Airbus Industrie A300 B4-203

Service difficulty reports · 1,357

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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 = 'A300B4203'
  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 WRNA201200006Gyro · unserviceableBOTH NR 1 & NR 2 YAW DAMPERS WOULD NOT ENGAGE. AIRCRAFT RETURNED TO AIRFIELD. LANDING NORMAL. MX FOUND NR 1 & NR 2 YAW RATE GYRO'S AT FAULT. REMOVED AND REPLACED NR 1 & NR 2 YAW RATE GYROS IAW 22-21-45. OP'S CHECK SATISFACTORY. A/C RETURNED TO SERVICE.May 11, 2012 · N821SC · Airbus A300B4203 · Speed-Attitude Correction SystemSDR WRNA201110210010Gps · malfunctionedNR 1 GPS MESSAGE "HEADING REQUIRED" RENDERING, GPS AND NR 1 AUTOPILOT INOPERATIVE. VECTORED SO ACFT STAYED ON HEADING MODE. AUTOPILOT NR 2 SELECTED BUT DID NOT ENGAGE. NOT SUCCESSFUL AFTER SEVERAL ATTEMPTS. RETURN TO AIRPORT. LANDED NORMAL. MX CHECKED WOct 21, 2011 · N821SC · Airbus A300B4203 · Global Positioning SystemSDR WRNA2009004Pitot Line · cloggedON TAKEOFF ROLL, DEPARTING FROM SJU, CREW NOTICED THAT THERE WAS NO AIRSPEED INDICATION FROM F/O INDICATOR. CAPTAIN INDICATOR SHOWING BETWEEN 75-80 KTS AND FLUCTUATING. ABORTED T/O PROCEDURES FOLLOWED. RETURNED TO GATE. MAINT FOUND PITOT LINES CLOGGED WITHDec 30, 2009 · N821SC · Airbus A300B4203 · Pitot/Static SystemSDR DHLA200900025Coalescer Bag · dirtyREPLACED NR 2 COALESCER P/N 20D10-3 IAW MM 21-51-16. THIS DOES NOT CLOSE DMI.Apr 14, 2009 · N364DH · Airbus A300B4203 · Humidity Control SystemSDR DHLA200900021Unknown · odorACFT HAS AN UNUSUAL ODOR COMING THRU THE A/C PACKS FLT DECK DUCT TEMP WAS AT 150 COMPT TEMP 68. RAN NR 1 AND NR 2 PACK SYS OPS CKED NORMAL ON GROUND IAW AMM 21-00-00 COULD NOT DUPLICATE NO UNUSUAL ODORSApr 1, 2009 · N364DH · Airbus A300B4203 · Air Distribution SystemSDR WRNA2009001Ground Wire · looseAFTER TAKEOFF, KRUEGER FLAP FAILED TO RETRACT. CREW REPORTED A "CONFIG" LIGHT ON MWP. ALSO, FLIGHT CHARACTERISTICS OF AIRCRAFT SEEMED DIFFERENT. DECISION MADE TO RETURN TO AIRFIELD. AIRCRAFT LANDED NORMAL, NO FUEL WAS DUMPED. MAINTENANCE UPON TROUBLESHOOTMar 17, 2009 · N501TR · Airbus A300B4203 · Flight Control System WiringSDR DHLA200800011AEngine · power lossDURING T/O ENG. 1 & 2 SPOOLED TO 60% N1, GO LEVERS SELECTED NR 1 ENG SPOOLED TO 80% N1 MAX, THROTTLE FULL FORWARD NO RESPONSE. OAT +5º C TAS LESS THAN 60KTS. REMOVED. CLEANED & INSTALLED PS-4 LINE. PERFORMED ACCELERATION CK ON NR 1 ENG. ENG. RUN OPS GOOD PEFeb 12, 2009 · N365DH · Airbus A300B4203 · Engine Fuel and ControlSDR WRN2009F00000Fire Loop · defectiveENGINE NR 1 SHUT DOWN IN FLIGHT DUE TO A FIRE INDICATION DURING FLIGHT FROM BDL TO BQN. BOTH FIRE BOTTLES WERE DISCHARGED. WARNING LIGHT EXTINGUISHED. ACFT LANDED NORMALLY. NO FUEL DUMPED. MX REPLACED 3 FIRE LOOPS AND AN AMPLIFIER. RUN UP CHECK OK. ACFTDec 19, 2008 · N510TA · Airbus A300B4203 · Fire DetectionSDR DHLA200800137Battery Pack · dischargedEMERGENCY LIGHTS BATTERIES 0 VOLTS.Dec 15, 2008 · N366DH · Airbus A300B4203 · Emergency LightingSDR DHLA200800108Battery Pack · inoperativeON PRE-DEPARTURE CHECK, EMERGENCY LIGHT OVER R1 DOOR INOPERATIVE, ACFT GROUNDED. R&R POWER SUPPLY IAW MM 33-51-14. OPS CHECKED OK IAW 33-51-00.Sep 30, 2008 · N367DH · Airbus A300B4203 · Emergency LightingSDR DHLA200800107Battery Pack · inoperativeON PRE-DEPARTURE CHECK, EMERGENCY LIGHT OVER R1 DOOR INOPERATIVE, ACFT GROUNDED. R&R POWER SUPPLY IAW MM 33-51-14. OPS CHECKED OK IAW 33-51-00.Sep 30, 2008 · N367DH · Airbus A300B4203 · Emergency LightingSDR DHLA200800106Power Supply · inoperativeON PRE-DEPARTURE CHECK, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE, ACFT GROUNDED. R&R POWER SUPPLY IAW MM 33-51-14. OPS CHECKED GOOD IAW 33-51-00.Sep 30, 2008 · N367DH · Airbus A300B4203 · Emergency LightingSDR WRN2008F00004Sill · fodAC AFTER TAKEOFF, LOUD WHISTLING NOISE HEARD AND AC HAD PROBLEMS PRESSURIZING. AC MADE UNSCHEDULED STOP, WITH NORMAL LANDING. FOUND F.O.D. AND DEBRIS IN MAIN CARGO DOOR SILL AREA. REMOVED F.O.D. AND DEBRIS FROM CARGO DOOR SEAL AREA IAW 52-70-00. SEAL FOR MAIN Jun 23, 2008 · N510TA · Airbus A300B4203 · Fuselage Miscellaneous StructureSDR WRN2008F00003Indicator · unserviceableDURING CRUISE, ENG NR1 EGT OFF SCALE HIGH INDICATION. POINTER AT 6 O`CLOCK POSITION. POINTER AND DIGITAL READOUT AGREED. AMBER EGT LIGHT ON, ENGINE EGT LIGHT ON MWP, AND SSC. AC RETURNED TO FIELD, ABNORMAL PROCEDURES WERE PERFORMED AND APPROX. 8500 LBS OF FUELJun 18, 2008 · N501TR · Airbus A300B4203 · Engine EGT/TIT Indicating SystemSDR WRN2008F00002Valve · stuckAFTER TAKEOFF, PRESSURIZATION MALFUNCTION OCCURRED. ACCOMPLISHED ABNORMAL PROCEDURES. AC RETURNED TO FIELD. LANDING NORMAL. MX FOUND GROUND VENT VALVE STUCK CLOSED. MX CLEANED AND RESET GROUND VENTING VALVE IAW 21-31-17, PG 501. OPS CHECKED SATISFACTORYJun 16, 2008 · N510TA · Airbus A300B4203 · Cabin Pressure Control SystemSDR WRN2008F00001Connector · dirtyAFTER TAKEOFF, APPROX 40 MINUTES INTO FLIGHT, AC TURNED BACK DUE TO NAV PROBLEMS WITH GPS SYSTEM. GPS SYS NR 2 PREVIOUSLY MEL, NR 1 GPS SYS WENT TO DR MODE. AIRCRAFT RETURNED TO BASE, NORMAL LANDING ACCOMPLISHED. MX CLEANED AND RESET CONNECTION ON GPS ANTENJun 16, 2008 · N505TA · Airbus A300B4203 · Global Positioning SystemSDR WRN2008F00000Gearbox · contaminatedON CLIMBOUT STJ FL230, OIL QTY DECREASING RAPIDLY. PERFORMED PRECAUTIONARY SHUTDOWN PROCEDURES, OIL PRESSURE WAS NOT LOST, OIL TEMP RISE TO 130 DEGREES. REPLACED GEARBOX IAW MM 72-60-01. OPS CHECK GOOD ON NR 2 ENGINE. (K)Jun 7, 2008 · N501TR · Airbus A300B4203 · Turbine Engine Reduction GearSDR WRNA20080039Control Valve · faultyDURING APPROACH TO BQN, LANDING GEAR FAILED TO EXTEND WITH SYSTEM 1 OR 2, RETURNED TO 2,000 FEET TO HOLD WHILE LOWERING GEAR MANUALLY. AFTER SUCCESSFUL EXTENSION OF GEAR, A SAFE LANDING WAS MADE. FIM 32-30-00 /107 INDICATED A FAULTY LANDING GEAR ELECTROVALVEMay 26, 2008 · N504TA · Airbus A300B4203 · Landing Gear Retraction/Extension SystemSDR WRNA20080038Uplock · unserviceableAFTER TAKEOFF, NOSE LANDING GEAR FAILED TO RETRACT. DUMPED FUEL AND RETURNED TO FIELD FOR A SAFE LANDING. REPLACED NOSE GEAR UP-LOCK ASSY IAW MM 32-31-14 PG 401. OPS CHECK GOOD IAW MM 32-30-00 PG 501. AIRCRAFT RELEASED FOR SERVICE.May 2, 2008 · N504TA · Airbus A300B4203 · Landing Gear Retraction/Extension SystemSDR WRNA200800037Csd · malfunctionedDURING FLIGHT, NR 1 CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY RISING OIL TEMPERATURE. DISCONNECTED CSD AND RETURNED TO MFM FOR A SAFE LANDING. REPLACED CSD IAW MM 24-11-11 PG 401 AND CSD OIL COOLER IAW 24-11-21 PAGE 401. AIRCRAFT RApr 29, 2008 · N510TA · Airbus A300B4203 · AC Generator-AlternatorSDR WRNA20080011Slide · no testDURING OPERATIONAL TEST, THE R-1 DOOR ESCAPE SLIDE/RAFT FAILED TEST, DID NOT FULLY INFLATE. REPLACED ESCAPE SLIDE/RAFT CONTACTED MAINTENANCE STATION WERE TEST WAS ACCOMPLISHED. SLIDE BOTTLE PRESSURE INDICATOR WAS IN THE 'GREEN', SLIDE DEPLOYED BUT DID NOT FUApr 8, 2008 · N506TA · Airbus A300B4203 · Escape SlideSDR WRNA20080010Duct · crackedAFTER TAKEOFF, NR 1 AND NR 2 BLEED FAULT LIGHTS AND APU MANIFOLD LIGHTS CAME ON AND WOULD NOT RESET. DUMPED 18,000 POUNDS OF FUEL AND RETURNED TO FIELD FOR A SAFE LANDING. FOUND NR 2 ENGINE BLEED AIR DUCT IN AIR CONDITIONING BAY CRACKED. REPLACED DUCT IAWApr 8, 2008 · N504TA · Airbus A300B4203 · Engine Bleed Air SystemSDR WRNA20080009Pin · disconnectedDURING DAILY CHECK, MAINTENANCE FOUND R1 EMERGENCY EXIT LIGHTS INOP. FOUND PIN NR 3 DISCONNECTED FROM LIGHT ASSY, RECONNECTED, OPS CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE.Mar 28, 2008 · N821SC · Airbus A300B4203 · Light System WiringSDR WRNA200800014Skin · corrodedDURING M96 CHECK, FOUND OUT OF LIMIT CORROSION ON FUSELAGE AT STR 6 TO FRAME 76. CUT OUT DAMAGED AREA 2.75 INCHES BY .75 INCHES AND INSTALLED FILLER FABRICATED FROM 2024 T3 0.090 AND REPAIR DOUBLER FABRICATED FROM 2024 T3 0.100 IAW A300 SRM 53-10-10.Mar 26, 2008 · N501TR · Airbus A300B4203 · Fuselage Main, Plate/SkinSDR DHLA200800035Apu · leakingBEFORE FLIGHT 102 ON GROUND IN SFO, 3 CABIN SMOKE DETECTORS ILLUMINATED ON THE GROUND. ON INSP FOUND APU TO BE LEAKING OIL. INGESTED INTAKE, SMOKE DET OK IAW AMM 26-10-0 DEFERRRED IAW MEL 49-11-01 DMI NR 32097. AIRCRAFT WAS GROUNDED.Mar 18, 2008 · N362DH · Airbus A300B4203 · APU Oil SystemSDR WRNA200800006Engine · failedAFTER TAKEOFF FROM MFM, CLIMBING THROUGH 15,000 FEET A LOUD EXPLOSION WAS HEARD FROM NR 1 ENGINE FOLLOWED BY SEVERE VIBRATION, ENGINE WAS RETARDED TO IDLE POWER, VIBRATION CONTINUED FOLLOWED BY LOW OIL PRESS LIGHT AND EGT INCREASE TO 963 DEGREES C. ENGINE WASMar 16, 2008 · N505TA · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR WRNA200800022Seat Track · crackedDURING M96 CHECK, MAIN CABIN SEAT TRACK AT FRAME 40 RBL 54 WAS FOUND CRACKED. REPLACED SEAT TRACK AT RBL 54 FROM FRAME 40 TO FRAME 44 +12 INCHES IAW SRM 53-10-10.Mar 3, 2008 · N501TR · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHLA200800019Bottle · reads lowR1 DOOR ESCAPE SLIDE PRESSURE IN RED. REMOVED AND REPLACED SLIDE ASSY. AIRCRAFT WAS GROUNDED.Mar 1, 2008 · N365DH · Airbus A300B4203 · Escape SlideSDR WRNA200800020Track · corrodedDURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD ZL-150-L403-501, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT AT FRAME 57. REMOVED AND REPLACED ROLLER TRACK IAW SRM 51-30-30.Feb 28, 2008 · N501TR · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR WRNA200800019Track · corrodedDURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD Z:-150-L403-5-01, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT BETWEEN FRAMES 58 TO 59. REMOVED AND REPLACED ROLLER TRACK IAW SRM 51-30-30.Feb 28, 2008 · N501TR · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR WRNA200800021Track · corrodedDURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD ZL-150-L403-501, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT AT FRAMES 54 TO 57. REMOVED AND REPLACED ROLLER TRACK IAW SRM 51-30-30.Feb 28, 2008 · N501TR · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR WRNA200800018Skin · corrodedDURING M96 CHECK, WHEN ACCOMPLISHING CPCP TASK CARD 55-2007-0602-1-01 SEVERAL AREAS OF CORROSION WERE FOUND OUT OF LIMITS ON LT ELEVATOR SKIN FROM CENTER LINE RIVETS TO I/B END CAP. REPLACED ELEVATOR IAW A300 MM 27-31-24.Feb 26, 2008 · N501TR · Airbus A300B4203 · Elevator, Plate/SkinSDR WRNA200800017Seat Track · corrodedDURING M96 CHECK, WHEN ACCOMPLISHING CPCP TASK CARD ZL-220-L403-9-01, CABIN SEAT TRACK WAS FOUND CORRODED AT FRAME 13B - 14C LBL 55. REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN FRAME 13B - 14C LBL 55 IAW A300 SRM 51-30-30 WITH SEAT TRACK FABRICATED FROM EFeb 26, 2008 · N501TR · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR WRNA200800016Skin · damagedDURING M96 CHECK, A 8 INCH BY 2 INCH CUT WAS FOUND IN SKIN BETWEEN FRAME 51 AND 52 AT STRINGER 36R TO 39R AFT OF RMLG DOOR CUT OUT. INSTALLED SKIN REPAIR DOUBLER AT FUSELAGE FRAME 51 TO 52 AND STRINGER 36R TO 39R IAW A300 SRM 53-10-10.Feb 26, 2008 · N501TR · Airbus A300B4203 · Fuselage Main, Plate/SkinSDR WRNA200800023Attach Fitting · corrodedDURING M96 CHECK, CORROSION WAS FOUND OUT OF LIMITS ON NR 3 (FROM OUTBOARD END) LEFT ELEVATOR ATTACH HINGE AT BONDING WIRE ATTACH POINT. REPLACED HINGE ATTACH IAW A300 M/M 55-51-31.Feb 23, 2008 · N501TR · Airbus A300B4203 · Elevator Tab, Attach FittingsSDR WRNA200800003Damper · failedAFTER TAKEOFF FROM IND, GEAR FAILED TO RETRACT ON BOTH SYSTEM A AND B, DIVERTED TO GSO, DUMPED APPROX 15,000 POUNDS OF FUEL AND MADE A SAFE LANDING. FOUND LEFT INBOARD PITCH DAMPER AT FAULT, REPLACED INBOARD PITCH DAMPER IAW A300 MM 32-11-15 PG 410, LEAK CHECJan 25, 2008 · N501TR · Airbus A300B4203 · Main Landing GearSDR DHLA200800004Uplock Switch · malfunctionedFLT 165, RIGHT MAIN GEAR DOOR DID NOT RETRACT AFTER GEAR EXTENDED. ABNORMAL PROCEDURE ACCOMPLISHED. CLEANED AND RESECURED RT MLG INBD DOOR UPLOCK SWITCHES, OPERATED GEAR DOORS. NO DEFECTS NOTED, REF M/M 32-30-00. OPS NORMAL AT THIS TIME. ACFT GROUNDED.Jan 10, 2008 · N364DH · Airbus A300B4203 · Landing Gear Door Retract SectionSDR DHLA200800003Skin · damagedLOWER FORWARD CARGO DOOR FUSELAGE LOWER FORWARD FRAME IS SCUFFED. DEFERRED IAW GMM 3.5 CAT I & LETTER REF. 942-057506/014/2008 ACCEPTABLE FOR 10 F.C. PLACARD INSTALLED.Jan 6, 2008 · N365DH · Airbus A300B4203 · Fuselage Main, Plate/SkinSDR WRNA200700064Damper · malfunctionedAFTER DEPARTURE WHEN RAISING GEAR, LEVER WOULD NOT GO PAST THE MID POSITION, GEAR POSITION LIGHTS REMAINED 'GREEN'. RETURNED TO FIELD AND MADE A SAFE LANDING. AIRCRAFT MAINTENANCE FERRIED TO CTS IN JAPAN FOR CORRECT ACTION. REPLACED LT GEAR PITCH DAMPER, AIDec 28, 2007 · N510TA · Airbus A300B4203 · Landing Gear Retraction/Extension SystemSDR DHLA200700095Power Supply · no testEMERGENCY EXIT LIGHT OVER THE R1 WILL NOT TEST. REPLACED R1 EMERGENCY LIGHT POWER SUPPLY AS PER MM 33-51-14. OPS NORM.Dec 27, 2007 · N367DH · Airbus A300B4203 · Emergency LightingSDR WRNA200700062B-Nut · looseAFTER LEVELING OFF AT 27,000' OBSERVED STEADY DECLINE IN OIL QUANTITY OF NUMBER 1 ENGINE, RETURNED TO FIELD AND MADE A SAFE LANDING, NO LOSS OF OIL PRESSURE. FOUND AND SECURED A LOOSE 'B' NUT AT AFT BEARING LINE, RE-SERVICED OIL AND ACCOMPLISHED LEAK CHECK, NDec 18, 2007 · N504TA · Airbus A300B4203 · Turbine Engine Oil SystemSDR DHLA200700081Autobrake Sys · malfunctionedDURING ROLL OUT WITH AUTOBRAKES ENGAGE (MIN) AFTER PRESSING BRAKES AUTO BRAKES CONTINUED TO BRAKE THE AIRCRAFT EVEN WITH THE AUTO BRAKE OFF LIGHT ILLUMINATED AND NO PRESSURE ON BRAKE PEDALS. PERFORMED OPERATIONAL CK OF AUTOBRAKE AND LIFT DUMPING CKS NORMAL IADec 12, 2007 · N367DH · Airbus A300B4203 · BrakeSDR DHLA200700079Sequence Valve · malfunctionedUPON GEAR RETRACTION, RT MAIN GEAR WOULD NOT RETRACT. UNSAFE LIGHT AND GEAR DOOR LIGHTS BOTH ILLUMINATED. PERFORMED LANDING GEAR UNSAFE INDICATION ABNORMAL PROCEDURE. LOWERED GEAR. GOT ALL 3 GREEN. CONTACTED MAINT AND FLIGHT CONTROL. RETURNED TO JFK.Dec 8, 2007 · N364DH · Airbus A300B4203 · Landing Gear Retraction/Extension SystemSDR DHLA200700067Light · inoperativeEMERGENCY EXIT LIGHT DISARM WARNING DOES NOT ILLUMINATE. REPLACED LIGHT BULBS ON DISARM CAPSULE PER MM 33-51-00. OPS TEST OK.Nov 23, 2007 · N363DH · Airbus A300B4203 · Emergency LightingSDR WRNA200700060Duct · brokenDURING TAKE OFF, NR 2 ENGINE EGT EXCEEDED 960 C, POWER WAS REDUCED BELOW TAKEOFF SETTING, EGT DROPPED BELOW 945 C. DURING CLIMB, NR 2 ENGINE MANIFOLD PRESS 10 PSI, BLEED VALVE REGULATOR LIGHT ON, THEN NR 2 -B- LOOP LIGHT ILLUMINATED, SWITCHED TO -A- LOOP, -A-Oct 31, 2007 · N506TA · Airbus A300B4203 · Pneumatic Distribution SystemSDR WRNA200700058Line · obstructedDURING TAKEOFF ROLL, FIRST OFFICERS AIR SPEED LAGGED BEHIND CAPTAINS BY 40-60 KNOTS, ABORTED TAKEOFF. FLUSHED DEBRIS FROM PITOT PRESSURE LINES, ACCOMPLISHED PITOT/STATIC TEST IAW 34-11-10 PAGE 501. TEST NORMAL. AIRCRAFT RELEASED FOR SERVICE.Oct 23, 2007 · N510TA · Airbus A300B4203 · Airspeed/Mach IndicatorSDR WRNA200700057Pitot Tube · leakingDURING TAKEOFF THE FIRST OFFICERS AIRSPEED INDICATOR LAGGED 40-60 KNOTS BEHIND CAPTAINS AIRSPEED INDICATOR. FOUND RT PITOT PROBE LEAKING, REPLACED RT PITOT PROBE IAW A300 MM 34-11-15 PAGE 401. ACCOMPLISHED LEAK CHECK IAW A300 MM 34-11-10 PAGE 501. AIRCRAFT Oct 23, 2007 · N510TA · Airbus A300B4203 · Airspeed/Mach IndicatorSDR WRNA200700051Circuit Breaker · weakAFTER TAKEOFF, FUEL PUMP NR 1; 1A; 2 CIRCUIT BREAKERS POPPED, AND AFCS AND FLIGHT ENGINEER PANEL LIGHTS WENT OFF. RETURNED TO FIELD AND MADE A SAFE LANDIBG. REPLACED FAULTY BREAKER IN 101VU PANEL.Oct 18, 2007 · N510TA · Airbus A300B4203 · Electrical Power System WiringSDR DHLA200700053Hydraulic System · contaminatedWITH ANTI-SKID IN ON /ALT THE LEFT BRAKES GRAB AND PULL AIRCRAFT TO THE LEFT. BLED BRAKING SYS GREEN AND YELLOW AND OPS CK NORMAL PER MM 32-42-00.Oct 12, 2007 · N362DH · Airbus A300B4203 · Hydraulic System, MainSDR WRNA200700065Bulkhead · crackedDURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD AT STR TIE END ANGLE FITTING AT 35R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40. APPLIED PROTECTIVE COATINGS IAW SRM 51-40Oct 11, 2007 · N510TA · Airbus A300B4203 · Fuselage Main, Bulkhead
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