Boeing 767-333

Service difficulty reports · 163

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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 aircraft_model_key = '767333'
  ORDER BY difficulty_date DESC"

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SDR CA150209001Actuator · failed(CAN) ON FINAL APPROACH, FLAPS WOULD NOT GO FROM 20 TO 25 IAW STANDARD OPERATING PROCEDURE, INCREASED SPEED & LANDED WITHOUT INCIDENT. NIL PAX REACTION, NIL EMER DECLARED WITH ATC. FLAP TE LOAD ALLEVIATION ACTUATOR REPLACED IAW AMM 27-51-30-401. TEST OF THE Feb 6, 2015 · Boeing 767333 · Trailing Edge Flap ActuatorSDR CA150204001Unknown · odor(CAN) ON DEPARTURE CREW DETECTED A STRONG ODOR IN THE COCKPIT, BOTH PILOTS FELT NAUSEOUS & ELECTED TO DIVERT BACK. THE CREW FOLLOWED THE OVERWEIGHT LANDING CHECKS & LANDED ON 08R WITHOUT FURTHER INCIDENT. EMER TRUCKS WERE CALLED OUT DUE OVERWEIGHT LANDING. Feb 3, 2015 · Boeing 767333 · Air Distribution SystemSDR CA150112005Target · out of tolerance(CAN) AFTER DEPARTURE, FLIGHT EXPERIENCED A SLAT ASYMMETRY ECAM WARNING. THE FLIGHT CONTACTED MTC BUT A RESET WAS UNSUCCESSFUL. DIVERTED. PSEU FAUTLED TARGET SW282. IAW AMM 27-88-01-902-001 FOUND INTERMEDIATE TARGET GAP OUT OF TOLERANCE. SW282 REPLACED AND AJan 12, 2015 · Boeing 767333 · Leading Edge Slat Position Indicating SystemSDR CA150112004Slat System · malfunctioned(CAN) DIVERTED DUE TO SLAT PROBLEM, UNABLE TO RESOLVE IN THE AIR. MOC ADVISED. SLAT PROXIMITY SENSORS CHECKED FOR CORRECT SENSOR TARGET GAP, SENSOR CONDITION AND ELECTRICAL SPLICE CONDITION IAW AMM 27-88-01 CHECKED SATISFACTORY. PSEU REPLACED. FSEU REPLACEJan 10, 2015 · Boeing 767333 · Leading Edge Slat Control SystemSDR CA140929001Idg · unserviceable(CAN) AIR RETURN FOR ENGINE GENERATOR UNSERVICEABLE. IDG REMOVED IAW J/C B767-24-11-01-004-001-04-0-A60A, NEW IDG INSTALLED IAW J/C B767-24-11-01-404-002-04-0-3D42, IDG OIL SYSTEM FLUSHED IAW AMM 12-13-03-301.Sep 26, 2014 · Boeing 767333 · AC Generator-AlternatorSDR CA140926011Actuator · stiff(CAN) ON FINAL APPROACH, CREW EXPERIENCED A LANDING GEAR DISAGREE. A MISSED APPROACH WAS CONDUCTED AND THE QRH WAS CARRIED OUT WHICH CLEARED THE MESSAGE. A SECOND APPROACH AND LANDING WAS CARRIED OUT WITHOUT FURTHER EVENT. ON PSEU FOUND 421/422 "GEAR LEVER DOSep 25, 2014 · Boeing 767333 · Landing Gear Door ActuatorSDR CA140924004Drain · odor(CAN) ODOR SIMILAR TO THE SMELL OF BURNING RUBBER COMING FROM THE AREA OF THE AFT LAVATORIES. UNABLE TO ISOLATE OR IDENTIFY. ODOR HAS DISSIPATED AND FLIGHT CONTINUING. MOC ADVISED. FOUND CHEMICAL ODOR COMING FROM THE SINK DRAIN, DRAIN FLUSHED WITH WATER AND Sep 23, 2014 · Boeing 767333 · Waste Disposal SystemSDR CA140922002Oil System · leaking(CAN) IN CRUISE AT FL380, CREW REPORTED LEFT ENGINE LOW OIL QUANTITY TO DISPATCH AND MTC. PLAN WAS TO MONITOR AND CONTINUE. QUANTITY DROPPED OFF. CREW SHUT DOWN LEFT ENGINE AND ADVSD THEY WERE DIVERTING. CREW ADVSD ATC THEY HAD A MECHANICAL EMERGENCY IN PROGRSep 19, 2014 · Boeing 767333 · Turbine Engine Oil SystemSDR CA140822009Coffeemaker · odor(CAN) AFTER DEPARTURE, AN ACRID ODOR HAD RETURNED ON THE ACFT. THE CREW ELECTED TO RETURN WHERE A PAN WAS DECLARED AND AN OVERWEIGHT LANDING WILL BE CARRIED OUT. ERS WILL BE RESPONDING. MAINTENANCE CONTROL, DUTY PILOT AND CORP SAFETY ADVISED. RESOLUTION ARAug 21, 2014 · Boeing 767333 · Buffet/GalleysSDR CA140821006Coffeemaker · odor(CAN) PAN PAN DECLARED WITH ATC FOR PRIORITY HANDLING ON ARRIVAL IAW BURING ODOR FROM MID GALLEY. ESTIMATED LANDING WEIGHT, 144,500 KGS. FOUND COFFEEMAKER IN MID GALLEY AT POSITION 6416 CIRCUIT BREAKER POPPED. MAINTENANCE STAFF REMOVED THE COFFEEMAKER AND Aug 20, 2014 · Boeing 767333 · Buffet/GalleysSDR HALA2014060400077Warning Message · false activationRA DISPLAYED INTERMITTENT ON THE CAPTAIN`S ADI. ACCOMPLISHED FIM 34-33-809 AND SYS CHECKED OK; BITE CHECKED IAW 34-33-810. NO FAULT NOTED.Jun 4, 2014 · N583HA · Boeing 767333 · Air Data ComputerSDR CA140225005Hose · failed(CAN) AFTER PUSHBACK, STATION ADVISED THE CREW THAT LIQUID WAS DISCOVERED ON THE GROUND AT THE GATE IN THE VICINITY OF WHERE THE MAIN GEAR WAS POSITIONED. CREW ELECTED TO RETURN TO THE GATE AND NOTED A DECREASE IN THE RT HYD QTY. ATC WAS NOTIFIED AND EMERGENFeb 22, 2014 · Boeing 767333 · Brake Anti-Skid SectionSDR CA131202011Pump · failed(CAN) AIR RETURN DUE TO RT HYDRAULIC PRIMARY PUMP INOPERATIVE, QRH STATES 3 REQUIRED BEFORE ETOPS ENTRY, ELECTED TO RETURN LT AFTER DISCUSSION WITH MOC. RESOLUTION: RT ENGINE EDP REPLACED IAW AMM 29-11-05-404-115-0-01. REPLACED CASE DRAIN FILTER IAW 29-11-17Nov 30, 2013 · Boeing 767333 · Hydraulic Pump (Electric/Engine), MainSDR CA131021020Transceiver · failed(CAN) DURING DEPARTURE VHF 1 FAILED. CABIN/FLT DECK COMMUNICATION ALSO FAILED. AFTER CONSULTATION WITH CHIEF DUTY PILOT CAPTAIN ELECTED TO RETURN. ACFT APPROXIMATELY 21,000K OVERWEIGHT UPON LANDING. NR 1 VHF TRANCEIVER REPLACED IAW AMM 23-12-01-401. LT Oct 20, 2013 · Boeing 767333 · VHF Communications SystemSDR CA131017001Oven · failed(CAN) SMOKE ODOR IN MID GALLEY. BREAKERS PULLEY, ODOR DISSIPATED. NO FOOD OR PLASTIC IN OVENS, APPEARS TO BE IN WIRING. SMOKE ODOR FROM OVEN CONTROLLER, TOP OF OVEN VENT AND BACK OF THE OVEN. OVEN FAN MOTOR CHECKED , THERE IS BLACK MARKER IN IT. GALLEY WIOct 16, 2013 · Boeing 767333 · Buffet/GalleysSDR CA130930003Fan · failed(CAN) NOXIOUS FUMES DETECTED IN FLIGHT DECK AND CABIN. IN DISCUSSIONS WITH MOC RECIR FAN SELECTED OFF, C/B PULLED AND ODOR RAPIDLY DISSIPATED. RESOLUTION: LT CABIN AIR RECIRCULATION FAN REPLACED IAW AMM 21-25-01, PB 401. FUNCTION CHECKED SERVICEABLE.Sep 27, 2013 · Boeing 767333 · Air Distribution FanSDR CA130805017Gasket · leaking(CAN) DURING THE FLIGHT THE CREW REPORTED AN INCREASING FUEL IMBALANCE IN THE WING TANKS THAT ULTIMATELY REACHED APPROXIMATELY 1900KG. ON ARRIVAL MAINTENANCE FOUND A LEAKING FUEL FEED LINE ON THE RT ENGINE. FOUND FWD GASKET LEAKING ON LINE, PN 9378M19G07 TO HAug 2, 2013 · Boeing 767333 · Engine Fuel DistributionSDR CA130621003Pump · failed(CAN) DURING ENROUTE CLIMB EICAS RECEIVED FOR LT ENGINE HYDRAULIC PUMP OVERHEAT FOLLOWED SHORTLY AFTER BY LT QTY AND PRESSURE GOING TO ZERO. FLIGHT RETURNED. LT EDP REPLACED IAW AMM 29-11-05-404-115-0-01. LEAK AND FUNCTION CHECK SERVICE ENGINE EDP PRESS ANDJun 19, 2013 · Boeing 767333 · Hydraulic Pump (Electric/Engine), MainSDR CA130524004Probe · failed(CAN) PAN PAN DECLARED WITH LT ATC AS A RESULT OF LOSS OF TAT PROBE, AUTO THRUST AND DEGRADED L NAV/VNAV MODE. ENGAGED DUTY PILOT/MOC TAT PROBE REPLACED IAW AMM 34-12-02, PB 401, CHECKS OK.May 22, 2013 · Boeing 767333 · Outside Air Temperature Indicator/SensorSDR CA130516004Transmitter · failed(CAN) SHORT FINAL, APROX 2000 FT FLAP ASYMMETRY OCCURRED. EXECUTED A GO-AROUND, PLANNED A FLAP 1 LANDING, APROX SPEED 170KTS, FULL REVERSE USED. NO PAN OR EMERGENCY DECLARED, HOWEVER ATC HAD ARFF ON STANDBY FOR POTENTIAL OF HOT BRAKES (NO HOT BRAKES). FSEU May 12, 2013 · Boeing 767333 · Trailing Flap Position Indicating SystemSDR CA130426002Pca · leaking(CAN) WHILE TAXIING FOR DEPARTURE THE ACFT DEVELOPED A LEAK FROM THE LT HYD SYS AND RETURNED TO THE GATE. CTR, LT HYD SYS, RUDDER PCA REPLACED IAW J/C B767-27-21-02-422-038-8A98. INDEPENDENT CHECK CARRIED OUT.Apr 25, 2013 · Boeing 767333 · Rudder ActuatorSDR CA130218008Fmc · failed(CAN) ON DEPARTURE WHEN FLAPS SELECTED UP, FLIGHT EXPERIENCED ECAM AND AURAL FLAP WARNINGS. CREW ATTEMPTED A RESELECTION OF FLAPS FOLLOWED BY CIRCUIT BREAKER RESETS WITHOUT SUCCESS. A DIVERSION WAS CARRIED OUT WHERE AN OVERWEIGHT LANDING TOOK PLACE. FMR M14Feb 15, 2013 · Boeing 767333 · Trailing Edge Flap Control SystemSDR CA130114010Skin · failed(CAN) ON APPROACH, CREW EXPERIENCE A LIGHTNING STRIKE. THE FLIGHT ALSO EXPERIENCED A L/E SLAT ASYMMETRY WHEN LOWERING FLAPS FROM 15 TO 20. MAINTENANCE CONTROL ADVISED LIGHTNING STRIKE CHECK DONE IAW AMM 05-51-19-22-001. NO FINDING THIS FMR IS NOW CONSIDEREDJan 7, 2013 · Boeing 767333 · Leading Edge Slat Control SystemSDR CA121204009Fuel Cell · leaking(CAN) IN CRUISE PASSENGERS REPORTED FLUID COMING FROM LT WING. F/O VISUALLY CHECKED AND REPORTED LT WING, SOAKED. RT WING DRY. FUEL DISCREPENCY OF 400 DECIDED TO RETURN TO DEPARTED STA. LT WING THOROUGHLY CHECKED FOR SIGN OF FUEL LEAK OR PATCH OR ODOR. UNDec 1, 2012 · Boeing 767333 · Fuel StorageSDR CA121017002Stick Shaker · malfunctioned(CAN) ON DEPARTURE THE CREW EXPERIENCED A FALSE STICK SHAKER IN CLIMB. T/O SPEED AND ATTITUDE WAS NORMAL. MOC ADVISED. ASR TO FOLLOW. FIM 27-32-00-815-802 STALL WARNING MODULE, SWM, BITE PROCEDURE CARRIED OUT AND ALL TEST PASSED. SYSTEM OK AND SERVICEABLEOct 16, 2012 · Boeing 767333 · Stall Warning SystemSDR CA120713004Water System · failed(CAN) THE ACFT LOST ALL WATER PRESSURE WITH THE TANKS SHOWING LESS THAN HALF FULL. A PHONE PATCH WITH MAINTENANCE CONTROL WAS CONDUCTED AND A WATER LEAK WAS SUSPECTED. THERE WERE NO OTHER ASSOCIATED FAILURES SO THE FLIGHT ELECTED TO RETURN WHERE AN OVERWEIGHTJul 12, 2012 · Boeing 767333 · Potable Water SystemSDR CA120712004Actuator · cracked(CAN) 15 MINUTES AFTER TAKEOFF THE CREW REPORTED THE LOSS OF THE LT HYDRAULIC SYSTEM. THE FLIGHT RETURNED AND LANDED APPROXIMATELY 14 000KG OVER MAXIMUM LANDING WEIGHT. THERE WERE NO ACFT HANDLING ISSUES AND NO EMERGENCY WAS DECLARED HOWEVER ERS DID MEET THE AJul 12, 2012 · Boeing 767333 · Drag Control ActuatorSDR CA120628006Windshield · failed(CAN) WHILE ENROUTE BETWEEN 50W AND 40W AT FL350, PRIOR TO ENTERING ETOPS AIRSPACE THE F/O`S WINDSCREEN SHATTERED. THE DAMAGE APPEARED TO BE THE OUTER PANE. AFTER DISCUSSION WITH MAINTENANCE IT WAS AGREED THAT A DIVERSION WAS THE BEST COURSE OF ACTION. THE FLJun 27, 2012 · Boeing 767333 · Flight Compartment WindowsSDR CA120404010Unknown · odor(CAN) AS A RESULT OF A VERY STRONG ODOR IN ROWS 25-27 SEATS D, E AND F. THE CREW ELECTED TO RETURN WHERE AN OVERWEIGHT LANDING OCCURRED. ENGINE RUN ACCOMPLISHED OF EACH ENGINE FOR 30 MIN WITH NO ODOR OF MUSKY SOCKS. SEAT CARPET REPLACED AND AREA DEODORIZED Apr 2, 2012 · Boeing 767333 · Air Distribution SystemSDR CA120214002Wire · broken(CAN) AIRBORNE RETURN AFTER HPSOV FAILURE. EMERGENCY DECLARED, NORMAL APPROACH & LANDING CONDUCTED. FOUND CONNECTOR ON LT HPSOV CONTROLLER LOOSE. CONNECTOR SECURED AND BLEED TEST CARRIED OUT. CHECKED SERVICE DETAILS AND FOUND NO CONTINUITY BETWEEN TERMINALFeb 13, 2012 · Boeing 767333 · Pneumatic System WiringSDR CA120125001Engine · surges(CAN) ON FINAL APPROACH, CAPTAIN AND F/O OBSERVED THAT THE RIGHT HAND ENGINE WAS NOT RESPONDING PROPERLY TO THROTTLE INPUTS. EGT LIMITS EXCEEDED. ENGINE SURGING WAS NOTED AND PASSENGER REPORTED HAVING OBSERVED TORCHING.Jan 24, 2012 · Boeing 767333 · Engine (Turbine/Turboprop)SDR CA120120002Blade · fractured(CAN) THE NR 2 ENGINE HAD A DRAMATIC TREND SHIFT INTO LT, AND IMMEDIATE ACTION WAS TAKEN WITH THE RESULTS. THE FOLLOWING SHIFTS WERE IDENTIFIED: CRUISE FUEL FLOW INCREASE BY 2.6 PERCENT. CRUISE CORE SPEED INCREASE BY 0.650 PERCENT. CRUISE EGT INCREASE BY 15Jan 14, 2012 · Boeing 767333 · Turbine SectionSDR CA110809003Terminal · damagedWHILE IN CRUISE, EICAS MESSAGE SHOWED AIR CONDITIONING PACK INOP. FLIGHT DIVERTED FOR REPAIRS. HPSOV EICAS ILLUMINATED MULTIBLE TIMES AFTER LEVEL OFF AT FL320. CHECKLIST QRH COMPLETED MULTIPLE TIMES. MEL 36-11-02 APPLIED, HPSOV WAS SECURED CLOSED. FOUND LUGAug 4, 2011 · Boeing 767333 · Pneumatic System WiringSDR CA110725002Compressor · failed(CAN) CREW REPORT A FOUL ODOR EMANATING THROUGH CABIN ON CLIMB, ODOR DISSIPATED IN CRUISE. ON DESCENT/APPROACH, A TOXIC SMELL PERMEATED THROUGHOUT CABIN. SOME CREW MEMBERS WERE REPORTING SORE THROAT ASSOCIATED WITH THE TOXIC ODOR AND WANTED TO USE OXYGEN MASJul 24, 2011 · Boeing 767333 · Turbine Engine Compressor SectionSDR CA110708009Sensor · failedAFTER DEPARTURE, IN A RT TURN THROUGHT 5000FT TO 7000FT, A L/E ASYMMETRY ICAS MESSAGE WAS RECEIVED WHEN THE FLAPS WERE BEING MOVED TO THE UP POSITION. ATC WAS ADVISED AND THE FLIGHT LEVELED OFF AT 7000 FT AND SPEED REDUCED. THE QRH PROCEDURE WAS FOLLOWED BUT TJun 29, 2011 · Boeing 767333 · Leading Edge Slat Position Indicating SystemSDR CA110623001Scoop · dislodgedDURING 635, NR1 ENG GEARBOX SCAVENGE OIL PUMP STRAINER ASSY REPLACEMENT, FOUND IDG GEARSHAFT OIL SCOOP ADRIFT IN BOTTOM OF GEARBOX. THIS ISSUE HAS BEEN ADDRESSED BY MFG TO ALLOW FOR CONTINUED OPERATION WITHOUT THE SCOOP INSTALLED UNTIL THE NEXT GEARBOX O/H.Jun 20, 2011 · Boeing 767333 · Turbine Engine Oil SystemSDR CA110704010Union · leakingEICAS C HYD QTY MESSAGE 4 HRS AFTER T/O. C HYD QTY SHOWED 0.46 TURNED OFF C HYD PRESS TO SAVE FLUID. QTY SLOWLY DROPPED TO 0.35. FRM 29-11-15-00. HYD LEAK FOUND AT C2 PUMP PRESSURE LINE. SEAL REPLACED AT PUMP UNION IAW AMM 29-11-02, PB401. LEAK CHECK OK. Jun 19, 2011 · Boeing 767333 · Hydraulic System, MainSDR CA110621005Fitting · leakingTHE CREW EXPERIENCED A LOW HYD SYS PRESSURE AND DECLARED AN EMERGENCY PRIOR TO LANDING. EICAS C HYD QTY MESSAGE 4 HRS AFTER T/O. C HYD QTY SHOWED 0.46 TURNED OFF C HYD PRESS TO SAVE FLUID. QTY SLOWLY DROPPED TO 0.35. FRM 29-11-15-00 HYD LEAK FOUND AT C2 PUMJun 19, 2011 · Boeing 767333 · Hydraulic System, MainSDR CA110603001Engine · failedDURING CLIMB, FLIGHT EXPERIENCED A FAILURE OF THE LEFT ENGINE. CREW ELECTED TO DIVERT. NR 1 ENGINE REPLACED IAW AMM.Jun 1, 2011 · Boeing 767333 · Engine (Turbine/Turboprop)SDR CA110324004Receptacle · contaminated(CAN) AFTER DEPARTURE, THE AIRCRAFT BEGAN EXPERIENCING PROBLEMS WITH THE RIGHT SIDE EGT INDICATION IN NORMAL AND STANDBY. RIGHT HAND EGT ON UPPER EICAS AND STANDBY ENGINE INDICATOR WENT BLANK ON CLIMB OUT. OCCASIONALLY EGT WOULD INDICATE BUT ERRONEOUSLY. CREW Mar 23, 2011 · Boeing 767333 · Engine Indicating System WiringSDR CA110124006Actuator · failedFLIGHT CREW REPORTED THAT DURING APPROACH A FLIGHT SPOILER PANEL REMAINED DEPLOYED WITH ASSOCIATED ACFT ROLL. THE AUTOPILOT WAS DISCONNECTED AND THE REMAINDER OF THE APPROACH WAS HAND FLOWN. AFTER LANDING IT WAS CONFIRMED THE NR 1 SPOILER PANEL ON THE LT SIJan 24, 2011 · Boeing 767333 · Drag Control ActuatorSDR CA110125021Control Module · unserviceable(CAN) DURING APPROACH A FLIGHT SPOILER PANEL REMAINED DEPLOYED WITH ASSOCIATED AIRCRAFT ROLL. THE AUTOPILOT WAS DISCONNECTED AND THE REMAINDER OF THE APPROACH WAS HAND FLOWN. AFTER LANDING IT WAS CONFIRMED THE ONE SPOILER PANEL ON THE LEFT SIDE WAS STILL DEPLOJan 23, 2011 · Boeing 767333 · Drag Control ActuatorSDR CA110124005Electronic Unit · unserviceableGOING THROUGH 15000 UNCONTROLLED TAIL OSCILLATION BACK AND FORTH - DISCONNECTED AUTOPILOT STILL OSCILLATIONS - CALL FROM F/A - VERY VIOLENT IN TAIL- SLOWED ACFT & STOPPED - NO WARNING LIGHTS. ON INVESTIGATION FOUND RT YAW DAMPER CHANNEL FAILING TEST, WITH INOJan 22, 2011 · Boeing 767333 · Flight ControllerSDR CA110105009Windshield · failedIN CRUISE, ELECTRICAL ARCING OBSERVED FROM FIRST OFFICER NR 1 WINDSHIELD. POPPING SOUND HEARD WHEN WINDSHIELD HEAT SELECTED OFF. OUTER WINDOW WAS COMPLETELY SHATTERED. FLIGHT CONTINUED TO DESTINATION. FIRST OFFICER NR 1 WINDOW ASSY REPLACED PER AMM 56-11-01Jan 4, 2011 · Boeing 767333 · Flight Compartment WindowsSDR CA101222002Adc · failed(CAN) AS A RESULT OF AN AIR DATA COMPUTER FAILURE, IN CONSULTATION WITH MTC AND DISPATCHER AND SOC, RETURN TO POINT OF DEPARTURE WHERE AN OVERWEIGHT LANDING OF 167.5KGS WAS CARRIED OUT.CREW REQUESTED EMERGENCY VEHICLES TO STAND BY BUT EMERGENCY NOT DECLARED. Dec 21, 2010 · Boeing 767333 · Air Data ComputerSDR CA101202001Transceiver · damaged(CAN) OVERWEIGHT LANDING ON ACCOUNT OF AIRBORNE RETURN DUE TO WEATHER RADAR FAILURE, APPROXIMATE LANDING WEIGHT 152.0. CREW REQUESTED CFR TO BE ON STANDBY. FOUND BADLY DAMAGED PIN ON TRANSCEIVER (PIN2 ON C CONNECTOR) WX TRANSCEIVER REPLACED AS PER AM 34-43-0Dec 1, 2010 · Boeing 767333 · Weather Radar SystemSDR CA101122012Shutoff Valve · leaking(CAN) ELEC FLAP/SLAT MESSAGE AT CRUISE. DUE TO CTR HYD LEAK. FLAP/SLAT HYD SHUTOFF VALVE MODULE REPLACED AS PER AMM 29-11-00/201. LEAK CHECK AND FLT CONT OPS CHK, OK. MODULE INSTALLED DATE: 2004-01-13 OVERWEIGHT LANDING ACCOUNT OF MECHANICAL DIVERSION DUE Nov 20, 2010 · Boeing 767333 · Hydraulic System, MainSDR CA101110010Latch · failed(CAN) LT THRUST REVERSER COWL BAND LATCH FOUND BROKEN AT THE LOWER LATCH POSITION IPC 78-31-05 ITEM 127.Nov 8, 2010 · Boeing 767333 · Engine Thrust ReverserSDR CA101015001Pseu · failedAFTER TAKEOFF AND IN CLIMB THE CREW REPORTED FLAP/SLATS ASSYMETRY. DISCUSSIONS WITH MX TO RECTIFY THE PROBLEM WERE UNSUCCESSFUL AND THE FLIGHT RETURNED TO DEPARTURE, APPROX 25,000K OVERWEIGHT FSEU LAST LEG CODES 27-81021 & 27-81042. PSEU BIT FAULTS NR 10 & S3Oct 14, 2010 · Boeing 767333 · Leading Edge Slat Control SystemSDR CA100914002Wire · chafedINFLIGHT ENTERTAINMENT SYS NOT WORKING FOR SEATS 25-40DEF AND 26-38HK. IFE FAN TRU C/B POPPING. TROUBLESHOOTING REVEALED THAT 4 IFE WIRES IN THE FWD EE COMPARTMENT WERE CHAFING AGAINST THE AFT SIDE OF RACK E3-2 AND CAUSED THE C/B TO TRIP. THE WIRES WERE REPLSep 13, 2010 · Boeing 767333 · Electrical Power System Wiring
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