE THE ORIGINAL ISSUE. GAINED ACCESS TO INSIDE OF DO
- [SDR DXTA2026091409705](https://openairdocs.org/sdr/DXTA2026091409705.md): Unknown · odor · Sep 14, 2026 · N259QS · Cndair CL6002B16 · Air Distribution System
  > IN THE DESCENT, THE FA SITTING ON SEAT 9 NOTICED A BURNING SMELL COMING FROM THE BACK OF THE CABIN. NO SMOKE WAS PRESENT. PERFORMED TORQUE CHECK ON PAX COOLING TURBINE IAW MM 21-51-00, CHECKED GOOD. R & R SOCK ON PAX SIDE ACM IAW MM 21-51-13 (OLD/NEW PN: 1808
- [SDR DXTA2026091509695](https://openairdocs.org/sdr/DXTA2026091509695.md): Engine · faulted · Sep 13, 2026 · N200QS · Cndair CL6002B16 · Engine (Turbine/Turboprop)
  > DURING LT ENGINE START, TECHNICIANS ENCOUNTERED A RAPID INCREASE IN ITT AND THE FIRE WATCH NOTIFIED THEM OF VISIBLE FIRE. THE CHECKLIST WAS USED AND THE ENGINE FIRE BOTTLE WAS DISCHARGED. REMOVED CUSTOMERS LEFT ENGINE INSTALLED REPAIRED ENGINE. WORKED PE
- [SDR DXTA2026091409666](https://openairdocs.org/sdr/DXTA2026091409666.md): Fcu · illuminated · Sep 11, 2026 · N248QS · Cndair CL6002B16 · Trailing Edge Flap Control System
  > SELECTING FLAPS 45. FLAP FAIL CAS MESSAGE. FLAPS STUCK AT 30. FLAPS WILL NOT EXTEND OR RETRACT. REMOVED FAULTY FCU. INSTALLED REPAIRED UNIT P/N 8-341-06, S/N D860. PERFORMED ALL OPERATIONAL CHECKS WITH NO DISCREPANCIES. ALL WORK DONE WITH REFERENCE C650-AM
- [SDR DXTA2026091409670](https://openairdocs.org/sdr/DXTA2026091409670.md): Seal · leaking · Sep 11, 2026 · N253QS · Cndair CL6002B16 · Passenger/Crew Doors
  > DURING CLIMB AND DESCENT BELOW 10000 FT WE CAN HEAR LOUD WIND/SUCTION NOISE COMING FROM MAIN CABIN DOOR. CABIN DIF/RATE SHOWED NORMAL VALUES. VERIFIED CREW SQUAWK. TECHS REMOVED FAULTY MAIN CABIN DOOR SEAL AND REPLACED WITH CUSTOMER PROVIDED NEW ASSY. IAW AMM
- [SDR DXTA2026090809569](https://openairdocs.org/sdr/DXTA2026090809569.md): Gas Spring · out of adjust · Sep 5, 2026 · N215QS · Cndair CL6002B16 · Passenger/Crew Doors
  > AFTER FLIGHT MAIN ENTRY DOOR DIFFICULT TO OPEN AND IS VERY JERKY AS IT LOWERS AND STOPS AT TIMES. ADJUSTED THE FWD AND AFT MAIN DOOR GAS SPRINGS IAW AMM 52-11-31. PERFORMED A SATISFACTORY FUNCTIONAL TEST OF THE MAIN DOOR GAS SPRINGS AND OPS CHECK OF PASSNEGE
- [SDR DXTA2026081409247](https://openairdocs.org/sdr/DXTA2026081409247.md): Idg · failed · Aug 11, 2026 · N228QS · Cndair CL6002B16 · AC Generator-Alternator
  > ON DESCENT, "GEN 2 OFF" CAS MESSAGE DISPLAYED. WE RAN THE QRH AND WERE UNABLE TO GET THE GENERATOR TO COME BACK ONLINE. WHEN THE GEN WENT OFFLINE IT TRIPPED OFF THE STAB TRIM CH1 AND MACH TRIM. THE "AP PITCH TRIM" AND NOSE DOWN TRIM CAS MESSAGES DISPLAYED. THE
- [SDR DXTA2026081209220](https://openairdocs.org/sdr/DXTA2026081209220.md): Controller · faulty · Aug 10, 2026 · N219QS · Cndair CL6002B16 · Brake Anti-Skid Section
  > A SKID OTBD AMBER CASS MESSAGE CAME ON DURING LANDING PHASE. RAN QRH, DIVERTED TO KBED. REMOVED AND REPLACED ANTI-SKID CONTROLLER IAW AMM 32-44-04. OPS CHKS FOUND NORMAL.
- [SDR DXTA2026081009227](https://openairdocs.org/sdr/DXTA2026081009227.md): Module · faulted · Aug 7, 2026 · N261QS · Cndair CL6002B16 · Cabin Pressure Control System
  > AFTER TAKEOFF THE AIRCRAFT WOULD NOT PRESSURIZE. WE USED QRH (CABIN ALT) FOR GUIDANCE, AND TRIED MANUAL MODE AND THE AIRCRAFT STILL WOULD NOT PRESSURIZE. REPLACED DEFECTIVE CABIN PRESSURE CONTROLLER IAW AMM 21-31-13-400-801, NO DEFECTS NOTED. REPLACED DEFECTI
- [SDR DXTA2026081009190](https://openairdocs.org/sdr/DXTA2026081009190.md): Sensor · faulted · Aug 7, 2026 · N234QS · Cndair CL6002B16 · Fuel Quantity Sensor
  > INFLIGHT AT CRUISE WE NOTICED THAT THE TAIL TANK FUEL WAS NOT TRANSFERRING. SHORTLY THERE AFTER WE RECEIVED TAIL XFER SOV OPEN FOLLOWED BY AUTO TAIL XFER CAS MESSAGES. WE FOLLOWED QRH PROCEDURE FOR TAIL XFER SOV OPEN AND WERE ABLE TO MANUALLY TRANSFER THE TAIL
- [SDR DXTA2026080709146](https://openairdocs.org/sdr/DXTA2026080709146.md): Indication Sys · malfunctioned · Aug 4, 2026 · N263QS · Cndair CL6002B16 · Central Warning
  > CLIMBING THROUGH FL370 - FL390, POWER SWITCHED FROM CLB TO MCT ON ITS OWN. SHORTLY AFTER RECEIVED A LT ENG CAUTION & LT N2 WENT TO 0. ALL OTHER ENG PARAMETERS NORMAL. AFTER A COUPLE OF SECS, CAUTION DISAPPEAR & N2 WOULD RETURN TO NORMAL. IT DID THIS REPETEDLY
- [SDR DXTA2026080609121](https://openairdocs.org/sdr/DXTA2026080609121.md): Smoke Detector · defective · Aug 2, 2026 · N253QS · Cndair CL6002B16 · Smoke Detection
  > RED CAS SMOKE TOILET LIGHT STAYED ON DURING FLGHT NO SMOKE OR FUMES DETECTED CORRECTIVE ACTION: REPLACED SMOKE DETECTOR. OPS CHECK GOOD. IAW CL650 SMM 26-14-01
- [SDR DXTA2026072709024](https://openairdocs.org/sdr/DXTA2026072709024.md): Trim System · failed · Jul 25, 2026 · N244QS · Cndair CL6002B16 · Flight Control System
  > AT CRUISE FL380 BOTH STAB TRIM FAILED AT 2.2 FOLLOWED BY MACH TRIM. RAN CHECKLIST AND DID NOT CLEAR.
- [SDR DXTA2026072708997](https://openairdocs.org/sdr/DXTA2026072708997.md): Warning Message · illuminated · Jul 25, 2026 · N244QS · Cndair CL6002B16 · Flight Control System
  > AT CRUISE FL380 BOTH STAB TRIM FAILED AT 2.2 FOLLOWED BY MACH TRIM. RAN CHECKLIST AND DID NOT CLEAR.
- [SDR DXTA2026071708818](https://openairdocs.org/sdr/DXTA2026071708818.md): Wire · damaged · Jul 14, 2026 · N258QS · Cndair CL6002B16 · Electrical Power System Wiring
  > DURING POST FLIGHT WHILE COMPLETING MAINTENANCE WRITE UP, COPILOT WENT TO OPEN FLIGHT ATTENDANT CONTROL PANEL TO COLLAR A BREAKER AND NOTICED SMOKE COMING OUT OF THE TOP OF CIRCUIT BREAKER PANEL. NOTHING WAS TOUCHED ON THE PANEL. COPILOT & FLIGHT ATTENDANT CA
- [SDR DXTA2026071508812](https://openairdocs.org/sdr/DXTA2026071508812.md): Warning System · malfunctioned · Jul 13, 2026 · N225QS · Cndair CL6002B16 · Door Warning System
  > REQUIRES MULTIPLE ATTEMPTS WHEN SHUTTING MAIN CABIN DOOR TO GET RED "PASSENGER DOOR" EICAS MSG TO EXTINGUISH, EVEN THOUGH ALL GREEN FLAGS ARE VISIBLE AND EXTERIOR HANDLE AND VENT FLAP ARE CONFIRMED FLUSH. PERFORMED OPERATIONAL TEST OF THE PASSENGER DOOR, OPS
- [SDR DXTA2026071408811](https://openairdocs.org/sdr/DXTA2026071408811.md): Handle · no discrepancy · Jul 13, 2026 · N211QS · Cndair CL6002B16 · Passenger/Crew Doors
  > MAIN DOOR WILL NOT OPEN. HANDLE STAYS FLUSH WITH DOOR. CYCLED MAIN ENTRY DOOR HANDLE KEY LOCK. COMPLETED SEVERAL SATISFACTORY OPENING AND CLOSINGS OF THE MAIN ENTRY DOOR FROM EXTERIOR AND INTERIOR OF THE AIRCRAFT. IAW AMM 52-11-00.
- [SDR DXTA2026070908711](https://openairdocs.org/sdr/DXTA2026070908711.md): Control Panel · faulted · Jul 6, 2026 · N253QS · Cndair CL6002B16 · Cabin Pressure Control System
  > IMMEDIATELY AFTER TAKEOFF, NOTICED AIRCRAFT WAS NOT PRESSURIZING IN AUTO MODE. CLIMBED TO 5000' AND RAN MANUAL PRESSURIZATION QRH WITH NEGATIVE RESULTS. REMOVED AND REPLACED CABIN PRESSURIZATION PANEL WITH A NEW CUSTOMER SUPPLIED UNIT, OPS CHECK SATISFACTORY.
- [SDR DXTA2026070608660](https://openairdocs.org/sdr/DXTA2026070608660.md): Handle · lack of lube · Jul 3, 2026 · N261QS · Cndair CL6002B16 · Passenger/Crew Doors
  > UPON CLIMB OUT THE CABIN WAS NOT PRESSURIZING (REPEAT WRITE UP) AND THERE WAS SIGNIFICANT AIRFLOW THRU THE MAIN CABIN DOOR. AFTER WE LEVELED AT 5000FT FOR AWHILE THE DOOR SEAL AIRFLOW DECREASED AND THE CABIN BEGAN TO PRESSURIZE. WHILE PERFORMING OTHER MAINTENA
- [SDR DXTA2026061808476](https://openairdocs.org/sdr/DXTA2026061808476.md): Battery · inoperative · Jun 16, 2026 · N211QS · Cndair CL6002B16 · Emergency Lighting
  > EMERGENCY SIGN ABOVE MAIN CABIN DOOR INOP. REPEAT WRITE UP CORRECTIVE ACTION: REMOVED EMER POWER SUPPLY AND INSTALLED CUSTOMER SUPPLIED EMER POWER SUPPLY.WORKED IAW SMM 33-51-05. PERFORMED SATISFACTORY OPS CHECKS OF THE EMER LIGHT SYSTEM IAW MM 33-51-00-710
- [SDR DXTA2026061708456](https://openairdocs.org/sdr/DXTA2026061708456.md): Handle · stuck · Jun 15, 2026 · N211QS · Cndair CL6002B16 · Passenger/Crew Doors
  > CLEARED SEAL AND TRIED TO OPEN DOORS SEVERAL TIMES SENT ME A MESSAGE THAT HE WAS UNABLE TO OPEN TRIED SEVERAL ATTEMPTS UNABLE TO OPEN DOOR HANDLE WAS OUT AND UNABLE TO TURN SEVERAL ATTEMPTS WAS ABLE TO RESET PLUNGER TO FLUSH POSITION CHECKED F
- [SDR DXTA2026061608457](https://openairdocs.org/sdr/DXTA2026061608457.md): Power Supply · no test · Jun 15, 2026 · N211QS · Cndair CL6002B16 · Emergency Lighting
  > WHEN DOING EMERGENCY LIGHTS TEST WE FOUND THAT THE EXIT SIGN OVER THE MAIN CABIN DOOR WILL NOT TURN ON. REPEAT WRITE UP. REMOVED EMERGENCY BATTERY AND INSTALLED CUSTOMER SUPPLIED OVERHAULED EMERGENCY BATTERY PERFORMED OPS CHECK OF EMERGENCY BATTERIES WITH NO
- [SDR DXTA2026061608441](https://openairdocs.org/sdr/DXTA2026061608441.md): Roller · contaminated · Jun 14, 2026 · N248QS · Cndair CL6002B16 · Passenger/Crew Doors
  > THE DOOR IS JAMMED AND WILL NOT OPEN OR LOCK. WENT IN THROUGH THE BAG DOOR AND TRIED TO OPEN IT. PERFORMED GENERAL VISUAL INSPECTION OF VENT PAX DOOR AND ASSOCIATED COMPONENTS AND FOUND ROLLERS CAKED IN GREASE AND DIRT. CLEANED AND RE-LUBE ROLLERS AS REQUIR
- [SDR DXTA2026061508444](https://openairdocs.org/sdr/DXTA2026061508444.md): Battery Pack · discharged · Jun 14, 2026 · N211QS · Cndair CL6002B16 · Emergency Lighting
  > WHEN DOING THE EMERGENCY LIGHT TEST WE FOUND THAT THE EXIT SIGN OVER THE MAIN ENTRANCE DOOR WILL NOT TURN ON. STARTED APU AND PLACED EMERGENCY LIGHT SWITCH IN ARM POSITION. ALLOWED 15 MINUTES FOR THE EMERGENCY LIGHTING BATTERY TO CHARGE. PERFORMED A SATISFAC
- [SDR DXTA2026061608430](https://openairdocs.org/sdr/DXTA2026061608430.md): Seal · leaking · Jun 13, 2026 · N245QS · Cndair CL6002B16 · Passenger/Crew Doors
  > MAIN DOOR WAS MAKING A LOUD NOISES ON APPROACH INTO MORRISTOWN. PASSENGERS AND FLIGHT ATTENDANT NOTICE IT. NO NOISE ON TAKEOFF. REMOVED MAIN CABIN ENTRY DOOR SEAL & INSTALLED NEW MAIN CABIN ENTRY DOOR SEAL IAW CL350 52-11-28. ALL OPS AND LEAK CHECKS GOOD.
- [SDR 3J7R0615202600001](https://openairdocs.org/sdr/3J7R0615202600001.md): Lamp · failed · Jun 13, 2026 · N217QS · Cndair CL6002B16 · Emergency Lighting
  > EXTERIOR WINDOW EMERGENCY EXTT LAMP WILL NOT ILLUMINATE.SINGLE LAMP IS AFT OF THE EMER WINDOW EXIT
- [SDR DXTA2026060108276](https://openairdocs.org/sdr/DXTA2026060108276.md): Sensor · defective · May 29, 2026 · N206QS · Cndair CL6002B16 · Trailing Flap Position Indicating System
  > WHILE CLIMBING THROUGH FL370 WE RECEIVED FLAP OVER SPEED CLACKER WITH ASSOCIATED VMO LIMIT MESSAGE ON ATS. FLAP AND GEAR INDICATIONS APPEARED ON MFD, BUT FLAPS WERE STILL AT 0. COMPLIED WITH QRC & QRH PROCEDURES. FLAP & GEAR INDICATIONS APPEARED & DISAPPEAR
- [SDR DXTA2026051908121](https://openairdocs.org/sdr/DXTA2026051908121.md): Coffeemaker · faulty · May 17, 2026 · N241QS · Cndair CL6002B16 · Buffet/Galleys
  > FA NOTICED WISPY SMOKE FROM COFFEE MAKER. FO GOT UP TO LOOK AND SMOKE WAS ALREADY GONE, WITH NO SMELL NOTICED. IT LASTED MAYBE 20-30 SECONDS. COFFEE MAKER WAS TURNED OFF AND FLIGHT CONTINUED UNEVENTFULLY. CORRECTIVE ACTION: REMOVED FAULTY GALLEY COFFEE MAKER P
- [SDR DXTA2026051808101](https://openairdocs.org/sdr/DXTA2026051808101.md): Counterbalance · out of adjust · May 15, 2026 · N217QS · Cndair CL6002B16 · Passenger/Crew Doors
  > MAIN CABIN DOOR VERY HARD TO CLOSE BY HAND AND DOOR DROPS FAST WHEN OPENING VERY HEAVY DOOR. NEEDS ADJUSTMENT PERFORMED ADJUSTEMENT OF THE MED COUNTERBALANCES IAW CL-650 AMM 52-11-31 PERFORMED FUNCTIONAL CHECK OF THE MED COUNTER BALANCES IAW CL-650 AMM 52-11
- [SDR 2026FA0000364](https://openairdocs.org/sdr/2026FA0000364.md): Windshield · failed · May 14, 2026 · N317RA · Cndair CL6002B16 · Flight Compartment Windows
  > LH WINDSHIELD SHATTERED DURING CLIMB PASSING THROUGH FL 280 AIRSPEED 280 KNTS. OATAPPROXIMATELY -34 DEGREES C. NO IMPACT OBSERVED TO CAUSE BREAK.
- [SDR 2026FA0000363](https://openairdocs.org/sdr/2026FA0000363.md): Windshield · failed · May 14, 2026 · N317RA · Cndair CL6002B16 · Flight Compartment Windows
  > LH WINDSHIELD SHATTERED DURING CLIMB PASSING THROUGH FL 280 AIRSPEED 280 KNTS. OAT APPROXIMATELY -34 DEGREES C. NO IMPACT OBSERVED TO CAUSE BREAK.
- [SDR DXTA2026051508060](https://openairdocs.org/sdr/DXTA2026051508060.md): Air Filter · dirty · May 12, 2026 · N238QS · Cndair CL6002B16 · Air Distribution System
  > WHEN TURNING APU BLEEDS ON, YOU GET A STRONG DIRTY SOCK SMELL FROM THE AIR. IT DISSIPATED WHEN USING ENGINE BLEEDS BUT CAME BACK ONCE WE WENT BACK TO APU BLEEDS. IT IS STRONGER ON THE GROUND VS INFLIGHT. CORRECTIVE ACTION: REMOVED BOTH L/H AND R/H FILTER SOC
- [SDR DXTA2026050807989](https://openairdocs.org/sdr/DXTA2026050807989.md): Acm · odor · May 7, 2026 · N213QS · Cndair CL6002B16 · Cabin Cooling System
  > AFTER LANDING A BURNING SMELL WAS NOTICED IN THE COCKPIT DURING TAXI. SEEMED TO BE COMING FROM MAIN GASPERS UP FRONT. UPON SHUTDOWN WE INSPECTED THE TIRES, THE NOSEBAY AVIONICS, THE AFT EQUIPMENT BAY FOR ANY SIGN OR SMELL. COULD NOT LOCATE. TURNED THE COCKPIT
- [SDR DXTA2026050607940](https://openairdocs.org/sdr/DXTA2026050607940.md): Circuit Breaker · damaged · May 4, 2026 · N264QS · Cndair CL6002B16 · Equipment/Furnishings Wiring
  > SMOKE & SPARKS COMING FROM BEHIND GALLERY CONTROL PANEL DURING TAXI OUT. APPEARS TO BE COMING FROM CABLE FROM THE DISPLAY TO THE CB PANEL. REMOVED DAMAGED CIRCUIT BREAKER INSTALLED CUSTOMER SUPPLIED NEW CIRCUIT BREAKER IAW SMM 24-03-03. REMOVED DAMAGED CIRCUI
- [SDR DXTA2026050707926](https://openairdocs.org/sdr/DXTA2026050707926.md): Pushrod · worn · May 3, 2026 · N209QS · Cndair CL6002B16 · Passenger/Crew Doors
  > WHILE DESCENDING BETWEEN 10000-8000FT A LOUD SOUND SIMILAR TO RUSHING AIR COULD BE HEARD FROM THE MAIN ENTRY DOOR. AT THE SAME TIME THE CABIN RATE DEPRESSURIZED AT A RATE OF 3200' DOWN UNTIL IT SETTLED AT A NORMAL RATE SHORTLY THEREAFTER (10SECS OR SO). THE FL
- [SDR DXTA2026050407877](https://openairdocs.org/sdr/DXTA2026050407877.md): Coalescer Bag · dirty · May 1, 2026 · N258QS · Cndair CL6002B16 · Humidity Control System
  > AFTER APU STARTUP AND SWITCHING FROM THE ENGINE BLEEDS TO THE APU BLEEDS A BURNING SMOKE SMELL WAS NOTED, BUT NO VISIBLE SMOKE IN THE COCKPIT NOR CABIN. AFTER LANDING A FAINT HINT AND TASTE OF SMOKE WAS NOTED IN THE AFT CABIN NEAR THE LAVATORY. THE BURNING S
- [SDR DXTA2026050407880](https://openairdocs.org/sdr/DXTA2026050407880.md): Coalescer Bag · dirty · May 1, 2026 · N228QS · Cndair CL6002B16 · Humidity Control System
  > ON INITIAL CLIMBOUT AN UNKNOWN ODOR/FUME BECAME PREVALENT IN BOTH THE COCKPIT AND THE CABIN. ALL CREWS EYES STARTED BURNING, NO SMOKE DETECTED OR OTHER CAS MESSAGES, ETC TO HELP DETERMINE ANY ISSUE. THE SMELL APPEARED TO BEGIN PERHAPS RIGHT AFTER THE APU WAS
- [SDR DXTA2026042907809](https://openairdocs.org/sdr/DXTA2026042907809.md): Support · faulted · Apr 26, 2026 · N256QS · Cndair CL6002B16 · Passenger/Crew Doors
  > WHEN OPENING MAIN DOOR, SUPPORT FOOT DID NOT EXTEND. ABLE TO EXTEND IT MANUALLY BY PULLING IT OUT. AFTER CLOSING THE DOOR FOOT REMAINED EXTENDED. REMOVED AND REPLACED DOOR SUPPORT FOOT ACTUATING ROD ASSEMBLY PER AMM 52-11-25-000-802, 52-11-25-400-801. OPS
- [SDR DXTA2026042707761](https://openairdocs.org/sdr/DXTA2026042707761.md): Guide · damaged · Apr 23, 2026 · N211QS · Cndair CL6002B16 · Passenger/Crew Doors
  > MAIN CABIN DOOR STRUT DID NOT EXTEND WHEN DOOR OPENED. REPLACED DAMAGED GUIDE RAIL TRACKS IAW SRM 51-42-08. OPS CHECK GOOD IAW 52-11-25-710-801
- [SDR 2026F00075](https://openairdocs.org/sdr/2026F00075.md): Windshield · broken · Apr 20, 2026 · N317RA · Cndair CL6002B16 · Flight Compartment Windows
  > LT WINDSHIELD BROKE DURING CLIMB PASSING THROUGH FL 280 AIRSPEED 280 KNTS. OAT APPROXIMATELY -34 DEGREES C. NO IMPACT OBSERVED TO CAUSE BREAK.
- [SDR FJ7A202605270001](https://openairdocs.org/sdr/FJ7A202605270001.md): Control Unit · intermittent · Apr 12, 2026 · N171AM · Cndair CL6002B16 · Stabilizer Control System
  > ON APRIL 12, 2025, WHILE AIRCRAFT N171AM WAS TAXIING FROM THE RAMP AT FORT LAUDERDALE EXECUTIVE AIRPORT (FXE), THE FLIGHT CREW OBSERVED AN EICAS MESSAGE INDICATING “STAB CH 2 INOP.” THE CREW ATTEMPTED TO RESET THE SYSTEM; HOWEVER, THE RESET WAS UNSUCCESSFUL. T
- [SDR DXTA2026040907560](https://openairdocs.org/sdr/DXTA2026040907560.md): Selector · faulted · Apr 6, 2026 · N253QS · Cndair CL6002B16 · Cabin Pressure Control System
  > ON DEPARTURE, AIRCRAFT FAILED TO PRESSURIZE. NO CONTROL OF PRESSURIZATION VIA AUTO OR MANUAL. DURING CLIMB AND DECENT HEARD AIR RUSHING NOISE FROM MAIN CABIN DOOR. AFTER LANDING NOTICED VENT DOOR FLAP LOOSE ON MAIN CABIN DOOR. REMOVED NEW SEAL IAW MM 52-11-2
- [SDR DXTA2026040707520](https://openairdocs.org/sdr/DXTA2026040707520.md): Cabin Pressure · malfunctioned · Apr 3, 2026 · N216QS · Cndair CL6002B16 · Cabin Pressure Control System
  > ON DEPARTURE, OUR AIRPLANE WAS NOT PRESSURIZING. WE CONTINUED TO CLIMB, AND AT ABOUT 3500 FEET. THE AIRPLANE STARTED TO RAPIDLY PRESSURIZE. WHEN IT HIT A NEGATIVE ALTITUDE, I SELECTED MANUAL, WITH THE RATE KNOB AT ZERO, AND THEN IT GOT VERY HOT IN THE COCKPIT,
- [SDR DXTA2026040307464](https://openairdocs.org/sdr/DXTA2026040307464.md): Actuator · defective · Mar 30, 2026 · N251QS · Cndair CL6002B16 · Passenger/Crew Doors
  > MAIN CABIN DOOR ON OPENING GETS REALLY HEAVY TO SLOW ITS MOMENTUM BEFORE IT TOUCHES THE GROUND. REPLACED DOOR ACTUATOR. OPS CHECK GOOD. IAW CL650 AMM 52-11-31.

Next page: https://openairdocs.org/model/bombardier-cl-600-2b16/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 = 'CL6002B16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/bombardier-cl-600-2b16/reports

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