GE CF34-3B1

Service difficulty reports · 5,402

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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 AMTA200700150Warning System · malfunctionedAFTER BLOCK OUT APU GEN OFF LIGHT ILLUMINATED, RESENT TURNED OFF GEN LIGHT AND APU DOOR EICAS MSG APPEARED. RESET CB APU BATT BUS. PERFORMED APU BITE IAW FIM 49-11-00, FIG 103, NO FAULTS. RAN APU NO DEFECTS FOUND. APU DOOR CLOSES ON SHUTDOWN. (K)Mar 22, 2007 · N552TZ · Boeing 75733N · APU Indicating SystemSDR COMA0760277Pump · faultyFLIGHT 9476 - EN ROUTE CVG-GRR LEFT ENGINE OIL PRESSURE INDICATION WAS ERRATIC, CREW DECLARED AN EMERGENCY AND PERFORMED AN IN-FLIGHT SHUTDOWN. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE LUBRICATION MODULE.Mar 22, 2007 · N451CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200740150Channel · crackedCARGO DOOR FWD TRUCK BOTTOM U-CHANNEL CRACKED APPROX .1 INCH LONG. (K) [SUP 05-09-07] MAINTENANCE REMOVED AND REPLACED CARGO DOOR FORWARD U-CHANNEL IAW CRJ 200 SRM 51-42-06. (M)Mar 20, 2007 · N416AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR COMA0760269Check Valve · faultyFLIGHT 9456 - EN ROUTE LGA-CVG RECEIVED A LEFT ENGINE WARNING MESSAGE, CREW DECLARED AN EMERGENCY AND PERFORMED AN INFLIGHT SHUTDOWN OF THE LEFT ENGINE. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE OIL PUMP CHECK VALVE.Mar 19, 2007 · N451CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA200718038Connector · shortedAFTER TAKEOFF ACCESS BUSS CAUTION MESSAGE AND FOLLOWED BY SEVERAL CAUTIONS MESSAGES. FOUND ADG XFER K2XD CONTACTOR HAD A SHORTED TERMINAL. REPLACED CONTACTOR, TERMINAL AND ESSENTIAL TRU 1. OPERATIONAL CHECKS GOOD.Mar 19, 2007 · N864AS · Cndair CL6002B19 · Electrical Power System WiringSDR TRAX200700397Turbine · crackedCRACK FOUND ON NR 2 ENGINE LPT AT 9 O'CLOCK POSITION MEASURING 0.300 INCH MARKED PER SB CF34-3B1-72-A022 01.Mar 19, 2007 · N837AS · Cndair CL6002B19 · Turbine SectionSDR A6WA200740142Support Bracket · crackedHYDRAULIC LINE SUPPORT BRACKET (ASSY PN 601R75262-153) CRACKED APPROX .1 INCH LONG IN CEILING RT WHEEL WELL FWD OF TRANSDUCER BRACKET. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-153 IAW CRJ 200Mar 19, 2007 · N416AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200740143Channel · crackedHYDRAULIC TRANSDUCER HOT CHANNEL (ASSY PN 601R75262-157) CRACKED APPROX 1 INCH LONG IN CEILING RT WHEEL WELL. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-157 IAW BSC STANDARD REPAIR 601R-53-0044Mar 19, 2007 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740144Channel · crackedHYDRAULIC TRANSDUCER HOT CHANNEL (ASSY PN 601R75262-159) CRACKED APPROX .1 INCH LONG IN CEILING LT WHEEL WELL. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-159 IAW BSC STANDARD REPAIR 601R-53-004Mar 19, 2007 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740152Skin · ground damageLAV TRUCK HIT AC - 4 INCH HOLE IN FUSELAGE FS 615, WL 73. MAINTENANCE PERFORMED A MAJOR REPAIR BY CUTTING AWAY DAMAGED SKIN AND INSTALLING A 14 INCH X 8 INCH EXTERNAL REPAIR DOUBLER IAW EO 601R-11202. (K)Mar 19, 2007 · N432AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA0703013Unknown · unknownCREW REPORTED A RIGHT PACK OFF EICAS MESSAGE ON TAKEOFF. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLEANED THE AIR CONDITION CONTROL PANEL IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE PERFORMEMar 19, 2007 · N216PS · Cndair CL6002B19 · Cabin Cooling SystemSDR CA070321013Ecu · malfunctioned(CAN) GROUND CREW REPORTED FLAMES FROM APU EXHAUST DURING PUSHBACK. COCKPIT HAD NO FIRE INDICATIONS. CREW SHUTDOWN AND PASSENGERS DEPLANED. MAINTENANCE INSPECTED AND APU MEL`D. LATER MAINTENANCE TROUBLESHOOTING FOUND APU ECU WITH FAULT/ERROR CODES. APU ECU REPMar 19, 2007 · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA200740140Intercostal · crackedRT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX .8 INCHES LONG. (K) [SUP 05-09-07] MAINTENANCE REMOVED AND REPLACED RIGHT FS 625 INTERCOSTAL AT STRINGER 14R IAW CRJ 200 SRM 51-42-06. (M)Mar 18, 2007 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740141Intercostal · crackedLT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. (K) [SUP 05-09-07] MAINTENANCE REMOVED AND REPLACED LEFT FS 625 INTERCOSTAL AT STRINGER 14L IAW CRJ200 SRM 51-42-06. (M)Mar 18, 2007 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740131Floor Support · crackedFS 280.0 FLOOR SUPPORT ANGLE PN 600-34017-595 CRACKED APPROX .2 INCHES LONG ON AFT SIDE FS 280.0 OB OF LBL 9.0. (K) [SUP 05-17-07] MAINTENANCE REPAIRED DAMAGED SECTION, DRILLED NEW SECTION OF ANGLE AND SPLICES IAW REO 601R-53-11-136 STEPS 1-6 ANGLE P/N 600-Mar 17, 2007 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740132Floor Support · crackedFS 280.0 FLOOR SUPPORT ANGLE PN 600-34017-595 CRACKED APPROX .2 INCHES LONG ON AFT SIDE FS 280.0 OB OF RBL 9.0. (K) [SUP 05-17-07] MAINTENANCE DAMAGED SECTION DRILLED NEW SECTION OF ANGLE AND SPLICES IAW BOMBARDIER REO 601R-53-11-136. (M)Mar 17, 2007 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740133Fitting · crackedFS 280.0 FLOOR SUPPORT CLIPS PN 601R3113-58 CRACKED APPROX .1 INCH LONG AT IB AND OB SIDE RBL 9.0. (K) [SUP 05-17-07] MAINTENANCE REPLACED INBOARD AND OUTBOARD CLIPS AT FS 280 RBL9 IAW CRJ SRM 51-40-11, 52-42-06 AND 51-42-21. (M)Mar 17, 2007 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740134Fitting · crackedFS 280.0 FLOOR SUPPORT CLIPS PN 601R31113-57 CRACKED APPROX .1 INCH LONG AT IB AND OB SIDE LBL 9.0. (K) [SUP 06-05-07] MAINTENANCE REPLACED INBOARD AND OUTBOARD CLIPS AT FS 280 LBL 9 IAW CRJ 200 SRM 51-40-11, 51-42-02, 51-42-21. (M)Mar 17, 2007 · N415AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740135Skin · corrodedRT WING PLANK ACCESS HOLE AT 640 AB HAS MINOR PITTING IN CRITICAL AND NON-CRITICAL AREA. (K) [SUP 06-05-07] MAINTENANCE CLEANED EDGE OF FUEL TANK ACCESS DOOR SKIN CUTOUT. BLENDED CORROSION IN DETAIL AREA I AND IV TO DEPTH OF .002 IAW STEPS 1-4 OF BOMBARDIMar 17, 2007 · N415AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740136Skin · corrodedRT WING PLANK ACCESS HOLE AT FUEL PANEL 650CB HAS MINOR CORROSION AROUND APPROX 90 PERCENT OF BONDING AREA. (K) [SUP 06-05-07] MAINTENANCE SANDED CORRODED AREA TO REMOVE DAMAGE MAX BLEND .004 IAW BSC EO NR 601R-57-11217. (M)Mar 17, 2007 · N415AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740145Support Bracket · crackedHYDRAULIC LINE SUPPORT BRACKET (ASSY PN 601R75262-153) JUST FWD OF TRANSDUCER IN CEILING OF RT MLG WHEEL WELL CRACKED APROX .1 INCH LONG. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-153 IAW CRJ SMar 16, 2007 · N415AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200740146Bracket · crackedHYDRAULIC TRANSDUCER BRACKET PN 601R75262-157 CRACKED APPROX .1 INCH LONG IN CEILING OF RT MLG WHEEL WELL. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-157 IAW CRJ SRM 51-42-06. (M)Mar 16, 2007 · N415AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200740147Channel · crackedHYDRAULIC TRANSDUCER HOT CHANNEL PN 601R75262-159 CRACKED APPROX .1 INCH LONG IN CEILING OF LT MLG WHEEL WELL. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-159 IAW CRJ SRM 51-42-06. (M)Mar 16, 2007 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740164Smoke Detector · malfunctionedSMOKE TOILET CASS MESSAGE AFTER TAKEOFF WITH LAV SMOKE ALARM ACTIVATED RAN QRH, MESSAGE EXTINGUISHED ALARM OFF F/A REPPORTED NO INDICATION OF SMOKE OR FIRE ON INSPECTION. RAN ENGINE WITH APU AIR SWITCH OVER TO BLEED AIR AND NO SMOKE CAUTION MESSAGE WITH EITHEMar 16, 2007 · N440AW · Cndair CL6002B19 · Smoke DetectionSDR A6WA200740158Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED AT PAX DOOR ASST PULLEY BRACKET. (K) [SUP 06-05-07] CUTOUT DAMAGED SECTION AND REPAIRED IAW BOMBARDIER REO 601R-52-11-513 REV A AND BSC EO 601R-52-11280. (M)Mar 15, 2007 · N415AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740148Angle · crackedLT FS 625.00 OBLIQUE ANGLE IS CRACKED 1.5 INCHES LONG IN AFT RADIUS. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-21 AND BSC EO 601R-53-11218. (M)Mar 14, 2007 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740149Angle · crackedRT FS 625.00 OBLIQUE ANGLE IS CRACKED 1.5 INCH LONG IN AFT RADIUS. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE NEW SERVICEABLE ANGLE P/N 601-35012-52 IAW CRJ SRM 51-42-21 AND BSC EO 601R-53-11207. (M)Mar 14, 2007 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740153Flap System · malfunctionedUPON FLAP SELECTION, FLAP FAIL MESSAGE APPEARED 8 DEGREES FLAP NOTED. (K) [06-13-07] REMOVED/REPLACED FLEX DRIVESHAFT SER NR 12973 TSN 25 CSN 23. REMOVED AND REPLACED FECU SER NR 1354 TSN 6945 CSN 6437. (M)Mar 13, 2007 · N421ZW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740201Sill · corrodedCARGO DOOR SILL PLATE HAS MINOR SURFACE CORROSION IN AREA OF NUTPLATES FROM FS 574 TO 621. (M) REPAIRED CARGO DOOR SILL PLATE IAW SRM 51-21-01 AND 51-25-01. (K)Mar 13, 2007 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740112Wire · damagedPROXIMITY SYSTEM FAULT WHITE STATUS MESSAGE. INSTALLED NEW WIRES FROM P4MB TO PROXIMITY SWITCH S38. WIRES INSTALLED WERE RED AND BLUE IAW WDM 20-12-00. OPS CHECK GOOD. (K)Mar 12, 2007 · N408AW · Cndair CL6002B19 · Landing Gear System WiringSDR A6WA200740118Flap · malfunctionedAFTER TAKEOFF WHILE RETRACTING FLAPS FROM 20 DEGREES. COMPLIED WITH QRH, FLAPS FAIL CAUTION MESSAGE ON ED1. COMPLIED WITH SUPPLEMENT 98-018A, NO FLAP TWISTING, SKEWING OR DEFORMATION NOTED. RESET CIRCUIT BREAKER ONCE, MESSAGE CLEARED, FLAPS OPERATE NORMALLYMar 12, 2007 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740113Warning System · activatedWHEN SELECTING FLAPS FROM 8 DEGREES TO 20 DEGREES, A FLAP CAUTION MESSAGE OCCURRED IN FLIGHT. (K)Mar 11, 2007 · N417AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740114Drive Shaft · lack of lubeFLAPS FAILED AT 20 AFTER DEPARTURE. CLEANED AND LUBRICATED ALL RT FLAP DRIVE SHAFTS. OPS CHECK GOOD. (K)Mar 11, 2007 · N421ZW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR VNAA0703007Bpsu · failedCREW REPORTED A FLAPS FAIL CAS MESSAGE ON DESCENT. CREW LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BRAKE AND POSITION SENSOR UNIT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.Mar 10, 2007 · N249PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740117Flap · malfunctionedFLAPS FAIL CAUTION WHILE IN FLIGHT, FAILED AT 30. COMPLIED WITH AWAC SUPPLEMENT 98-018A, NO FLAP TWISTING, SKEWING OR DEFORMATION NOTED. RESENT CIRCUIT BREAKERS ONCE, MESSAGE CLEARED. FLAPS OPERATE NORMALLY. PLACED ON 72 HOUR WATCH. (K)Mar 9, 2007 · N464AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740122Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED IAW REO 601R-52-11-513, REV A. (K)Mar 8, 2007 · N453AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740093Solenoid · leakingFUEL LEAK AND RUNNING DOWN BELLY SURFACE UNDER TAIL. FOUND APU FUEL SOLENOID LEAKING DRAINING OUT FUSELAGE BELLY DRAIN. DEACTIVATED APU, NO LEAK NOTED, REMOVED AND REPLACED FUEL SOLENOID AND O-RING AT LOWER ELBOW FITTING IAW AMM 49-31, NO LEAKS NOTED. (K)Mar 7, 2007 · N449AW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA200740106Proximity Switch · malfunctionedCLIMBING THRU 14,000 FT GOT PAX DOOR LATCH CAUTION MESSAGE, FOLLOWED BY PAX DOOR (RED) WARNING MESSAGE, COMPLIED WITH QRH NO PRESSURIZATION PROBLEM NOTED. NO ABNORMAL NOISE OR ALIGNMENT INDICATION NOTED. DIVERTED, RED WARNING MESSAGE CLEARED BELOW 16,000 FT,Mar 7, 2007 · N404AW · Cndair CL6002B19 · Door Warning SystemSDR CA070308003Gearbox · failed(CAN) DURING CLIMB, THE RT ENGINE WAS NOT ABLE TO ACHIEVE CLIMB POWER. THE AIRCRAFT DIVERTED TO ANOTHER AIRPORT AND LANDED UNEVENTFULLY. INVESTIGATION REVEALED THAT THE THROTTLE GEARBOX HAS AN AREA WHERE MOVEMENT OF THE THROTTLE HAS NO EFFECT ON THE MFC. THIS Mar 7, 2007 · Cndair CL604 · Power LeverSDR A6WA200740095Proximity Switch · defectiveINFLIGHT, PAX DOOR WARNING MESSAGE. COMPLIED WITH QRH CHECKLIST, LANDED AT 46,000. REMOVED AND REPLACED PS5MB AND PS6MB PROXIMITY SWITCHES IAW AMM 52-70-04. OPS CHECK OF PASSENGER DOOR GOOD. PSEU FOUND NO FAULTS. (K)Mar 6, 2007 · N404AW · Cndair CL6002B19 · Door Warning SystemSDR VNAA0703006Flap System · malfunctionedCREW REPORTED A FLAPS FAIL CAS MESSAGE ON DESCENT. MAINTENANCE INSPECTED AND COMPLIED WITH THE SERVICE LETTER 00-001. SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.Mar 6, 2007 · N202PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740092Connector · defectiveCIRCUIT BREAKER PANEL 1, K3 POPPED (WEATHER RADAR RT). REMOVED AND REPLACED RADAR ANTENNA ELEC CONNECTOR AND WEATHER RADAR ANTENNA IAW AMM 34-41-01. REMOVED AND REPLACED WEATHER RADAR CONTROL PANEL IAW 34-41-04, RAN OPS CHECK OF WEATHER RADAR IAW AMM 34-41-0Mar 5, 2007 · N428AW · Cndair CL6002B19 · Navigation System WiringSDR A6WA200740094Service Door · malfunctionedSERVICE DOOR WILL NOT OPEN. CYCLED DOOR, OPENED NORMAL. (K)Mar 5, 2007 · N410AW · Cndair CL6002B19 · Service DoorsSDR A6WA200740091Flt Controls · unknownABORTED TAKEOFF AT 110 KNOTS. FLIGHT CONTROLS FELT UNRESPONSIVE IN ROLL, CONTROL YOKE FULL LT DEFLECTION, AIRCRAFT STILL WANTED TO ROLL RT. MAX BTMS = 5, TOW =40,800. INSPECTED AILERON RUDDER, ELEVATOR FLAPS, SPOILERONS, STAB TRIM, RUDDER TRIM AND AILERON TMar 4, 2007 · N470ZW · Cndair CL6002B19 · Flight Control SystemSDR VNAA0703003Oil System · lowCREW REPORTED A NR 2 IDG CAS MESSAGE ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE IDG NR 2 OIL LEVEL LOW. MAINTENANCE PROPERLY SERVICED THE OIL LEVEL IAW MM. AIRCRAFT WAS RELEASED FOR Mar 4, 2007 · N251PS · Cndair CL6002B19 · AC Generation SystemSDR A6WA200740098Bulkhead · crackedVISUAL INDICATION OF CRACK IN FWD PRESSURE BULKHEAD FS202.75, WL69.0, LBL23.71 (JUST BELOW PARKING BRAKE CABLE). MEASURES APPROX 1.0 INCH LONG. MAINTENANCE CUT-OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-11-563. (K)Mar 4, 2007 · N450AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200740116Acm · malfunctionedCABIN FILLED WITH VISIBLE SMOKE. SHUTDOWN PACKS, SMOKE DISSIPATED. TROUBLESHOT SYSTEM FOUND RT AIR CYCLE MACHINE BAD. REMOVED AND REPLACED RT AIR CYCLE MACHINE IAW 21-51-10. OPS CHECK GOOD. (K)Mar 3, 2007 · N461AW · Cndair CL6002B19 · Cabin Cooling SystemSDR VNAA0703002Pseu · failedCREW REPORTED A PAX DOOR/SERVICE DOOR CAUTION MESSAGE IN FLIGHT. CREW DIVERTED TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PROX SENSOR ELECTRONIC UNIT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FORMar 3, 2007 · N244PS · Cndair CL6002B19 · Door Warning SystemSDR A6WA200740090Relay · damagedON AC SYNOPTIC PAGE, ADG BUSS DISPLAYED IN WHITE. AC1 AND AC2 BUSS SHOW WHITE LINES TO ESS BUSS, ESS BUSS IS GREEN. REMOVED AND REPLACED ADG ESSENTIAL TRANSFER CONTACTOR (KX2D). PERFORMED OPS CHECK, OPS CHECK GOOD. REF AMM 24-51-31. (K)Mar 2, 2007 · N448AW · Cndair CL6002B19 · Alternator-Generator DriveSDR A6WA200740111Relay · failedON AC ELECTRICAL SYNOPTIC PAGE ADG BUS DISPLAYED IN WHITE. AC1 AND AC2 BUS SHOW WHITE LINES TO ESS BUS, ESS BUS IS GREEN. REMOVED AND REPLACED K2XD RELAY IAW AMM 24-51-31. OPS CHECK GOOD. (K)Mar 2, 2007 · N460AW · Cndair CL6002B19 · AC Power Distribution System
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