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 02090301Slat · delaminatedskin delamination and honeycomb missing trailing edge of slat inboard right wing. An uneventful landing was accomplished. Further investigation revealed delamination of fixed leading edge wing panel (aft of #6 leading edge slat) approx. 10'X24", and hole in upSDR 02082901Pump · failedCrew called with Left Engine Driven Hyd. pump overheat and later with Left Hyd. Qty. loss. Aircraft returned to LAS, an uneventful landing was accomplished. Further investigation revealed that the #1 Engine E.D.P. had suffered mechanical failure, causing loss SDR 02081203Lanyard · displacedLeft Entry Door light came on in flight. Visual inspection showed door not fully closed. Interior handle would pop out of closed detent repeatedly.Found L2 Door Slide Girt/Girt Bar assy. unsecured, reinstalled Girt/Girtbar Assy per M/M 25-66-01. L2 Door ops chSDR 02081204PushrodLeft Center Door EICAS Message/Light appeared in flight. Handle popped up, out of locked position.Adjusted cocking pushrod in accordance with M/M 52-11-00 and 52-11-13. Handle torque test as per M/M 52-11-00 was good.SDR CA020816004Bearing · seized(CAN) CREW REPORTING RUDDER PEDAL HARD TO MOVE ON GROUND. AFTER INVESTIGATION, MAINT FOUND A ROLLER BEARING SEIZED IN THE CAM ROLLER ARM ASSY. OF THE RUDDER FEEL CENTERING MECHANISM MAINTENANCE REPLACED THE ROLLER AND TESTED THE RUDDER PEDAL FORCES IAW AMM 2SDR 02080101Lamp · burned outEmergency Escape Path Lighting INOP at multiple rows. Upon further investigation, lamps found to be burned out. Relamped and Operationally checked, as per M/M 33-51-10; Ops ck good. Aircraft returned to service.SDR 02070901Control Unit · malfunctionedAFTER DISCONNECT, BEGAN TO TAXI, HEARD MUFFLED POPPING NOISE. LEFT ENGINE QUIT. RETURNED TO GATE. BVCU BITE FAILED, BVCU REMOVED AND REPLACED. FUNCTIONAL CHECK GOOD AS PER M/M. AIRCRAFT RETURNED TO SERVICE.SDR 02051701Transmitter · fluctuatesRight Engine fuel flow fluctuation on climbout. An uneventful flight occured. Upon return to LAS, removed and replaced fuel flow transmitter. Ops check good as per M/M 73-31-01SDR 02050301Light · inoperativeEMERGENCY LIGHT FOR SEAT 22 A/B/C INOP. REMOVED AND REPLACED E-PATH LIGHT AT 22 A/B/C AS PER M/M 33-51-11; OPS CHECK GOOD.SDR 02042401BulbEmergency Light out, at row 24. Re-lamped as per M/M 33-51-11; Operational Check good.SDR 02040701Wire · shortedEmergency Interior light at seat 5D INOP. T/S identified wire shorted to ground. Repaired short, replaced fuse, ops check good as per m/m 33-51-11SDR 02032901Fuse · blownCabin Emergency Lights row 7abc to 15abc INOP. Replaced battery pack fuse on L-2 door I.A.W. MM33-51-00, Ops. Check goodSDR CA020328009Tie Bolt · sheared(CAN) DURING A "RAMP 1 CHECK" ONE TIE BOLT WAS FOUND BROKEN ON NR 6 MAIN WHEEL ASSY. MAINTENANCE REPLACED THE MAIN WHEEL ASSY.I.A.W. MM 33-45-01.SDR 02021501Warning System · activatedUPON FLAP RETRACTION LEADING EDGE LIGHT AND SLAT DISAGREE MESSAGE ILLUMINATE. LIGHT REMAINED ON DURING ACCOMPLISHMENT OF ABNORMAL CHECK LIST. TROUBLESHOOTING SYSTEM.SDR 02021101Warning System · activatedUPON FLAP RETRACTION LEADING EDGE LIGHT AND SLAT DISAGREE MESSAGE ILLUMINATE. LIGHT REMAINED ON DURING ACCOMPLISHMENT OF ABNORMAL CHECK LIST. TROUBLESHOOTING SYSTEM.SDR 2002F00240Pump · failedDURING CRUISE, LT ENGINE HYD OVERHEAT EICAS MESSAGE CAME ON FOLLOWED BY LT HYD SYSTEM AND LOSS OF LT HYDRAULIC SYSTEM PRESSURE. INVESTIGATION REVEALED LEFT ENGINE DRIVEN PUMP (EPD) FAILED. REPLACED PUMP. CASE DRAIN AND PRESSURE FILTERS FOR BOTH EDP AND ACMPSDR 2002F00242Floor Support · corrodedFOUND CORROSION ON FLOOR SUPPORT BS 1675, RBL 56, WL 208. CLEANED UP CORROSION, FOUND TO BE BEYOND ACCEPTABLE LIMITS PER SRM 53-00-01. REMOVED AND REPLACED SUPPORT. (M)SDR 02022501Floor Support · corrodedDURING C-CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BS 1675, RBL 56, WL 208. CORROSION CLEANED UP, DETERMINED TO BEYOND ACCEPTABLE LIMITS. REPLACED FLOOR SUPPORT.SDR CA020201016Clamp · loose(CAN) DURING DEFECT INVESTIGATION, FOUND ON NR 1 ENGINE IN THE STRUT AREA, JUST BELOW THE REVERSE FLOW CHECK CONTROLLER, A CLAMP WITH BURNED RUBBER ON IT. PROCEEDED WITH AN AIR LEAK INVESTIGATION AND FOUND A LEAKING CLAMP. THE CLAMP WAS REPLACED.SDR ANCF200200002Switch · malfunctionedDURING TAKE OFF LEFT ENGINE N3 WENT TO OVER SPEED AND SHOWED DIFFERENCE BETWEEN ENGINE PARAMETERS, LH ENGINE HIGHER THAN THE RT, THE ENGINE DIDN’T SHUT DOWN, THE CREW PROCEEDED TO RETURN TO EDR. CORRECTIVE ACTION: PERFORMED BITE TO BVCU, FOUND ALTITUDE SWITSDR 2002F00233Spring · failedLE SLAT DISAGREE EICAS MESSAGE BETWEEN FLAPS 1 AND 0 ON RETRACTION. AIRCRAFT RETURNED TO DEPARTURE STATION. SLATS FOUND TO BE BINDING, LUBED AND OPERATIONAL CHECK PER AMM. ON NEXT DEPARTURE DISCREPANCY REPEATED. AIRCRAFT RETURNED TO DEPARTURE STATION. FURSDR 2002F00070Floorbeam · corrodedDURING C-CHECK, FLOORBEAM UPPER CHORD FOUND CORRODED, BS 324, RBL 58, WL 208. REPAIRED UPPER CHORD PER SRM. (M)SDR 2002F00069Skin · chafedRIGHT OUTBOARD MAIN FLAP, OUTBOARD END, LEADING EDGE 3 INCHES FROM END CHAFFED. DRESSED OUT AND INSTALLED REPAIR PER SRM. REINSPECTED USING HFEC EVERY C-CHECK. (M)SDR 2002F00068Skin · chafedLEFT FORWARD OUTBOARD FLAP, OUTBOARD END, LEADING EDGE CHAFED. DRESSED OUT AND INSTALLED REPAIR EPR SRM. REINSPECTION USING HFEC EVERY C-CHECK. (M)SDR 2002F00067Skin · chafedRIGHT OUTBOARD MAIN FLAP, INBOARD END, LEADING EDGE GOUGE 24 INCHES LONG. DRESSED OUT AND INSTALLED REPAIR PER SRM. REINSPECTION USING HFEC EVERY C-CHECK. (M)SDR 2002F00066Skin · chafedRIGHT OUTBOARD MAIN FLAP, OUTBOARD END, LEADING EDGE 56 INCHES FROM INBOARD END. DRESSED OUT AND INSTALLED REPAIR PER SRM. REINSPECTION USING HFEC EVERY C-CHECK. (M)SDR 2002F00061Floor Support · corrodedDURING C-CHECK, L1 DOOR THRESHOLD FLOOR SUPPORT WAS FOUND CORRODED. REPLACED SUPPORT PER SRM. (M)SDR 2002F00017Battery Pack · dischargedR2 EMERGENCY LIGHT ABOVE DOOR AND AISLE AND OUTSIDE DOOR FAILED TEST. REMOVED AND REPLACED BATTERY PACK ABOVE R2 DOOR. OPERATIONAL CHECK GOOD. (M)SDR 2002F00065Angle · corrodedDURING COMPLIANCE WITH CPCP TASK CORROSION FOUND ON KEEL BEAM LOWER L ANGLE BRACKETS AT BS 1139, LBL 4 TO RBL 4, WL 143. MANUFACTURED AND REPLACED L ANGLE PER SRM. (M)SDR 2001F00754Control Head · malfunctionedSMOKE FROM AROUND NR 2 TRANSPONDER CONTROL HEAD. REMOVED AND REPLACED NR 2 TRANSPONDER CONTROL HEAD, SYSTEM OPS CHECK GOOD. (M)SDR 2001F00645Bolt · out of positionAFTER LANDING, RIGHT THRUST REVERSER WOULD NOT STOW. INVESTIGATION REVEALED THAT THE ROD END BOLT AT THE SLEEVE ATTACH POINT HAD MIGRATED OUT. REPLACED BOLT, THRUST REVERSER OPERATIONAL CHECKED GOOD. (M)SDR ANCF200100020Seal · out of positionDURING TAKEOFF CARGO DOOR LIGHT CAME ON AFT CARGO DOOR NR 2. AIRPLANE DID NOT PRESSURIZE. CREW RETURNED TO CTG. REPOSITIONED SEAL IN AFT CARGO DOOR FRAME IAW AMM 52-71-00. CHECKED ALL AFT DOOR FRAME, FOUND NORMAL.SDR CA011211021Torque Tube · cracked(CAN) DURING INTER 1 CHECK, THE INSPECTION CARRIED OUT ON THE CAPTAIN SEAT REVEALED THAT THE SEAT TORQUE TUBE WHICH HAS THE ELECTRICAL WIRING FOR THE VERTICAL ADJUSTMENT GOING THROUGH ,HAD 4 CRACKS ON THE TUBE.SDR CA011211020Wire Harness · damaged(CAN) 1-) DURING INTER 1 CHECK INSPECTION , THE NR 1 ENGINE EEC PATCH MODULE LOOM INTO CONNECTOR D1380 REVEALED DAMMAGED TO THE WIRING AT CLIPPING POINT CP2281. PROBLEM FOUND WAS CAUSED BY WIRING CHAFFING INTO CLIP CP2281 THAT HAD ITS RUBBER INSULATOR TORNAND SDR CA011211012Wire Harness · damaged(CAN) DURING INSPECTION , FOUND DAMAGE OF THE WIRING HARNESS THAT GOES TO THE P1 PROBE HEATER NOSE COWL INTERFACE CONNECTOR. TYPE OF DAMAGES ON THE TWISTED SHIELDED PAIR WIRES CABLE FOUND OUTER JACKET AND SCREEN DAMAGE BY ABRASION.SDR ANCF200100017Actuator · failedRUDDER RATIO LIGHT ILLUMINATED IN FLIGHT. EICAS MESSAGE RUDDER RATIO DISPLAYED, CREW DECIDED TO RETURN TO EDR. ACCOMPLISHED FIM 27-09-00, WAS REPLACED RUDDER RATIO CHANGER ACTUATOR IAW AMM 27-21-13 PAGE 209, TEST OK IAW AMM 27-21-00 PAGE 501.SDR CA011211023Duct · cracked(CAN) NR 2 ENGINE STARTER DUCT CRACKED JUST BELOW THE UPPER FLANGE.SDR 2001F00449Idg · defectiveON CLIMB-OUT, THE LEFT IDG LIGHT CAME ON. DISCONNECTED IDG AND RETURNED TO STATION. BPCU INTERROGATION INDICATED TRIP DUE TO LOW OIL PRESSURE. IDG REPLACED, OPS CHECK GOOD. (M)SDR CA010808032Door · missing(CAN) AIRCRAFT ARRIVED ON STATION WITH NR 2 ENGINE OIL SERVICING DOOR MISSING. ROLLS ROYCE SERVICE BULLETIN RB 211-71-B592 WAS INCORPORATED ON THE DOOR. A NEW ACCESS DOOR WAS INSTALLED. NEW SPRING CLIP FROM GOODRICH WILL BE INSTALL WHEN MODIFICATION BECOME AVASDR 2001F00166Connector · disconnectedFOUND FLOOR ESCAPE PATH LIGHTING LENS MISSING AT ROW 12 AND AT ROW 25, LIGHT INOPERATIVE. AT ROW 12 REPLACED LENS, P/N 81000-22701. AT ROW 25 RECONNECTED CONNECTOR SYSTEM, OPERATIONAL CHECK GOOD. (M)SDR CA010626008Tube · cracked(CAN) TORQUE TUBE CRACKED WHERE THE CUTOUT HAS BEEN MADE FOR THE WIRING TO GO THROUGHT. THIS IS THE SECOND SEAT WE FIND WITH THE SAME PROBLEM.SDR 2001F00051Battery Pack · dischargedFOUND EMERGENCY LIGHTS AT ROWS 27 AND 29 INOPERATIVE. DURING TROUBLESHOOTING FOUND BATTERY PACK AT DOOR R3 WITH LOW VOLTAGE. REPLACED BATTERY PACKS AT AFT GALLEY RIGHT AND DOOR R3, SYSTEM OPS CHECKED GOOD. (M)SDR N8T2001F00000Fuse · blownEMERGENCY LIGHTS ON SEATS 7 THROUGH 15 INOPERATIVE. REPLACED FUSE IN BATTERY PACK. (M)SDR 20010525SG008Light · inoperativeFOUND EMERGENCY LIGHTS ROW 11 INOPERATIVE. REPLACED LAMPS. (M)SDR CA010626024Duct · leaking(CAN) #1 ENG THRUST REVERSER DEACTIVATED AS PER MEL. INVESTIGATION FOUND THE PYLON MOUNTED FAN THRUSR REVERSER ELECTRICAL HARNESS PN LJ6579 AND LJ 76580 MELTED AND HEAVELY DAMAGED. HOT AIR LEAK FROM HP2 ANDHP7 BLEED AIR DUCT PN 312N5321-7 AND 312N5306-1 ALSO CSDR 20010529SG001Wire · exposedWIRES STICKING OUT FROM UNDER COVER. RESTOWED WIRES AND SECURED COVER. (M)SDR 20010529SG002Light · inoperativeEMERGENCY LIGHTS AT ROW 4 INOPERATIVE. REPLACE LAMPS. (M)SDR PI22001F00000Housing · crackedDURING INSPECTION THE HP OUTLET GUIDE VANE LEADING EDGE VANE FILLET REGION. ACCESS THROUGH HIGH PRESSURE COMPRESSOR STAGE 6 AIR OFFTAKE. A BORESCOPE INSPECTION NOTED ON THE LEFT SIDE 3 CRACKS OVER 5 INCHES. RIGHT SIDE 2 CRACKS ON THE HOUSING MEASURING 7 INSDR 20010425AP008Hose · rupturedLOST LEFT HYDRAULIC SYSTEM IN FLIGHT, RETURNED TO STATION AND MADE AN UNEVENTFUL LANDING. INSPECTION REVEALED BURST HOSE ASSEMBLY IN LEFT MLG WHEEL WELL. REPLACED HOSE, SERVICED SYSTEM AND OPERATIONAL CHECKED GOOD. (M)SDR 02031401Battery Pack · dischargedAFT CABIN SEAT EMERGENCY LIGHTS FROM L3 DOOR INOP. REPLACED BATTERY CHARGER ASSY. OPS CHECK GOOD IAW 33-51-15.
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