# Service difficulty reports: Canadair CL600-1A11

A list on [Canadair CL600-1A11](https://openairdocs.org/model/canadair-cl600-1a11.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 69 reports

- [SDR CA190402017](https://openairdocs.org/sdr/CA190402017.md): Lanyard · wrong part · Nov 12, 2018 · Cndair CL6001A11 · Crew Oxygen System
  > (CAN) FOLLOWING AN ISSUE ON THE CL605 (CL6-CA-35-7), TCCA HAS REQUESTED BOMBARDIER TO CONFIRM THAT CL600/601 WAS NOT IMPACTED BY THIS ISSUE. BOMBARDIER CONDUCTED A SAMPLING IN SERVICE AND DISCOVERED THAT A SIMILAR ISSUE WAS POTENTIALLY PRESENT ON THE FLEET.
- [SDR CA140106008](https://openairdocs.org/sdr/CA140106008.md): Thrust Reverser · failed · Jan 3, 2014 · Cndair CL6001A11 · Engine Thrust Reverser
  > (CAN) RIGHT THRUST REVERSER DEPLOYMENT JAN 3. 2014. ACFT DEPARTED YOW. TAKEOFF WENT WITHOUT INCIDENT. CLIMBING THROUGH 5000 FT. WE HEARD A BANG, ACFT YAWED AND BUFFETED. REVERSER UNLOCK LIGHT CAME ON & AUTO THROTTLE RETARD SNAPPED RT THROTTLE TO IDLE. WE
- [SDR 2012FA0000169](https://openairdocs.org/sdr/2012FA0000169.md): Carbon Seal · defective · Mar 12, 2012 · N396KM · Cndair CL6001A11 · AC Generator-Alternator
  > AFTER PERFORMING SEVERAL PREFLIGHTS, IT WAS NOTED THAT THE NR 2 INTEGRATED DRIVE GENERATOR HAD AN INCREASE IN THE FREQUENCY AND QUANITY OF OIL SERVICING. AFTER INVESTAGATING THE CAUSE, IT WAS DETERMINED THAT THE DRIVE END CARBON SEAL WAS LEAKING, ALLOWING PRE
- [SDR 2008FA0000537](https://openairdocs.org/sdr/2008FA0000537.md): Skin · corroded · Jul 24, 2008 · N100QR · Cndair CL6001A11 · Wing, Plate/Skin
  > SURFACE CORROSION (PITTING) DISCOVERED ON BOTH WINGS LOWER SURFACES ADJACENT TO AND OB OF WHEEL WELLS, CORROSION DEEMED UNUSUALLY SEVERE. (K)
- [SDR ZLJ2008F00000](https://openairdocs.org/sdr/ZLJ2008F00000.md): Skin · corroded · Jul 24, 2008 · N100QR · Cndair CL6001A11 · Fuselage Main, Plate/Skin
  > SURFACE CORROSION DISCOVERED ON FUSELAGE SKIN ADJACENT TO PRE-COOLER EXHAUSTS ON LT AND RT SIDES OF FUSELAGE. DISCREPANCY DISCOVERED WHILE PERFORMING PROCEDURE C53-00-814. CORROSION DEEMED TO BE UNUSUALLY SEVERE. (K)
- [SDR 2007F00069](https://openairdocs.org/sdr/2007F00069.md): Windshield · cracked · Dec 13, 2007 · N900LG · Cndair CL6001A11 · Flight Compartment Windows
  > EN ROUTE AT FL330, THE CAPTAIN NOTICED A CRACK IN THE EXTERIOR PANEL OF THE LT FWD WINDSHIELD. THE APPROPRIATE CHECKLIST WAS COMPLETED AND A SPEED REDUCTION AND DECENT REQUESTED. WHILE DESCENDING A LOUD (POP) AND SUBSEQUENT WHISTLING WAS HEARD. A FURTHER SPEED
- [SDR WAI2007F00001](https://openairdocs.org/sdr/WAI2007F00001.md): Fire Loop · shorted · Mar 6, 2007 · N403WY · Cndair CL6001A11 · Fire Detection
  > FLIGHT CREW REPORTED LT ENGINE FIRE DETECTION FAIL LIGHT CAME ON JUST PRIOR TO ROTATION, THEN FIRE LIGHT CAME ON JUST PRIOR TO ROTATION, THEN FIRE WARNING CAME ON AT 1,500 FT DURING CLIMB. STAYED ON AFTER DISCHARGING BOTH FIRE BOTTLES. RETURNED TO BASE AFTER
- [SDR 2007F00023](https://openairdocs.org/sdr/2007F00023.md): Fire Loop · shorted · Mar 6, 2007 · N403WY · Cndair CL6001A11 · Fire Detection
  > FLIGHT CREW REPORTED LT ENGINE FIRE DETECTION FAIL LIGHT CAME ON JUST PRIOR TO ROTATION, THEN FIRE WARNING CAME ON AT 1,500 FEET DURING CLIMB. STAYED ON AFTER DISCHARGING BOTH FIRE BOTTLES. RETURNED TO BASE, AFTER LANDING, APPEARED TO BE NO FIRE. FOUND LT ENGI
- [SDR 2006FA0000563](https://openairdocs.org/sdr/2006FA0000563.md): Adg · deployed · Apr 24, 2006 · N777GD · Cndair CL6001A11 · AC Generation System
  > AIR DRIVEN GENERATOR (ADG) UNEXPECTED DEPLOYED ON POST TAKEOFF CLIMB OUT. PRECAUTIONARY LANDING ACCOMPLISHED. ADG MECHANICALLY RETRACTED/ SAFED; AIRCRAFT FERRIED TO MAINTENANCE DEPOT. ALL WORK ACCOMPLISHED IAW MM. (K)
- [SDR 2006FA0000589](https://openairdocs.org/sdr/2006FA0000589.md): Battery · leaking · Apr 12, 2006 · N673TS · Cndair CL6001A11 · Emergency Locator Beacon
  > A STRONG ACIDIC ODOR WAS PRESENT AFTER REMOVING ELT BATTERY FROM ELT INSPECTION FOUND A THICK WHITE LIQUID ON THE NEGATIVE SIDE OF ONE BATTERY CELL. THE EXPIRATION DATE OF THE ELT BATTERY IS APRIL 2010 (4 MORE YEARS). THE ELT BATTERY OUTPUT IS 13.2 VOLTS. (
- [SDR 2005FA0000845](https://openairdocs.org/sdr/2005FA0000845.md): Floor Support · cracked · May 24, 2005 · N40HJ · Cndair CL6001A11 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT LOCATED AT RBL 9.0 FS 460 CRACKED AT FLANGE. DURING FLOORBEAM REPLACEMENT A VISUAL INSPECTION REVEALED CRACK AT FLANGE. INSPECTED 3 OTHER FLOOR SUPPORTS IN AIRCRAFT, NO OTHER CRACKS FOUND. THE FLOOR SUPPORT IS CURRENTLY INCLUDED IN THE 60 MONT
- [SDR DJFA2006372](https://openairdocs.org/sdr/DJFA2006372.md): Fuel Control · unknown · Oct 18, 2003 · N602CW · Cndair CL6001A11 · Fuel Control/Turbine Engines
  > AT FLIGHT LEVEL 390 FT NR 2 ENGINE SHUTDOWN ON IT'S OWN. PILOTS DESCENDED AND AT FLIGHT LEVEL 100 FT THEY WERE ABLE TO GET THE ENGINE STARTED. LANDED WITH NO FURTHER PROBLEMS.
- [SDR DJFA200300003](https://openairdocs.org/sdr/DJFA200300003.md): Fuel Control · malfunctioned · Oct 18, 2003 · N602CW · Cndair CL6001A11 · Fuel Controlling System
  > AT FLIGHT LEVEL 390 FT NR 2 ENGINE SHUTDOWN ON IT'S OWN. PILOTS DESENDED AND AT FLIGHT LEVEL 100 FT, WAS ABLE TO GET THE ENGINE STARTED. LANDED WITH NO FURTHER PROBLEMS.
- [SDR 103901](https://openairdocs.org/sdr/103901.md): Duct · disconnected · Sep 4, 2003 · N895CC · Cndair CL6001A11 · Air Distribution System
  > DETECTED A RISE IN CABIN ALTITUDE THAT WAS NOT CONSIDERED NORMAL. MADE A PRECAUTIONARY DESCENT AND PERFORMED THE CABIN PRESSURE LOW CHECKLIST. LANDED AIRCRAFT AT INTENDED DESTINATION WITHOUT INCIDENT. FOUND A/C DISTRIBUTION DUCT FORWARD OF APU DISCONNECTED.
- [SDR EXO2003F00001](https://openairdocs.org/sdr/EXO2003F00001.md): Mount · cracked · Jan 21, 2003 · N678CG · Cndair CL6001A11 · Engine Thrust Reverser
  > DURING INSPECTION OF THE RT THRUST REVERSER TRANSLATING SLEEVE. THE TOP JACKSCREW MOUNTING WAS FOUND CRACKED AROUND THE O-RING.
- [SDR EXO2003F00000](https://openairdocs.org/sdr/EXO2003F00000.md): Thrust Reverser · damaged · Nov 21, 2002 · N63HJ · Cndair CL6001A11 · Engine Thrust Reverser
  > DURING CLIMB THROUGH FL130 A LOUD BANG FOLLOWED BY RT THRUST REVERSER UNLOCK LIGHT, RETURNED TO AIRPORT. FOUND 12 O'CLOCK BALL SCREW ACTUATOR AFT ATTACH POINT FAILED CAUSING TRANSLATING STRUCTURE TO MOVE DOWN AND AFT ENOUGH TO CAUSE OTHER TWO ATTACH POINTS TO
- [SDR CA020517008](https://openairdocs.org/sdr/CA020517008.md): Crossbeam · cracked · Apr 4, 2002 · Cndair CL6001A11 · Vertical Stabilizer
  > (CAN) DURING INTERNAL STRUCTURAL INSPECTION OF THE TAIL AREA, A 5/8 INCH CRACK WAS FOUND ON THE RUDDER CONTROL CROSS BEAM SUPPORT (EMPENNAGE).THE PROBABLE CAUSE MAY BE THAT ON THE LOWER LT OUTBOARD RIVETS WITH BELLOW MINIMUM EDGE DISTANCE. IN ADDITION, THE RIV
- [SDR J8G2001F00000](https://openairdocs.org/sdr/J8G2001F00000.md): Bearing · defective · Jun 29, 2001 · N710HL · Cndair CL6001A11 · Turbine Section
  > FLIGHT CREW NOTICED SMOKE IN THE CABIN AFTER TAKE-OFF FROM AIRPORT. THE AIRCRAFT RETURNED TO THE AIRPORT WITH NO FURTHER INCIDENT. INITIAL TROUBLESHOOTING INDICATED EXCESSIVE OIL PRESENCE AT NR 2 BEARING ON THE RIGHT ENGINE. DEFECT WITH NR 2 BEARING CONFIRM
- [SDR 20010612CW007](https://openairdocs.org/sdr/20010612CW007.md): Windshield · delaminated · Jun 4, 2001 · N103HB · Cndair CL6001A11 · Flight Compartment Windows
  > OUTER FACE PLY DELAMINATION OF LEFT HAND PILOTS WINDSHIELD. PLY SEPARATION WAS BEYOND LIMITS OF MANUFACTURES STRUCTURAL REPAIR MANUAL TO CONTINUE OPERATION.
- [SDR 20010612CW006](https://openairdocs.org/sdr/20010612CW006.md): Window · debonded · Jun 4, 2001 · N103HB · Cndair CL6001A11 · Flight Compartment Windows
  > PILOTS LEFT SIDE WINDOW WAS DISBONDED AT FORWARD VERTICAL EDGE.
- [SDR 20010427CW001](https://openairdocs.org/sdr/20010427CW001.md): Windshield · cracked · Apr 5, 2001 · N63HJ · Cndair CL6001A11 · Flight Compartment Windows
  > DURING CRUISE FLIGHT, LEFT WINDSHIELD CRACKED. CREW CALLED MAINTENANCE. MAINTENANCE ADVISED TO TURN HEAT OFF. DELAMINATION STOPPED, CONTINUED TO DESTINATION.
- [SDR 20001019SH026](https://openairdocs.org/sdr/20001019SH026.md): Compressor · cracked · Aug 31, 2000 · N602AS · Cndair CL6001A11 · APU Core Engine
  > CUSTOMER REPORTED HIGH OIL CONSUMPTION AND OIL SMELL IN CABIN. APU DISASSEMBLED FOR COMPRESSOR REPAIR. DURING MAINTENANCE, FOUND COMPRESSOR ROTOR CRACKED AT SEVERAL VANE PLATFORM AREAS, NO FRACTURE NOTED, APU DID NOT FAIL. COMPRESSOR ROTOR PN 3822014-2 SN 9
- [SDR 20001019SH025](https://openairdocs.org/sdr/20001019SH025.md): Compressor · fractured · Aug 9, 2000 · N920DS · Cndair CL6001A11 · APU Core Engine
  > CUSTOMER REPORTED APU FAILURE, SUDDEN STOPPAGE, AND GEARBOX FAILURE. ACFT WAS ON GROUND AND APU IDLE, NOT LOADED. APU SUSTAINED A POWER GROUP CONTAINED SEPARATION FAILURE AND UNCONTAINED GEARBOX FAILURE. TEARDOWN REVEALED COMPRESSOR ROTOR FAILURE, VANE PLAT
- [SDR CA000724013](https://openairdocs.org/sdr/CA000724013.md): Turbine · seized · Jul 8, 2000 · Cndair CL6001A11 · Turbine Section
  > (CAN) AFTER LANDING, DURING ROLLOUT, THE CREW DEPLOYED THE THRUST REVERSER AND THE RT ENGINE SHUTDOWN. THE AIRCRAFT CONTINUED TO THE HANGAR AND AN INITIAL EVALUATION OF THE ENGINE REVEALED THAT THE TURBINE WHEEL HAD SEIZED.FURTHER DETAILS OF THE ENGINE INSPECT
- [SDR CA000724012](https://openairdocs.org/sdr/CA000724012.md): Engine · failed · Jul 5, 2000 · Cndair CL6001A11 · Engine (Turbine/Turboprop)
  > (CAN) DURING CRUISE AT 41,000 FT THE FLIGHT CREW NOTICED A SMALL SURGE IN POWER ON THE RT ENGINE FOLLOWED ABOUT 10 SECONDS LATER BY A DECREASE IN RPM AND INCREASE IN ITT. THE ENGINE AND AIRCRAFT IMMEDIATELY BEGAN VIBRATING, WITH THE RT ENGINE VIBE METER INDICA
- [SDR CA000516033](https://openairdocs.org/sdr/CA000516033.md): Fan · failed · Apr 11, 2000 · Cndair CL6001A11 · Turbine Engine Bypass Section
  > (CAN) FOLLOWING A/C ROTATIONAT 100AGL THE NUMBER 2 ENGINE AUTOMATICALLY SHUTDOWN WITH AN OVERSPEED INDICATION. N1 FAN WOULD NOT ROTATE. ENGINE REPLACED.
- [SDR 20000424SH010](https://openairdocs.org/sdr/20000424SH010.md): Heater · inoperative · Mar 12, 2000 · N750GT · Cndair CL6001A11 · Windshield/Door Rain/Ice Removal
  > PILOT'S RIGHT FRONT WINDSHIELD HEATER INOPERABLE. (X)
- [SDR 2000ZZZX836](https://openairdocs.org/sdr/2000ZZZX836.md): Fitting · cracked · Mar 2, 2000 · N751DB · Cndair CL6001A11 · Fuselage Miscellaneous Structure
  > IN THE LAST 2 MONTHS HAVE FOUND 3 T-FITTINGS CRACKED AND LEAKING. (TWO ON 600 CHALLENGER, ONE ON 601). ONE DID CAUSE AN INTERRUPTION OF A FLIGHT. ALL THREE ARE ALUMINUM FITTINGS THAT HAD NOT BEEN DISTURBED SINCE MANUFACTURE.
- [SDR CA991230029](https://openairdocs.org/sdr/CA991230029.md): Actuator · intermittent · Dec 20, 1999 · Cndair CL6001A11 · Stabilizer Actuator
  > (CAN) DURING POST INSTALLATION TEST, CHANNEL 2 FOUND OPERATING INTERMITTENTLY. DURING TRIM COMMAND MOTOR WOULD OPERATE BUT SCREW JACK WOULD NOT ALWAYS TURN. COMPONENT RECIEVED IN THIS CONDITION FROM SUPPLIER.
- [SDR CA991230028](https://openairdocs.org/sdr/CA991230028.md): Actuator · failed · Dec 20, 1999 · Cndair CL6001A11 · Stabilizer Actuator
  > (CAN) DURING POST INSTALLATION TESTING,CHANNEL 2 FOUND HARD FAILED. UNIT WAS RECEIVED IN THIS CONDITION FROM SUPPLIER. 0.0 HOURS
- [SDR 99ZZZX4400](https://openairdocs.org/sdr/99ZZZX4400.md): Bracket · cracked · Sep 23, 1999 · N491DB · Cndair CL6001A11 · Fuselage Miscellaneous Structure
  > INSPECTION OF THE ADG BAY REVEALED THE ATTACH BRACKET, IN TWO PLACES, TO BE CRACKED. REMOVED AND REPLACED WITH A NEW BRACKET. LANDINGS: 4,672.
- [SDR 99ZZZX3566](https://openairdocs.org/sdr/99ZZZX3566.md): Duct · chafed · Aug 30, 1999 · N601SA · Cndair CL6001A11 · Engine Bleed Air System
  > DURING SCHEDULED INSPECTION, THE BLEED AIR DUCT, PN 215-0809-501, WAS FOUND CHAFING ON NR 2 BEARING OIL TUBE, PN 2-263-060-01. BOTH PARTS WERE CHAFED BEYOND LIMITS AND REQUIRED REPLACEMENT. OIL TUBE CHAFED 50 PERCENT WALL THICKNESS AND BLEED AIR DUCT CHAFED
- [SDR 20001212AP012](https://openairdocs.org/sdr/20001212AP012.md): Windshield · cracked · Aug 16, 1999 · N63HJ · Cndair CL6001A11 · Fuselage Main, Structure
  > TAKEOFF FROM PUEBLO, COLORADO WAS NORMAL. AFTER 1:45 OF FLIGHT, A CRACK APPEARED ON THE LEFT WINDSHIELD. THE LEFT WINDSHIELD HEAT C/B WAS MANUALLY SWITCHED OFF; WEATHER WAS CAVU TO FXE. (M)
- [SDR 99ZZZX3568](https://openairdocs.org/sdr/99ZZZX3568.md): Windshield · cracked · Aug 16, 1999 · N63HJ · Cndair CL6001A11 · Flight Compartment Windows
  > PILOT'S WINDSHIELD CRACKED (OUTER LAYER ONLY) IN CRUISE FLIGHT.
- [SDR CA990119007](https://openairdocs.org/sdr/CA990119007.md): Valve · failed · Jan 7, 1999 · Cndair CL6001A11 · Landing Gear Door Retract Section
  > (CAN) NOSE GEAR DOORS FAILED TO OPEN WHEN GEAR SELECTED DOWN. PROBLEM INTERMITTENT AFTER COLD SOAK AT ALTITUDE.
- [SDR 98ZZZX4312](https://openairdocs.org/sdr/98ZZZX4312.md): Idg · failed · Nov 6, 1998 · N90UC · Cndair CL6001A11 · AC Generator-Alternator
  > THE NR 2 GENERATOR DROPPED OFF-LINE ON LANDING. MAINTENNACE FOUND THE INTEGRATED DRIVE GENERATOR (IDG) DIFFERENTIAL INDICATORS POPPED AND THE OIL BLACK. THE OIL-OUT LINE FILTER REVEALED CHUNKS OF METAL. SUSPECT THE CONSTANT SPEED DRIVE FAILED (CSD). SUBMIT
- [SDR 99ZZZX436](https://openairdocs.org/sdr/99ZZZX436.md): Bulkhead · cracked · Oct 27, 1998 · N550CW · Cndair CL6001A11 · Fuselage Main, Bulkhead
  > CRACKED BULKHEAD WEB AT FS 409. REF: SB 600-679. DATE SEPT 10, 1997. AD 97-24-02 AMEND 39-10209 EFFECT DATE 12-3-97. FS 409 REPAIRED ERGINEERING ORDER 600-53-175.
- [SDR CA980608009](https://openairdocs.org/sdr/CA980608009.md): Relay · failed · May 30, 1998 · Cndair CL6001A11 · DC Generating System
  > (CAN) BATTERY CHARGER ANNUNCIATOR ILLUMINATED DURING GROUND OPERATION. RELAY KP7A FOUND FAULTY. WHEN RELAY IS LATCHED BY A DC SENSE CIRCUIT, IT, IN TURN, WILL ALLOW THE AC BUS TO OPERATE BATTERY CHARGER. PART TC: 4,348.
- [SDR 98ZZZX3215](https://openairdocs.org/sdr/98ZZZX3215.md): Spacer · misinstalled · Mar 29, 1998 · N818TH · Cndair CL6001A11 · Turbine Section
  > HPN - NORMAL TAKEOFF EN ROUTE BAHAMAS. APPROX 1 HR EN ROUTE AT FL 310, PILOT NOTED NR 1 ENG VIBRATION INCREASE FROM.3 M/S TO.6 M/S AND INCREASE IN ENG NOISE. ALL OTHER ENG INDICATIONS WITHIN NORMAL PARAMETERS. ENG NOISE SUBSIDED THEN INCREASE IN ENG VIBRA
- [SDR 98ZZZX533](https://openairdocs.org/sdr/98ZZZX533.md): Sensor · misinstalled · Jan 22, 1998 · N19HF · Cndair CL6001A11 · Airfoil Anti/De-ice System
  > LEFT AND RIGHT WING ANTI-ICE FAIL LIGHTS CAME ON INTERMITTENTLY ANY TIME WING ANTI-ICE SYSTEM SELECTED. FOUND THE LEFT AND RIGHT WING TEMP SENSORS INSTALLED BACKWARDS FROM THE FACTORY. INSTALLED NEW SENSORS PER MM. SYSTEM WORKED NORMALLY ON NEXT FLIGHT.
- [SDR 97ZZZX5136](https://openairdocs.org/sdr/97ZZZX5136.md): Tire · defective · Nov 25, 1997 · N90UC · Cndair CL6001A11 · Tire
  > DURING POST-FLIGHT INSPECTION, A BUBBLE WAS FOUND ON THE SIDEWALL OF TIRE. AFTER TIRE WAS REPLACED, THE S/N WAS CHECKED AGAINST ANOTHER TIRE THAT HAD BEEN REMOVED PREMATURELY FOR AIR LEAKING FROM WEEP HOLES IN SIDEWALL. THAT TIRE S/N WAS 7102030. SINCED THE
- [SDR 97ZZZX4716](https://openairdocs.org/sdr/97ZZZX4716.md): Heater Element · exploded · Nov 7, 1997 · N711SX · Cndair CL6001A11 · Buffet/Galleys
  > THE HEATER ELEMENT FAILED WITH AN EXPLOSIVE LIKE CHARGE THAT SENT THE FAILED ELEMENT AND WIRES INTO THE HONEYCOMB GALLEY TOP.
- [SDR 97ZZZX3498](https://openairdocs.org/sdr/97ZZZX3498.md): Cell · shorted · Jul 22, 1997 · N100LR · Cndair CL6001A11 · DC Generator-Alternator
  > AIRCRAFT BATTERY CHARGER DROPPING OFF-LINE. REMOVED AND SHIPPED BATTERY TO INSPECTION AND SERVICE. FOUND SHORTED CELL, STRAPS HAD BURNED SMALL HOLE THROUGH SIDE OF CELL. BATTERY WILL BE SHIPPED BACK TO MANUFACTURER DUE TO LOW TSN.
- [SDR CA970314005](https://openairdocs.org/sdr/CA970314005.md): Gen Control Unit · failed · Mar 7, 1997 · Cndair CL6001A11 · DC Generating System
  > (CAN) DURING FLIGHT APU STARTED AND STABILIZED. THE #2 AC ESSENTIAL BUS WAS KNOCKED OFF LINE. APU GENERATOR CONTROL UNIT REPLACED AS WELL AS #2 GENERATOR CONTROL UNIT.
- [SDR 96ZZZX5475](https://openairdocs.org/sdr/96ZZZX5475.md): Tee Fitting · leaking · Oct 8, 1996 · N100LR · Cndair CL6001A11 · Hydraulic System, Main
  > 50 HRS AFTER MAJOR INSP, DEVELOPED LEAK IN LT WHEELWELL. FOUND NR 6 ELBOW CRACKED AND LEAKING. NEXT DAY FOUND HYD FLUID LEAKING OUT OF LT WHEELWELL AGAIN. FOUND NR 6 TEE FITTING CRACKED AND LEAKING. REPLACED BOTH. PRE-FLIGHTED A/C ON THIRD DAY FOR TRIP AN
- [SDR 96ZZZX5474](https://openairdocs.org/sdr/96ZZZX5474.md): Tee Fitting · leaking · Oct 8, 1996 · N100LR · Cndair CL6001A11 · Hydraulic System, Main
  > 50 HRS AFTER MAJOR INSP, DEVELOPED LEAK IN LT WHEELWELL. FOUND NR 6 ELBOW CRACKED AND LEAKING. NEXT DAY FOUND HYD FLUID LEAKING OUT OF LT WHEELWELL AGAIN. FOUND NR 6 TEE FITTING CRACKED AND LEAKING. REPLACED BOTH. PRE-FLIGHTED A/C ON THIRD DAY FOR TRIP AN
- [SDR 96ZZZX5473](https://openairdocs.org/sdr/96ZZZX5473.md): Elbow · leaking · Oct 8, 1996 · N100LR · Cndair CL6001A11 · Hydraulic System, Main
  > 50 HRS AFTER MAJOR INSP, DEVELOPED LEAK IN LT WHEELWELL. FOUND NR 6 ELBOW CRACKED AND LEAKING. NEXT DAY FOUND HYD FLUID LEAKING OUT OF LT WHEELWELL AGAIN. FOUND NR 6 TEE FITTING CRACKED AND LEAKING. REPLACED BOTH. PRE-FLIGHTED A/C ON THIRD DAY FOR TRIP AN
- [SDR CA960703019](https://openairdocs.org/sdr/CA960703019.md): Id Generator · defective · Jul 17, 1996 · Cndair CL6001A11 · AC Generator-Alternator
  > (CAN) GENERATOR TRIPPPING OFF LINE. METAL IN SCAVENGE FILTER AND ON CHIP DETECTOR. COMPONENT CAUSING TROUBLE WILL HAVE TO BE DETERMINED ON TEARDOWN.
- [SDR 96ZZZM1323](https://openairdocs.org/sdr/96ZZZM1323.md): Outflow Vlv · malfunctioned · Jun 24, 1996 · N601WW · Cndair CL6001A11 · Pressure Regulator/Outflow Valve
  > APPROX TWO HOURS INTO FLIGHT, CABIN PRESSURIZATION BEGAN TO FLUCTUATE 300 FEET IN AUTO MODE. AIR RUSHING NOISE COULD BE HEARD IN BAGAGE AREA. THE ELECTRO/PNEUMATIC OUTFLOW VALVE WAS REPLACED DURING AT 1200 HOUR INSPECTION APPROXIMATELY (8) FLIGHT HOURS PRIOR
- [SDR 96ZZZX3018](https://openairdocs.org/sdr/96ZZZX3018.md): Support · cracked · May 9, 1996 · N68SD · Cndair CL6001A11 · Engine Cowling System
  > DURING 300-HOUR ENGINE INSPECTION, A 6.5 INCH HORIZONTAL CRACK WAS FOUND IN THE FAN COWL SUPPORT AT 3 O'CLOCK POSITION. ALSO, VARIOUS BRACKETRY ATTACHED TO COWL ASSY FOUND TO HAVE SMALL CRACKS.

Next page: https://openairdocs.org/model/canadair-cl600-1a11/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 = 'CL6001A11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/canadair-cl600-1a11/reports

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