GE CF34-3B1

Service difficulty reports · 5,402

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 = 'CF343B1'
  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 A6WA200540024Warning System · malfunctionedUPON GEAR RETRACTION, NOSE DOOR END GEAR DISAGREE WARNING MESSAGE ILLUMINATED. CYCLED NLG WITH LINKS ATTACHED OPS CHECK GOOD OK FOR RETURN TO SERVICE IAW. (K)Jan 28, 2005 · N449AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR VNAA0501010Warning Light · illuminatedDURING CLIMBOUT FROM BHM, AS THE FLAPS WERE RETRACTED TO ZERO DEGREES, THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2276 FOLLOWED THE QRH, CONTINUED THE FLIGHT TO PHL, AND MADE AN UNEVENTFUL LANDING. THE CREW DID DECLARE AN EMERGENCY AND THJan 27, 2005 · N230PS · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA200540027Skin · corrodedFOUND CORROSION ON RT LOWER WING PLANK UNDER THE FOLLOWING FUEL PANELS 640BB AND 650GB. PERFORMED A MAJOR REPAIR BY REMOVING CORROSION IAW REO. (K)Jan 27, 2005 · N414ZW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540028Skin · corrodedMWC 170 CORROSION EXISTS ON LOWER WING PLANK UNDER FUEL PANEL 510AB. PERFORMED A MAJOR REPAIR BY REMOVING CORROSION IAW REO. (K)Jan 27, 2005 · N414ZW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540026Bushing · migratedRT MLG AFT TRUNNION BUSHING IS MIGRATED .046 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 2ND OVERSIZED BUSHING MODIFIED TO A 1ST OVERSIZED IAW EO.Jan 26, 2005 · N414ZW · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR A6WA200540032Floor Support · crackedCABIN FLOOR SUPPORT STRUCTURE AT FS280, LBL 9.0. THE OB CLIP IS CRACKED IN RADIUS AT TOP. (K) REMOVED CRACKED CLIP AND INSTALLED NEW FABRICATED CLIP IAW BRAS EO 601R-53-5924. (M)Jan 26, 2005 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05096Channel · crackedDURING A C-CHECK, THE MLG WHEEL WELL CHANNEL AT FS 529, RHS UNDER THE UPLOCK BOX WAS FOUND BENT AND CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE MLG WHEEL WELL CHANNEL AT FS 529, RHS IAW EO. (K)Jan 26, 2005 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA050127004Lamp · burned(CAN) UPON LANDING THE CREW WHILE WORKING IN THE GALLEY AREA CLEANING UP NOTICED A BURNING ODOR. AFTER OPENING A SLIDING DOOR IN THE GALLEY THE FUMES BECAME STRONGER. MAINTENANCE REMOVED THE LIGHT COVER AND FOUND THE END OF THE BULB HAD BECOME HOT AND DISCOLJan 26, 2005 · Cndair CL604 · Passenger Compartment LightingSDR A6WA200540035Intercostal · crackedLT SIDE FS621 THROUGH 625.3 INTERCOSTAL AT STR 14L IS CRACKED IN RADIUS APPROXIMATELY 1.0 INCH. (K) REMOVED AND REPLACED INTERCOSTAL IAW CRJ 200 SRM 51-42-06. (M)Jan 25, 2005 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540036Intercostal · crackedRT SIDE FS621 THROUGH 625.3 INTERCOSTAL AT STR 14R IS CRACKED IN RADIUS APPROXIMATELY 1.0 INCH. FABRICATED INTERCOSTAL FROM S6144-3 7075 T62-050 INSTALLED IAW CRJ-200 SRM 51-42-06. (M) (K)Jan 25, 2005 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540034Rib · crackedMWC 60. RT WING STATION 53.6 BUTT RIB IS CRACKED .5000 INCH LONG IN UPPER AFT RADIUS. REPAIRED RT WING STATION 53.60 BATT RIB IAW MFG EO 601R-57-51-046, REV B.Jan 25, 2005 · N412AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA20050033Rib · crackedLT WING STATION 53.6 BUTT RIB IS CRACKED, 1 INCH LONG IN UPPER AFT RADIUS. REPAIRED LT WING STATION 53.60, BATT RIB IAW MFG REPAIR EO 601R-57-51-046, REV B.Jan 25, 2005 · N412AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540030Intercostal · crackedLT SIDE FS621 THROUGH FS 625.3 INTERCOSTAL AT STR 14L IS CRACKED IN RADIUS APPROXIMATELY 1.0 INCH LONG. (K) REMOVED AND REPLACED FS 621-625.3 INTERCOSTAL ANGLE AT STRINGER 14L IAW BRAS EO 601R-53-5933. (M)Jan 24, 2005 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540031Intercostal · crackedRT SIDE FS621 THROUGH FS623.3 INTERCOSTAL AT STR 14R IS CRACKED IN RADIUS APPROXIMATELY 1.1 INCH LONG. REMOVED AND REPLACED FS 621-625.3 INTERCOSTAL ANGLE AT STRINGER 14R IAW BRAS EO 601R-53-5933. (M) (K)Jan 24, 2005 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05080SConnector · dirtyDURING APPROACH, UPON GEAR EXTENSION THE CREW RECEIVED A LT MAIN GEAR DISAGREE MESSAGE WITH AN ASSOCIATED (GEAR DISAGREE) EICAS WARNING. THE CREW INITIATED A CLIMB TO PATTERN ALTITUDE TO RUN THE CHECK LISTS AND THEN HEARD A THUD FOLLOWED BY THE LT MLG COMING Jan 24, 2005 · N879AS · Cndair CL6002B19 · Landing Gear Position and WarningSDR MASA200500056Fuel Control · contaminatedASH 9432 CLT TO CLT, RETURNED TO THE FIELD FOR THE NR 2 HYDRAULIC SYSTEM LOW PRESSURE AND QUANTITY. MX FOUND EVIDENCE OF HYD FLUID IN THE LT WING FUEL SYSTEM. MX TOOK FLUID SAMPLES FROM E1 AND E2 FUEL FILTER. FOUND DAMAGED LINE IN RT TANK. MX COULD NOT REPJan 24, 2005 · N27172 · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR VNAA0501008Handle · unsecureAFTER TAKEOFF FROM DCA FLIGHT 2445 WAS CLIMBING THRU 8000 FT WHEN THE CARGO DOOR CAUTION MESSAGE ILLUMINATED. THE CREW DECIDED TO RETURN TO DCA TO HAVE MAINTENANCE INSPECT THE CARGO DOOR. NO EMERGENCY WAS DECLARED. NO LOSS OF PRESSURIZATION WAS REPORTED. TJan 23, 2005 · N220PS · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA200540038Support Bracket · crackedGPU RECEPTACLE IS BENT EXTERNAL DOOR WILL NOT CLOSE. REMOVED CRACKED SUPPORT ASSY AND INSTALLED NEW SUPPORT ASSY (PN 600-33283-33) IAW CRJ SRM, PAINTED IAW SRM. SOLID RIVETS INSTALLED IAW SRM. (K)Jan 23, 2005 · N413AW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR A6WA200540022Apu · failedAPU FAILED AND SHUTDOWN ON TAKEOFF ROLL AND ROTATION. TRIED TO RELIGHT ON DESCENT, RAN APPROXIMATELY 3 MINUTES AND SHUTDOWN. STRONG FUEL SMELL PRESENT IN CABIN. PERFORMED APU OPS CHECK IAW AMM. INSPECTED AND FOUND NO EVIDENCE OF FUEL LEAK. NO FAULTS ON ECJan 22, 2005 · N439AW · Cndair CL6002B19 · APU Core EngineSDR ASOA05053Vane · malfunctionedDURING TAKEOFF, THE STALL WARNING SYSTEM ACTIVATED EXCEPT THE PUSHER. THE AIRCRAFT DID NOT STALL. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT AOA VANJan 21, 2005 · N885AS · Cndair CL6002B19 · Stall Warning SystemSDR ASOA05054Regulator Valve · malfunctionedDURING CRUISE, AT APPROXIMATELY 37,000 FT, CREW RECEIVED A RT PACK HIGH TEMP MASTER CAUTION. CREW REQUESTED DESCENT TO 25,000 FT WHILE COMPLYING WITH CHECKLIST FOLLOWED BY THE RT PACK HIGH TEMP MASTER CAUTION GOING OUT. PACK DID NOT RESET OR COME ON. UPON LEJan 21, 2005 · N909EV · Cndair CL6002B19 · Pneumatic Distribution SystemSDR ASOA05055Light · inoperativeDURING A C-CHECK, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT LAMP BY THE SERVICE DOOR. (K)Jan 21, 2005 · N861AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05057Step · brokenDURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 21, 2005 · N886AS · Cndair CL6002B19 · Entrance StairsSDR VNAA0501007Connector · contaminatedFLAPS SELECTED TO 8 DEG ON APPROACH, FLAPS FAIL CAUTION MESSAGE ILLUM. RIGHT FLAPS INDICATED 0 DEG & LEFT 2 DEG. C/W QRH, DECLARED AN EMERGENCY, MADE AN UNEVENTFUL LANDING WITH ZERO FLAPS. MX DEPLOYED FLAPS TO 20 DEG, AIRCRAFT FERRIED TO DAY. MX INSPECTED Jan 20, 2005 · N226JS · Cndair CL6002B19 · Electrical ConnectorsSDR ASOA05050Step · brokenDURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE FORWARD ATTACH ROD. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE FORWARD ATTACH ROD. MAINTENANCE REMOVED AND REPLACED THE PASSENGER Jan 20, 2005 · N860AS · Cndair CL6002B19 · Entrance StairsSDR ASOA05046Nut · missingDURING A GROUND INSPECTION, THE FORWARD EMERGENCY FLOOR LEVEL FLOODLIGHT BY THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A NUT MISSING ON THE GROUND STUD TO THE FORWARD EMERGENCY FLOOR LEVEL FLOODLIGHT BY THE PASSENGER DOOR. OPERATIONAL Jan 19, 2005 · N902EV · Cndair CL6002B19 · FastenersSDR ASOA05047Priority Valve · malfunctionedDURING TAKEOFF, UPON GEAR RETRACTION, A LOUD NOISE FROM THE NOSE GEAR WAS NOTICED ACCOMPANIED BY A MOMENTARY (DISAGREE) WARNING AND TRIPLE CHIME. THE NOISE CONTINUED FOLLOWED BY THE NOSE GEAR RETRACTING WITH ALL INDICATIONS SHOWING NORMAL. AN EMERGENCY WAS DJan 19, 2005 · N846AS · Cndair CL6002B19 · Landing Gear SelectorSDR VNAA0501006Control Unit · failedDURING APPROACH TO PIT, WHEN THE FLIGHT SPOILER HANDLE WAS MOVED TO DEPLOY, A FLIGHT SPOILER FAULT WHITE STATUS MESSAGE WAS DISPLAYED. THE PILOT RETURNED THE FLIGHT SPOILER HANDLE TO THE NORMAL POSITION AND MADE AN UNEVENTFUL LANDING. NO INCORRECT FLIGHT SPOJan 18, 2005 · N251PS · Cndair CL6002B19 · Drag Control SystemSDR ASOA05036Support Beam · crackedDURING A C-CHECK, THE AFT EQUIPMENT BAY CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE AFT EQUIPMENT BAY CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO. (K)Jan 18, 2005 · N903EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR ASOA05037Clip · crackedDURING A C-CHECK, THE LT AND RT FS484 INTERCOSTAL AFT CLIPS OB WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT FS 484 INTERCOSTAL AFT CLIPS OB IAW EO. (K)Jan 18, 2005 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05038Clip · crackedDURING A C-CHECK, THE LT FS 484 INTERCOSTAL AFT CLIP IB WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 484 INTERCOSTAL AFT CLIP IB IAW EO. (K)Jan 18, 2005 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05039Plate · crackedDURING A C-CHECK, THE CARGO COMPARTMENT FLOOR LANDING SILL PLATE AT FS605 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT FLOOR LANDING SILL PLATE AT FS 605 IAW EO. (K)Jan 18, 2005 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05040Support Beam · crackedDURING A C-CHECK, THE RT LOWER OB ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT LOWER OB ENGINE SUPPORT BEAM AT BL 36.20 IAW EO. (K)Jan 18, 2005 · N903EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR ASOA05041Clip · crackedDURING A C-CHECK, THE RT IB CLIP AT FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT IB CLIP AT FS 280. (K)Jan 18, 2005 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05042Clip · crackedDURING A C-CHECK, THE LT AND RT CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT AND RT CLIPS AT FS 625. (K)Jan 18, 2005 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05043Tire · damagedAFTER DEPARTING, THE CREW WAS ADVISED THAT THE MLB TOWER HAD FOUND TIRE DEBRIS ON THE RUNWAY AND SUSPECTED IT WAS FROM THEIR AIRCRAFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT CONTINUED ON, LANDING SAFELY UPON ARRIVAL. MAINTENANCE FOUND DAMAGE TO THE RT IBJan 18, 2005 · N859AS · Cndair CL6002B19 · TireSDR ASOA05044Floor Support · crackedDURING A C-CHECK, THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 IAW EO. (K)Jan 18, 2005 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540020Seal · failedAFTER TAKEOFF, RECEIVED RED NOSE DOOR GEAR MESSAGE AND RED GEAR DISAGREE MESSAGE. REMOVED AND REPLACED NOSE LANDING GEAR STRUT SEALS. RESERVICED NLG STRUT, OPS CHECK GOOD. (K)Jan 18, 2005 · N404AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR A6WA200540021Connector · loosePASSENGER DOOR OUTER HANDLE MESSAGE ILLUMINATED DURING FLIGHT. DIVERTED, FOUND PAX DOOR HARNESS PLUG (P7MB) LOOSELY CONNECTED. REMOVED, INSPECTED AND CLEANED DOOR HARNESS. REPLACED DOOR HARNESS, OPS CHECK GOOD. (K)Jan 18, 2005 · N418AW · Cndair CL6002B19 · Door Warning SystemSDR VNAA0501014Control System · malfunctionedON SHORT FINAL INTO PHL THE FLAPS STUCK AT 30 DEGREES WHEN THE CREW OF FLIGHT 2304 SELECTED FLAPS 45. THE FLIGHT LANDED UNEVENTFULLY. PSA MAINTENANCE RESET CIRCUIT BREAKERS AND CYCLED THE FLAPS IAW BOMBARDIER SERVICE LETTER RJ-SL-00-001. THE FLAP SYSTEM OPEJan 17, 2005 · N228PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540019Coalescer Bag · dirtySUSPECT LT PACK. PERFORMED OPS CHECK OF BOTH LT AND RT PACKS. RT OPS NORMAL, LT PACK EMITS ODOR DURING OPERATION. REMOVED AND REPLACED COALESCER SOCK ON LT PACK. OPS CHECK NORMAL. (K)Jan 17, 2005 · N455AW · Cndair CL6002B19 · Humidity Control SystemSDR ASOA05034Light · inoperativeDURING A GROUND INSPECTION, AN EXTERNAL EMERGENCY LIGHT ON THE RT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EXTERNAL EMERGENCY LIGHT LAMP ON THE RT SIDE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 16, 2005 · N862AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05033Wire · pinchedDURING A GROUND INSPECTION, THE LOWER FORWARD EMERGENCY LIGHT ON THE BULKHEAD BY THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A WIRE TO THE LOWER FORWARD EMERGENCY LIGHT ON THE BULKHEAD BY THE PASSENGER DOOR PINCHED BY A TIE WRAP CAUSING Jan 15, 2005 · N902EV · Cndair CL6002B19 · Light System WiringSDR ASOA05027Cover · missingDURING A GROUND INSPECTION, THE EMERGENCY EXIT SIGN COVER BY THE PASSENGER DOOR WAS FOUND MISSING. MAINTENANCE INSTALLED AN EMERGENCY EXIT SIGN COVER BY THE PASSENGER DOOR. AIRCRAFT OK FOR SERVICE. (K)Jan 14, 2005 · N827AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05028Lamp · burned outDURING AN A-CHECK, THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 14, 2005 · N909EV · Cndair CL6002B19 · Emergency LightingSDR ASOA05029Lamp · burned outDURING HANGAR MAINTENANCE, THE LT EXTERIOR SECOND FROM THE FROM EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT EXTERIOR SECOND FROM THE FRONT EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 14, 2005 · N905EV · Cndair CL6002B19 · Emergency LightingSDR ASOA05030Step · brokenDURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (K)Jan 14, 2005 · N849AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05024Proximity Sensor · out of adjustAFTER TAKEOFF, THE CREW RECEIVED A (GEAR UP DISAGREE) MESSAGE. THE QRH WAS COMPLIED WITH, AND EMERGENCY DECLARED AND THE AIRCRAFT RETURNED TO DEPARTURE, LANDING SAFELY. MAINTENANCE ADJUSTED THE UPLOCK PROXIMITY TARGET ON THE LEFT MAIN LANDING GEAR (MLG). OPJan 12, 2005 · N820AS · Cndair CL6002B19 · Landing Gear Position and WarningSDR CA050115001Idg · inoperative(CAN) LOSS OF BOTH IDGS ON APPROACH FOLLOWED BY AN ADG DEPLOYMENT. NO PROBLEM WAS REPORTED WITH THE ADG. FLIGHT CREW DECIDED TO ABORT THE APPROACH. EMERGENCY WAS DECLARED. THE CREW DECIDED TO START DE APU TO POWER THE AIRCRAFT BUSES. THE AIRCRAFT LANDED. THJan 11, 2005 · Cndair CL6002B19 · AC Generation SystemSDR ASOA05022Light · inoperativeDURING A GROUND INSPECTION, THE EMERGENCY CEILING LIGHT AT ROW 14 A/B WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVE AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW 14 A/B. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 9, 2005 · N832AS · Cndair CL6002B19 · Emergency Lighting
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