GE CF6-50C2

Service difficulty reports · 719

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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 = 'CF650C2'
  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 XN0A1318Bleed Valve · malfunctionedENGINE NR 2 BLEED AIR TEMP HI LIGHT ILLUMINATED AFTER TAKEOFF. REGUL FAULT LIGHT ALSO ILLUMINATED. REMOVED AND REPLACED FAN AIR VALVE IAW A300 AMM CHAPTER 36-11-16 AND REMOVED AND REPLACED HIGH PRESSURE BLEED VALVE IAW A300 AMM CHAPTER 36-11-12. PERFORMED EApr 18, 2006 · N473AS · Airbus A300B4203 · Compressor Bleed ValveSDR 06FDEA1446Engine · damagedNR 2 ENG S/N 530393, RT LPT CASE 3 O'CLOCK POSITION BURN THRU HOLE APPROX .500" DIAMETER, AND HEAT DISTRESS AROUND LPT TURBINE CASE. REMOVED AND REPLACED NR 2 ENG PER FEDEX W/C 71T1101, W/C 71T1701 AND N/R 563.Apr 13, 2006 · N320FE · Doug DC1030 · Engine (Turbine/Turboprop)SDR CLC2006F00002Duct · brokenON CLIMB OUT- NR 1 ENGINE FIRE DETECTOR ILLUMINATED. RETURNED TO DEPARTURE AIRPORT. INSPECTION OF AREA (ENGINE) FOUND BLOWN DUCT. REPLACED ENGINE. (K)Apr 7, 2006 · N306FV · Doug DC1030F · Fire DetectionSDR CNMA20060008Motor · noisyWITH AUTOPILOT ENGAGED VIBRATION COULD BE FELT IN FLOOR AND A (GRINDING) NOISE WAS DETECTED IN THE TAIL SECTION. REPLACED SEVERAL COMPONENTS INCLUDING GEARBOX ASSY, PRIMARY TRIM MOTOR, DRUM ASSY, HORIZONTAL STAB CHAIN DRIVE, FOUND DETERIORATED CONNECTOR TO THApr 5, 2006 · N270AX · Doug DC1030 · Auto Flight SystemSDR WRNA200600006Mec · unserviceableENGINE NR 2 FAILED TO INCREASE BEYOND 80 PERCENT N1 UPON POWER APPLICATION ON T/O. T/O WAS REJECTED PER ABNORMAL PROCEDURES. TROUBLE SHOOT AND FOUND MEC TO BE FAULTY. REMOVED AND REPLACED NR 2 ENGINE MEC. LEAK CHECK, OPS CHECK AND RIG CHECK NORMAL IAW A-30Mar 24, 2006 · N502TA · Airbus A300B4203 · Fuel Control/Turbine EnginesSDR WRLA2006009Fire Warning · false activationAPU AUTOSHUTDOWN WITH A FIRE WARNING ALERT. FIRE AGENT CYLINDER 1 DISCHARGED. REPLACED NR 1 REAR FIRE BOTTLE PER MM CHAP 26. INSPECTED APU AREA FOR LEAK AND POSSIBLE FIRE DAMAGE, NONE FOUND. OK FOR CONTINUED SERVICE.Mar 8, 2006 · N14075 · Doug DC1030 · Fire DetectionSDR WLRA2006002Fitting · corrodedWHILE PERFORMING INSPECTION OF THE FLAP SUPPORT ATTACH FITTINGS DURING A5 CHECK, FOUND CORROSION ON THE LEFT WING INBOARD FLAP SUPPORT FITTING HOLE. REWORKED AND REPAIRED HOLE PER ERA 06-57-09 AND MM57-44-07, INSPECTED REPAIRS ALL NORMAL.Feb 7, 2006 · N304 · Doug DC1030F · Wing, Control Surface Attach FittingsSDR WRLA2006003Attach Fitting · corrodedWHILE PERFORMING INSPECTION OF THE FLAP SUPPORT ATTACH FITTINGS DURING A5 CHECK, FOUND CORROSION ON THE LEFT WING OUTBOARD FLAP SUPPORT FITTING HOLE. REWORKED AND REPAIRED HOLE PER ERA 06-57-09 AND MM57-44-07, INSPECTED REPAIRS ALL NORMAL.Feb 7, 2006 · N304 · Doug DC1030F · Wing, Control Surface Attach FittingsSDR WRLA2006004Attach Fitting · corrodedWHILE PERFORMING INSPECTION OF THE FLAP SUPPORT ATTACH FITTINGS DURING A5 CHECK, FOUND CORROSION ON THE RIGHT WING INBOARD FLAP SUPPORT FITTING HOLE. REWORKED AND REPAIRED HOLE PER ERA 06-57-09 AND MM57-44-07, INSPECTED REPAIRS ALL NORMAL.Feb 7, 2006 · N304 · Doug DC1030F · Wing, Control Surface Attach FittingsSDR XN0A1289Pump · false indicationYELLOW SYSTEM PUMP PRESS MAGNETIC INDICATOR AMBER. TRANSFERED TO DMI NR 6054 IAW ENA MEL CHAPTER 29-32-02. PLACARDS INSTALLED. REPLACED YELLOW SYSTEM PRESSURE SWITCH PER A300 AMM CHAPTER 29-32-29, PERFORMED LEAK CHECK. THIS ACTION CLEARS DMI 6054. PLACARDS REMJan 12, 2006 · N372PC · Airbus A300B4203 · Hydraulic Pressure IndicatorSDR XN0A1288Steering Sys · inoperativeNOSE WHEEL TILLER STEERING INOP. BLEED GREEN SYSTEM NOSE STEERING VALVE, SYSTEM OPS CHECKS GOOD IAW AMM CHAPTER 29-11-00. (STATUS:ORIG/CLOSED).Jan 11, 2006 · N372PC · Airbus A300B4203 · Landing Gear Steering SystemSDR DHL2005362013Indicator · inoperativeLANDING GEAR INDICATOR FORWARD LT MAIN INOP. S/O PANEL INDICATES 3 GREEN. REMOVED AND REPLACED LANDING GEAR IND. UNIT ON CENTER PNL IAW M/M 32-61-14 SYS OPS CHECKED SERVICABLE ON GRD.Dec 21, 2005 · N362DH · Airbus A300B4203 · Landing Gear Position and WarningSDR DHL2005362012Proximity Sensor · inoperativeFRONT PANEL LANDING GEAR GREEN DOWN AND LOCKED INDICATOR NOT ILLUMINATED (LT MAIN) LIGHT TEST OK NR 2 SYSTEM OK. REMOVED AND REPLACED PROXIMITY DETECTOR UNIT SYS OPS CHECKED SERVICEABLE ON GRD IAW M/M 32-61-12Dec 20, 2005 · N362DH · Airbus A300B4203 · Landing Gear Position and WarningSDR XN0A1285Gyro · inoperativeNR 3 DG INOPERATIVE. PLACED NR3 DG ON DEFERRAL IAW MEL 34-11-07 CAT C DMI NR 51005 PLACARDS INSTALLED. (ORIG/OPEN)Dec 16, 2005 · N472AS · Airbus A300B4203 · Directional Gyro and Indicating SystemSDR 05FDEA04308Repair · noneLT WING L/E EXT SKIN FOUND FLUSH DOUBLER DIM 2.75 INCHES BY 2.75 INCHES AT STA XORS 521. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 39 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3.Dec 14, 2005 · N302FE · Doug DC1030 · Aircraft StructuresSDR 05FDEA04309None · noneLT WING L/E EXT SKIN FOUND FLUSH DOUBLER DIM 2.25 INCHES BY 1.75 INCHES AT STA XORS 532. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 39 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 E3.Dec 14, 2005 · N302FE · Doug DC1030 · Standard Practices/StructuresSDR 05FDEA04310Doubler · damagedPERFORMED INSPECTION IAW EO 8-5100-7-5001-P1 FOUND DOUBLER DIM 15 INCHES BY 14 INCHES LT EXT FUS STA 595 LONG 46 TO LONG 48. PERFORMED A GVI OF REPAIR IAW SRM 53-20-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-1D E3.Dec 14, 2005 · N302FE · Doug DC1030 · Fuselage Main, StructureSDR 05FDEA04311Repair · unknownRT WING SLAT NR 2 FOUND DOUBLER REPAIR ON UPPER SKIN T/E OB SIDE DIM 3 INCHES BY 3 INCHES. REMOVED REPAIR IAW SRM 51-35-01 PAGE 13 AND SRM 51-33-01 PAGE 34/47. CLEANED AREAS AND REMOVED PART IAW SRM 51-41-01 VOL 2. PERFORMED INSPECTION IAW NDI SPM08. FOUNDDec 14, 2005 · N302FE · Doug DC1030 · Wing StructureSDR WRNA20050030Outflow Valve · unserviceableAFTER TAKEOFF USING SYSTEM NR1 NOTICED AFT OUTFLOW VALVE STAYED FULL OPEN. OPPOSITE SYSTEM SELECTED, NO HELP, UNABLE TO CLOSE MANUALLY. WITH BOTH PACKS ON COULD MAINTAIN 8500 FT CABIN ALTITUDE AT 14000 FT. DUMPED FUEL TO SAFE LANDING WEIGHT (APPROX 2600 GALS)Dec 13, 2005 · N506TA · Airbus A300B4203 · Pressure Regulator/Outflow ValveSDR 05FDEA04243Fitting · failedREMOVED NR 2 ENG REF W/C 71T1101 WHILE LOWERING ENGINE AFT LT MOUNT BROKE, TEARING WEB AND CRACKED ANGLES ALSO BOTH T/R HALVES DAMAGED. TURNED OVER TO DAY SHIFT FOR FURTHER EVALUATION. REPLACED WEB AND FITTINGS AS REQUIRED REF DWG AVB7318 AND SRM 51-00-01 Dec 12, 2005 · N303FE · Doug DC1030F · Turbine Engine Oil SystemSDR XN0A1282Connector · disconnectedLT LOW SPEED AILERON WILL NOT CONNECT FOR TAKE-OFF AND THE RT LOW SPEED AILERON IS CONNECTED. CONNECTED THE LT LOW SPEED AILERON CONNECTOR PLUG, SYSTEM OPS CHECKS GOOD IAW AMM 27-11-01.THIS CLEARS DMI NR 5967.(STATUS:ORIG/CLOSED)Dec 10, 2005 · N307FV · Airbus A300B4203 · Aileron Control SystemSDR XN0A1280Exciter · faultyNO LIGHT UP ON NR1 ENGINE ON (B) IGNITION. FOR T/S TRIED (A) IGNITION BUT NO LIGHT-UP. ABNORMAL PROCEDURES CARRIED OUT IAW QUICK REFERENCE HANDBOOK. REPAIRED (B) SYSTEM IGNITION EXCITER IAW AMM 74-11-01 OPS CK GOOD. PLACED (A) SYSTEM ON DMI LOG NR 5959 IAWDec 6, 2005 · N473AS · Airbus A300B4203 · ExciterSDR DHL2005367006Switch · dirtyNOSE GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. CLEANED CONNECTOR ON NOSE GEAR DOOR CLOSE SWITCH. OPS CHECKS SERVICEABLE ON GRD IAW M/M 32-22-11Nov 27, 2005 · N367DH · Airbus A300B4203 · Landing Gear Position and WarningSDR DHL2005367005Downlock Switch · inoperativeDURING THE APPROACH THE LANDING GEAR WAS EXTENDED AND THE GREEN NOSE GEAR DOWN LIGHT ON THE FWD CENTER PANEL DID NOT ILLUMINATE. THE GREEN NOSE GEAR DOWN LIGHT DID ILLUMINATE ON THE SECOND OFFICERS PANEL. REMOVED AND REPLACED NOSE GEAR DOWN AND LOCKED SWITCH Nov 24, 2005 · N367DH · Airbus A300B4203 · Landing Gear Position and WarningSDR WRLA2005146Engine · overheatedBRU-DAY DIVERSION TO YYZ BECAUSE OF NR 1 ENGINE HIGH EGT AND HIGH FUEL FLOW. BEGINNING/DURING DESCENT INTO YYZ THE ENGINE FIRE WARNING BEGIN FLICKERING LIGHT AND ENGINE WAS SHUTDOWN PER ENGINE FIRE/FAILURE CHECKLIST. FLICKERING LIGHT WAS IN FIRE HANDLE AND SNov 4, 2005 · N303 · Doug DC1030F · Engine (Turbine/Turboprop)SDR CLC2006F00005Switch · malfunctionedON APPROACH THE FLAP/SLAT HANDLE ON EXTENSION HAD SLAT DISAGREE LIGHT (ON). WENT TO ABNORMAL CHECK LIST A-5-1, AND A-5-9, AND COMPLIED WITH SAME. EMERGENCY WAS DECLARED. LANDING AT DESTINATION UNEVENTFUL. FINDINGS: RT GROUND SENSING SWITCH BAD. REPLACED RNov 2, 2005 · N612GC · Doug DC1030F · Drag Control SystemSDR WRNA20050024Filter · dirtyNR 1 ENGINE FUEL CLOG LIGHT ILLUMINATED. FUEL DUMPED, AIRCRAFT RETURNED TO BASE. LANDING NORMAL. FUEL FILTER DIRTY, REMOVED AND REPLACED FUEL FILTER, CLEANED FUEL STRAINER IAW 73-12-03. FUNCTIONAL CHECK SATISFACTORY, AIRCRAFT RETURNED TO SERVICE.Oct 23, 2005 · N502TA · Airbus A300B4203 · Aircraft Fuel Filter/StrainerSDR DHL2005364003Selector Valve · inoperativeON THE GROUND DURING TAXI WHEN MAKING LARGE TURN REQUIRING MORE THAN 10 DEG TILLER. TILLER IS VERY DIFFICULT TO TURN; REQUIRES TWO HANDS. ALSO DURING THIS TIME, WHEN PRESSING THE RUDDER PEDALS, CAN FEEL A HIGH FREQUENCY VIBRATION IN RUDDER PEDALS. DURING LANDOct 2, 2005 · N364DH · Airbus A300B4203 · Landing Gear Door Retract SectionSDR ARWA20050910Engine · malfunctionedON TAKEOFF, NR 1 ENGINE ADVANCED TO 40 PERCENT N1 AND WOULD NOT GO BEYOND, ALL OTHER PARAMETERS NORMAL. ENTERED ON DMI NR19537 AS PER MEL 77-11-1 CAT "B" REFER TO DDG 77-1 C/W. PERFORMED NR 1 ENGINE RUN-UP IN ACCORDANCE WITH M/M 71-00-00. FOUND N1 INDICATIOSep 18, 2005 · N526MD · Doug DC1030 · Engine (Turbine/Turboprop)SDR XNOA1265Solenoid · failedNR 2 ENGINE WOULD NOT ACCELERATE ON TAKEOFF. TROUBLESHOOT GROUND IDLE SOLENOID AND TRANFERRED TO DMI 5726 IAW MEL 73-30-02 CAT-C. CLEARED & RESEATED NR 2 ENG FTL IDLE SOLENOID C/P OPS CHECK NORMAL IAW A300 MM 73-21-00. DMI 5726 CLEARED.Sep 16, 2005 · N372PC · Airbus A300B4203 · Fuel Controlling SystemSDR XN0A1265Solenoid · malfunctionedNR 2 ENGINE WOULD NOT ACCELERATE ON TAKEOFF. TROUBLESHOOT GROUND IDLE SOLENOID AND TRANFERRED TO DMI NR 5726 IAW MEL 73-30-02 CAT-C. CLEARED AND RESEATED NR 2 ENG FTL IDLE SOLENOID C/P, OPS CHECK NORMAL IAW A300 MM 73-21-00. DMI NR 5726 CLEARED (STATUS:ORIGSep 16, 2005 · N372PC · Airbus A300B4203 · Fuel Controlling SystemSDR WRNA200500022Compressor · stalledNR 1 ENGINE COMPRESSOR STALLED 4 TIMES CLIMBING THROUGH 15,500 FT. AFTER COMPRESSOR STALL, WITH SAME THROTTLE ANGLE, NR 1 ENG N1 WAS 98.4 PERCENT WHILE NR 2 WAS 104 PERCENT. ALL OTHER PRIMARY ENGINE PARAMETERS WERE FLUCTUATING. WHEN THE NR 1 THRUST LEVER WASep 14, 2005 · N821SC · Airbus A300B4203 · Turbine Engine Compressor SectionSDR XN0A1259Control System · malfunctionedDURING TAKEOFF, FLARE ROLL ELEVATOR CONTROL WAS VERY DIFFICULT TO MANEUVER THE AIRCRAFT. CARRIED OUT INSPECTION PER A300 FIM CHAPTER 27-31-00 FIGURE 101 SHEET NR 1 & 2 NO FAULTS FOUND. CARRIED OUT INSPECTION PER A300 AMM CHAPTER 27-33-14 & 27-33-00 OF THE ARTAug 19, 2005 · N371PC · Airbus A300B4203 · Rudder Control SystemSDR XN0A1258Regulator · failedON CLIMBOUT, GOT NR 1 ENGINE TEMP HIGH AND REGUL FAULT LIGHTS. TEMP WAS PEGGED AT 300 DEGREES C. PERFORMED QRH WITH NO CHANGE. LT AND CENTER MANIFOLD LIGHTS CAME ON. REDUCED THROTTLE TO IDLE. TEMP REDUCED AND LIGHTS EXTINGUISHED. REMOVED AND REPLACED NR Aug 18, 2005 · N224KW · Airbus A300B4203 · Pneumatic Distribution SystemSDR XN0A1255Compressor · stalledAFTER TAKEOFF NR 1 ENG BEGAN COMPRESSOR STALLING AT 700 FT AGL. (ORIG/OPEN)Aug 11, 2005 · N370PC · Airbus A300B4203 · Fuel Controlling SystemSDR XN0A1251Csd · disconnectedNR 1 GENERATOR TRIP OFF. NO VOLT AND FREQ. ITEM TRANSFER TO DMI NR 5616 IAW MEL 24-11-01 CAT - (B), NR 1 CSD DISCONNECTED. (ORIG/OPEN)Aug 5, 2005 · N371PC · Airbus A300B4203 · AC Generation SystemSDR CLC2005F00008Cable · burnedON TAXI OUT THE NR 2 AC BUSS CIRCUIT BREAKERS POPPED OUT. SMELLED SMOKE IN COCKPIT, TAXIED BACK TO THE RAMP. FOUND BURNED WIRES AND FEEDER CABLES BELOW LAVATORY FLOOR FOR THE NR 2 GENERATOR, ALL THREE PHASES. GENERATOR FEEDER CABLES FOR NR 1 AND 3 GENERATORAug 4, 2005 · N279AX · Doug DC1030 · Electrical Power System WiringSDR CLC2005F00009Cable · burnedON TAXI OUT, THE NR 2 AC BUSS CIRCUIT BREAKERS POPPED OUT. SMELLED SMOKE IN COCKPIT, TAXIED BACK TO THE RAMP. FOUND BURNED WIRES AND FEEDER CABLES BELOW LAVATORY FLOOR FOR THE NR 2 GENERATOR, ALL 3 PHASES. GENERATOR FEEDER CABLES FOR NR 1 AND 3 GENERATORS AAug 4, 2005 · N279AX · Doug DC1030 · AC Generation SystemSDR DHL2005366502Slat Track · crackedDURING C-CHECK, DISCREPANCY AS FOLLOWS N/R 021215 DISCREPANCY AS FOLLOWS, RT WING NR 1 SLAT LOWER, IB OF NR 1 TRACK AT EDGE HAS A CRACK. REMOVED SKIN TO REPLACE CRACK ANGLE IAW SRM. MATERIAL USED 2024-0, .063 INCH THICK PO NR 1004297 HEAT TREATED TO 2024-T4Jul 25, 2005 · N366DH · Airbus A300B4203 · Leading Edge DevicesSDR XN0A1243Engine · malfunctionedON TAKEOFF NR 1 ENGINE EGT EXCEED LIMITS, ABORTED TAKEOFF AT APPROXIMATELY 120KTS.Jul 5, 2005 · N371PC · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR XN0A1242Engine · overtempDURING TAKEOFF NR 1 ENGINE EGT EXCEED LIMIT. RED EGT LIGHT ON, LESS THAN 100KTS. PER A300 MM 72-00-00 INSPECTED ENG INLET & EXHAUST, PERFORMED BOROSCOPE INSPECTION ON STAGE. 1 & 2 HPT BLADES, INSPECTED EGT INDICATION SYSTEM AS PER A300 MM 77-21-00. NO DEFEJul 4, 2005 · N371PC · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR XN0A050629001Window · lack of lubeCAPTAIN`S WINDOW LOCK PIN WILL NOT ENGAGE. LUBED AND CYCLED CAPTAIN`S WINDOW. OPS CK GOOD 56-12-00. (ORIG/CLOSED)Jun 29, 2005 · N474AS · Airbus A300B4203 · Flight Compartment WindowsSDR ARWA20050604Pump · failedAFTER LANDING IN KMIA, NR 2 ENGINE OIL PRESSURE DROP DOWN TO 20 PSI; SHUTDOWN ENGINE NR 2. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER AND REMOVED AND REPLACED OIL PUMP IN ACCORDANCE WITH DC-10 M/M 9-20-04. OPERATIONAL CHECK NORMAL IN ACCORDANCJun 10, 2005 · N478CT · Doug DC1030F · Turbine Engine Oil SystemSDR WRLA2005086Coupler · damagedAIR TURNBACK INITIAL CLIMB OBSERVED MASTER WARNING & ENG FIRE WARNING LIGHT & BELL CAME ON & THEN OFF. NR 2 ENG NACELLE TEMP 260 DEG, NR 1 & 3 160 DEG. REDUCED ENG THRUST LEVER TOWARD IDLE TEMP FOLLOWED, PUSHED LEVER FORWARD & TEMP INCREASED, TESTED FIRE WARJun 8, 2005 · N303 · Doug DC1030F · Pneumatic SystemSDR XN0A1234Fuel Control · erraticNR 2 FUEL FLOW ERRATIC. TRANSFERRED TO DMI NR 5396 IAW A-300 MEL 73-30-01 CAT "B". (STATUS:ORIG/OPEN)May 7, 2005 · N373PC · Airbus A300B4203 · Fuel Controlling SystemSDR WRLA2005084Fuel Sys · leakingDIVERSION DUE TO 1+20HR INTO FLIGHT NR 3 FUEL FLOW STARTED TO INDICATE 15,000 LBS PER HOUR ON THE NEEDLE, 29,320 ON DIGITAL. FUEL USED ON NR 3 ROSE TO OVER 5,000 LBS MORE THAN 1 AND 2. ENGINE SHUTDOWN PER PROCEDURES. FUEL PRESSURE ON NR 3 STILL INDICATES 80Apr 7, 2005 · N14075 · Doug DC1030 · Engine Fuel and ControlSDR 05FDEA00659O-Ring · leakingNR 1 ENG EXCESSIVE OIL USAGE OR LOSS, AT ENG START HAD 19 QTS AFTER ENGINE START WAS APPROX 17 QTS. AT 1.5 HRS INTO FLT READ 11 QTS AND STILL DROPPING 7 QTS AT TOUCHDOWN 4 HRS 10 MIN TOTAL TIME. REMOVED NR 10 DRIVE ADAPTER, FOUND O-RING SEAL ON IDLER GEAR SMar 28, 2005 · N317FE · Doug DC1030 · Turbine Engine Oil SystemSDR WRNA200500006Engine · unserviceableDURING CLIMBOUT NR 2 ENGINE EXCEEDED EGT LIMITS. WHEN LIMITS WERE IN NORM OPERATING RANGE NO RESPONSE WAS SEEN WHEN THROTTLES WERE ADVANCED. FUEL DUMP PROCEDURES FOLLOWED, AIRCRAFT RETURNED TO AIRPORT, LANDING NORMAL. REMOVED AND REPLACED NR 2 ENGINE IAW A3Mar 18, 2005 · N501TR · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR DHL2005365002Garlock Seal · leakingCREW REPORTED THAT ACFT LOSING OIL QUANTITY FROM 18 QUARTS BEFORE TAKEOFF THEN 10 QUARTS SHORTLY AFTER TAKEOFF,THEN DOWN TO 3 QUARTS AT 0545Z AND AT 0612Z 1 QT OIL QUANTITY REPORTED. NR 1 CSD LEAKING AT GARLOCK GEARBOX DRAIN CAVITY. R/R GARLOCK SEAL & O-RING IJan 25, 2005 · N365DH · Airbus A300B4203 · Turbine Engine Oil SystemSDR WRLA2005005Gps · malfunctionedITEM: WOA174/25 DAY/LAX AIR TURNBACK DUE TO FAILURE OF NAVIGATION SYSTEM. AFTER TO, NR 3 GPS WORKED BUT WOULD NOT CROSS TALK. AFTER 2:30 MIN CAPT LOST HIS ROLL BAR AND NR 1 GPS WOULD NOT PROVIDE NAV DATA. SHORTLY AFTERWARDS NR 2 GPS HAD ALERT "NAV DATA BASEJan 25, 2005 · N304 · Doug DC1030F · Global Positioning System
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