Boeing 757-236
Service difficulty reports · 2,544
Newest first. General aviation reporting is voluntary.
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 = '757236' 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.
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 = '757236' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 20010425AP009Switch · failedAFTER ENGINE START, RIGHT ENGINE AUTO SHUTDOWN WITH EICAS MESSAGE RT ENG SPAR VALVE AND SPAR VALVE LIGHT. REMOVED AND REPLACED RIGHT ENGINE SHUTOFF SWITCH IN FIRE CONTROL PANEL. (M)SDR CA010307014Bolt · sheared(CAN) DURING ROUTINE CHECK FOUND NR 1 ENGINE RT C DUCT AFT FORWARD BOLT SHEARED. AIRCRAFT WAS FERRIED ON A FERRY FLIGHT PERMIT WITH BOEING SUPPORT AND BOLT REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR 20010316SG005Drain Valve · inoperativeRIGHT ENGINE DID NOT SHUTDOWN WITH FUEL CONTROL SWITCH (2 ATTEMPTS), PULLED FIRE HANDLE. ENGINE STILL DID NOT SHUTDOWN. RECYCLED FUEL SWITCHES AGAIN, ENGINE SHUTDOWN. REPLACED PRESSURIZING AND DRAIN VALVE, OPS CHECKED GOOD. (M)SDR 20010207SG019Cable · brokenDURING ROUTINE C-CHECK, FOUND L2 DOOR EMERGENCY ESCAPE SLIDE DEPLOY RELEASE CABLE SAFETY STRING BROKEN AT PARACHUTE PIN. REPLACED SLIDE ASSEMBLY. (M)SDR 20010207SG018Cable · brokenDURING ROUTINE C-CHECK, FOUND L1 DOOR EMERGENCY ESCAPE SLIDE DEPLOY RELEASE CABLE BREAKAWAY STRING BROKEN AT PARACHUTE PINS. REPLACED ESCAPE SLIDE. (M)SDR 20010214SG002Transducer · inoperativeAIR RETURN DUE TO AFTER TAKEOFF CREW O2 DROPPED TO 10 PSI. RETURNED TO NORMAL AFTER LANDING. PLACARDED CREW 02 PRESS INDICATION ON EICAS PER MEL 35-11-02 SIT 1. PRESSURE TRANSDUCER INOPERATIVE. REPLACED TRANSDUCER AND RETURN TO SERVICE. (M)SDR CA010103021Expansion Ring · leaking(CAN) HP 6 EXPANSION DUCT LEAK CAUSING BURNS TO DIFFERENT COMPONENTS IN THE AREA (NR 1 PYLON). THE MAJOR COMPONENT THAT WAS AFFECED IS THE C DUCT RT SIDE THE FWD UPPER CORNER IS DELAMINATED AND REQUIRED REPAIR MANY OTHER PARTS HAD DAMAGES AND NEEDED REPLACEMENSDR 20010112SG057Switch · dirtyAT START OF DESCENT, FL 390, FORWARD ACCESS DOOR EICAS MESSAGE CAME ON. CONTINUED DESCENT AND MESSAGE WENT OUT AT ABOUT 5,000 FEET. INVESTIGATION REVEALED NO DEFECTS, CLEANED UNLOCK SWITCH AS PRECAUTION. (M)SDR CA010103018Control Valve · stuck(CAN) AFTER LANDING, PILOT REPORTED THAT NR 1 ENGINE THROTTLE WAS JAMMED AT IDLE. FOUND NR 1 DCV (DIRECTIONAL CONTROL VALVE) STUCKED IN EXTEND POSITION. DCV WAS REPLACED AND THROTTLE WAS SERVICE.SDR 20010112SG056Anti-Ice Valve · intermittentDURING CLIMB, ANTI-ICE VALVE NR 2 ENGINE FAILED TO OPEN. DURING TAXI IN, VALVE OPENED. REPLACED ANTI-ICE VALVE AND HIGH PRESSURE SWITCH, SYSTEM OPERATIONAL CHECK GOOD. (M)SDR 20010112SG039Eec · malfunctionedDURING TAKEOFF, NR 1 ENGINE WOULD NOT MAKE TAKEOFF POWER, ABORTED TAKEOFF AT 122 KTS. AIRCRAFT RETURNED TO GATE. ENGINE POWER ASSURANCE RUN ACCOMPLISHED (TEST 13) PLACED LEFT EEC ON MEL. ENGINE RUN CHECKS WITHIN LIMITS. UPON RETURN TO MAINTENANCE BASE, EECSDR 20010112SG002Oven · dirtySHORTLY AFTER TAKEOFF, SMOKE AND FIRE WAS REPORTED IN AFT GALLEY NR 2 OVEN. HAND FIRE EXTINGUISHER WAS DISCHARGED INTO OVEN. AIRCRAFT RETURNED TO DEPARTURE STATION AND MADE AN UNEVENTFUL LANDING. INVESTIGATION REVEALED THAT FOOD HAD SPILLED OUT OF TRAYS ON SDR 20001215AP001O-Ring · damagedON CLIMB, CREW NOTIFIED OF FUEL COMING FROM TOP OF RT WING. AN UNEVENTFUL UNSCHEDULED LANDING ACCOMPLISHED INVESTIGATION REVEALED O-RING BETWEEN STRUCTURE AND FUEL CAP ADAPTER WAS EXTRUDED. REMOVED ADAPTER AND REPLACED O-RING. (M)SDR CA000808015Engine · smoke(CAN) 1. DURING TAKEOFF AT 70 KTS, SMOKE OBSERVED IN COCKPIT AND AT 4L POSITION. TAKEOFF ABORTED. NR ENGINE (LT) REPLACED AS PER M.M. 71-00-02. IDLE & TAKEOFF RUNS C/O AS PER M.M. 71-00-00/501, EBGUBE CGECJED SERVICEABLE.3. DMI 18463, L/H ENGINE OIL FILTER EISDR CA000808018Wheel · failed(CAN) DURING TAXI, IT WAS OBSERVED THAT NR 8 MAIN WHEEL ASSEMBLY WAS BLOWN. NR 8 MAIN WHEEL ASSEMBLY REPLACED IAW MM 32-46-01. NO PROBLEM DURING SUBSEQUENT FLIGHTS.SDR CA000808016Pump · failed(CAN) DURING DESCENT EICAS MESSAGES INDICATED LT HYDRAULIC QUANTITY, THEN LT HYDRAULIC EDP AND THEN LT HYDRAULIC OVERHEATED PUMP WAS TURNED OFF. EDP CHANGED I.A.W. M.M. 29-11-05. LEFT OIL FILTER EICAS MESSAGE OBSERVED. DMI 18663 RAISED I.A.W. M.E.L. 79-35-2.AISDR CA000714013Retainer · corroded(CAN) DURING SLIDE/RAFT REPLACEMENT, THE GIRT BAR RETAINER PLATE FOUND SPLIT IN HALF DUE TO EXCESSIVE CORROSION. PLATE REPLACED AND FLEET CAMPAIGN WILL BE DONE TO VERIFIED THE CONDITION OF THE PLATE AS PER SPECIAL INSPECTION 3-25-30 REV-0.SDR CA000621030Bolt · sheared(CAN) WHILE MECHANIC WAS CARRYING OUT HIS INSPECTION HE OBSERVED THAT NR 7 MAIN WHEEL ASSEMBLY TIE BOLTS WERE SHEARED OFF (X3). MAIN WHEEL ASSEMBLY WAS REMOVED & SERVICEABLE ASSEMBLY WAS INSTALLEDI.A.W. M.M. 32-45-01. NO FUTHER PROBLEMS ON SUBSEQUENT FLIGHTS.SDR CA000614054Tube · worn(CAN) P1 AIR TUBE SECTION BETWEEN P1 PROBE AND NOSE COWL AFT BULKHEAD FOUND SHAFT IN EXCESS OF 50 PERCENT OF TUBE WALL UNDER ATTACH CLAMP. DEFECT FOUND DURING C CHECK BY ICELAND AIR INSPECTOR.SDR CA000315006Packing · deteriorated(CAN) DURING CLIMB LT ENG HYD QTY DECREASED BY 20 PERCENT, CREW TURNED OFF LT HYD SYS HYD PUMP AND LANDED STFELY. REPLACED PACKING AND TEST SERV. DURING DEICING NR 1 HYD PUMP FAILED. REPLACED, PLUS CASE AND RETURN FILTERS REPLACED.SDR N8TA00011001Control Panel · shortedDURING CLIMB, CREW NOTICED SMOKE SMELL IN FLIGHT DECK. AIRCRAFT RETURNED TO STATION, NORMAL LANDING ACCOMPLISHED. INVESTIGATION REVEALED SHORTED ATC TRANSPONDER CONTROL PANEL. REMOVED PANEL, SECURED HARNESS AND RETURNED AIRCRAFT TO MAINTENANCE BASE. (M)SDR N8TA00010001Heater · malfunctionedBURNING ELECTRICAL SMELL OBSERVED, TURNED OFF FLOOR AND SHOULDER HEATERS SMELL WENT AWAY. PLACED ON MEL 21-45-1-1. (M)SDR CA000203019Duct · cracked(CAN) A CRACKED APU SUPPLY DUCT IN THE AFT CARGO NEAR THE TWO FIRE EXTINGUISHERS BOTTLES CAUSED THE PRESSURE TO BUILD UP TOO HIGH RUPTURING THE SAFETY RELIEF ALLOWING THE BOTTLED TO DISCHARGE. SUPPLY DUCT AND BOTTLES REPLACED.SDR CA991231054Pump · failed(CAN) PRECAUTIONARY REPLACEMENT MEASURE TAKEN OF HP FUEL PUMP AS PER MMSDR CA991103097Bolt · broken(CAN) DURING INSP FOUND MW WITH WITH PORTION OF LUG BOLT MISSING. BOLTS REPLACED .SDR CA990818011Harness · chafed(CAN) DURING TAXI BY MAINTENANCE TO POSITION THE AIRCRAFT ON GATE, THE POSITION SENSOR ELECTRONIC UNIT STARTED TO SMOKE. AT L1 DOOR AFTER LAVATORY, FOUND A TWELVE WIRE BUNDLE SEVERELY CHAFED BY THE LAVATORY DUMP CABLE WHICH RESULTED IN AN ELECTRICAL SHORT BETSDR CA990219029O-Ring · damaged(CAN) PILOT NOTICED DISCREPANCY OF 800 KG BETWEEN CALCULATED AND TOTALIZER FUEL, ABOUT 30 SECONDS LATER GOT FUEL CONFIGURATION ECIAS MESSAGE. PRECAUTIONARY ENGINE SHUTDOWN AND AIRCRAFT RETURNED TO POINT OF DEPARTURE. POST- FLIGHT INSPECTION FOUND FUEL LEAK BSDR CA990219027Pump · failed(CAN) ON TAKEOFF ROLL, ENGINE OIL PRESSURE LIGHT AND ECAIS OIL PRESSURE LIGHT CAME ON. TAKEOFF WAS ABORTED. INVESTIGATION FOUND OIL PUMP SCAVENGE PUMP DRIVE SHAFT SLIPPED OUT OF THE SPLINES DUE TO IMPROPER INSTALLATION. SERVICEABLE PUMP AND DRIVE SHAFT INSTSDR CA990119027Valve · failed(CAN) DURING CRUISE AT FL 350 FEET, THE CABIN ALTITUDE STARTED TO FLUCTUATE 1,000 FEET PER MINUTE. CHANGED THE SELECTOR TO AUTO NR 1, NO CHANGE. DURING DESCENT FROM 350 FEET, THE CABIN RATE STAYED 1,500 FEET PER MIN CLIMB. MANUAL CONTROL NON-EFFECTIVE. OXYSDR CA990311077Flex Hose · ruptured(CAN) EICAS MESSAGE LEFT HYDRAULIC QUANTITY WENT DOWN TO ZERO. LEFT ELECTRIC AND EDP SHUT DOWN. FOUND RIGHT GEAR TRUCK POSITIONER HYDRAULIC FLEX HOSE RUPTURED. REPLACED.SDR CA981125088Bearing · seized(CAN) UNABLE TO STOW RIGHT THRUST REVERSER AFTER LANDING. THRUST REVERSER DIRECTIONAL CONTROL ROD END BEARINGS SEIZED, REPLACED.SDR CA980916063Bolt · sheared(CAN) BOLT MISSING FROM NR 5 WHEEL ASSY. BOLT SHEARED AT THREADED PORTION. REST OF BOLT IN WHEEL. WHEEL REPLACED.SDR CA980916066Line · broken(CAN) AT FL 350, THE FLIGHT CREW HAD INDICATION OF SMOKE IN THE FLIGHT DECK. NO SMOKE WAS REPORTED IN THE CABIN AND ALL ENGINE PARAMETERS WERE NORMAL. THE FLIGHT WAS DIVERTED. AT 10,000 FEET, THE NR 1 ENGINE OIL QUANTITY WAS READING 8, OIL TEMPERATURE 135, SDR CA980331019Transmitter · cracked(CAN) AFTER TAKEOFF HAD TO RETURN DUE TO LEADING EDGE SLAT LOCKED BETWEEN UP AND NR 1 POSITION. LANDED OVERWEIGHT. OVERWEIGHT LANDING CHECK CARRIED OUT OK AND SLAT PDU POSITION REPLACED.SDR 98ZZZX1048Vanes · damagedFLT CZ23556 - DURING APPROACH SHENZHENG AT 600M, RT ENGINE MADE SLIGHT SURGING SOUND AND LATER, ELECTRICAL POWER TRANSFERRED. A LOT OF EICAS MESSAGES APPEARED. RT ENGINE UNCOMMANDED SHUT DOWN, ACFT SAFELY LANDED. CHECKED BVCU AND FOUND '04' CODE, TPU HAD '4SDR CA960620021Duct Assembly · seal damage(CAN) SIGN OF OVERHEAT DETECTED AT ENGINE OUTBOARD 'C' DUCT ACCESS PANEL, TOP. AIR OFF TAKE DUCT ASSEMBLY FROM HP6 STAGE WAS LEAKING HOT AIR. DUCT REMOVED AND DETERIORATED EXPANSION JOINT SEAL WAS FOUND. OTHER SIGNS OF OVERHEAT DETECTED, THRUST REVERSER HYDRAUSDR CA960614008Cable · broken(CAN) AIRCRAFT HAD TO REJECT TAKEOFF DUE TO ENGINE NOT REACHING TO POWER BECAUSED OF THROTTLE JAM. THRUST REVERSER CABLE BROKEN RESULTING A FEEDBACK CABLE CAM IN UNLOCK POSITION. CAM REPOSITIONED AND THRUST REVERSER DEACTIVATED AS PER MM AND RELEASED AS PER MESDR CA960227021Tail Section · damaged(CAN)TAIL SECTION STRUCK RUNWAY DUE TO OVER ROTATION ON LANDING. REPAIRED IN ACCORDANCE WITH SRM.SDR CA960129021Switch · failed(CAN)DURING TAKEOFF ROLL THE LEADING EDGE SLAT ASYMMETRY MESSAGE OCCURRS AND THE AIRCRAFT ABORTED THE TAKEOFF. AFTER VERIFICATION THE FLAP SLAT ELECTRONIC UNIT WAS REPLACED. SAME MESSAGE OCCURRED ON NEXT F LIGHT. L/H FLAP LOSS SWITCH REPLACED.SDR 95ZZZX5520Rotary Actuator · defectiveWHEN OPERATED DURING FLIGHT 3555, 'LE SLAT DISAGREE' MESSAGE DISPLAYED. THE LE SLAT COULD NOT BE EXTENDED. FOUND THE ROTARY ACTUATOR AT THE RT WING TIP HAD DEFECT. AS MAINTENANCE HAD NO REPAIR PARTS, THE FLIGHT WAS CANCELLED. OPERATOR SENT MAINTENANCE PEOPSDR 95ZZZX2247Fseu · malfunctionFLT 3158 - THE FLAP FAILED TO EXTEND WHILE APPROACHING. EXTENDED THE FLAP BY STANDBY MODE. ON THE GROUND, EXTENDED AND RETRACTED THE FLAP BY NORMAL MODE AND OKAY, BUT 'ELEVATOR DISAGREE' MESSAGE APPEARED. THE FLIGHT WAS DELAYED. CHECK FOUND FSEU SHOWED NO SDR 95ZZZX2244Pcu · leaksFLT 3554 - THE LEFT SYSTEM LEAKED HYDRAULIC TO 0.3 WHILE APPROACHING. CHECK FOUND LEFT PCU FOR ELEVATOR HAD SERIOUS LEAKAGE. REPLACED PCU. OKAY.SDR 95ZZZX2246Pump · failedFLT 3551 - DURING TRANSIT, THE HYDRAULIC PUMP FOR LT ENGINE LEAKED. CANCELLED THE FLIGHT. SENT MAINTENANCE TO REMOVE FAULT. REPLACED THE DRIVING HYDRAULIC PUMP FOR LT ENGINE. THE REPLACED HYDRAULIC PUMP WAS SENT TO MANUFACTURER FOR REPAIR.SDR 95ZZZX2245Hydraculic Line · failedFLT 3551. 'L HYD QTY' MESSAGE DISPLAYED AFTER TAKEOFF. THE LEFT HYDRAULIC QUANTITY DECREASED RAPIDLY. INTERRUPTED THE FLIGHT AND EXTENDED LANDING GEAR WITH STANDBY SYSTEM. TOWED TO PARKING APRON AFTER LANDING. CHECK FOUND THE HYDRAULIC DUCT FOR LT LANDING
Back to Boeing 757-236