# Service difficulty reports: Canadair CL-600-2A12 A list on [Canadair CL-600-2A12](https://openairdocs.org/model/canadair-cl-600-2a12.md). Newest first. General aviation reporting is voluntary. Page 1 of 2 · 78 reports - [SDR 2021FA0000132](https://openairdocs.org/sdr/2021FA0000132.md): Flap Track · binding · Feb 19, 2021 · N601RC · Cndair CL6002A12 · Trailing Edge Flaps > FAILURE OF THE FLAPS AT 10 DEGREES. CORRECTIVE ACTION WAS LUBRICATION OF THE FLAP ACTUATORS IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUALS FOLLOWED BY AN OPERATIONAL CHECK - [SDR MXIA201902084](https://openairdocs.org/sdr/MXIA201902084.md): Switch · cracked · Feb 7, 2019 · N824DH · Cndair CL6002A12 · Landing Gear Position and Warning > DURING APPROACH, GEAR WAS SELECTED DOWN. NOSE GEAR GREEN LIGHT DID NOT COME ON & NOSE DOOR REMAINED OPEN. AS PER THE CHECKLIST THE GEAR WAS SELECTED UP, THE MAINS RETRACTED BUT THE NOSE DOOR REMAINED OPEN. GEAR WAS RE-SELECTED DOWN AND NORMAL GEAR DOWN INDICAT - [SDR 2017FA0000234](https://openairdocs.org/sdr/2017FA0000234.md): Tire · bulged · May 25, 2017 · N601RC · Cndair CL6002A12 · Tire > PRE-FLIGHT WALK AROUND REVEALED A SMALL BULGE IN THE NR 2 MAIN TIRE. THE BULGE WAS ONLY EVIDENT WHEN THAT SPECIFIC AREA OF THE TIRE WAS ON THE BOTTOM. THE BULGE WENT AWAY WHEN THE AIRCRAFT WAS ROLLED FORWARD. - [SDR 4DUA20170101](https://openairdocs.org/sdr/4DUA20170101.md): Flap System · failed · Jan 26, 2017 · N947KK · Cndair CL6002A12 · Trailing Edge Flap Control System > DURING THE FINAL APPROACH, A FLAPS FAIL LIGHT WHEN THE FLAPS WERE PLACED IN THE 45 DEGREE POSITION. CONTINUED TO AVIATE AND GET THE AIRCRAFT ON THE GROUND. REPORTED A LOSS OF 15-20 KTS DURING THE SHORT FINAL FLARE STAGE. THE LANDING PHASE BECAME UNSTABLE AN - [SDR 2016FA0000582](https://openairdocs.org/sdr/2016FA0000582.md): Dimmer · melted · Nov 28, 2016 · N601RC · Cndair CL6002A12 · Flight Compartment Lighting > FLIGHT CREW REPORTED A PORTION OF THE PILOTS INSTRUMENTATION BACK LIGHTING INOPERATIVE, TECHNICIAN REPLACED FAULTY INCANDESCENT LAMP DIMMER, VISUALLY INSPECTING FAULTY INCANDESCENT LAMP DIMMER REVEALED OUT PUT 7 1/2 AMP CIRCUIT BREAKER LV2 MELTED AND CIRCUIT B - [SDR 2016FA0000247](https://openairdocs.org/sdr/2016FA0000247.md): Tire · failed · May 17, 2016 · N601RC · Cndair CL6002A12 · Tire > RIGHT MAIN INBD TIRE HAS A PORTION OF THE TREAD THAT SEPARATED ON LANDING. NEW TIRE WAS INSTALLED AT WHEEL ASSY O/H. - [SDR 1KSA2015FA0000513](https://openairdocs.org/sdr/1KSA2015FA0000513.md): Skin · corroded · Oct 19, 2015 · N97SG · Cndair CL6002A12 · Fuselage Main, Plate/Skin > DURING ROUTINE MAINTENANCE FOUND CORROSION UNDER VHF ANTENNA AT FS 360, BL0 AND UNDER TRANSPONDER ANTENNA, FS 386, LBL4. - [SDR LOMA2015FA0000280](https://openairdocs.org/sdr/LOMA2015FA0000280.md): Warning Light · illuminated · Jun 13, 2015 · N807MM · Cndair CL6002A12 · Pneumatic System > RIGHT FUSELAGE BLEED WARNING CAME ON. - [SDR 3BOR20150605001](https://openairdocs.org/sdr/3BOR20150605001.md): Wire · melted · Jun 5, 2015 · N601PR · Cndair CL6002A12 · Electrical Power System Wiring > ELECTRICAL POWER WAS LOST DURING CRUISE FLIGHT. ACFT MADE AN UNSCHEDULED LANDING. VISUAL INSPECTION FOUND SEVERAL WIRES TO BE MELTED, SINGED AND/OR HEAT STRESSED, AND CIRCUIT BREAKERS TO BE SINGED AND/OR HEAT STRESSED IN CIRCUIT BREAKER PANEL CBP-A. ROOT CA - [SDR LOMA2014FA0000687](https://openairdocs.org/sdr/LOMA2014FA0000687.md): Loop · defective · Dec 4, 2014 · N807MM · Cndair CL6002A12 · Fire Protection System > RIGHT 10TH STAGE BLEED WARNING LIGHT CAME ON DURING DECENT. LANDED FOR REPAIR. REPLACED RT 10TH STAGE BLEED AIR WARNING LOOP A ELEMENT. - [SDR LOMA2014FA0000688](https://openairdocs.org/sdr/LOMA2014FA0000688.md): Valve · leaking · Nov 25, 2014 · N807MM · Cndair CL6002A12 · Pneumatic Distribution System > RIGHT 10TH STAGE WARNING LIGHT CAM ON DURING DECENT. - [SDR LOMA2015F00009](https://openairdocs.org/sdr/LOMA2015F00009.md): Shutoff Valve · leaking · Nov 18, 2014 · N807MM · Cndair CL6002A12 · Compressor Bleed Valve > RIGHT 10TH STAGE BLEED AIR WARNING ILLUMINATED. DIVERTED FOR REPAIR. REPLACED 10TH AND 14TH STAGE BLEED AIR SHUTOFF VALVES. - [SDR CA140606002](https://openairdocs.org/sdr/CA140606002.md): Control Cable · failed · Jun 5, 2014 · Cndair CL6002A12 · Elevator Tab Control System > (CAN) DURING AN 60 MONTH INSPECTION. THE TECH FOUND BY VISUAL CHECK UP, WHEN HE OPEN THE PANEL IN THE VERTICAL STABILIZER RT SIDE. - [SDR LOMA2014042500279](https://openairdocs.org/sdr/LOMA2014042500279.md): Detection Sys · false activation · Apr 22, 2014 · N807MM · Cndair CL6002A12 · Overheat Detection > RIGHT 10TH STAGE DUCT FAIL LIGHT ILLUMINATED DURING FLIGHT. TROUBLESHOT AND FOUND NO BLEED AIR LEAKS FROM RT 10TH STAGE MANIFOLD. FALSE INDICATION. REPLACED ALL OVERHEAT DETECTOR LOOPS FOR RT 10TH STAGE BLEED AIR LEAK DETECTION SYSTEM. - [SDR BQVA20130507001](https://openairdocs.org/sdr/BQVA20130507001.md): Support Angle · corroded · May 3, 2013 · N57MH · Cndair CL6002A12 · Passenger/Crew Doors > CABIN DOOR WAS REMOVED AND SENT TO REPAIR FACILITY FOR COMPLIANCE OF BOMBARDIER SERVICE BULLETIN 601-0613 R1. THE FOLLOWING ITEMS WERE FOUND WITH CORROSION DURING SERVICE BULLETIN COMPLIANCE: AFT SUPPORT ANGLE P/N 600-31902-65 LOWER END, ATTACH CLIP P/N 600- - [SDR 2012F00197](https://openairdocs.org/sdr/2012F00197.md): Water Heater · shorted · Sep 21, 2012 · N125PS · Cndair CL6002A12 · Potable Water System > ENROUTE, CABIN ATTENDANT DETECTED AND SAW SMOKE COMING FROM THE GALLEY AREA. CONFIRMED LOCATION OF SMOKE AND PULLED ALL CIRCUIT BREAKERS TO GALLEY AND CAPTAIN SHUTOFF ALL GALLEY AND CABIN POWER. DECLARED AN EMERGENCY AND LANDED. TROUBLESHOT AND INSPECTED, F - [SDR WWQA201209240001](https://openairdocs.org/sdr/WWQA201209240001.md): Water Heater · shorted · Sep 21, 2012 · N125PS · Cndair CL6002A12 · Water/Waste System Wiring > WHILE ENROUTE, THE CABIN ATTENDANT DETECTED AND SAW SMOKE COMING FROM THE GALLEY AREA. CAPTAIN HAD THE F/O GO BACK TO VERIFY & HELP LOCATE WHERE THE SMOKE WAS COMING FROM. ONCE CONFIRMED LOCATION OF SMOKE, HAD THE CABIN ATTENDANT PULL ALL CIRCUIT BREAKERS - [SDR 2012FA0000203](https://openairdocs.org/sdr/2012FA0000203.md): Controller · failed · Feb 14, 2012 · N275MT · Cndair CL6002A12 · Electrical Power System > AIRCRAFT ON RAMP, APU WAS SHUTDOWN AFTER RUNS AND ADG AUTOMATICALLY DEPLOYED. THIS OPERATION SHOULD NOT HAVE HAPPENED UNLESS ACFT IS IN THE AIR. TROUBLESHOOTING FOUND THE CONTROLLER FAILED. RECOMMENDED REPLACEMENT TO CUSTOMER AND THIS WAS ACCOMPLISHED. UNK - [SDR CA111102004](https://openairdocs.org/sdr/CA111102004.md): Seal · bent · Nov 1, 2011 · Cndair CL6002A12 · Ailerons > (CAN) HARD CHAFING CONDITION AND DAMAGED MOVING PART HAVE BEEN FOUND BY MX PERSONNEL WHILE PERFORMING POST FLIGHT CHECK FOLLOWING ACFT FIRST FLIGHT. RT AILERON OTBD LOWER L/E PANEL HAD SEVERELY COME INTO CONTACT WITH RT AILERON OTBD LOWER GAP SEAL. INTERFERE - [SDR 2011FA0000384](https://openairdocs.org/sdr/2011FA0000384.md): Selector · failed · Jun 17, 2011 · N601VH · Cndair CL6002A12 · Landing Gear Selector > LANDING GEAR DID NOT EXTEND NORMALLY. ALTERNATE EXTENSION USED SUCCESSFULLY FOR DOWN AND LOCKED. - [SDR CA110615007](https://openairdocs.org/sdr/CA110615007.md): Gps · malfunctioned · Jun 11, 2011 · Cndair CL6002A12 · Global Positioning System > APPROXIMATELY ONE HOUR AFTER TAKEOFF AND ENROUTE, CREW REPORTED BACK TO MX THAT BOTH GPS RECEIVERS HAD LOST THE SATELITE FIX AND HAD STARTED TO REACQUIRE. CREW ALTERED THEIR FLIGHT PATH TO RETURN AND APPROX 10 MINUTES LATER BOTH GPS HAD REACQUIRED THE SATELIT - [SDR CA110418006](https://openairdocs.org/sdr/CA110418006.md): Tube · chafed · Apr 18, 2011 · Cndair CL6002A12 · Aircraft Fuel Distribution System > (CAN) MOTIVE FLOW SENSE LINE, RT, T/O MAIN EJECTOR PRESSURE SWITCH CHAFED THROUGH UNDER AND BY CLAMP, PN 417-4. THE ANTI-CHAFE MATERIAL WAS IN PLACE ON THE CLAMP BUT IT WAS ALSO WORN THROUGH EXSPOSING THE METAL PORTION OF THE CLAMP TO THE TUBE. THIS CAUSED - [SDR CA120426011](https://openairdocs.org/sdr/CA120426011.md): Pin · misinstalled · Jan 12, 2011 · Cndair CL6002A12 · Nose/Tail Landing Gear > (CAN) THROUGH AN SRPSA, 58446, REPORTED DAMAGE TO THE ANTI-ROTATION TAB OF SIDE STAY FITTING 601-10374-1/-2. AFTER INVESTIGATION, SHAFT, 600-10237-5 WAS FOUND INSTALLED ON SIDE STAY FITTING 601-10374-1/-2 ON AC 3010 BY ERROR. - [SDR 2011F00005](https://openairdocs.org/sdr/2011F00005.md): Tire · failed · Dec 23, 2010 · N39CD · Cndair CL6002A12 · Tire > DURING LANDING, THE NR 2 TIRE TREAD SEPARATED FROM THE TIRE. THE TIRE STAYED INFLATED. WHEN THE TREAD SEPARATED, IT CUT THE NR 2 ANTI-SKID HARNESS IN HALF AND DAMAGED THE LT INBD FLAP BEYOND LIMITS. NO PROBLEMS EXISTED FROM THE HARNESS BEING CUT AS THE CREWS O - [SDR 2010FA0000201](https://openairdocs.org/sdr/2010FA0000201.md): Frame · cracked · Feb 5, 2010 · N500PG · Cndair CL6002A12 · Fuselage Main, Frame > FWD FUSELAGE FRAME AT FS235 ABOVE FLOOR, PILOTS AND COPILOTS SIDE, FOUND CRACKED. DURING 240 MONTH INSP. - [SDR 2010FA0000200](https://openairdocs.org/sdr/2010FA0000200.md): Frame · cracked · Feb 4, 2010 · N500PG · Cndair CL6002A12 · Fuselage Main, Frame > FWD FUSELAGE FRAME AT FS 235 ABOVE FLOOR, PILOTS AND COPILOTS SIDE, FOUND CRACKED DURING 240 MONTH INSP. - [SDR WWQ2007F00001](https://openairdocs.org/sdr/WWQ2007F00001.md): Wire Harness · shorted · Aug 5, 2007 · N39CD · Cndair CL6002A12 · Landing Gear System Wiring > DURING APPROACH, THE CREW EXTENDED THE LANDING GEAR (NORMAL PROCEDURE). SEVERAL SECONDS AFTER THE GEAR EXTENSION THE NOSE LANDING GEAR DOWN AND LOCKED GREEN LIGHT EXTINGUISHED AND THE NOSE GEAR DOORS OPENED AND CLOSED. A FEW SECONDS LATER THE DOORS CYCLED AG - [SDR 2007FA0000000](https://openairdocs.org/sdr/2007FA0000000.md): Engine · failed · Dec 1, 2006 · N388DB · Cndair CL6002A12 · Engine (Turbine/Turboprop) > RT ENGINE FAILURE AT T/O. ALL INDICATIONS WERE NORMAL ON ENGINE START AND TAXI. UPON THRUST ADVANCEMENT FOR TAKEOFF, AT APPROXIMATELY 60 PERCENT N1 WE HEARD AND FELT A COMPRESSOR STALL. THE THRUST LEVER WAS IMMEDIATELY RETARDED TO IDLE AND TEMPERATURES WERE NO - [SDR 2006FA0000949](https://openairdocs.org/sdr/2006FA0000949.md): Windshield · cracked · Sep 7, 2006 · N150MH · Cndair CL6002A12 · Flight Compartment Windows > LT WINDSHIELD (PILOTS) OUTER-PLY CRACKED DURING FLIGHT. NO KNOWN CAUSE AS TO THE EVENTS LEADING TO CRACK. KNOWN TO BE A COMMON FAILURE ON CHALLENGER ACRYLIC WINDSHIELD AND SIDE WINDOWS. WHETHER DUE TO IMPACT OF SOME SORTS OR WINDSHIELD NEAT FAILURE OR DELA - [SDR DJFA2005103](https://openairdocs.org/sdr/DJFA2005103.md): Relief Valve · leaking · May 30, 2005 · N633CW · Cndair CL6002A12 · Fuel Storage > SHORTLY AFTER T/O, TOWER REPORTED FUEL SPRAYING FROM RT WING. CREW VISUALLY VERIFIED, RETURNED AND LANDED WITHOUT INCIDENT. INSP FOUND FUEL LEAKING FROM RT WING VENT. WING FUEL PRESSURE RELIEF VALVE FOUND TO BE OPEN. EXTENDED REFUELING TEST WAS PERFORMED - [SDR DJFA2005086](https://openairdocs.org/sdr/DJFA2005086.md): Bulb · burned out · Apr 25, 2005 · N633CW · Cndair CL6002A12 · Landing Gear Position and Warning > CREW REPORTED THAT UPON GEAR EXTENSION THEY DID NOT RECEIVE THE NOSE GEAR DOOR INDICATION. A FLY-BY PAST THE TOWER WAS PERFORMED TO VERIFY NOSE GEAR POSITION. DOOR INDICATION WOULD NOT TEST, AND A MANUAL GEAR EXTENSION WAS PERFORMED. GREEN NOSE GEAR DOOR LI - [SDR 041251](https://openairdocs.org/sdr/041251.md): Clamp · broken · Apr 12, 2005 · N601RC · Cndair CL6002A12 · APU Bleed Air System > APU HAD BEEN RUNNING ON THE GROUND FOR APPROXIMATELY ONE HOUR AND SHUT ITSELF DOWN DUE TO HIGH OIL TEMP AS INDICATED BY (BYTE) LIGHT. VISUAL INSPECTION SHOWED THAT BLEED AIR ELBOW HAD BROKEN OFF OF EXHAUST STACK CLAMP AT THE WELD. RECOMMEND REGULAR VISUAL IN - [SDR N382005F00003](https://openairdocs.org/sdr/N382005F00003.md): Gcu · burned · Feb 16, 2005 · N163WG · Cndair CL6002A12 · Airborne Auxiliary Power Unit (APU) System > UPON AIRCRAFT TEST FLIGHT FOR COMPLETION OF TAWS INSTALLATION. AIRCRAFT EXPERIENCED SMOKE IN THE CABIN AND COCKPIT. CREW DECLARED AND EMERGENCY LANDING AND PERFORMED AN UNEVENTFUL LANDING, USING NORMAL PUBLISHED EMERGENCY PROCEDURE. TROUBLESHOOTING FOUND TH - [SDR 2004F00032](https://openairdocs.org/sdr/2004F00032.md): Windshield · cracked · Nov 25, 2003 · N163WG · Cndair CL6002A12 · Flight Compartment Windows > LEFT WINDSHIELD FAILED IN FLIGHT, OUTER PANE CRACKED AND SEPARATED. CREW FOLLOWED CHECKLIST PROCEDRUES AND LANDED AT A SUITABLE AIRFIELD. (M) - [SDR N382003F00001](https://openairdocs.org/sdr/N382003F00001.md): Fuel Control · failed · Aug 1, 2003 · N163WG · Cndair CL6002A12 · Fuel Control/Turbine Engines > AT APPROXIMATELY 0650 PACIFIC TIME, WHILE ON CLIMB OUT AND CLIMBING THROUGH 5500 FT MSL THE AIRCRAFT EXPERIENCED AN UNCOMMANDED SHUTDOWN OF THE LEFT ENGINE. ALL CHECKLISTS AND PROCEDURES WERE FOLLOWED. AN EMERGENCY WAS DECLARED, AND AN UNEVENTFUL LANDING WAS - [SDR SH52003F00000](https://openairdocs.org/sdr/SH52003F00000.md): Fuel Control · inoperative · Feb 14, 2003 · N500PG · Cndair CL6002A12 · Fuel Control/Turbine Engines > AIRCRAFT WAS HOLDING ON TAXIWAY WITH WINDS OVER 40 KNOTS AND BLOWING SNOW. A/C WAS BEHIND A/C WHICH WAS KICKING UP ADDITIONAL SNOW. PILOT PUT ON THE COWL ANTI-ICE. APPROXIMATELY ONE MINUTE LATER THE RIGHT ENGINE SHUTDOWN UNCOMMANDED, AIRCRAFT RETURNED TO HA - [SDR SH52002F00000](https://openairdocs.org/sdr/SH52002F00000.md): Sill · cracked · Jan 9, 2002 · N711SX · Cndair CL6002A12 · Fuselage Main, Structure > DURING SCHEDULED INSPECTION FOUND LOWER WINDSHIELD SILL CRACKED (PRIMARY STRUCTURE) ON LEFT AND RIGHT SIDE OF COCKPIT. BOTH CRACKS ARE AT FS 235.0 WL 110.5 AND RUN ALONG THE BASE OF A WEB LEFT CRACK IS 1.5 INCHES LONG, RIGHT IS 1.0 INCH LONG. CRACKS IN THIS - [SDR QXEA0101591](https://openairdocs.org/sdr/QXEA0101591.md): Seal · dented · Sep 25, 2001 · N606QX · Cndair CL6002A12 · Passenger/Crew Doors > PDX - MAIN CABIN DOOR SEAL MATING SURFACE IS DENTED MIDWAY ALONG THE FORWARD LENGTH OF DOOR APERATURE. REPAIRED IAW EA R-53-03. - [SDR CA010912014](https://openairdocs.org/sdr/CA010912014.md): Handle · broken · Sep 9, 2001 · Cndair CL6002A12 · Service Doors > (CAN) THE RAMP PERSONNEL BROKE THE OUTER HANDLE OF THE SERVICE DOOR DURING NORMAL OPERATION. THE PERSON WORKING REPORTED THAT HE DID NOT USED ANY EXCESSIVE FORCE TO OPEN THE DOOR. THE MAINTENANCE REPLACED THE OUTER HANDLE ON THE SERVICE DOOR. - [SDR CA010501008](https://openairdocs.org/sdr/CA010501008.md): Windshield · cracked · Apr 16, 2001 · Cndair CL6002A12 · Flight Compartment Windows > (CAN) R/H WINDSHIELD CRACKED WHILE ON APPROACH. MAINTENANCE REMOVED AND REPLACED RT WINDSHIELD WITH NEW UNIT. AIRCRFT BACK IN SERVICE. - [SDR CA000720014](https://openairdocs.org/sdr/CA000720014.md): Battery · wrong part · Jun 20, 2000 · Cndair CL6002A12 · Emergency Locator Beacon > (CAN) UPON ELT RECERTIFICATION, A NON TC APPROVED BATTERY WAS FOUND IN THE UNIT.ONLY THE DM U158-1 IS APPROVED BY TC (REF AWN BO14, EDITION 4) FOR USE IN THIS ELT. CORRECT BATTERY WAS INSTALLED AND ELT RECERTIFIED.SUP - [SDR 20000620SH027](https://openairdocs.org/sdr/20000620SH027.md): Potentiometer · failed · May 25, 2000 · N601AA · Cndair CL6002A12 · Flight Compartment Lighting > A DIMMER POT (R3LM) WAS FOUND BURNT AND MELTED AFTER IT WAS REPORTED THE NR 1 F/D WAS TRIPPING THE CIRCUIT BREAKER ON THE DC ESSENTIAL BUSS. THE POT IS PART OF THE PILOTS LIGHTING CONTROL PANEL. (X) - [SDR CA000519016](https://openairdocs.org/sdr/CA000519016.md): Actuator · failed · May 15, 2000 · Cndair CL6002A12 · Stabilizer Actuator > (CAN) WHILE TAXING TO RAMP PILOT MOVED STAB TRIM TO NOSE DOWN POSITION. CHANNEL 1 NOSE DOWN FAIL LIGHT CAME ON AND ACT WOULD NOT MOVE. MAINT CHANGED PITCH TRIM ACTUATOR AND RETURNED A/C TO SERVICE. - [SDR 20000503SH050](https://openairdocs.org/sdr/20000503SH050.md): Window Post · cracked · Apr 13, 2000 · N608CW · Cndair CL6002A12 · Passenger Compartment Windows > DURING THE ACCOMPLISHMENT OF THE AIRCRAFT MANUFACTURER''S REQUIRED 6,600 HOUR CHECKS, A CRACK WAS NOTED ON THE UPPER SURFACE OF THE WINDSCREEN LOWER SILL FRAME AT BS 235 LEFT. THE CRACK WAS NOTED DURING INSPECTION WHICH WAS ACCOMPLISHED AT TT: 6,552.2 HOURS. - [SDR 20000424SH011](https://openairdocs.org/sdr/20000424SH011.md): Heater · inoperative · Mar 15, 2000 · N651CW · Cndair CL6002A12 · Windshield/Door Rain/Ice Removal > PILOT''S LEFT FRONT WINDSHIELD HEAT ELEMENT INOPERATIVE. (X) - [SDR 2000ZZZX109](https://openairdocs.org/sdr/2000ZZZX109.md): Cover · cracked · Dec 10, 1999 · N998JR · Cndair CL6002A12 · Engine Cowling System > THE LEFT NOSE COWL AIRLINE COVER (POCKET) FOR THE 14TH STAGE T/R PDU LINE SHOWS SIGNS OF HEAT DAMAGE AND IS BUCKLED AND CRACKED. - [SDR CA991209046](https://openairdocs.org/sdr/CA991209046.md): Actuator · failed · Nov 13, 1999 · Cndair CL6002A12 · Trailing Edge Flap Actuator > (CAN) OCCASIONALLY FLAPS FAILED IN COLD WEATHER. NR 3 ACTUATOR REPLACED AND PROBLEM WENT AWAY. - [SDR CA991028064](https://openairdocs.org/sdr/CA991028064.md): Brake · failed · Oct 7, 1999 · Cndair CL6002A12 · Brake > (CAN) TECHNICIAN NOTICED THE RIGHT OUTBOARD MAIN WHEEL WAS FLAT. THE FUSE PLUG WAS FOUND MELTED AS WELL AS A LOCALIZED WEAR (FLAT SPOT) ON THE TIRE. IT WAS NOTICED THAT THE WHEEL HAD OVERHEATED AND SUFFERED PREMATURE WEAR CAUSED BY THE BRAKE WHICH WAS STUCK O - [SDR CA990521046](https://openairdocs.org/sdr/CA990521046.md): Engine · making metal · May 13, 1999 · Cndair CL6002A12 · Engine (Turbine/Turboprop) > (CAN) AT 7,000 FEET, A SHEARING NOISE WAS HEARD FROM NR 2 ENGINE. THE ENGINE WAS SHUT DOWN. POST-FLIGHT INSPECTION FOUND METAL IN THE MAIN OIL FILTER AND CHIP DETECTOR. THE ENGINE WAS REMOVED AND SENT FOR INVESTIGAITON. - [SDR CA990226006](https://openairdocs.org/sdr/CA990226006.md): Pump · malfunctioned · Feb 2, 1999 · Cndair CL6002A12 · Turbine Engine Oil System > (CAN) NR 2 ENGINE LOW OIL PRESSURE LIGHT IN-FLIGHT. POST-FLIGHT INSPECTION FOUND THE NR 2 ENGINE OIL PUMP WAS INOPERATIVE. Next page: https://openairdocs.org/model/canadair-cl-600-2a12/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 = 'CL6002A12' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/canadair-cl-600-2a12/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.