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 A6WA200740206Bracket · crackedRT HYDRAULIC TRANSDUCER BRACKET (PN 601R75262-157) CRACKED APPROX .2 INCH LONG IN RT MLG WHEEL WELL CEILING. INSTALLED NEW BRACKET IAW SRM 51-42-06. (K)Apr 18, 2007 · N417AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740200Flap System · malfunctionedFLAPS FAIL IN FLIGHT WHEN FLAPS 8 DEGREES SELECTED, FLAPS FAILED AT 0 DEGREES. VISUALLY INSPECTED EACH OB FLAP NO EVIDENCE OF TWISTING, SKEWING OR ABNORMAL DEFORMATION NOTED. OB FLAP POSITION INDICATION ARE NOT OUTSIDE GO RANGE. FLAP FAIL MESSAGE NOT ILLUMIApr 17, 2007 · N448AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0704009Switch · failedCREW REPORTED A STAB TRIM AND MACH TRIM CAUTION MESSAGE ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PITCH TRIM DISCONNECT SWITCH IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 27-4Apr 16, 2007 · N244PS · Cndair CL6002B19 · Stabilizer Control SystemSDR COMA0760317Flap System · failedFLAPS FAIL MSG AT 30 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE (FIRST EVENT) MAINTENANCE ACTION, PARAGRAPH (G) 1,2,3, (A,B,C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.Apr 14, 2007 · N720SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0760314Sensor · faultyDURING CLIMB WITH WING A-ICE SWITCHES OFF, RECEIVED WING OVERHEAT MSG WITH TRIPPLE AURAL CHIME AND RED INDICATION ON EICAS. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. REPLACED THE LT WING OVERHEAT SENSOR.Apr 13, 2007 · N816CA · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR TRAX200700511Oil System · lowLEFT ENGINE SHUTDOWN, LOW OIL. EMERGENCY DECLARED. FLTS 4449, 4578 CX.Apr 10, 2007 · N680BR · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA070413001Cowling · departed(CAN) A/C EXPERIENCED A THRUST REVERSER UNLOCK IN FLIGHT AT A CRUISE FLIGHT LEVEL OF 16000 FEET WITH AN APPROXIMATE SPEED OF 280 KNOTS. A SMALL VIBRATION IN THE AIRFRAME WAS FELT BY THE CREW PRIOR TO RECEIVING THE (REVERSER UNLOCK) MSG, FOLLOWED BY A LOUD BANApr 7, 2007 · Cndair CL6002B19 · Engine Thrust ReverserSDR TRAX200700474Support Beam · crackedLT ENGINE SUPPORT BEAM LOWER WEB CRACKED AT FWD IB NUT PLATE FOR ACCESS PANEL. [SUP 4-23-07] COMPLIED WITH ALL FAA APPROVED DATA.Apr 6, 2007 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR TRAX200700475Support Beam · crackedRT ENGINE SUPPORT BEAM LOWER WEB CRACKED AT FWD INBD NUT PLATE FOR ACCESS PANEL [SUP 4-23-07] REPAIRED IAW ALL FAA APPROVED DATA.Apr 6, 2007 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR TRAX200700476Unknown · unknownFLAPS FAIL CAUTION WHEN FLAPS SELECTED TO 8 STAYED AT 0 THE WHOLE TIME (EMERGENCY DECLARED).Apr 6, 2007 · N920EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740188Unknown · odorSTRONG FUEL ODOR IN COCKPIT AFTER ENGINE SHUTDOWN, APU IS RUNNING. PERFORMED INSPECTION OF FUEL LINES AND FUEL DRAINS, NO FUEL ODORS OR LEAKS DETECTED AT THIS TIME, OK FOR RETURN TO SERVICE. (K)Apr 6, 2007 · N427ZW · Cndair CL6002B19 · Air Distribution SystemSDR TRAX200700471Skin · crackedRANRC 390. LT BONDED SKIN COMMON TO FS 640.00 FRAME IS CRACKED. COMPLIED WITH LT BONDED SKIN FS 640 REPAIR, IAW EC/TC REO 601R-53-61-506 (JA10220/RA328) 04/12/07.Apr 5, 2007 · N830AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR TRAX200700472Flap System · failedFLAPS FAIL ON APPROACH WHEN SELECTING FROM 0 DEG TO 8 DEG. {EMERGENCY DECLARED}Apr 5, 2007 · N889AS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0704002Trim Switch · dirtyCREW REPORTED THE STAB AND MACH TRIM FAILED ON TAKEOFF. CREW ELECTED TO RETURN TO CHO AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE F/O'S CONTROL WHEEL. MAINTENANCE CLEANED THE HORIZONTAL STAB TRIM SWITCHES ON F/O'S CONTROL WHEEL. MAINTENANCE PERFApr 5, 2007 · N218PS · Cndair CL6002B19 · Stabilizer Control SystemSDR A6WA200740187Unknown · warning lightLT WINDSHIELD HEAT MESSAGE ILLUMINATED IN FLIGHT. COMPLIED WITH QRH. [07-31-07] COMPLIED WITH CONNECTION OF SPARE TEMP SENSORS IAW AMM 30-41-06. OPS CHECK GOOD. (K)Apr 5, 2007 · N410AW · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR VNAA0704001Oil System · lowCREW REPORTED THE NR 2 GENERATOR KICKED OFF LINE DURING TAKEOFF ROLL. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 2 ENGINE IDG. MAINTENANCE PROPERLY SERVICED THE IDG OIL LEVEL. MAINTENANCE PERFORMED OPS Apr 4, 2007 · N247JS · Cndair CL6002B19 · AC Generator-AlternatorSDR CA070409002Plug · missing(CAN) AFTER TAKEOFF FROM SOUTH BEND (SBN), THE AIRCRAFT CLIMBED TO FL 290. SHORTLY AFTER REACHING CRUISE ALTITUDE, THE RT ENGINE OIL PRESS WARNING ILLUMINATED FOLLOWED BY A DROP IN THE OIL PRESSURE ON THE RT OIL PRESSURE GAUGE. THE FLIGHT CREW PERFORMED THE QApr 4, 2007 · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR REXA200700051Plug · missingAFTER TAKEOFF FROM SBN, THE AIRCRAFT CLIMBED TO FL290. SHORTLY AFTER REACHING CRUISE ALTITUDE, THE RIGHT ENGINE OIL PRESSURE WARNING ILLUMINATED FOLLOWED BY A DROP IN OIL PRESSURE ON THE RT OIL PRESSURE GAUGE. THE FLIGHT CREW PERFORMED THE QRH AND REDUCED POApr 3, 2007 · N8836A · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200740181Angle · cracked625 OBLIQUE ANGLE CRACKED IN RADIUS APPROX 1.0 INCH LONG, LT SIDE. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE, P/N 601-35012-51, IAW CRJ SRM 51-42-06. (M)Apr 3, 2007 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740182Angle · cracked625 OBLIQUE ANGLE CRACKED IN RADIUS APPROX 1.0 INCH LONG, RT SIDE. (K) [SUP 5-1-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601-35012-52, IAW CRJ SRM 51-42-06. (M)Apr 3, 2007 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740184Fan · obstructedREQUEST INSPECTION OF ODOR IN BACK OF AIRPLANE. INSPECTED AIRCRAFT FOR ODORS, NO SIGNS OF ELECTRICAL DISCREPANCIES. CLEANED CABIN TEMP SENSOR FAN, DUE TO BLOCKAGE, FAN CHECKS OK. DETERMINED ODOR FROM LAV. OK FOR SERVICE AT THIS TIME. (K)Apr 3, 2007 · N456ZW · Cndair CL6002B19 · Cabin Temperature SensorSDR CA070404003Wire Harness · damaged(CAN) DURING AN INSPECTION, THE RUDDER POSITION TRANSMITTER HARNESS WAS FOUND TO BE DAMAGED. THE CAUSE OF THE DAMAGE WAS FOUND TO BE IMPROPER ROUTING BY COMPARING WITH ANOTHER A/C S/N 7163. THE ACTUAL ROUTING DRAWING WHERE REQUESTED FROM BOMBARDIER AND THE HARApr 3, 2007 · Cndair CL6002B19 · Flight Control System WiringSDR A6WA200740168Floorbeam · crackedRT FS 484.0 ANGLE CRACKED APPROX .1 INCH LONG AT PRESSURE FLOORBEAM RBL 27.0. (K) [SUP 5-1-07] MAINTENANCE REMOVED CRACKED ANGLE AT FS 484 RBL 27 ON THE PRESSURE FLOORBEAM AND INSTALLED A NEW SERVICEABLE ANGLE P/N 601R31171-9 IAW CRJ 200 SRM 51-42-06 AND 51Apr 2, 2007 · N451AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740169Angle · crackedLT FS 484.0 ANGLE CRACKED APPROX .1 INCH LONG AT PRESSURE FLOOR SUPPORT BEAM LBL 27.0. (K) [SUP 5-1-07] MAINTENANCE REMOVED ANGLE AT FS 484 LT LBL 27 IAW CRJ 200 SRM 51-42-06 AND FABED A NEW ANGLE FROM S6144-14 EXTENSION AND INSTALLED NEW ANGLE IAW BSC SR 6Apr 2, 2007 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740171Intercostal · crackedRT FS 484.0 INTERCOSTAL CRACKED APPROX .1 INCH LONG AT PRESSURE FLOORBEAM RBL 36.0. (K) [SUP 5-1-07] MAINTENANCE CUT AWAY DAMAGED ATTACHMENT FLANGE FABRICATED ANGLE FROM S6144-14 AND INSTALLED ANGLE IAW BOMBARDIER REO 601R-53-41-059A AND BSC SR 601R-53-0030A.Apr 2, 2007 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740172Floor Support · crackedRT FS 621.00 FLOOR SUPPORT ANGLE CRACKED APPROX .5 INCH LONG. (K) [SUP 5-1-07] MAINTENANCE REMOVED DAMAGED SECTION OF THE RIGHT FLOOR SUPPORT ANGLE AT FS 621 AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-53-61-117. (M)Apr 2, 2007 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740183Unknown · unknownUPON LANDING THRUST REVERSERS WOULD NOT DEPLOY UNTIL AFTER 3,000 FT ROLLOUT, NEITHER REVERSER WOULD UNLOCK UNTIL BRAKES TOOK EFFECT. PERFORMED BRAKES OPS TEST IAW 32-43-00, PERFORMED ANTI-SKID COMPUTER BITE TEST IAW 32-44-06. INTERROGATED MDC, NO FAULTS FOUNApr 2, 2007 · N468AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA200740185Pcu · malfunctionedVIBRATION NOTED AT 10,000 FT AIRSPEED 310 KNOTS, SLOWED TO 260 KNOTS, VIBRATION STOPPED. GEAR WAS UP. REMOVED AND REPLACED RT SPOILER PCU REF AMM 27-62-01, OPS CHECK GOOD AT THIS TIME. REMOVED SPOILER PCU SER NO MAL 5041, PN 270007, TSN: 11492 CSN: 10286. Apr 2, 2007 · N417AW · Cndair CL6002B19 · Drag Control SystemSDR A6WA200740179Attach Fitting · crackedPAX DOOR ASSIST MOTOR SUPPORT FITTING (PN 601R317745-7) CRACKED APPROX .2 INCHES LONG. (K)Apr 1, 2007 · N457AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740180Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE CRACKED APPROX 1.5 INCH LONG. (K) [SUP 05-09-07] MAINTENANCE CUTOUT DAMAGED SECTION AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-53-11-513 REV A. (M)Apr 1, 2007 · N457AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA070404009Control Unit · malfunctioned(CAN) SHORTLY AFTER TAKEOFF, FLIGHT EXPERIENCED A HSTA RUNAWAY. ACFT HAD JUST DEPARTED RUNWAY AND FLAPS WERE RETRACTED TO 0 DEGREES. AUTOPILOT DISENGAGED. TRIM SELECTION INPUT MADE. STABILIZER TRIM CONTINUED TO RUN & ASSOCIATED AURAL ALERT SOUNDED. IMMEDIATApr 1, 2007 · Cndair CL6002B19 · Stabilizer Control SystemSDR A6WA200740166Intercostal · crackedLT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL AT STRINGER 14L BETWEEN FS 621 AND 625.30 IAW CRJ 200 SRM 51-42-06. (M)Mar 31, 2007 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740167Intercostal · crackedRT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX .9 INCH LONG. (K) [SUP 05-01-07] MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL FROM 621 TO 625.30 AT STRINGER 14R IAW CRJ 200 SRM 51-42-06. (M)Mar 31, 2007 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740174Floor Support · crackedRT FS 621.0 FLOOR SUPPORT ANGLE CRACKED APPROX.3 INCH LONG. (K) [SUP 05-01-07] MAINTENANCE CUT AWAY CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)Mar 31, 2007 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740175Floor Support · crackedLT FS 621.0 FLOOR SUPPORT ANGLE CRACKED APPROX .3 INCH LONG. (K) [SUP 05-01-07] MAINTENANCE CUT AWAY CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)Mar 31, 2007 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740176Angle · crackedLT FS 484.0 ANGLE AT LBL 27.0 CRACKED APPROX .1 INCH LONG AT FLOOR SUPPORT BEAM. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-54-41-059 REV A AND BSC SR 601R-53-0029B. (M)Mar 31, 2007 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740177Intercostal · crackedLT FS 484.0 INTERCOSTAL CRACKED AT LBL 36.0 APPROX .1 INCH LONG AT FLOOR SUPPORT BEAM. (K) [SUP 05-09-07] MAINTENANCE CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR FLANGE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BSC SR 601R-53-0030A. (M)Mar 31, 2007 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740178Intercostal · crackedRT FS 484.0 INTERCOSTAL CRACKED AT RBL 36.0 APPROX .1 INCH LONG AT FLOOR SUPPORT BEAM. (K) [SUP 5-9-07] MAINTENANCE CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR FLANGE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BSC SR 601R-53-0030A. (M)Mar 31, 2007 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740173Skin · corrodedWING PLANK AT WS 54.897 HAS SEVERAL PITS ON AFT EDGE THE DEEPEST IS .005 INCH. (K) [SUP 05-01-07] MAINTENANCE REMOVED CORROSION AND REPAIRED AREA IAW REO 601R-57-21-030. (M)Mar 30, 2007 · N457AW · Cndair CL6002B19 · Wing, Plate/SkinSDR VNAA0703022Fuel Sys · leakingMAINTENANCE REPORTED SMELLING FUMES WHILE INSIDE THE COCKPIT AFTER TROUBLESHOOTING THE APU AND THE APU RUNNING. MAINTENANCE INVESTIGATED AND FOUND THE APU ON FIRE. FIRE WAS EXTINGUISHED USING THE APU FIRE BOTTLE. MAINTENANCE INSPECTED AND FOUND A FUEL LEAK Mar 30, 2007 · N237PS · Cndair CL6002B19 · APU Engine Fuel and ControlSDR CA070404011Apu · failed(CAN) TECHNICIAN WAS TROUBLESHOOTING THE APU FOR APU AUTO SHUTDOWN, LOSS OF APU DOOR POSITION ON STATUS PAGE. ECU CODE: 109,224,91 MAINTENANCE FOUND THE ELECTRICAL CONNECTOR FOR OIL TEMP SENSOR PARTIALLY INSTALLED ( CODE 91). RESECURED THE CONNECTOR AND PROCMar 30, 2007 · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) SystemSDR A6WA200740163Access Panel · corrodedLT LOWER WING PLANK FUEL ACCESS PANEL CUTOUT FOR FUEL PNL 540 CB HAS CORROSION IN NON-CRITICAL AREA APPROX 6.0 INCHES DEEP AND .020 WIDE. (K) [SUP 05-17-07] MAINTENANCE REPAIRED CORROSION BY BLENDING OUT CORROSION. PERFORMED NDT, ROTO PEENED AREA, SANDED RMar 28, 2007 · N416AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740160Support · crackedINTERCOSTAL SUPPORT FOR THE NR 1 HYDRAULIC PRESSURE/RETURN FILTERS AS CRACKED APPROX .2 INCH AT THE LOWER AFT CORNER. (K) [SUP 05-09-07] MAINTENANCE REPAIRED SUPPORT IAW BSC EO 601R-53-11285 BY CUTTING OUT CRACK, LPI TO ENSURE CRACK REMOVED, PRIME AND PAINTMar 27, 2007 · N416AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740161Support · crackedINTERCOSTAL SUPPORT FOR THE NR 2 HYDRAULIC PRESSURE/RETURN FILTERS IS CRACKED APPROX .2 INCH AT THE LOWER AFT CORNER. (K) [SUP 05-09-07] MAINTENANCE REPAIRED SUPPORT IAW BSC EO 601R-53-11285 BY CUTTING OUT DAMAGE, LPI TO ENSURE CRACK REMOVED, PRIME AND PAINMar 27, 2007 · N416AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740157Unknown · odorAFTER ROTATION, NOTICED ODOR LIKE (BURNED TOAST) IN COCKPIT. FLIGHT ATTENDANT REPORTED SIMILAR ODOR IN CABIN, STRONGER TOWARDS THE REAR OF THE CABIN. BOTH PACKS OPERATING ON APU. TRANSFERRED TO ENGINE BLEEDS, SMELL DISSIPATED. NO VISIBLE SMOKE SEEN. OPS CMar 27, 2007 · N409AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA200740156Controller · malfunctionedPITOT BASE HEAT CAUTION MESSAGE CAME ON AFTER TAKEOFF. QRH COMPLIED WITH, UPON LANDING TAT PROBE HEAT, LT STATIC HEAT, LT AOA HEAT, RT STATIC HEAT, AND RT AOA HEAT CAUTION MESSAGE ALL CAME ON. REMOVED AND REPLACED ADS NR1 HEAT CONTROLLER IAW AMM 30-13-15 ANDMar 25, 2007 · N412AW · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR A6WA200740155Flap System · malfunctionedFLAPS FAIL CAUTION MESSAGE ON DEPARTURE. INSPECTED FLAPS, NO EVIDENCE OF SKEW FOUND. RESET FLAP SYSTEM IAW AMM SUPPLEMENT 98-018B. FLAPS OPS CHECK OK. (K)Mar 25, 2007 · N461AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740162Vertical Beam · crackedFS 409.0 + 128.0 VERTICAL BEAM AT RBL 27.0 IS CRACKED .4 INCH. (K) [SUP 05-09-07] MAINTENANCE TRIMMED OUT DAMAGED AREA, PERFORMED EDDY CURRENT, FABRICATED REPAIR ANGLE AND INSTALLED IAW BOMBARDIER REO 601R-53-41-056 REV E AND BSC EO 601R-53-11286. (M)Mar 24, 2007 · N416AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6W2007F00000Duct · crackedINSPECTED APU AND FOUND UPPER AND LOWER INTAKE DUCTS CRACKED BEYOND LIMITS IAW AMM 49-14-01. REMOVED AND REPLACED UPPER AND LOWER APU INTAKE DUCTS. OPERATIONAL CHECK GOOD IAW 49-52-01. UPPER DUCT, TSN 7728, LOWER DUCT, TSN 11740. (K)Mar 23, 2007 · N405AW · Cndair CL6002B19 · APU Bleed Air SystemSDR VNAA0703016Light · odorCREW REPORTED A STRONG ELECTRICAL ODOR COMING FROM THE LAVATORY AREA. MAINTENANCE INSPECTED THE LAV AND SURROUNDING AREA INCLUDING OPS TESTING THE LAV LIGHT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPS TEST GOOD, NO DEFECTS NOTED AT THIS TIME. MAMar 23, 2007 · N226JS · Cndair CL6002B19 · Passenger Compartment Lighting
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