GE CF34-8C1

Service difficulty reports · 1,415

Newest first. General aviation reporting is voluntary.

Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ASOA05356Post · corrodedDURING HANGAR MAINTENANCE, THE FS 280 BULKHEAD, DOOR POST AT LBL 11.128 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 BULKHEAD, DOOR POST AT LBL 11.128 IAW EO. (K)Apr 7, 2005 · N703EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA05355Floorbeam · corrodedDURING HANGAR MAINTENANCE, THE FS 280 TRANSVERSE BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 TRANSVERSE BEAM IAW EO. (K)Apr 7, 2005 · N703EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA05354Bulkhead · corrodedDURING HANGAR MAINTENANCE, THE FS 280 LT AND RT LOWER BULKHEAD WEB WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 LT AND RT LOWER BULKHEAD WEB IAW EO. (K)Apr 7, 2005 · N703EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA05308Wire · brokenDURING AN (A) CHECK, THE OVERHEAD EMERGENCY CEILING LIGHT AT ROW 4 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER THE CEILING PANEL TO THE NR 2 EMERGENCY CEILING LIGHT AT CONNECTOR J357. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)Apr 5, 2005 · N741EV · Cndair CL6002C10 · Light System WiringSDR ASOA05313Sill · corrodedDURING HANGAR MAINTENANCE, THE RT OB FLOOR SILL PLATE AT FS 280 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINT REPAIRED THE RT OB FLOOR SILL PLATE AT FS 280 IAW EO. (K)Apr 2, 2005 · N790EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA05312Floor Support · corrodedDURING HANGAR MAINTENANCE, THE FS 280 FLOOR SUPPORT ANGLE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINT REPAIRED THE FS 280 FLOOR SUPPORT ANGLE IAW EO. (K)Mar 28, 2005 · N790EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA0503014Warning System · activatedDURING DESCENT THRU 17000 (CLT TO CLE) THE MACH TRIM & STAB TRIM CAUTION MESSAGES ILLUMINATED. THE CREW OF FLIGHT 2239 DECLARED AN EMERGENCY AND MADE A SUCCESSFUL REDUCED FLAP LANDING IN CLE. MAINTENANCE CYCLED POWER AND OPERATIONALLY CHECK THE MACH TRIM & SMar 27, 2005 · N719PS · Cndair CL6002C10 · Stabilizer Control SystemSDR ASOA05311Panel · crackedDURING HANGAR MAINTENANCE, THE RT LUNCH BOX UPPER PANEL ASSY AT THE HYDRAULIC CASE DRAIN LOCATION WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT LUNCH BOX UPPER PANEL ASSY AT THE HYDRAULIC CASE DRAIN LOCATION IAW. (K)Mar 26, 2005 · N709EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA05310Floorbeam · corrodedDURING HANGAR MAINTENANCE, THE FS 280 FLOORBEAM WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 FLOORBEAM IAW EO. (K)Mar 26, 2005 · N709EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA05309Bulkhead · corrodedDURING HANGER MAINTENANCE, THE LT AND RT FS 280 LOWER WEB AT THE BULKHEAD WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT AND RT FS 280 LOWER WEB AT THE BULKHEAD IAW EO. (K)Mar 26, 2005 · N709EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA0503008Cap · unsafetiedEN ROUTE (CLT TO GSO) A FLIGHT ATTENDANT NOTICED A NOISE COMING FROM THE RIGHT SIDE OF THE AIRCRAFT AT THE WING AREA. THE CREW WAS NOTIFIED. THE CREW OF FLIGHT 2249 HAD NO INDICATION OF MALFUNCTIONS AND CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. Mar 14, 2005 · N709PS · Cndair CL6002C10 · Fuel StorageSDR MASA200500214Pressure Switch · inoperativeRETURNED TO GATE FOR LEFT ENGINE OIL PRESSURE WARNING MESSAGE UPON ENGINE START. PILOT DID SHUT THE ENGINE DOWN AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE PRESSURE SWITCH AND IT OPS CHECKED GOOD.Mar 13, 2005 · N927LR · Cndair CL6002D24 · Engine Oil Indicating SystemSDR VNAA0503007Warning Light · illuminatedUPON LANDING AT MKE, AFTER THE NOSE WHEEL CONTACTED THE RUNWAY, THE STEERING INOP CAUTION MESSAGE ILLUMINATED. NOSE WHEEL STEERING WAS INOPERATIVE EVEN AFTER RESETTING MULTIPLE TIMES. THE CREW OF FLIGHT 2207 CLEARED THE RUNWAY USING BRAKES AND DIFFERENTIAL PMar 10, 2005 · N723PS · Cndair CL6002C10 · Landing Gear Steering SystemSDR VNAA0503012Trim System · malfunctionedTHE STAB TRIM CAUTION MESSAGE ILLUMINATED IN FLIGHT. THE CREW OF FLIGHT 2239 FOLLOWED THE QRH, CONTINUED TO DESTINATION, AND MADE AN UNEVENTFUL LANDING. MAINTENANCE RESET THE STAB TRIM SYSTEM IAW CRJ 700 SERVICE LETTER SL-27-028. THE MESSAGE CLEARED AND THEMar 9, 2005 · N706PS · Cndair CL6002C10 · Stabilizer Control SystemSDR VNAA0503006Shutoff Valve · failedDURING CLIMB (CLT TO PWM) UPON SELECTION OF COWL ANTI ICE, THE L COWL A/I & L ENG BLEED CAUTION MESSAGES ILLUMINATED. THE SYNOPTIC PAGE SHOWED VALUES IN WHITE NOT IN AMBER. THE CREW OF FLIGHT 2234 RETURNED TO CLT AND MADE AN UNEVENTFUL LANDING. AFTER TROUBLMar 7, 2005 · N703PS · Cndair CL6002C10 · Pneumatic SystemSDR CA050308001Window · cracked(CAN) WE HAVE RECEIVED A REPORT WHICH WE FEEL IS A REPORTABLE EVENT. RT SIDE WINDOW CRACKED DURING DESCENT AT ABOUT 4000 FEET. COPILOT'S SIDE WINDOW REPLACED IAW AMM AND THE AIRCRAFT RETURNED TO SERVICE.Mar 3, 2005 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA050303002Window · broken(CAN) CLIMBING THROUGH FL340, THE CAPT DV WINDOW SHATTERED. DIVERTED. REMOVED AND REPLACED WINDOW.Feb 28, 2005 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA050303001Fan · shorted(CAN) AFTER TAKEOFF, CREW REPORTED SMOKE IN THE COCKPIT. DECLARED EMERGENCY AND RETURNED SAFELY TO FIELD. NO FURTHER INCIDENTS REPORTED. ALSO, SMOKE AFT LAV MASTER WARNING ILLUMINATED. INSPECTED AIRCRAFT AND FOUND ELECTRICAL SMOKE SMELL ORIGINATING FROM GALLFeb 28, 2005 · Cndair CL6002C10 · Air Distribution FanSDR VNAA0502013Valve · failedWHILE CLIMBING AFTER TAKEOFF (CLT TO CLE) THE L ENG BLEED CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2239, FOLLOWED THE QRH, RETURNED TO CLT DUE TO ICING CONDITIONS AT DESTINATION, AND MADE AN UNEVENTFUL LANDING. AFTER TROUBLESHOOTING THE SYSTEM, PSA MAFeb 16, 2005 · N168MD · Cndair CL6002C10 · Pneumatic Distribution SystemSDR CA050215014Window · cracked(CAN) COPILOT SIDE WINDOW CRACKED. WINDOW REPLACED IAW AMM.Feb 12, 2005 · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA0502010Sensor · failedDURING CRUISE (CLT TO TLH) THE ELEVATOR SPLIT CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2245 FOLLOWED THE QRH, DIVERTED TO JAX, AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS INSPECTED BY CONTRACT MAINTENANCE AND THE DISCREPANCY WAS DETERMINED TO BE Feb 10, 2005 · N725PS · Cndair CL6002C10 · Elevator Control SystemSDR VNAA0502009Transmitter · out of positionDURING CLIMBOUT (IAD TO CLT) THE ELEVATOR SPLIT CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2231 FOLLOWED THE QRH, RETURNED TO IAD, AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS INSPECTED BY CONTRACT MAINTENANCE AND THE DISCREPANCY WAS DETERMINED TO BFeb 9, 2005 · N725PS · Cndair CL6002C10 · Elevator Control SystemSDR VNAA0502008Transmitter · out of positionAFTER DEPARTURE (CLT TO TLH) THE ELEVATOR SPLIT CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2232 FOLLOWED THE QRH, RETURNED TO CLT, AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE AT CLT REPOSITIONED THE RT ELEVATOR POSITION TRANSMITTER IAW CRJ 700 AMM 2Feb 8, 2005 · N725PS · Cndair CL6002C10 · Elevator Control SystemSDR CA050209001Crossbeam · corroded(CAN) CORROSION FOUND AT FS280 (MAINLY RT SECTION) AND CRACKS AT LBL/RBL 9.0 AT FLOORBEAM ATTACHMENT FITTING. REPAIR TO BE PERFORMED USING GENERIC REPAIR ENGINEERING ORDERS (GEN REOS) 670-53-11-045, -046,-047, -052 AND IS MODSUM IS670531100026.Feb 2, 2005 · Cndair CL6002C10 · Fuselage Main, StructureSDR CA050202001Acm · seized(CAN) RT PACK AUTOFAIL MESSAGE ON EICAS WITH RT PACK FAILING AFTER START OF ENGINE NR1. MANUAL TEMP SELECTED WHICH RESULTED WITH THE LAV SMOKE DETECTOR ACTIVATING AND SMOKE ENTERING THE AFT CABIN. PACK TEMP OBSERVED AT 98 DEGREES JUST BEFORE AUTOFAIL. THE AFeb 1, 2005 · Cndair CL6002C10 · Air Conditioning SystemSDR SIMA200503404Power Supply · dischargedDURING A CHECK INSPECTION, FOUND NR 1 EMERGENCY POWER SUPPLY INOPERATIVE. REPLACED NR 1 EMERGENCY POWER SUPPLY. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K) (SW21200503055)Jan 28, 2005 · N521AE · Cndair CL6002C10 · Emergency LightingSDR ASOA05052Warning System · malfunctionedDURING APPROACH, FOLLOWING SELECTION OF THE FLAPS TO 8 DEGREES, THE CREW RECEIVED A (SLATS FAIL) MESSAGE. THE QRH WAS COMPLIED WITH AND EMERGENCY VEHICLES REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY. MAINTENANCE NOTED THAT THE MAIJan 21, 2005 · N719EV · Cndair CL6002C10 · Leading Edge Slat Position Indicating SystemSDR ASOA05056Light · missingDURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTING NEAR THE GALLEY WAS FOUND MISSING. MAINTENANCE INSTALLED THE EMERGENCY FLOOR LIGHT STRIP NEAR THE GALLEY. (K)Jan 21, 2005 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA05049Hydraulic Line · leakingDURING APPROACH, AT APPROXIMATELY 300 FT CREW RECEIVED A MASTER CAUTION SINGLE CHIME. EICAS SHOWED HYDRAULIC 2 LOW PRESSURE. PARKING BRAKE-BRAKE PRESSURE. RT THRUST REVERSER INOP, ALONG WITH FLIGHT SPOILER DEPLOY ADVISORY MESSAGES. HYDRAULIC SYNOPTIC PAGE Jan 20, 2005 · N718EV · Cndair CL6002C10 · Hydraulic System, MainSDR ASOA05045Seal · dirtyDURING A GROUND INSPECTION, THE CREW REPORTED THE PASSENGER DOOR WAS HARD TO CLOSE WITH AN AIR LEAK NOTICED AROUND THE DOOR DURING FLIGHT. MAINTENANCE CLEANED AND INSPECTED THE PASSENGER DOOR SEAL. MAINTENANCE THEN PRESSURIZED THE AIRCRAFT WITH NO LEAKS NOTEJan 19, 2005 · N701EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA05048Warning System · malfunctionedDURING TAKEOFF, THE CREW RECEIVED A GEAR DISAGREE WARNING. THE QRH WAS COMPLIED WITH AND THE LANDING GEAR WAS RECYCLED. ALL INDICATIONS SHOWED GREEN (UP AND LOCKED). WITH ALL INDICATIONS SHOWING NORMAL, THE FLIGHT CONTINUED. AN EMERGENCY WAS DECLARED AS A Jan 19, 2005 · N713EV · Cndair CL6002C10 · Landing Gear Position and WarningSDR CA050310005Ejector · stuck(CAN) WHILE PARKED IN BREST, THE CREW NOTICED AND UNCOMMAND FUEL TRANSFERED INTO THE CENTER TANK DURING THE NIGHT. THE NEXT REVENUE FLIGHT WAS CANCELED FOR TROUBLESHOOTING. TROUBLESHOOTING (JAN. 13, 2005) REVEALED A LEAK ON THE LT TRANSFER EJECTOR PUMP. THEJan 13, 2005 · Cndair CL6002C10 · Fuel Transfer ValveSDR VNAA0501004Pump · failedEN ROUTE FROM STL TO CLT THE HYD EDP 1A CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2214 FOLLOWED CRJ 700 QRH PROCEDURES. HYDRAULIC PRESSURE, TEMPERATURE, AND QUANTITY WERE GOOD WITH PUMP 1B OPERATING. THE FLIGHT CONTINUED TO CLT AND MADE AN UNEVENTFUL Jan 10, 2005 · N706PS · Cndair CL6002C10 · Hydraulic Pump (Electric/Engine), MainSDR ASOA05021Warning Light · illuminatedDURING CLIMB OUT, THE CREW RECEIVED AN (NWS INOP MSSG) ON EICAS. THE NOSE WHEEL STEERING (NWS) FAULT SUBSEQUENTLY CLEARED AND THE AIRCRAFT CONTINUED. THE QRH WAS COMPLIED WITH AND THE CREW RESET THE NWS SYSTEM UPON LANDING IN IAH SAFELY. THE TOWER ROLLED EMJan 9, 2005 · N713EV · Cndair CL6002C10 · Landing Gear Steering SystemSDR ASOA05020Glowstrip · damagedDURING HANGAR MAINTENANCE, THE EMERGENCY FLOOR LIGHT STRIP AFT OF ROW 12-C WAS FOUND NEEDING REPLACEMENT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY PHOTO LUMINESCENT STRIP AFT OF ROW 12-C. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 8, 2005 · N703EV · Cndair CL6002C10 · Emergency EquipmentSDR VNAA0501002Actuator · failedSHORTLY AFTER TAKEOFF FROM CLT THE AMBER PITCH FEEL CAUTION LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO CLT AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE AFTER TROUBLESHOOTING REMOVED & REPLACED THE NR 2 PITCH FEEL ACTUATOR IAW CRJ 700 AMM 27-31-23-400-801Jan 6, 2005 · N703PS · Cndair CL6002C10 · Flight Control SystemSDR CA050209002Crossbeam · corroded(CAN) DURING ONGOING C-CHECK OF A/C 5 CRACKS AND SLIGHT CORROSION WERE FOUND ON FS 280.0 CROSSBEAM P/N CC670-34175-7 AND ANGLE P/N CC670-33292-9 AT LBL 9.0 AND RBL 9.0. NOTE: REPAIR TO BE PERFORMED WITH ACOMBINATION OF GEN REOS 670-53-11-045, -046, -047, -05Jan 5, 2005 · Cndair CL6002C10 · Fuselage Main, StructureSDR QXEA200600013Controller · malfunctionedON FLT 2453, STEERING INOP CAUTION MESSAGE AFTER ARMING THE SYSTEM. ACCOMPLISHED RESET PROCEDURE IAW MX CONTROL. MESSAGE WENT AWAY FOR APPROX 30 SECONDS. ACCOMP RESET PROCEDURE A SECOND TIME IAW MTX CONTROL AND RETURNED TO GATE. MX INTERROGATED MDC FAULT HISJan 5, 2005 · N600QX · Cndair CL6002C10 · Landing Gear Steering SystemSDR ASOA05012Anchor Fitting · corrodedDURING C-CHECK, THE PASSENGER DOOR FORWARD CABLE ANCHOR FITTING AND PLATE WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR FORWARD CABLE ANCHOR FITTING AND PLATE. (K)Jan 4, 2005 · N823AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR SIMA2005004Battery Pack · dischargedCABIN EMERGENCY LIGHT SWITCH LEFT SELECTED ON, LIGHT ARE INOPERATIVE. REPLACED NR 1, 2, 3, AND 4 EMERGENCY BATTERY PACKS. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. PN 2013-1A, SN (NR1 72797), (NR2 65477), (NR3 82281), AND (NR4 84125). (SW21200503034)Jan 1, 2005 · N506AE · Cndair CL6002C10 · Emergency LightingSDR CA050110001Acm · seized(CAN) THE AIRCRAFT RETURNED TO FIELD AFTER LAV SMOKE DETECTOR WENT OFF AND VISIBLE SMOKE IN CABIN. AN EMERGENCY WAS DECLARED AND AN EMERGENCY EVACUATION WAS PERFORMED AFTER LANDING. NOTE: IT WAS REPORTED THAT SOMEONE BROKE BOTH ANKLES DURING THE EVACUATION FDec 29, 2004 · Cndair CL6002C10 · Cabin Cooling SystemSDR SIMA200435701Wire · brokenDURING CREW PREFLIGHT 4 FLOOR PROXIMITY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE FOR THE LIGHTS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 4 BATTERY PACKS WERE ALSO CHANGED DURING TRODec 20, 2004 · N506AE · Cndair CL6002C10 · Light System WiringSDR CA041224002Ejector · cracked(CAN) OVERNIGHT, APPROX 1200 LBS OF FUEL TRANSFERED INTO THE CENTER TANK. THE FLT HAD REPORTED AN INCREASE OF 120 LBS IN 10 MINUTES, HOWEVER IT WAS NOT DETERMINED IF THE FUEL TRANSFER WAS NOTED ON GROUND OR IN FLT BY THE CREW. MAINTENANCE FOUND THE LT MAINDec 20, 2004 · Cndair CL6002C10 · Aircraft Fuel Distribution SystemSDR SIMA200434901Charger · inoperativeEMERGENCY EXIT LOCATOR LIGHTS ABOVE THE GALLEY FOR THE PASSENGER DOOR AND SERVICE DOOR DO NOT ILLUMINATE. REPLACED NR 1 EMERGENCY LIGHT BATTERY AND CHARGER IAW AMM. OPERATIONAL CHECK GOOD IAW AMM. AC RETURNED TO SERVICE.Dec 12, 2004 · N502AE · Cndair CL6002C10 · Emergency LightingSDR CA041210004Adapter · failed(CAN) AFTER INSTALLING ALL FOUR BRAKES, WE BLED THE SYSTEM. WHILE DOING THE NR 2 BRAKE BLEEDING, THE NR 1 BRAKE BLEED PORT ADAPTER SHEARED AND BECAUSE OF THE HYDRAULIC PRESSURE THE ADAPTER HIT OUTBOARD MLG DOOR. HYDRAULIC SYSTEM PRESSURE WAS IMMEDIATLY STOPPEDDec 10, 2004 · Cndair CL6002C10 · BrakeSDR COMA0460669Oil System · overservicedFLIGHT 5729 HIGH OIL TEMP CAUTION MESSAGE. FOUND ENGINE OIL SYSTEM OVERFILLED. DRAINED SYSTEM AND SERVICED TO PROPER LEVEL.Dec 8, 2004 · N918CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA041224004Door · separated(CAN) WHILE CLIMBING THRU 16,000 FT, THE FLT CREW HEARD A STRANGE NOISE. ALL COCKPIT INDICATIONS WERE NORMAL. UPON POST FLT INSPECTION, MAINTENANCE FOUND THE RT MAIN GEAR DOOR MISSING.Dec 3, 2004 · Cndair CL6002C10 · Landing Gear DoorsSDR COMA0470081Blade · dirtyFLIGHT 4997 - N1 VIBE, BECAME UNCONTROLLABLE. REPLACED THE ENGINE FAN BLADES.Nov 30, 2004 · N368CA · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR SIMA200433601Battery Pack · inoperativeDURING PREFLIGHT CHECK SOME OF THE EMERGENCY LIGHTS WOULD NOT COME ON. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY POWER SUPPLY BATTERY PACK IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501341)Nov 27, 2004 · N519AE · Cndair CL6002C10 · Emergency LightingSDR CA041129002Window · cracked(CAN) THE RT SIDE WINDOW CRACKED WHILE IN CRUISE. A NEW WINDOW WAS INSTALLED AS IAW AMM.Nov 23, 2004 · Cndair CL6002C10 · Flight Compartment Windows
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