British Aerospace BAE 146 SERIES 300A

Service difficulty reports · 481

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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 aircraft_model_key = 'BAE146300A'
  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 AU510002205Hose · failedNOSE LANDING GEAR RETRACTION ACTUATOR FLEXIBLE HYDRAULIC HOSE RUPTURED. LOSS OF GREEN SYSTEM HYDRAULIC FLUID.Dec 12, 2005 · Bag BAE146300A · Landing Gear Retraction/Extension SystemSDR AU510001941Frame · cracked(AUS) FUSELAGE FRAME 41 AND FRAME 43 CRACKED. FOUND DURING INSPECTION IAW AD/BAE146/116. (OTHER CAUSE: MATERIAL ) (CASA NR 510001941)Dec 12, 2005 · Bag BAE146300A · Fuselage Main, FrameSDR AU510001940Frame · cracked(AUS) FUSELAGE FRAME 43 CRACKED. FOUND DURING INSPECTION IAW AD/BAE146/116. (OTHER CAUSE: MATERIAL ) (CASA NR 510001940)Dec 12, 2005 · Bag BAE146300A · Fuselage Main, FrameSDR AU510001797Jackshaft · corroded(AUS) LT CENTER AND RT OB LIFT SPOILER JACKS CORRODED BEYOND LIMITS IN PISTON THREADS FOR EYE ENDS. FOUND DURING INSPECTION IAW AAES ER BA6-27-60-23B AND BAE SYSTEMS SB 27-176. (CASA NR 510001797)Dec 12, 2005 · Bag BAE146300A · Drag Control ActuatorSDR AU510001750Indicator · damaged(AUS) AIRCRAFT EXPERIENCED A HIGH SINK RATE DURING LANDING. INVESTIGATION FOUND THAT THE MAIN LANDING GEAR AND TAILSKID CONTACTED THE GROUND CAUSING DAMAGE TO THE TAIL STRIKE INDICATOR. (CASA NR 510001750)Dec 12, 2005 · Bag BAE146300A · Auxiliary Gear (Tail Skid)SDR AU510001495Selector · failedLANDING GEAR SELECTOR LEVER WOULD NOT MOVE TO THE `UP` POSITION.Dec 12, 2005 · Bag BAE146300A · Landing Gear SelectorSDR AU510001709Wire · shortedRT INNER FUEL BOOST PUMP PRESSURE SWITCH TO PRINTED CIRCUIT BOARD WIRE SHORT CIRCUITED.Oct 8, 2005 · Bag BAE146300A · Fuel System WiringSDR AU510001967Bolt · shearedCENTER FUEL TANK WING SPAR ATTACHMENT BOLTS (4OFF) HAD SHEAR BOLT HEADS. FUEL LEAKING FROM CENTER TANK AT RT FRONT CORNER ABOVE THE WING TO FUSELAGE ATTACHMENT LINK AT FRAME 26 RIB 2.Jun 10, 2005 · Bag BAE146300A · Wing SparSDR AU510001664Hinge · corrodedRT MAIN LANDING GEAR DOOR HINGE FITTINGS CORRODED IN BORES. BEARING HOUSINGS ALSO CONTAINED PITTING AND RUST DEPOSITS ON THE OUTER SURFACES. FOUND DURING INSPECTION IAW BAE SYSTEMS ISB 52-113 REV 1 AND AAES AD ER BA6-32-10-43B AND UK CAA AD G-2005-0017.Feb 8, 2005 · Bag BAE146300A · Landing Gear DoorsSDR A6WA200460066Acm · odorNR 2 PACK WAS INADVERTENTLY SWITCHED ON FOR APPROX 10 MINUTES ENROUTE. PILOTS NOTICED ODOR IN COCKPIT, PACK SWITCHED OFF AND A PUFF OF WHITE SMOKE CAME OUT OF VENT IN COCKPIT THEN SMOKE ODOR DISSIPATED. MAINTENANCE REMOVED AND REPLACED RIGHT HAND AIR CYCLE MDec 30, 2004 · N616AW · Bag BAE146300A · Cabin Cooling SystemSDR A6WA200460054Oxygen Mask · missingROWS 14 AND 16 DEF HAVE NR O2 MASKS INSTALLED IN PSU BOXES. MAINTENANCE INSTALLED PASSENGER ALL O2 MASKS AS REQUIRED IAW 35-20-45.Nov 10, 2004 · N612AW · Bag BAE146300A · Passenger Oxygen SystemSDR AUS20040512Rib · cracked(AUS) NR 1, NR 3 AND NR 4 PYLONS HAD NR 4 RIB CRACKED IN THE LOWER FLANGE RADIUS. PYLON NR 1, CRACK LENGTH 22.86MM (0.9IN) PYLON NR 3, CRACK LENGTH 12.7MM (0.5IN) PYLON NR 4, CRACK LENGTH 20.32 (0.8IN).Jun 15, 2004 · Bag BAE146300A · Nacelle/Pylon, Frame/Spar/RibSDR AUS20040501Firewall · cracked(AUS) APU FIREWALL CRACKED AT 7 O'CLOCK POSITION. FOUND DURING INSPECTION IAW AD/BAE146/053.Jun 10, 2004 · Bag BAE146300A · Fuselage Main, BulkheadSDR A6WA200460019Skin · scratchedAFT CARGO DOOR SCRATCHES BEYOND THE ALLOWABLE SRM LIMITS. MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS. MAINTENANCE CUT DAMAGED AREA OUT IAW BAE SRM 52-32-11 FIG 201 PARA 3B PER BAE FAX BARA/AVR/6767/04-DC. HFEC INSPECTION C/O ON CUT OUT REPAIR, NO CRACKS NJun 2, 2004 · N611AW · Bag BAE146300A · Cargo/Baggage DoorsSDR A6WA200460016Floorbeam · crackedCRACK LOCATED IN THE LOWER RADIUS OF FLOORBEAM 33B AT LBL 62.0 INCHES. MAINTENANCE REQUESTED REPAIRS FROM MFG SYSTEMS REF AVMAX FAX 611-1908002. REPAIRED IAW BAE FAX BARA/AVR/6759/04-DC AND BARA/AVR/6752/04-02. PRIMED IAW BAE 146 AMM 20-10-11. (M)May 26, 2004 · N611AW · Bag BAE146300A · Fuselage Main, Floor BeamSDR AUS20040444Computer · faulty(AUS) FLAP COMPUTER FAULTY.May 20, 2004 · Bag BAE146300A · Trailing Edge Flap Control SystemSDR AUS20040429Link · fractured(AUS) MAIN LANDING GEAR ASSISTOR JACK TRIANGULAR LINK FAILED AT JACK ATTACHMENT POINT.May 17, 2004 · Bag BAE146300A · Landing Gear Retraction/Extension SystemSDR AUS20040410Intercostal · corroded(AUS) AFT CABIN FLOOR INTERCOSTAL CONTAINED LEVEL 2 CORROSION ON THESIDE AND UPPER SURFACES. THE INTERCOSTAL DAMAGE WAS LOCATED INZONE 251 BETWEEN FRAMES 41 AND 53 AT BL9 LH. AREA OF CORROSION MEASURED 38.1MM (1.5 IN) IN LENGTH BY 3.175MM (0.125 IN) IN WIDTH AMay 17, 2004 · Bag BAE146300A · Fuselage Miscellaneous StructureSDR AUS20040405Frame · corroded(AUS) LT FUSELAGE FRAME 43 CONTAINED LEVEL 2 CORROSION ON THE FORWARD FACE AT FLOOR LEVEL. DAMAGE WAS LOCATED AT ZONE 20 FRAME 43 STA 726.9 AND WAS 38.1MM (1.5IN) LONG BY 38.1MM (1.5IN) WIDE AND 4.546MM (0.179IN) DEEP. CAUSE OF DAMAGE WAS ASSESSED AS ENVIRONMEMay 17, 2004 · Bag BAE146300A · Fuselage Main, FrameSDR AUS20040401Actuator · seized(AUS) RT NR 2 LIFT SPOILER ACTUATOR SPINDLE SEIZED IN LOCKED POSITION WITH THE ACTUATOR EXTENDED. FOUND DURING INSPECTION IAW AD/BA6-27-60-16D BAE MANDATORY ISB 27-137.May 17, 2004 · Bag BAE146300A · Drag Control ActuatorSDR A6WA200460014Fuel Control · fluctuatesWHILE IN VMC CLIMBING THROUGH 16000 FEET THE NR 3 ENGINE N1 FLUCTUATION FOLLOWED BY FUEL FLOW DROPPING TO ZERO. ENGINE WAS SHUTDOWN, REMAINDER OF FLT MIN N2 OF 8 PERCENT, N1 26, 10 PSI, OIL QUANT 3/4 FULL. MAINTENANCE REMOVED AND REPLACED NR 3 FUEL CONTROL UMay 9, 2004 · N611AW · Bag BAE146300A · Fuel Control/Turbine EnginesSDR AUS20040372Angle · corroded(AUS) RT REAR ENTRY SILL PLATE ATTACHMENT ANGLE CONTAINED LEVEL 2 CORROSION ON THE UPPER SURFACE. AREA OF CORROSION 48.26MM (1.9IN) LONG BY 20.8MM (0.82IN) WIDE AND 0.584MM (0.023IN) DEEP. LOCATION OF CORROSION, ZONE 252 STRINGER 19, BETWEEN FRAMES 41AND 43May 7, 2004 · Bag BAE146300A · Fuselage Miscellaneous StructureSDR AUS20040351Seat Track · corroded(AUS) SEAT TRACKS CORRODED. PN HC538J0343-001 RT IB SEAT TRACK FOUND CORRODED ON UPPER SURFACE. CORROSION MEASURES 106.68MM (4.2IN) LENGTH, 24.13MM (0.95IN) WIDTH WITH DEPTH OUT OF LIMITS. LOCATION, ZONE 251, FRAME 40, RBL 21 RT. REPORTED CAUSE OF DEFECT,May 6, 2004 · Bag BAE146300A · Fuselage, Seat/Cargo Attach FittingsSDR AUS20040345Bolt · corroded(AUS) FORWARD OUTER ATTACHMENT SPECIAL BOLT SHAFT CORRODED AND PLATING MISSING. CORROSION WAS LOCATED APPROXIMATELY 12.7MM (0.5IN) DOWN FROM THE BOLT HEAD. AREA OF CORROSION 25.4MM (1IN) IN LENGTH BY 9.39MM (0.370IN) IN WIDTH BY0.127MM (0.005IN) DEPTH.BOLTS AMay 6, 2004 · Bag BAE146300A · FastenersSDR AUS20040379Seat Track · corroded(AUS) CABIN FLOOR STRUCTURE CONTAINED LEVEL 2 CORROSION IN THE FOLLOWING AREAS: PN HC536H1063-001 RT OB SEAT TRACK END ON UPPER SURFACE. AREA OF CORROSION MEASURED 38.1MM (1.5IN) IN LENGTH BY 12.7MM (0.5IN) IN WIDTH WITH A DEPTH OF 2.54MM (0.10IN). CORROSIMay 5, 2004 · Bag BAE146300A · Fuselage, Seat/Cargo Attach FittingsSDR AUS20040357Frame · cracked(AUS) CABIN CROWN FRAME TO SKIN STRUCTURE ANGLE CLEATS (8OFF) CRACKED FROM BEND RADIUS EDGE. THE ANGLE CLEATS ARE LOCATED IN FOLLOWING AREAS: FRAME 19A BETWEEN STRINGERS 1 AND 2 LT. FRAME 19A BETWEEN STRINGERS 2 AND 3 LT 3. FRAME 19B BETWEEN STRINGERS 1 AND May 5, 2004 · Bag BAE146300A · Fuselage Main, FrameSDR AUS20040339Plate · corroded(AUS) INSP OF REAR CABIN WET AREA AT FLOOR LEVEL FOUND CORROSION IN FOLLOWING PLATES: SHEAR PLATE PN HC538H1183-000 LOCATED ON TOP OF LONGITUDINAL BEAM FRAME 43 RBL 34. CORROSION WAS LOCATED ON UPPER SURFACE MEASURING 17.018MM (0.67IN) LENGTH, 16.002MM (0.63May 5, 2004 · Bag BAE146300A · Fuselage Main, StructureSDR A6WA200460012Angle · crackedFOUND CRACK IN THE NR 4 PYLON AT THE FORWARD END OF THE CENTER ANGLE JUST AFT OF RIB NR 3. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 615-18830001. (M)Apr 12, 2004 · N615AW · Bag BAE146300A · Nacelle/Pylon Miscellaneous StructureSDR AUS20040237Pin · cracked(AUS) FAIL SAFE PIN ASSEMBLY OF THE RT FLAP TAB NR 2 HINGE BOLT CRACKED. FOUND DURING NDT INSPECTION.Mar 31, 2004 · Bag BAE146300A · Trailing Edge Flap Control SystemSDR AUS20040148Plate · corroded(AUS) RT ELEVATOR TAB NR 1 HINGE UPPER REINFORCEMENT PLATE CONTAINED LEVEL 2 CORROSION. CORROSION DIMENSIONS WERE 25.4MM (1IN) BY50.8MM (2IN) AND PENETRATING TO FULL DEPTH.Mar 3, 2004 · Bag BAE146300A · Elevator, Tab StructureSDR AUS20040129Bolt · cracked(AUS) RUDDER FIXED HINGE BOLT CRACKED UNDER BOLT HEAD. BOLT IS LOCATED AT VERTICAL STABILISER RIB 5. CRACK LENGTH 2.286MM (0.090IN). FOUND DURING NDT INSPECTION.Feb 26, 2004 · Bag BAE146300A · FastenersSDR AUS20040065Harness · faulty(AUS) NR 4 ENGINE FIRE WARNING SYSTEM WIRING HARNESS FAULTY.Feb 5, 2004 · Bag BAE146300A · Fire DetectionSDR AUS20031342Display · wrong part(AUS) ELECTRONIC DISPLAY UNIT (EDU) WAS INCORRECT PART. MANUFACTURERS AME PLATE WAS IN RED WHICH INDICATED THAT IT WAS AN ENGINEERING EVALUATION UNIT. THE AIRWORTHY UNITS HAVE A BLACK NAMEPLATE. AND CARRY THE PN 4066192-901. PERSONNEL/MAINTENANCE ERROR. UDec 12, 2003 · Bag BAE146300A · Flight Environment DataSDR A6WA200360044Skin · lightning strikeDAMAGE NOTED ON LEFT SIDE OF FUSELAGE DURING LIGHTNING STRIKE INSPECTION. EXIT BURN MARK LOCATED 8 INCHES AFT OF FRAME 19C BETWEEN STRINGER 21 AND 22 AT CENTER AND APPROX .375 INCH IN DIAMETER BY .010 INCHES DEPTH. MAINTENANCE BLENDED DAMAGE TO A SMOOTH MIRROOct 2, 2003 · N611AW · Bag BAE146300A · Fuselage Main, Plate/SkinSDR AUS20030929Gcu · failed(AUS) NR 1 GENERATOR CONTROL UNIT (GCU) FAILED.Sep 12, 2003 · Bag BAE146300A · AC RegulatorSDR AUS20030922Hose · ruptured(AUS) LT MLG RETRACTION JACK FLEXIBLE HYDRAULIC HOSE RUPTURED. LOSS OF GREEN SYSTEM HYD FLUID.Sep 10, 2003 · Bag BAE146300A · Landing Gear Retraction/Extension SystemSDR AUS20030830Seal · failed(AUS) LT GROUND SPOILER FLOW VALVE RETURN LINE CONNECTOR O-RING SEAL LEAKING. GRADUAL LOSS OF APPROXIMATELY TEN LITRES OF HYDRAULIC FLUID.Aug 17, 2003 · Bag BAE146300A · Drag Control SystemSDR AUS20030555Skin · corroded(AUS) LT AND RT LOWER WING SKINS CORRODED IN AREA OF FUEL PUMP WATER SCAVENGE GUARDS AT RIB 15. FOUND DURING INSPECTION IAW ER BA6-28-10-7 AND ISB 28-028.Jun 4, 2003 · Bag BAE146300A · Wing, Plate/SkinSDR AUS20030410Speed Brake · faulty(AUS) UNCOMMANDED AIRBRAKE OPERATION. EXTENSIVE INVESTIGATION AND TESTING COULD FIND NO CAUSE FOR THE PROBLEM.Apr 9, 2003 · Bag BAE146300A · Drag Control SystemSDR AUS20030363Pin · damaged(AUS) LT MAIN LANDING GEAR DIRECTIONAL LINK UPPER ATTACHMENT PIN FOUND TO BE MIGRATING FROM THE LUG LOCATED AT FRAME 29. LOCKING PLATE AND PIN INCORRECTLY FITTED. MAIN LANDING GEAR IS A NEWLYOVERHAULED UNIT AND HAD ONLY JUST BEEN FITTED TO THE AIRCRAFT 48CYCLEMar 23, 2003 · Bag BAE146300A · Main Landing Gear Strut/Axle/TruckSDR AUS20030121Skin · corroded(AUS) RT LOWER WING SKIN CHAFED ON WATER SCAVENGE PIPE DEBRIS GUARDS. CORROSION WAS ALSO FOUND IN THE SAME AREA BETWEEN FRAME 14 AND FRAME 15.Feb 6, 2003 · Bag BAE146300A · Wing, Plate/SkinSDR AUS20030120Skin · corroded(AUS) LT WING LOWER SKIN CORRODED BEYOND LIMITS. FOUND DURING X-RAY INSPECTION.Feb 6, 2003 · Bag BAE146300A · Wing, Plate/SkinSDR AUS20021456Wire · worn(AUS) NR 4 GENERATOR DIFFERENTIAL PROTECTION CIRCUIT WIRE XB108 CHAFED IN AREA ADJACENT TO IDG.Dec 28, 2002 · Bag BAE146300A · Electrical Power System WiringSDR AUS20021452Circuit Board · faulty(AUS) RT MAIN LANDING GEAR UPLOCK SENSOR PRINTED CIRCUIT BOARD (GJ21) FAULTY.Dec 10, 2002 · Bag BAE146300A · Landing Gear Position and WarningSDR AUS20021338Cable · chafed(AUS) NR 4 THROTTLE LEVER CABLE FOULING ON CENTER ROOF PANEL. PREVIOUS MAINTENANCE HAD BEEN CARRIED OUT FOR BATTERY PACK REPLACEMENT. PERSONNEL/MAINTENANCE ERROR.Nov 15, 2002 · Bag BAE146300A · Power LeverSDR AUS20021184Manifold · leaking(AUS) NR 3 ENGINE RT FUEL MANIFOLD LEAKING AT MANIFOLD TO COMBUSTOR CASE JOIN. EVIDENCE OF FIRE AROUND LEAK.Oct 18, 2002 · Bag BAE146300A · Engine Fuel DistributionSDR A6WA200260044Floor Support · corrodedCORROSION FOUND ON FLOOR SUPPORT STRUCTURE FRAME 15 - 2.5 INCH PORT OF AIRCRAFT CENTERLINE RIL.Oct 10, 2002 · Bag BAE146300A · Fuselage Miscellaneous StructureSDR AUS20021106Cooling Fan · failed(AUS) LT ELECTRONIC FLIGHT INDICATION SYSTEM (EFIS) FAN FAILED. INVESTIGATION FOUND FAN BLADE CRACKED AND RUBBING ON GRILL.Oct 7, 2002 · Bag BAE146300A · Air Distribution FanSDR AUS20020714Brake · overheated(AUS) BOTH LT MAIN LANDING GEAR BRAKES OVERHEATED TO 800 DEGREES C.Jul 6, 2002 · Bag BAE146300A · BrakeSDR AUS20020591Buss · failed(AUS) NR 2 AC BUS FAILED. THE FOLLOWING COMPONENTS WERE REPLACED:- 1. NR 4 GENERATOR CONTROL UNIT 2. GENERATOR LINE CONTACTOR 4XB33. NR 4 ENGINE GENERATOR AND CSDJun 13, 2002 · Bag BAE146300A · AC Generation System
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