GE CF34-8C1

Service difficulty reports · 1,415

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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 engine_model_key = 'CF348C1'
  ORDER BY difficulty_date DESC"

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SDR ASOA06161Step · crackedDURING A HANGAR INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE CRACKED AT THE ATTACHMENT POINT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Feb 7, 2006 · N710EV · Cndair CL6002C10 · Entrance StairsSDR VNAA0602003Proximity Sensor · failedWHEN ATTEMPTING TO RETRACT THE LANDING GEAR, THE CREW RECEIVED A GEAR DISAGREE WARNING. THE QRH WAS FOLLOWED. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR CENTERED NR 2 PROXIMITY SENSOR FAILED. THE SENSOR WAS REPLFeb 6, 2006 · N719PS · Cndair CL6002C10 · Landing Gear Position and WarningSDR VNAA0602002Proximity Sensor · malfunctionedWHEN ATTEMPTING TO RETRACT THE LANDING GEAR, THE CREW RECEIVED A -GEAR DISAGREE- WARNING. THE QRH WAS FOLLOWED. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. AFTER TROUBLESHOOTING MAINTENANCE ADJUSTED THE LT NOSE LANDING GEAR LOCK POSITION PROXIMIFeb 4, 2006 · N719PS · Cndair CL6002C10 · Landing Gear Position and WarningSDR QXEA200600205Fadac · malfunctionedDEN - ON TAXI FOR FLIGHT 4298, L/R FADEC FAULT STATUS MESSAGE. RETURNED TO THE GATE. LEFT AND RIGHT FADEC FAULT 2 STATUS MSGS CLEARED WHEN ENGINES SHUTDOWN. PERFORMED SELF TESTS OF LEFT AND RIGHT FADEC'S IN MDC, SELF TEST GOOD. HISTORY SHOWS LEFT AND RIGHTJan 31, 2006 · N601QX · Cndair CL6002C10 · Fuel Controlling SystemSDR VNAA0601020Door · openDURING CLIMBOUT THE CREW REPORTED AN OPEN ACCESS DOOR. THE FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AC ELECTRICAL GROUND POWER DOOR OPEN. THE DOOR AND FUSELAGE WERE INSPECTED AND NO DISCREPANCIES WERE FOUND. THE DOOR WAS PRJan 29, 2006 · N702PS · Cndair CL6002C10 · Service DoorsSDR ASOA06137Lamp · burned outDURING A HANGAR INSPECTION, THE EMERGENCY CEILING LIGHT, SECOND FROM THE FRONT, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING LIGHT, SECOND FROM THE FRONT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. Jan 28, 2006 · N744EV · Cndair CL6002C10 · Emergency LightingSDR COMA0570133Sensor · malfunctionedFLT 5276 - RT ENGINE LOW FUEL PRESSURE CAUTION. REPLACED THE LOW PRESSURE SENSOR.Jan 23, 2006 · N371CA · Cndair CL6002C10 · Fuel Pressure SensorSDR SWIA200616161Connector · brokenFLAPS HALFSPEED STATUS MSG. REPAIRED WIRING AT LT BPSU CONNECTOR PLUG MPE9P1 AND MPE9P2 IAW WM 20-17-10. OPERATIONAL CHECK OK.Jan 21, 2006 · N706SK · Cndair CL6002C10 · Flight Control System WiringSDR ASOA06107Angle · crackedDURING A HANGAR INSPECTION, THE PASSENGER DOOR AFT DRAG ANGLE, ABOVE THE ASSIST MOTOR PULLEY, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR AFT DRAG ANGLE, ABOVE THE ASSIST MOTOR PULLEY, IAW REO 670-52-11-072. (K)Jan 21, 2006 · N712EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA06098Panel · crackedDURING A C-CHECK, THE FORWARD AND AFT PASSENGER DOOR SIDEWALL, AT THE HANDRAIL SUPPORT BRACKET, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD AND AFT PASSENGER DOOR SIDEWALL, AT THE HANDRAIL SUPPORT BRACKET, IAW REO 670-52-11-104. (Jan 17, 2006 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA0601015Structure · ground damageWHILE PARKED AT THE GATE THE RIGHT WING TIP LEADING EDGE TRANSITION FAIRING AND OUTBOARD SLAT WERE HIT BY A VEHICLE. THE FAIRING WAS DENTED AND THE SLAT WAS DENTED & CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT WING TRANSITION FAIRING AND OUTBOARD SLAJan 17, 2006 · N708PS · Cndair CL6002C10 · Wing Main, Frame StructureSDR ASOA06096Door · unknownDURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND TO BE DIFFICULT TO CLOSE, ACCOMPANIED BY UNUSUAL NOISE DURING THE TAKEOFF ROLL AND GREEN INDICATIONS ON THE SYNOPTIC PAGE. MAINTENANCE LUBRICATED THE PASSENGER DOOR AND SEAL WITH NO DEFECTS NOTED. OPERJan 16, 2006 · N717EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA06095Lamp · burned outDURING A GROUND INSPECTION, NUMEROUS BULBS WERE FOUND INOPERATIVE IN BOTH LOWER EMERGENCY ROW EXIT SIGNS. MAINTENANCE REMOVED AND REPLACED THE NECESSARY LAMPS IN BOTH OF THE LOWER EMERGENCY ROW EXIT SIGNS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. Jan 15, 2006 · N708EV · Cndair CL6002C10 · Emergency LightingSDR ASOA06091Battery · dischargedDURING A GROUND INSPECTION, EMERGENCY LIGHTING WOULD NOT ILLUMINATE. MAINTENANCE CHARGED THE EMERGENCY LIGHTING SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 13, 2006 · N722EV · Cndair CL6002C10 · Emergency LightingSDR VNAA0601011Structure · lightning strikeDURING APPROACH THE CREW REPORTED A LIGHTNING STRIKE TO THE FUSELAGE NOSE SECTION AND THE RADAR FAILED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED EN ROUTE & DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE RADOME, LT HOJan 13, 2006 · N709PS · Cndair CL6002C10 · Aircraft StructuresSDR ASOA06086Step · separatedDURING A HANGAR INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND SEPARATED AT THE ATTACH STAY ROD BRACKET TO THE STEP COMPOSITE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 10, 2006 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA0601005Shock Absorber · failedAFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT AND THE CREW REPORTED A GEAR DISAGREE WARNING. THE CREW DECLARED AN EMERGENCY, FOLLOWED THE QRH, AND RETURNED TO CLT. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THAT THE NOSE LANDING GEAR SHOCK FAILED TO EXTJan 9, 2006 · N719PS · Cndair CL6002C10 · Main Landing Gear Strut/Axle/TruckSDR ASOA06081Floor Support · corrodedDURING A C-CHECK, THE FORWARD FLOOR SUPPORT, AT FS 280, WAS FOUND TO BE CORRODED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF APPROPRIATE CORRECTIVE ACTION. (K)Jan 9, 2006 · N713EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASO2006F00000Floor Support · corrodedDURING A C-CHECK, THE PASSENGER DOOR SILL FLOOR SUPPORT ANGLE, AT FS310 TO FS349, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR SILL FLOOR SUPPORT ANGLE, AT FS310 TO FS349, IAW SRM 51-42-10. (K)Jan 4, 2006 · N713EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA200600007Computer · malfunctionedON FLIGHT 4219, FUEL CHANNEL 1/2 FAIL CAUTION MESSAGE. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. REPLACED FUEL QUANTITY GAGING COMPUTER. FOUND WATER LEAKING FROM ICE BUCKET IN GALLEY THROUGH THE FLOOR ON TO THE FQGC. OPERATIONAL CHECKS GJan 3, 2006 · N601QX · Cndair CL6002C10 · Fuel StorageSDR VNAA0601002Skin · lightning strikeTHE CREW REPORTED A POSSIBLE LIGHTNING STRIKE IN FLIGHT. MAINTENANCE PERFORMED A DETAILED LIGHTNING STRIKE INSPECTION. DAMAGE WAS FOUND ON THE RT HORIZONTAL STABILIZER AFT TIP AND ON TOP OF THE FUSELAGE NOSE SECTION FORWARD OF THE COCKPIT. ALL DAMAGE WAS REJan 2, 2006 · N723PS · Cndair CL6002C10 · Horizontal Stabilizer, Plate/SkinSDR ASOA06080Unknown · crackedDURING A C-CHECK, A SUSPECTED CRACK WAS FOUND AT FS 280, LBL9 AND RBL9. MAINTENANCE REPAIRED THE CRACK AT FS 280, LBL 9 AND RBL 9, IAW REO. (K)Dec 31, 2005 · N713EV · Cndair CL6002C10 · Aircraft StructuresSDR ASOA06079Unknown · corrodedDURING C-CHECK, CORROSION WAS FOUND AT FS 280. MAINTENANCE REPAIRED THE CORRODION AT FS 280 BY INSTALLING NEW WEBS IAW SRM. (K)Dec 31, 2005 · N713EV · Cndair CL6002C10 · Aircraft StructuresSDR ASOA06078Handle · crackedDURING A C-CHECK, THE FORWARD AVIONICS BAY DOOR HANDLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FORWARD AVIAONICS BAY DOOR HANDLE IAW SRM 51-42-06. (K)Dec 31, 2005 · N713EV · Cndair CL6002C10 · Electrical/Electronic Compartment DoorsSDR ASOA06077Structure · crackedDURING A C-CHECK, THE PASSENGER DOOR, BELOW THE TOP STEP ON THE FORWARD SIDE, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR, BLEOW THE TOP STEP ON THE FORWARD SIDE, IAW REO. (K)Dec 31, 2005 · N713EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA051166Pulley · crackedDURING A C-CHECK, THE PASSENGER DOOR, ABOVE THE QASSIST CABLE PULLEY, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR, ABOVE THE ASSIST CABLE PULLEY, IAW REO. (K)Dec 31, 2005 · N713EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA051167Crossbeam · crackedDURING C-CHECK, THE FS 280, AT LBL 9 AND RBL 9, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 280 CROSSBEAM, AT LBL 9 AND RBL 9, IAW EO700-53-0061. (K)Dec 31, 2005 · N713EV · Cndair CL6002C10 · Fuselage Main, StructureSDR QXEA200501852Engine · malfunctionedDEN - ON TAXI OUT NR 1 ENGINE FLAMED OUT. RETURNED TO THE GATE. MAINTENANCE RESTARTED ENGINE AND IT OPERATED NORMALLY. INTERROGATED MDC ENGINE EXCEEDENCE FOUND R ENG ITT ROSE TO 1102 C DEGREES FOR 4.4 SEC DURING OPERATION. C/W INSPECTION OF ENGINE OPERATEDDec 29, 2005 · N611QX · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SWIA200516077Plate · bindingMAIN CABIN PASSENGER DOOR HARD TO OPEN. RESECURED PAX DOOR OUTER HANDLE FLUSH SPRING LOADED PLATE. OPERATED PAX DOOR FROM INSIDE, OPERATIONAL CHECK GOOD.Dec 29, 2005 · N705SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA200516079Windshield · crackedCAPTAIN'S WINDSHIELD SHATTERED ON TOUCHDOWN. REPLACED CAPTAIN'S WINDSHIELD IAW CRJ 700 MM 56-11-01.Dec 28, 2005 · N701SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA200516078Control Panel · malfunctionedAILERON TRIM WILL NOT TURN LWD. REPLACED AILERON TRIM CONTROL PANEL IAW CRJ AMM CHAP 27-12-00. OPERATIONAL CHECK GOOD.Dec 27, 2005 · N701SK · Cndair CL6002C10 · Aileron Tab Control SystemSDR QXEA200501830Actuator · leakingDEN - ON FLIGHT 4325 FOUND A FUEL LEAK ON THE RIGHT ENGINE. UPON INSPECTION FOUND FUEL LEAKING FROM NR 2 ENG SLAVE VG ACTUATOR OVERBOARD DRAIN LINE. REMOVED AND REPLACED NR 2 ENG SLAVE VG ACTUATOR IAW AMM TASK 75-30-03-000-801-A01 AND 75-30-03-400-801-A01 LEADec 26, 2005 · N602QX · Cndair CL6002C10 · Engine Fuel DistributionSDR VNAA0512021Access Door · openDURING CLIMBOUT THE CREW REPORTED AN OPEN ACCESS DOOR. THE FLIGHT RETURNED TO SRQ AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AC ELECTRICAL GROUND POWER DOOR OPEN. THE DOOR WAS INSPECTED AND NO DAMAGE WAS FOUND. THE DOOR WAS PROPERLY SECURED AND THEDec 25, 2005 · N716PS · Cndair CL6002C10 · DoorsSDR VNAA0512020Panel · openDURING CLIMBOUT THE CREW REPORTED A BANGING SOUND FROM THE RIGHT SIDE OF THE FORWARD FUSELAGE. THE FLIGHT RETURNED TO TLH AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE EXTERNAL SERVICE PANEL DOOR OPEN. THE DOOR WAS INSPECTED AND NO DAMAGE WAS FOUND. TDec 24, 2005 · N716PS · Cndair CL6002C10 · Fluid Service DoorsSDR VNAA0512015Door · openTHE CREW REPORTED A LOUD SQUEALING NOISE FROM THE MAIN LANDING GEAR AREA OF THE FUSELAGE. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE REFUEL DOOR OPEN. INSPECTION REVEALED NO DAMAGE. THE DOOR WAS PROPERLY SECURED AND THE ADec 18, 2005 · N716PS · Cndair CL6002C10 · Fluid Service DoorsSDR VNAA0512011Wire · shortedTHE WING ANTI-ICE SENSOR CAUTION MESSAGE ILLUMINATED DURING CLIMB. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE REPAIRED A CHAFED/SHORTED WIRE HARNESS IN THE LEFT WING LEADING EDGE AND REPLACED THE ANTI-ICE & LEAK DETECTION CONTROL UNIT WHICH FDec 14, 2005 · N718PS · Cndair CL6002C10 · Ice/Rain Protection System WiringSDR VNAA0512009Connector · dentedDURING CLIMB THE LT AND RT WING ANTI-ICE SYSTEMS CYCLED ON AND OFF. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE NR 2 - NR 3 SLAT TRACK CONNECTOR FLEX TUBE DENTED CAUSING REDUCED BLEED AIR FLOW TO THE LT OUTDec 8, 2005 · N708PS · Cndair CL6002C10 · Ice/Rain Protection System WiringSDR VNAA0512010Sensor · failedDURING CLIMBOUT THE LT WING A/I, RT WING A/I, & WING A/I SNSR CAUTION MESSAGES ILLUMINATED. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE REMOVED & REPLACED THE LEFT WING OUTBOARD ANTI-ICE SENSOR (MT33). THE WING ANTI-ICE SYSTEM OPERATIONALLY CDec 8, 2005 · N718PS · Cndair CL6002C10 · Airfoil Anti/De-ice SystemSDR VNAA0512007Actuator · failedDURING CLIMB THE PITCH FEEL CAUTION LIGHT ILLUMINATED. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE REMOVED AND REPLACED THE RT PITCH FEEL LINEAR ACTUATOR. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Dec 5, 2005 · N708PS · Cndair CL6002C10 · Elevator Control SystemSDR ASOA051058Seat Track · corrodedDURING A C-CHECK, THE SEAT TRACKS, FROM FS349 TO FS 985, RBL 9, WERE FOUND TO BE CORRODED BEYOND LIMITS. THIS MRR WILL REMAIN OPEN PENDING MATENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)Dec 4, 2005 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR COMA0570125Engine · overheatedFLIGHT 5281- RT MOTOR OVERTEMP DURING T/O, ITT 960 C. INSPECTED ENGINE AND FOUND NO DEFECTS. OPERATIONAL CHECKS WERE NORMAL.Dec 3, 2005 · N376CA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA0512005Controller · failedAFTER PUSHBACK THE CREW RECEIVED THE SMOKE AFT LAV WARNING AND SMELLED A BURNING ODOR. THE PASSENGERS WERE EVACUATED THROUGH THE PASSENGER DOOR AND THE AIRCRAFT WAS TOWED BACK ONTO THE GATE. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR CONDITIONING SYSTEM CDec 3, 2005 · N703PS · Cndair CL6002C10 · Air Conditioning SystemSDR ASOA051051Lens · crackedDURING A C-CHECK, THE EMERGENCY EXIT LIGHT LENS, OVER THE SERVICE DOOR, WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LENS IN THE EMERGENCY EXIT LIGHT, OVER THE SERVICE DOOR. (K)Dec 3, 2005 · N716EV · Cndair CL6002C10 · Emergency LightingSDR ASOA051050Lamp · burned outDURING A C-CHECK, THE AFT GALLEY FLOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE WILL REMOVE AND REPLACE THE LAMP IN THE AFT GALLEY FLOOR EMERGENCY EXIT LIGHT. (K)Dec 3, 2005 · N716EV · Cndair CL6002C10 · Emergency LightingSDR ASOA051048Lamp · burned outDURING A GROUND INSPECTION, THE AFT RT SIDE OVER WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT RT SIDE OVER WING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Dec 2, 2005 · N708EV · Cndair CL6002C10 · Emergency LightingSDR SWIA200515925Flap · out of rigFLAPS HALFSPEED STATUS MESSAGE IN TAXI OUT. RIGGED LT IB SKEW DETECTOR. CLEAR INHIBITS. OPERATIONAL CHECKS GOOD. IAW 27-51-00.Dec 1, 2005 · N762SK · Cndair CL6002C10 · Trailing Edge Flap Control SystemSDR QXEA200501730Engine · unknownOKC - ON PUSHBACK FOR FLIGHT 4188 DURING ENGINE START, THE NR 1 AUTO SHUTDOWN DURING START. RETURNED TO THE GATE. MAINTENANCE FOUND THE LEFT FADEC START ABORT MESSAGE IN MEMORY DUE TO SLOW N2 RESPONSE. MAINTENANCE SUSPECTED ICING. PERFORMED GROUND RUN OF EDec 1, 2005 · N601QX · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA0512001Structure · lightning strikeEVIDENCE OF LIGHTNING DAMAGE WAS FOUND ON THE LT WINGLET TIP TRAILING EDGE DURING THE 50 HOUR SERVICE CHECK. MAINTENANCE COMPLIED WITH A LIGHTNING STRIKE INSPECTION. NO FURTHER DAMAGE WAS FOUND. A TEMPORARY REPAIR WAS PERFORMED ON THE LT WINGLET TIP TRAILINDec 1, 2005 · N710PS · Cndair CL6002C10 · Wing StructureSDR SWIA200515926Sensor · malfunctionedAFTER POWER UP SLAT FAULT MSG CAME ON. REPLACED RT IB AND OB SLAT DISCONNECT SENSORS. IAW 27-81-39. OPERATIONAL CHECK GOOD.Nov 28, 2005 · N716SK · Cndair CL6002C10 · Leading Edge Slat Position Indicating SystemSDR VNAA0511020Shutoff Valve · failedTHE RIGHT COWL ANTI-ICE CAUTION MESSAGE ILLUMINATED WHEN RIGHT COWL ANTI-ICE WAS SELECTED. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE REMOVED & REPLACED THE RIGHT PRESSURE REGULATING & SHUTOFF VALVE. THE SYSTEM OPERATIONALLY CHECKED GOOD. TNov 22, 2005 · N703PS · Cndair CL6002C10 · Air Intake Anti/De-Ice System
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