Boeing 767-375

Service difficulty reports · 1,386

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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 = '767375'
  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 CA141229006Hose · ruptured(CAN) ARRIVED WITHOUT ISSUE AFTER THE AIRCRAFT EXPERIENCED A LOSS IN HYDRAULIC PRESSURE. RESOLUTION MAINTENANCE CREW FOUND LT HYDRAULIC FLEX LINE BETWEEN RUDDER RATIO CHANGER AND MODULE LEAKING. LINE REPLACED IAW 27-21-15 PB 201 AND AMM 20-10-10.Dec 28, 2014 · Boeing 767375 · Hydraulic System, MainSDR CA141229005Power Supply · failed(CAN) AIRCRAFT LOST THE FIRST OFFICER`S FLIGHT DIRECTOR, COMMAND BARS LOST AND AUTOLAND STATUS TO NO LAND 3 THE CREW ALSO HAD A FAINT ELECTRICAL ODOR IN THE COCKPIT. ELECTED TO DIVERT AND DECLARED AN EMERGENCY. RT FCC FOUND TO HAVE A BURNED OUT POWER SUPDec 28, 2014 · Boeing 767375 · Flight ControllerSDR CA141212004Module · failed(CAN) CREW REPORTED LOSS OF HYDRAULIC PRESSURE IN THE CENTRE HYDRAULIC SYSTEM. ATC WAS ADVISED. STATION WAS ADVISED. MTC WAS ADVISED. A PAN PAN PAN WAS DECLARED. ATC GAVE AC117 AN EXTENDED DOWNWIND WHILE THE CREW WENT OVER THE HYDRAULICS SYSTEM PROCEDURES. MTCDec 11, 2014 · Boeing 767375 · Hydraulic System, MainSDR CA141031019Engine · power loss(CAN) ON DEPARTURE FROM CDG, CREW REPORTED RIGHT ENGINE WAS UNABLE TO OBTAIN TOGA THRUST ON TAKE-OFF RIGHT TO FIREWALL.Oct 31, 2014 · Boeing 767375 · Engine (Turbine/Turboprop)SDR CA140714009Power Supply · failed(CAN) DURING TAKEOFF ROLL AN AURAL FIRE WARNING BEGAN TO CHIME, THERE WERE NO OTHER INDICATIONS. AFTER TALKING TO MAINTENANCE THE CREW ELECTED TO RETURN TO NRT AND LAND APPROXIMATELY 25 500KG OVERWEIGHT. NO PANPAN OR MAYDAY DECLARED. RESOLUTION: PERFORMED WEUJul 11, 2014 · Boeing 767375 · Overheat DetectionSDR CA140617003Antenna · failed(CAN) WEATHER RADAR FAILURE AFTER TAKEOFF, RETURNED. LANDING WEIGHT APPROXIMATELY 167.0K. EMERGENCY DECLARED WITH ATC DUE POSSIBILITY OF OVERHEATING BRAKES. EMS STANDING BY. MOC INFORMED. WEATHER RADAR ANTENNA MOUNT REPLACED. ANTENNA WAVEGUIDE SWITCHING UJun 16, 2014 · Boeing 767375 · Weather Radar SystemSDR CA140613001Circuit Card · failed(CAN) ON TAXI-IN, FLIGHT CREW RECEIVED AN AURAL FIRE WARNING. CONTINUED TO THE GATE, CRF WAS CALLED TO THE ACFT FOR PRECAUTIONARY REASONS. RAMP CREW WERE KEPT CLEAR, AND CRF CLEARED ACFT WITHOUT INCIDENT. MASTER WARNING MODULE, M618 REPLACED IAW AMM 31-51-0Jun 12, 2014 · Boeing 767375 · Central WarningSDR CA140602032Union · leaking(CAN) WHILE ENROUTE, ACFT RECEIVED EICAS MESSAGE REGARDING CENTER HYD QTY LOW. FLIGHT PROCEEDED TO DESTINATION, BUT DUE TO LOW HYDRAULIC QTY, MANUAL GEAR EXTENSION WAS PERFORMED. FLIGHT DECLARED EMERGENCY, AND TRANSPONDER CODE 7700 WAS SELECTED. ON ARRIVAL IMay 30, 2014 · Boeing 767375 · Hydraulic System, MainSDR CA140423003Valve · failed(CAN) RT THRUST REVERSER FAILED TO STOW ON ROLLOUT RUNWAY 33L. MOC NOTIFIED. RT ENGINE DIRECTIONAL PILOT CONTROL VALVE REPLACED, RT ENGINE DPV PRESSURE SWITCH MOISTURE PURGE, REF 6-78-30-00AC-04-01-01. RT REVERSER REACTIVATED AND OPS CHECKED, IAW 78-31-00-7Apr 23, 2014 · Boeing 767375 · Engine Thrust ReverserSDR CA140327007Actuator · damaged(CAN) FLIGHT DEPARTED AND CREW HAD WHAT FELT LIKE AN ENGINE FAILURE ON THE RT SIDE, ALL ENGINE PARAMETERS NORMAL. ACFT WAS STILL YAWING AND SHOWED 9 UNITS OF RUDDER TRIM. MOC AND DISPATCH CONSULT WITH FLIGHT. DUTY PILOT CALLED AND BRIEFED BUT DUE TO POOR WEAMar 26, 2014 · Boeing 767375 · Rudder Tab Control SystemSDR CA140319001Slat System · failed(CAN) ON FINAL, THE CREW HAD AN INDICATION OF L/E SLAT ASYMMETRY. ACTUAL L/E SLATS WERE IN THE CORRECT POSITION ON BOTH SIDES RESOLUTION: CARRIED OUT FMR STEPS 2 TO 4 AND NO FAULTS NOTED. STEP 5 ALSO CARRIED OUT. THE RESISTANCE WAS MEASURED AT 19.7 OHMS. SENSMar 18, 2014 · Boeing 767375 · Leading Edge Slat Control SystemSDR CA140217021Unknown · odor(CAN) CAPTAIN REPORTED STRONG ODOR OF OIL IN FLIGHT DECK. MOC WAS NOTIFIED. FUMES BECAME STRONG ENOUGH TO WARRANT THE DONNING OF OXYGEN MASKS IN THE FLIGHT DECK. AN HOUR LATER, THEY REPORTED THAT THE FUMES WERE DISSIPATING. LT ENGINE GROUND RUN WITH BLEEDS Feb 15, 2014 · Boeing 767375 · Air Distribution SystemSDR CA140206004Pneumatic System · malfunctioned(CAN) ECAM CABIN ALTITUDE DURING THE CLIMB. BOTH ENGINE BLEED PRESSURES REMAINED BELOW 20PSI, INSUFFICIENT TO PRESSURIZE CABIN. CREW REQUESTED DESCENT AND STARTED THE APU, SHORTLY THEREAFTER THE ENGINE BLEED SYS STARTED WORKING NORMALLY. AFTER CONSULTATION Feb 5, 2014 · Boeing 767375 · Pneumatic Distribution SystemSDR CA140121003Ring · rotated(CAN) TROUBLESHOOTING LOG BOOK REPORT L4870735 REPEAT OF LT BRAKE GRINDING NOISE ABV 10 KTS ON LANDING AND TAXI, FOUND NR 2 BRAKE ASSY HEAT SHIELD BROKEN FROM BRAKE ASSY. APPEARS HEATSHIELD ATTACHMENTS BROKEN AND FOUND RUBBING BETWEEN BRAKE ASSY AND WHEEL ASSJan 7, 2014 · Boeing 767375 · Landing Gear Brake SystemSDR CA131105008Unknown · odor(CAN) AT APPROXIMATELY 0150Z, IN CRUISE, AT FL340 THE CREW EXPERIENCED A FUME LIKE ODOR "STINKY SOCKS " NOT AN ELECTRICAL BURNING ODOR. THE CREW DAWNED THE COCKPIT O2 MASKS FOR 5 MINS TILL THE FUMES DISSIPATED. A PHONE PATCH BETWEEN DISPATCH, ACFT AND MOC WANov 4, 2013 · Boeing 767375 · Air Distribution SystemSDR CA131029007Coffeemaker · failed(CAN) APPROXIMATELY 2 HRS AFTER TAKEOFF THERE WAS A STRONG BURNING ODOR FROM COFFEEMAKER 1 OR 2 FOLLOWED BY AN ORANGE FLASH AND A PUFF OF WHITE SMOKE. THE CIRCUIT BREAKERS WERE PULLED AND THE CREW REPORTS ALL OK AT THIS TIME RESOLUTION: REPLACED COFFEEMAKER Oct 29, 2013 · Boeing 767375 · Buffet/GalleysSDR CA130906003Irs · failed(CAN) ON TAKEOFF WE GOT A CENTER IRS ON DC EICAS MESSAGE, DURING THE CLIMB THE ALIGN ILLUMINATE ON THE CENTER IRS. CONTACTED MOC AND WAS ADVISED TO RETURN TO BS. CTR IRS CHANGED IAW AMM 34-21-01-PB401.Sep 1, 2013 · Boeing 767375 · Attitude and Direction Data SystemSDR CA130731001Module · leaking(CAN) PRIOR TO ENTERING ETOPS AIRSPACE, THE CENTER HYDRAULIC WARNING LIGHT CAME ON, THE CREW WAS CONNECTED TO MAINTENANCE AND THRU A DISCUSSION THEY WERE ABLE TO EXTINGUISH THE WARNING LIGHT. HOWEVER THE PRESSURE WAS STILL LOW, BUT WITHIN NORMAL VALUES AND THJul 28, 2013 · Boeing 767375 · Hydraulic Pump (Electric/Engine), MainSDR CA130731002Actuator · failed(CAN) SOON AFTER DEPARTURE, THE ACFT LOST NR 2 PACK. UNABLE TO CONTINUE TO DESTINATION. ACFT LANDED OVERWEIGHT AND EMERGENCY EQUIPMENT WAS CALLED OUT. RT PACK CONTROLLER BITE TEST C/OUT. FOUND FAULTY RT PACK EXHAUST ACTUATOR. RT RAM AIR EXHAUST ACTUATOR REJul 24, 2013 · Boeing 767375 · Cabin Cooling SystemSDR CA130621002Hose · loose(CAN) FIRE TRUCKS WERE CALLED TO INVESTIGATE FUEL LEAKING FROM ACFT. MAY HAVE BEEN REPORTED AS A FUEL LEAK BY SOMEONE AT THE STATION BUT IT WAS A HYDRAULIC FLUID LEAK FROM THE TAIL OF THE ACFT. MOC SUSPECTS A COLD SOAKED YAW DAMPER ACTUATOR SEAL FAILURE. PUDJun 19, 2013 · Boeing 767375 · Hydraulic System, MainSDR CA130502006Actuator · failed(CAN) RUDDER TRIM NOT RESPONDING TO INPUTS. NO MOVEMENT ON FLIGHT CONTROL PAGE OR RUDDER TRIM POSITION ON PEDESTAL. RUDDER TRM RESET C/B NO FIX CLEANED RUDDER TRIM SW IAW AMM 27-21-23-102-017: NO FIX FIM 27-21-00-990-806 ACCOMPLIHED UP TO ITEM 54 POWER CHECMay 1, 2013 · Boeing 767375 · Rudder Tab Control SystemSDR CA130114007Hose · failed(CAN) AFTER ENGINE START "LT HYD SYS PRESS" AND "LT HYD QTY" CAUTION ILLUMINATED. HYD PRESSURE AND QTY SHOWED ZERO. LEAK FROM VERTICAL TAIL CONFIRMED VISUALLY BY GROUND CREW. DURING INSPECTION CHECK FOUND HYD LEAK ON RUDDER RATIO CHANGER HOSE. RUDDER RATIODec 28, 2012 · Boeing 767375 · Hydraulic System, MainSDR CA130103006Ballast · failed(CAN) BURNING ODOR EMANATING FROM A3 LAVATORY, L2 BAR AREA. GALLEY POWER SHUTDOWN, VIDEO SCREENS POWER SHUTDOWN IAW ADVISE FROM MOC. MAINTENANCE TRAVELING ON THE FLIGHT PERFORMED AN INSPECTION RECOMMENDED SHUTTING DOWN LAVATORY LIGHTING CIRCUIT. FOUND AFT GDec 25, 2012 · Boeing 767375 · Passenger Compartment LightingSDR CA121217006Indicator · failed(CAN) WHILE ENROUTE, APPROXIMATELY 2 HRS AFTER TAKEOFF THE CREW ADVISED THEY HAS LOST THEIR NAVIGATION SYSTEMS. AFTER DISCUSSION WITH MAINTENANCE IT WAS DETERMINED THAT A RE-SET ON THE GROUND WOULD BE REQUIRED. THE FLIGHT DIVERTED AND LANDED. OK FOR SERVICEDec 15, 2012 · Boeing 767375 · Navigation SystemSDR CA121121001Idg · failed(CAN) RIGHT GENERATOR FAILED FORCING CREW TO RETURN TO BASE AND PERFORMED AN OVER-WEIGHT LANDING. NO REPORT OF HARD LANDING, AND SINK RATE INDICATED WAS LOW TO MODERATE. OVERWEIGHT LANDING INSPECTION CARRIED OUT IAW J/C 6-220A, NO FAULT FOUND, OK FOR SERVICNov 20, 2012 · Boeing 767375 · AC Generator-AlternatorSDR CA121119007Track · fractured(CAN) THIS MORNING A FRACTURED OTBD DEFLECTION CONTROL TRACK WAS FOUND ON THE ACFT LT OTBD FLAP. A PRELIMINARY ENGINEERING INSPECTION FOUND DAMAGE TO THE WING T/E UPPER PANEL, PN 113T1346-113, FLAP L/E ACCESS PANEL AND AILERON CLOSURE CAP. NOTE: THIS IS A KNNov 15, 2012 · Boeing 767375 · Trailing Edge FlapsSDR CA120731001Control Unit · overheated(CAN) RIGHT FORWARD WINDOW HEAT TURNED OFF DUE OVERHEATING FUMES VERY EVIDENT.Jul 30, 2012 · Boeing 767375 · Windshield/Door Rain/Ice RemovalSDR CA120727015Idg · failed(CAN) ACFT WAS IN-FLIGHT FOR ALMOST 3 HRS, WHEN THEY HAD A LT GENERATOR FAILURE. APU WAS STARTED BUT THEN FAILED. APU STARTED UP AGAIN BUT HAD REDUCED ELECTRICAL OUTPUT. A DIVERSION WAS THEN SET UP. WHILE ENROUTE TO THE CREW THEN HAD A COMPLETE APU AUTO SHJul 27, 2012 · Boeing 767375 · AC Generator-AlternatorSDR CA120713006Unknown · odor(CAN) FLIGHT CREW ADVISED OF VERY STRONG ELECTRICAL SMELL THROUGHOUT THE COCKPIT AND CABIN. RAPID BUT ORDERLY DEPLANEMENT OF PASSENGERS AND CREW. LOCAL FIRE DEPARTMENT RESPONDED. MAINTENANCE: STRONG ODOR COMING FROM JETTY AREA PRIOR TO ENTERYING ACFT. C1 Jul 13, 2012 · Boeing 767375 · Air Distribution SystemSDR CA120604013Fuel Tank · leaking(CAN) WHILE ON THE GATE, ACFT BEGAN TO LEAK FUEL FROM THE RT WING AT THE SUMP AREA. APPROXIMATELY 2 SQUARE METERS IN SIZE. TIGHTEN THE SCREWS OF PRESS RELIEF PANEL IN RT SURGE TANK. NO HELP TRANSFERED THE FUEL FROM RT TANK TO CENTER TANK. NO HELP. DRAIN TJun 4, 2012 · Boeing 767375 · Fuel StorageSDR CA120522018Radar · failed(CAN) DUAL WEATHER RADAR FAILURE APPROXIMATELY 20 MINUTES AFTER DEPARTURE. OPERATING CREW ELECTED TO RETURN. ACFT LANDING OVER MAXIMUM LANDING WEIGHT. WEATHER RADAR SYSTEM RESET, OPS TEST CUT OUT IAW AMM 34-43-00.501. TEST PASSED, SYSTEM SERVICEABLE.May 20, 2012 · Boeing 767375 · Weather Radar SystemSDR CA120531004Fitting · fractured(CAN) THIS ENGINE PYLON MIDSPAR FITTING WAS FRACTURED DURING A 400 CYCLE REPEAT INSPECTION ON THE ENGINE PYLON.May 1, 2012 · Boeing 767375 · Nacelle/Pylon, Attach FittingsSDR CA120412001Slide · failed(CAN) DURING THE ACOMPLISHMENT OF SB 767-25A0260, THE LT OFF WING SLIDE UNLATCH ACTUATOR FAILED TO FULLY UNLATCH UNDER 175 IN/LBS IAW SB REQUIREMENT. ON FURTHER INVESTIGATION IT WAS DISCOVERED THAT THE MOST FWD LATCH DID NOT OPEN FULLY AND THIS CAUSED THE JAMMar 30, 2012 · Boeing 767375 · Escape SlideSDR CA120330003Warning Light · illuminated(CAN) ENROUTE, ON TRACK ECHO JUST AFTER CROSSING 30W, FLIGHT RECEIVED EICAS MESSAGE, RT ENGINE OIL FILTER CLOGGED. FLIGHT FOLLOWED QRH AND BROUGHT ENGINE BACK TO IDLE AND DESCENDED TO FL260 AND INITIATED A DIVERSION. MAINTENANCE CONTROL, FLIGHT SAFETY AND TMar 30, 2012 · Boeing 767375 · Turbine Engine Oil SystemSDR CA120312014Duct · ruptured(CAN) AFTER ARRIVING AT THE GATE AND DURING WALK-AROUND, FOUND NR 4 SLAT, LT WING, INBD BLOW OUT PANEL BLOWN WITH NO ANTI-ICING DUCT VISIBLE FROM THE OPENING. FURTHER INSPECTION REVEALED THE DUCTS TO BE DISINTEGRATED AND FRAYED WITH STRANDS OF TUBE MATERIAL BMar 5, 2012 · Boeing 767375 · Airfoil Anti/De-ice SystemSDR CA120306007Flap System · malfunctioned(CAN) FLIGHT CREW REPORTED ON APPROACH WHILE EXTENDING THE FLAPS FROM 15 TO 20 THEY WERE PROMPTED WITH A FLAP DISAGREE MESSAGE. THE CREW EXECUTED A GO-AROUND AND LANDED WITHOUT ISSUE ON THE SECOND APPROACH. ALT FLAPS RESET FLAPS INSPECTED, NO FAULTS FOUND FLMar 2, 2012 · Boeing 767375 · Trailing Edge Flap Control SystemSDR CA120124005Engine · shutdown(CAN) DURING PUSHBACK BOTH ENGINES STARTED NORMALLY, NR 1 ENGINE SHUTDOWN WITHOUT WARNING.Jan 23, 2012 · Boeing 767375 · Engine (Turbine/Turboprop)SDR CA120110002Wire · damaged(CAN) AFTER DEPARTURE, THE IN-CHARGE F/A NOTICED A SMOKE ODOR IN THE GALLEY. THE SMOKE WAS CONFIRMED BY THE CREW AND THE FLIGHT RETURNED AFTER DECLARING A "PAN PAN" WITH ATC. DAMAGED WIRES TO NR 2 FWD GALLEY OVEN REPAIRED AND NR 2 OVEN C/B REPLACED IAW ENGINEJan 9, 2012 · Boeing 767375 · Equipment/Furnishings WiringSDR CA111104002Slat System · malfunctioned(CAN) ACFT ENCOUNTERED AN "L/E SLAT ASYMMETRY EICAS" MESSAGE WHEN FLAPS 20 WAS SELECTED ON APPROACH. QRH PROCEDURES CARRIED OUT. AFTER LANDING, FLAPS WOULD NOT GO PAST FLAPS 1 WHEN SELECTED UP. BITE TEST OF FSEU PERFORMED, NO FAULT. OPS TEST PERFORMED IANov 2, 2011 · Boeing 767375 · Leading Edge Slat Control SystemSDR CA111026011Idg · failed(CAN) ACFT DISCONNECTED THE LT IDG APPROX 3 HR IN FLIGHT DUE TO THE DRIVE LIGHT AND ECAM MESSAGE ILLUMINATING. SCL FOUND THE 2 ADJUSMENT BOLT HEADS MISSING AND OIL IN THE COWL. THE IDG REQUIRED APPROX 3 LITRES OF OIL TO SERVICE. IMAGES 1 SHOWS THE BOLT HEADOct 7, 2011 · Boeing 767375 · AC Generator-AlternatorSDR CA110922008Indicator · frozen(CAN) DURING THE TAKEOFF, THE CREW REJECTED TAKEOFF DUE TO A LACK OF AIRSPEED INDICATION. CAPTAIN AIR SPEED INDICATOR FROZE ON APPROACH AT 150KTS WITH AN ORANGE FLAG DUE TO HOT BRAKES THE ACFT REMAINED ON THE RUNWAY TILL EMERGENCY VEHICLES ATTENDED. THE ACSep 15, 2011 · Boeing 767375 · Airspeed/Mach IndicatorSDR CA110830010Engine · overtemp(CAN) THE CREW REPORTED A 5 SECOND ENGINE OVERTEMP ON DEPARTURE. MAX TEMPERATURE REACHED WAS 965 DEGREES.Aug 29, 2011 · Boeing 767375 · Engine (Turbine/Turboprop)SDR CA110823004Skin · cracked(CAN) MX FOUND DURING WALKAROUND, FOUND NR 11 L/E SLAT SKIN DAMAGED. TOP SKIN TORN AWAY 13" WIDE, 6.5" FORE AND AFT, PULLED RIVETS ON BOTTOM. ACFT PULLED OFF SERVICE REQUIRING REPAIR AND POSSIBLY A SLAT CHANGE. TEMP REPAIR HAS BEEN INSTALLED, PENDING MFGAug 13, 2011 · Boeing 767375 · Leading Edge DevicesSDR CA110815011Indicator · failed(CAN) AT THE 80 KNT A/T CHECK ON TAKE-OFF FO`S A/T READ ZERO. REJECTED TAKEOFF AIR SPEED INDICATOR REPLACED MPN: 4039891-903,Aug 12, 2011 · Boeing 767375 · Air Data ComputerSDR CA110607014Contactor · looseRELAY FAILED IN FLIGHT CAUSING SEVERAL SYS FAILURES. PART WAS REPLACED ON SPEC. IT WAS NOTED THAT SEVERAL OF THE CONNECTING POSTS WERE LOOSE, ALMOST IF THE BONDING MATERIAL OR SOLDER HAD FAILED.Jun 3, 2011 · Boeing 767375 · Electrical Power System WiringSDR CA110503004Wire Harness · chafed(CAN) DURING OPERATIONAL CHECK OF HYDRAULIC POWER TRANSFER UNIT SYSTEM,ARCING WAS OBSERVED AT WIRING BUNDLE CLAMP (APPROX) 2 FEET FROM RIGHT HAND ACMP POWER CONNECTOR. OPERATIONAL CHECK STOPPED , WIRING CLAMP REMOVED WHICH REVEALED CHAFFING AND ARCING OF RT EMay 2, 2011 · Boeing 767375 · Hydraulic Power System WiringSDR CA110418003Autothrottle Sys · failed(CAN) CREW ADVISED FLIGHT DISPATCH THAT THEY WERE HAVING "AUTO-THROTTLE" PROBLEMS AFTER TAKEOFF. THE PROBLEM SEEMED TO BE AFFECTING FLIGHT CONTROLS , THE CREW, MOC AND FLIGHT DISPATCHER AGREED TO HAVE THE ACFT RETURN BACK TO POINT OF DEPARTURE. NO EMERGENCY WApr 16, 2011 · Boeing 767375 · Auto Throttle SystemSDR CA110323004Rvdt · misrigged(CAN) ON APPROACH THE CREW HAD A LE ASYMMETRY FAULT. PERFORMED A GO AROUND. QRH PROCEDURE WAS CARRIED OUT & THE FLIGHT THEN LANDED, FLAP & SLAT UNIT MSG M48. OTBD SLAT PDU RVDT MIS-RIG, SLAT & FLAPS ALTERNATE CYCLED. FLAP & SLATS OPERATED SEVERAL CYCLES ONMar 22, 2011 · Boeing 767375 · Leading Edge Slat Control SystemSDR CA110303001Sensor · failed(CAN) DURING THE APPROACH TO R23 AT APPROX 170 KTS THE LT ENGINE SPOOLED DOWN. THE ENGINE DID NOT SHUT DOWN. WHEN POWER WAS RE-APPLIED THE ENGINE SEEMED SLUGGISH TO RETURN TO POWER. THE FLIGHT CONTINUED TO LAND NORMALLY CIT SENSOR REPLACED IAW AMM 73-21-02Feb 28, 2011 · Boeing 767375 · Cylinder Head Temperature (CHT) Indicating SystemSDR CA110210011Power Supply · odorPRIOR TO DEPARTURE THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE CABIN, NO SMOKE WAS VISIBLE. FOUND INDIRECT CEILING LT POWER SUPPLY U/S AND INBD CEILING LTS AT ROW 34/35 U/S. POWER SUPPLY REPLACED, LIGHTING RESTORED. ODOR DISSIPATED.Feb 10, 2011 · Boeing 767375 · Passenger Compartment Lighting
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