# Service difficulty reports: Canadair CL-601-2A12

A list on [Canadair CL-601-2A12](https://openairdocs.org/model/canadair-cl-601-2a12.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 88 reports

- [SDR CA120928001](https://openairdocs.org/sdr/CA120928001.md): Heater · failed · Sep 21, 2012 · Cndair CL6012A12 · Water Line Anti-Ice System
  > (CAN) AFT GALLEY WATER TANK HEATING ELEMENT STAYED ON AND CAUSED THE SURROUNDING INSULATION BLANKET TO BURN AND CREATED SMOKE IN CABIN OF ACFT WHICH CAUSED A FLIGHT DIVERSION.
- [SDR CA101108005](https://openairdocs.org/sdr/CA101108005.md): Tire · failed · Nov 6, 2010 · Cndair CL6012A12 · Tire
  > (CAN) ON POST FLIGHT/DI INSPECTION (NEXT AM) NR 3 MAIN TIRE WAS FOUND TO BE DEFLATED AND ONE INNER RIB/STRIP OF RUBBER MISSING 3/4 AROUND TIRE. APPEARS TO HAVE SEPARATED CLEANLY FROM CARCASS SIGNS OF IMPACT ON TRAILING EDGE OF INBOARD FLAP AND FLAP SEAL AS WE
- [SDR DJFA2009006](https://openairdocs.org/sdr/DJFA2009006.md): Windscreen · cracked · Jan 27, 2009 · N664CW · Cndair CL6012A12 · Flight Compartment Windows
  > DURING CRUISE, CREW NOTED WHISTILING SOUNDS FROM THE LT WINDSCREEN. AFTER A BRIEF INSP, CREW NOTED (2) VERTICAL CRACKS SPANNING THE WINDSCREEN. AS THE ACFT BEGAN THE INITIAL DESCENT, THE CREW WITNESSED THE OUTER PLY OF THE WINDSCREEN DEPART THE ACFT. THE CR
- [SDR CA081016003](https://openairdocs.org/sdr/CA081016003.md): O-Ring · failed · Oct 10, 2008 · Cndair CL6012A12 · APU Engine Fuel and Control
  > (CAN) ACFT, PRIOR TO ENG START APU HAD AN UNCOMMANDED SHUTDOWN. WHILE CARRYING OUT COCKPIT TROUBLESHOOTING PILOTS OBSERVED APU BOOST PUMP FAIL LIGHT WAS ILLUMINATED. APU BOOST PUMP WAS SUSPECT BECAUSE IT HAD JUST BEEN CHANGED THE PREVIOUS DAY FOR SAME SNAG. BO
- [SDR CA080806007](https://openairdocs.org/sdr/CA080806007.md): Gearbox · defective · Aug 5, 2008 · Cndair CL6012A12 · Turbine Engine Accessory Drive
  > (CAN) DURING FLIGHT, CREW NOTICED THEY LOST THE NR1 ENGINE OIL INDICATION AND GOT THE RED LED. SHUTDOWN ENGINE AND MADE AN UNEVENTFUL LANDING. CREW NOTICED A PUDDLE OF OIL UNDER THE NR1 ENGINE AFTER LANDING. DURING THE TROUBLESHOOTING, THEY REMOVED THE DRAIN
- [SDR DJFA2008055](https://openairdocs.org/sdr/DJFA2008055.md): Heat Tape · burned · Jun 15, 2008 · N664CW · Cndair CL6012A12 · Air Distribution System
  > WHILE REFUELING THE AC, THE CREW NOTED A SIGNIFICANT AMOUNT OF SMOKE IN THE COCKPIT. OPEN (A)
- [SDR DJF2008F00004](https://openairdocs.org/sdr/DJF2008F00004.md): Unknown · smoke · Jun 15, 2008 · N664CW · Cndair CL6012A12 · Air Distribution System
  > WHILE REFUELING THE AC, THE CREW NOTED A SIGNIFICANT AMOUNT OF SMOKE IN THE COCKPIT. (SDR WILL BE COMPLETED AFTER MAINTENANCE/ INSPECTION IS COMPLETE). (K)
- [SDR CA080625008](https://openairdocs.org/sdr/CA080625008.md): Actuator · malfunctioned · Jun 12, 2008 · Cndair CL6012A12 · Stabilizer Actuator
  > (CAN) DURING A FLIGHT, PILOT REPORTED A PITCH TRIM CHANNEL NR1 INOP LIGHT ON. TROUBLESHOOT THE TRIM SYS AND FOUND NR1 TRIM ACTUATOR BRAKE COIL OPEN. HORIZ STAB TRIM ACTUATOR (P/N 600-92301-67/21207-008 S/N Y2003) WAS REPLACED WITH A REPAIRED UNIT WITH TSN 868
- [SDR CA080225005](https://openairdocs.org/sdr/CA080225005.md): Shaft · broken · Feb 22, 2008 · Cndair CL6012A12 · AC Generator-Alternator
  > (CAN) 3 MINUTES AFTER TAKEOFF, GENERATOR FAILED, AC RETURNED TO BASE. GENERATOR REMOVED, FOUND BROKEN SHAFT INSIDE THE IDG (NOT THE MAIN SHAFT). IT BROKE, MELTED THE COVER AND CAME OUT (TC NR 20080225005)
- [SDR DJFA2007133](https://openairdocs.org/sdr/DJFA2007133.md): Adg · burned · Nov 2, 2007 · N664CW · Cndair CL6012A12 · DC Generating System
  > DURING POST MAINTENANCE CHECK FLIGHT, CREW TESTED THE AIR DRIVEN GENERATOR SYSTEM (ADG). DURING THE TEST THE ADG FAILED LEAVING THE CREW IN COMPLETE ELECTRICAL BLACKOUT. ENGINE DRIVEN SYSTEM WAS BROUGHT BACK ON-LINE AND AIRCRAFT LANDED SAFELY. MAINTENANCE F
- [SDR CA070328003](https://openairdocs.org/sdr/CA070328003.md): Line · failed · Mar 23, 2007 · Cndair CL6012A12 · Hydraulic System, Main
  > (CAN) DURING ROUTINE SERVICING AFTER A/C ARRIVAL, HYD FLUID WAS NOTICED LEAKING OUT OF THE BOTTOM OF THE RUDDER AND RUNNING DOWN THE TAILCONE AND TO THE GROUND. PANELS WERE REMOVED TO LOCATE THE LEAK, FIGURING THAT THERE WAS A BAD RUDDER PCU LEAKING. WHAT WAS
- [SDR CA070301004](https://openairdocs.org/sdr/CA070301004.md): Rod · corroded · Mar 1, 2007 · Cndair CL6012A12 · Drag Control System
  > (CAN) DURING THE PILOT PRE-FLIGHT CHECKS THE LT FLIGHT SPOILER INDICATED DEPLOYED WHEN STOW WAS SELECTED. THE FLIGHT SPOILER STOW/DEPLOY HANDLE WAS STIFF AT THE STOW EXTREMELY. VISUAL CONFIRMATION REVEALED THAT THE FLIGHT SPOILER WAS NOT FULLY STOWED BUT THE R
- [SDR CA070221001](https://openairdocs.org/sdr/CA070221001.md): Bushing · failed · Feb 19, 2007 · Cndair CL6012A12 · Rudder Control System
  > (CAN) DURING FLIGHT THE CO-PILOTS RUDDER PEDAL ADJUSTMENT MECHANISM FAILED ALLOWING THE RUDDER PEDALS TO FALL FORWARD TO THE LIMIT OF THEIR TRAVEL. INSPECTION REVEALED THAT THE THREADED BUSHING IN THE ADJUSTMENT MECHANISM HAD FAILED ALLOWING THE SYSTEM TO DICO
- [SDR CA070125001](https://openairdocs.org/sdr/CA070125001.md): Actuator · inoperative · Jan 25, 2007 · Cndair CL6012A12 · Landing Gear Actuator
  > (CAN) RT MAIN LANDING GEAR UNLOCK INDICATION APPROX. 15 - 20 MIN. AFTER ARRIVAL, NO PUMP, NO GEAR COMMAND, LOCK PARTIALLY MOVED TO UNLOCK POSITION. RETRACTING ACTUATOR REPLACED AND AC RETURNED TO SERVICE.
- [SDR CA061010005](https://openairdocs.org/sdr/CA061010005.md): Flap System · malfunctioned · Oct 9, 2006 · Cndair CL6012A12 · Trailing Edge Flap Control System
  > (CAN) FLAP FAIL BETWEEN 20 DEGREES TO 0 DEGREE DURING RETRACTION OF THE FLAPS AT TAKEOFF, FLAPS RESET ON GROUND IAW OPERATING MANUAL NR 1 ABNORMAL PROCEDURE SECTION 10 P3-4. A/C RETURN TO SERVICE. NO SNAG. FLAP FAIL BETWEEN 20 DEGREES TO 0 DEGREE DURING RET
- [SDR CA060918001](https://openairdocs.org/sdr/CA060918001.md): Flap System · malfunctioned · Sep 18, 2006 · Cndair CL6012A12 · Trailing Edge Flap Control System
  > (CAN) FLAP FAILED ON TAKEOFF, A/C RETURNED AND LANDED SAFELY AT QB MAIN BASE, BREAKER WAS RESET IAW OPERATING MANUAL, COULDN`T DUPLICATED THE SNAG. A/C DID ONE FLIGHT AND RETURN TO BASE WITHOUT ANY SNAG.
- [SDR CA060828001](https://openairdocs.org/sdr/CA060828001.md): Pump · broken · Aug 28, 2006 · Cndair CL6012A12 · Engine Fuel Pump
  > (CAN) LT MAIN AND SCAVENGE EJECTOR FAILURE (MOTIVE FLOW FAILURE). FUEL PUMP SHAFT FOUND BROKEN. FUEL PUMP REPLACED AND AIRCRAFT RETURNED TO SERVICE. A/C HOURS; 25194:25 CYCLES; 29896 (TC NR 20060828001)
- [SDR CA070720009](https://openairdocs.org/sdr/CA070720009.md): Windshield · cracked · Jul 27, 2006 · Cndair CL6012A12 · Flight Compartment Windows
  > (CAN) LT WINDSHIELD OUTER PANE CRACKED IN FLIGHT WITH NO LOSS OF PRESSURIZATION. FLIGHT CONTINUED NORMALLY. NEW WINDSHIELD INSTALLED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20070720009)
- [SDR CA060728006](https://openairdocs.org/sdr/CA060728006.md): Engine · oil consumption · Jul 22, 2006 · Cndair CL6012A12 · Turbine Engine Oil System
  > (CAN) AIRCRAFT HAD TO SHUTDOWN THE RT ENGINE DURING FLIGHT, DUE TO LOW OIL PRESSURE. APPROX 3 HOURS INTO THE FLIGHT, THE PILOT REPORTED THE OIL PRESSURE WAS FLUCUTATING BETWEEN 45 AND 65 PSI, THEN DROPPED AGAIN TO 35 AND 55 PSI, AND FINALLY GOT A STEADY LOW OI
- [SDR CA060515003](https://openairdocs.org/sdr/CA060515003.md): Vent Line · corroded · May 3, 2006 · Cndair CL6012A12 · Fuel Storage
  > (CAN) REFUELLING WAS C/O, MASTER REFUEL PANEL CHECK C/O TO CHECK VALVE FOR OPERATION, WHAT WAS NOTICED, FUEL CAME OUT OUT OF THE LT NACA SCOOP APPROXIMATE 2 GALLON, THEN STOP. MAINT WAS ADVISED,THIS WAS ONLY HAPPENING WHEN A/C WAS PARK OVERNIGHT. SO MAINT CREW
- [SDR CA060428002](https://openairdocs.org/sdr/CA060428002.md): Transformer · inoperative · Apr 28, 2006 · Cndair CL6012A12 · Attitude Gyro and Indicating System
  > (CAN) LOSS OF NR 1 MASI, NR 1 ALTIMETER, FDR, NR 1 ADI PITCH AND ROLL INFO, COMPASS INFO, NR 1 ESSENTIAL BUS AND LOSS 26 VAC. CAUSE OF FAULT FOUND TO BE BROKEN WIRES AT T2XD POST NR 3. TRANSFORMER LOCATED ON BACK OF C/B PANEL C. (TC NR 20060428002)
- [SDR CA060407005](https://openairdocs.org/sdr/CA060407005.md): Hinge Fitting · cracked · Apr 5, 2006 · Cndair CL6012A12 · Landing Gear Doors
  > LHS MAIN LANDING GEAR (MLG) P/N CC670-10520-965, S/N 15042 AND RT MLG DOOR P/N CC670-10520-966, S/N (SAME AS RHS) WERE CRACKED AT THE AFT HINGE FITTING P/N CC670-10571-13 (SEE PIX.1) AND AT FORWARD HINGE FITTING P/N CC670-10570-5 (SEE PIX.2). LOOSE FASTERNERS
- [SDR DJFA2005179](https://openairdocs.org/sdr/DJFA2005179.md): Bulkhead · cracked · Dec 21, 2005 · N664CW · Cndair CL6012A12 · Fuselage Main, Bulkhead
  > DURING A SCHEDULED MAINTENANCE VISIT, A CRACK WAS DISCOVERED IN THE PRESSURE BULKHEAD WEB AT FUSELAGE STATION 409.00 WHILE PERFORMING AIRWORTHINESS DIRECTIVE 97-24-02, SERVICE BULLETIN 601-0501. THE CRACK IS LOCATED AT THE CORNER OF THE KEEL BEAM LINK CUTOUT
- [SDR CA051121001](https://openairdocs.org/sdr/CA051121001.md): Fuel Heater · cracked · Nov 21, 2005 · Cndair CL6012A12 · Fuel Heater
  > (CAN) FUEL LEAK AS BEEN FOUND ON SEVEN DAYS INSPECTION, TECHNICIAN HAS FOUND A CRACK IN A SOLDERED JOINT ON FUEL HEATER. THE FUEL HEATER HAS BEEN REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.
- [SDR DJFA2005159](https://openairdocs.org/sdr/DJFA2005159.md): Bulkhead · cracked · Oct 19, 2005 · N627CW · Cndair CL6012A12 · Fuselage Main, Bulkhead
  > DURING A ROUTINE MAINTENANCE VISIT, A CRACK WAS DISCOVERED IN THE PRESSURE BULKHEAD WEB AT FUSELAGE STATION 409.00 WHILE PERFORMING AD 97-24-02. THE CRACK WAS REPAIRED IAW EO NR 601-53-10-266, AND IN CONJUNCTION WITH DRAWING K600-31904. THE AIRCRAFT WAS RETU
- [SDR CA050826001](https://openairdocs.org/sdr/CA050826001.md): Heat Exchanger · leaking · Aug 19, 2005 · Cndair CL6012A12 · Engine Fuel/Oil Cooler
  > (CAN) DURING TROUBLESHOOTING TO FIND CAUSE FOR LOW OIL PRESSURE AT HIGH POWER IT WAS DISCOVERED THAT THE OIL HAD BECOME CONTAMINATED WITH FUEL AND SUBSEQUENTLY LOWERED IN VISCOSITY CAUSING LOW OIL PRESSURE READINGS. THE OIL TO FUEL HEAT EXCHANGER, FUEL HEATER/
- [SDR DJFA2005111](https://openairdocs.org/sdr/DJFA2005111.md): Selector Valve · inoperative · Jun 19, 2005 · N664CW · Cndair CL6012A12 · Landing Gear Retraction/Extension System
  > THE CREW REPORTED THAT DURING A NORMAL GEAR EXTENSION, THE NOSE WHEEL WOULD NOT EXTEND. THE LANDING GEAR WAS CYCLED TWICE, AND THE NOSE GEAR REMAINED RETRACTED. A MANUAL EXTENSION WAS PERFORMED, AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE
- [SDR DJFA2005104](https://openairdocs.org/sdr/DJFA2005104.md): Controller · broken · May 31, 2005 · N627CW · Cndair CL6012A12 · Landing Gear Position and Warning
  > AFTER MLG SELECTED DOWN, LT MLG INDICATOR LIGHTS DID NOT ILLUMINATE. CREW TESTED BULBS AND PERFORMED A FLY-BY PAST TOWER. CONTROLLER REPORTED THAT MLG APPEARED TO BE DOWN AND LOCKED. A MANUAL MLG EXTENSION PERFORMED AND AIRCRAFT LANDED WITHOUT FURTHER INCIDE
- [SDR CA050413003](https://openairdocs.org/sdr/CA050413003.md): Element · broken · Apr 13, 2005 · Cndair CL6012A12 · Autopilot System
  > (CAN) DURING A SCHEDULED 1200-HOUR CHECK, A FUNCTIONAL TEST OF THE RIGHT THRUST REVERSER AUTO THROTTLE RETARDER WAS CARRIED OUT. THE RIGHT THROTTLE FAILED TO RETURN TO IDLE POSITION WITH THE THRUST REVERSERMANUAL DEPLOYMENT. UPON INVESTIGATION IT WAS DISCOVERE
- [SDR CA050406005](https://openairdocs.org/sdr/CA050406005.md): Actuator · leaking · Apr 6, 2005 · Cndair CL6012A12 · Landing Gear Actuator
  > (CAN) NOSE LANDING GEAR ACTUATOR LEAKING AT ROD END PISTON. LIFE LIMITED PART AT 19480 CYCLES. A/C RETURN TO BASE ON SPECIAL FLIGHT PERMIT WITH GEAR DOWN.
- [SDR CA050222008](https://openairdocs.org/sdr/CA050222008.md): Gcu · inoperative · Feb 19, 2005 · Cndair CL6012A12 · AC Regulator
  > (CAN) A FEW MINUTES AFTER TAKE-OFF FROM AIRPORT WHILE SHUTTING DOWN THE APU, THE FLIGHT CREW HAD A SEVERE ELECTRICAL SMELL IN THE COCKPIT, BUT NO SMOKE APPEARS. THE FLIGHT CREW DECLARED AN EMERGENCY LANDING AT THE SAME AIRPORT. BACK TO THE MAINTENANCE FACILIT
- [SDR CA050215012](https://openairdocs.org/sdr/CA050215012.md): Connector · loose · Feb 10, 2005 · Cndair CL6012A12 · Landing Gear Retraction/Extension System
  > (CAN) ON APPROACH, NLG WOULD NOT DEPLOY UPON NORMAL SELECTION OF LANDING GEAR DOWN. EMER EXTENSION WAS COMPLETED, AC LANDED WITHOUT FURTHER INCIDENT, FOUND THAT (NLG) SELECTOR VALVE WAS AT FAULT. PINS IN CONNECTION TO EXTEND SOLENOID WHICH CONTROLS DOWN SELE
- [SDR CA050120008](https://openairdocs.org/sdr/CA050120008.md): Anti-Ice Valve · failed · Jan 20, 2005 · Cndair CL6012A12 · Ice/Rain Protection System
  > (CAN) FOLLOWING AN FAA, SUSPECTED UNAPPROVED PART REPORT, FOR A COWL ANTI ICE VALVE P/N: 300013000-002 S/N: 1596, MFG P/N: 601-97097-5, AN ADDITIONAL VALVE S/N:691, WAS FOUND TO HAVE BEEN REPAIRED AND CERTIFIED WITHOUT THE USE OF A PROPER CMM.
- [SDR CA050125009](https://openairdocs.org/sdr/CA050125009.md): Access Door · distorted · Jan 19, 2005 · Cndair CL6012A12 · Electrical/Electronic Compartment Doors
  > (CAN) THIS AIRCRAFT WAS INSPECTED AND TESTED AND FOUND TO EXHIBIT UNACCEPTABLE NOSE AVIONICS ACCESS DOOR DEFORMATION IN EXTREME COLD CONDITIONS. THE DEGREE OF DOOR CORNER CURLING EXCEEDS THE MANUFACTURERS LIMIT FOR SKIN WAVINESS FOR RVSM CERTIFICATION. THIS C
- [SDR CA050125008](https://openairdocs.org/sdr/CA050125008.md): Access Door · distorted · Jan 19, 2005 · Cndair CL6012A12 · Electrical/Electronic Compartment Doors
  > (CAN) THIS AIRCRAFT WAS INSPECTED AND TESTED AND FOUND TO EXHIBIT UNACCEPTABLE NOSE AVIONICS ACCESS DOOR DEFORMATION IN EXTREME COLD CONDITIONS. THE DEGREE OF DOOR CORNER CURLING EXCEEDS THE MANUFACTURERS LIMITS FOR SKIN WAVINESS FOR RVSM CERTIFICATION. (THIS
- [SDR CA050119002](https://openairdocs.org/sdr/CA050119002.md): Access Panel · distorted · Jan 18, 2005 · Cndair CL6012A12 · Fuselage Main, Plate/Skin
  > (CAN) AC REMOVED FROM HEATED HANGAR (20 DEG C) TO RAMP (-27 DEG C) T/E OF UPPER ELEC BAY ACCESS PANEL DEFLECTED.345 FROM AIRFRAME. FURTHER INVESTIGATION SHOWED DISTORTION THROUGHOUT PANEL WITH GREATEST DISTORTION AT CORNERS RANGING FROM.100IN TO.345 IN. SI
- [SDR CA050119001](https://openairdocs.org/sdr/CA050119001.md): Valve · improper part · Jan 17, 2005 · Cndair CL6012A12 · Ice/Rain Protection System
  > (CAN) FOLLOWING AN FAA, SUSPECTED UNAPPROVED PART REPORT, FOR A COWL ANTI-ICE VALVE PN 300013000-002, SN 1596, THREE (3) ADDITIONAL VALVES WERE FOUND TO HAVE BEEN REPAIRED AND CERTIFIED WITHOUT THE USE OF PROPER CMM. THE VALVES INVOLVED ARE S/N: 133R, 867, 691
- [SDR CA040729002](https://openairdocs.org/sdr/CA040729002.md): Generator · failed · Jul 27, 2004 · Cndair CL6012A12 · AC Generation System
  > DURING A ROUTINE POST MAJOR MAINTENANCE FLIGHT CHECK OF THE AIR DRIVEN TURBINE GENERATOR SYSTEM, THE SYSTEM FAILED TO TAKE THE ELECTRICAL LOAD, AS INDICATED BY THE AMMETER AND THE VOLTMETER, WHEN THE TURBINE WAS MANUALLY DEPLOYED. MAINTENANCE FINDINGS:- ADG O
- [SDR CA040603004](https://openairdocs.org/sdr/CA040603004.md): Aileron · mismanufactured · Jun 3, 2004 · Cndair CL6012A12 · Autopilot System
  > (CAN) WHILE INVESTIGATING A SNAG, DISCOVERED AN AILERON A/P QUADRANT ASSEMBLY P/N 40E22-84-1069-1 WHICH DID NOT MEET THE MANUFACTURER'S DRAWING IN THE INSTALLATION OF THE NR 1 COLLINS A/P SERVO, LOCATED IN THE LT MLG WHEEL WELL. FOR THE DISABLING OF THE NR1
- [SDR CA040423007](https://openairdocs.org/sdr/CA040423007.md): Potentiometer · intermittent · Apr 16, 2004 · Cndair CL6012A12 · Stall Warning System
  > (CAN) DURING TAKEOFF ROTATION, THE STICK SHAKER ACTIVATED ON THE LOW LEVEL, THE STALL PROTECT SYSTEM (SPS) WARBLER SOUNDED, THE SPS FAIL LIGHTS WENT TO A FLASH CYCLE AND THE STALL PUSH LIGHTS ACTIVATED. THE LT SPS NEEDLE WAS SWINGING BACK AND FORTH INTO THE S
- [SDR CA031113001](https://openairdocs.org/sdr/CA031113001.md): Engine · shutdown · Oct 14, 2003 · Cndair CL6012A12 · Engine (Turbine/Turboprop)
  > (CAN) DURING CRUISE AT FL 390, THE RT ENGINE SHUTDOWN. THE CREW REPORTED ALL ENGINE PARAMETERS WERE NORMAL AT THE TIME AND NO MESSAGES OR CAUTIONS WERE POSTED. THE CREW DECENDED AND PERFORMED A SUCCESSFUL WINDMILL RELIGHT AT 10,000 FT. FOLLOWED BY AN UNEVENT
- [SDR CA030903006](https://openairdocs.org/sdr/CA030903006.md): Actuator · failed · Aug 27, 2003 · Cndair CL6012A12 · Elevator Tab Control System
  > (CAN) ATTEMPT TO TRIM AIRCRAFT NOSE UP OR NOSE DOWN CAUSED BOTH PITCH TRIM CHANNELS TO INDICATE (OFF). THUS HORIZONTAL PITCH TRIM SYSTEM DE-ACTIVATED.
- [SDR CA030724002](https://openairdocs.org/sdr/CA030724002.md): Battery Pack · overheated · Jul 21, 2003 · Cndair CL6012A12 · Battery/Charger System
  > (CAN) THE BATTERY ASSEMBLY FOR NR 4 EMERGENCY LIGHTING POWER SUPPLY WAS REMOVED FOR BENCH CHECK. THE ASSEMBLY WAS INSPECTED AND FOUND THAT THE CELL TABS HAD BEEN OVERHEATED, INSULATION HAD BEEN MELTED OFF AND THE PLASTIC ENCLOSURE WAS ALSO DAMAGED. AN OPERATIO
- [SDR CA030731005](https://openairdocs.org/sdr/CA030731005.md): Bushing · failed · Jul 15, 2003 · Cndair CL6012A12 · Elevator Structure
  > (CAN) AFTER COMPLETION OF TASK, INSPECT ELEVATOR ATTACH BOLTS, VISUAL AND NDT INSPECTION, AND DURING POST INSTALLATION/INDEPENDENT INSPECTION, INSPECTOR NOTICED CLICKING NOISE, FOLLOWING INVESTIGATION FOUND (LT ELEVATOR): LT ELEVATOR ATTACH FITTING CRACKED, DU
- [SDR CA030122001](https://openairdocs.org/sdr/CA030122001.md): Fitting · broken · Jan 19, 2003 · Cndair CL6012A12 · Passenger/Crew Doors
  > (CAN) DOOR TENSION FITTING (UPPER FORWARD) BROKEN IN FLIGHT.
- [SDR CA021217006](https://openairdocs.org/sdr/CA021217006.md): Bearing · broken · Nov 11, 2002 · Cndair CL6012A12 · Aileron Control System
  > (CAN) DURING 300-600 HOUR INSPECTION AILERON PCU OPERATION TEST. FOUND AILERON QUADRANT IN RT WHEEL WELL IS NOISY (SNAPPING). AFTER REMOVING RT AILERON QUADRANT ASS FOR INVESTIGATION, FOUND RT QUADRANT ITEM 57 PAGE 27-11-00 FGURE 3 IN IPC BEARING IS DAMAGE (RA
- [SDR CA021125002](https://openairdocs.org/sdr/CA021125002.md): Bearing · broken · Nov 11, 2002 · Cndair CL6012A12 · Aileron Control System
  > (CAN) DURING 300-600 HOURS INSPECTION AILERON PCU OPERATION TEST, FOUND AILERON QUADRANT IN RT WHEEL WELL IS NOISY (SNAPPING).AFTER REMOVING RT/ AILERON QUADRANT ASSEMBLY FOR INVESTIGATION, FOUND RT/ QUADRANT, BEARING IS DAMAGED (RACES HALF WAY ROUND). CHANGE
- [SDR CA020926001](https://openairdocs.org/sdr/CA020926001.md): Wire · exposed · Sep 19, 2002 · Cndair CL6012A12 · Fire Protection System Wiring
  > (CAN) WIRING HARNESS FOR THE ENGINE FIRE BOTTLE SQUIBS LOCATED IN THE APU AREA HAD EXPOSED WIRES WHERE THEHARNESS ENTERS THE CONNECTOR PLUG FOR THE SQUIB.
- [SDR CA020925003](https://openairdocs.org/sdr/CA020925003.md): Wire Harness · exposed · Sep 18, 2002 · Cndair CL6012A12 · Fire Protection System Wiring
  > (CAN) WIRING HARNESS FOR THE ENGINE FIRE BOTTLE SQUIBS LOCATED IN THE APU AREA HAD EXPOSED WIRES WHERE THEHARNESS ENTERS THE CONNECTOR PLUG FOR THE SQUIB.
- [SDR CA020913010](https://openairdocs.org/sdr/CA020913010.md): Wire · shorted · Sep 9, 2002 · Cndair CL6012A12 · Fire Protection System Wiring
  > (CAN) ON A SCHEDULED MAINTENANCE INSPECTION OF THE FIRE BOTTLES, MECHANIC FOUND ON RT BOTTLE LT SQUIB WIRING TO BE EXPOSED AND TOUCHING EACH OTHER IN THE APU AREA. ANOTHER CL601 A/C INSPECTED AND FOUND SIMILAR PROBLEM WITH SQUIB WIRING (SAME BOTTLE AND SQUIB)

Next page: https://openairdocs.org/model/canadair-cl-601-2a12/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 = 'CL6012A12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/canadair-cl-601-2a12/reports

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