Boeing 757-28A
Service difficulty reports · 2,000
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 = '75728A' 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 = '75728A' 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 2002F00940Sensor · malfunctionedFLIGHT NUMBER 208. REJECTED TAKEOFF APPROX 100 KTS DUE TO EICAS MESSAGE EQUIPMENT OVHT ILLUMINATED. AFTER SELECTING ALT EQUIP COOLING, OVHT LIGHT EXTINGUISHED BRIEFLY, THEN REILLUMINATED. RETURNED TO GATE TO INVESTIGATE OVHT. MAINTENANCE REMOVED AIR FILTER ANDSDR 2002F00941Duct · leakingFLIGHT NUMBER 504. EICAS STATUS MESSAGE R STRUT OH DET 1 DISPLAYED DURING TAXI. MAINTENANCE REMOVED AND REPLACED ENGINE SUPPLY DUCT INACCORDANCE WITH M.M. 36-11-01. RAN ENGINE AND PERFORMED HIGH POWER TEST AND LEAK CHECK. AIRCRAFT RETURNED TO SERIVE.SDR 02092301Engine · vibratesAt FL 370, Rt. Eng. indicated 2.6-2.7 vib., aircraft returned to LAS. Further inspection revealed no defects as per RB211 M/M 72-31-13. (A tap test, blade lube, and power run were performed as per the noted M/M ref. Ops check good as per M/M Ref. noted. No oSDR 2002F00906B-Nut · loose(ORIG-CLOSED) FLIGHT NUMBER 205. DURING CRUISE EICAS MSG RT ENG OVHT DISPLAYED. EXTINGUISHED AFTER THRUST REDUCTION. MAINTENANCE TROUBLESHOT PER FIM 26-12-00 FOUND LOOSE B-NUT LINE ON PRSOV LINE. TIGHTENED LINE & TEST NR 4 COMPLIED WITH. SYSTEM CHECKED OK.SDR 02091101Pin · brokenCABIN EMERGENCY EGRESS LIGHTS INOP AT ROWS 22 AND 23. TROUBLESHOOTING REVEALED A BROKEN PIN IN THE FLOOR TRACK CONNECTOR. PIN WAS REPLACED, OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR SERVICE.SDR 02081301Switch · failedIN FLIGHT: RIGHT ENGINE SPOOLED BACK OVER A PERIOD OF ABOUT 5 MINUTES. ABOUT 3 INCH SPLIT IN THRUST LEVERS TO SYNC N1'S. ADVISED BY MAINTENANCE CONTROL TO SWITCH OFF ELC ON NR 2 ENGINE. APPEARED TO RETURN TO NORMAL. PRECAUTIONARY LANDING MADE. TROUBLESHOOSDR 02081202Clamp · looseClimbing through FL19.0, Left Engine Overheat Message; Reduced Thrust light out. Troubleshoot per F.I.M. 26-11-00, found loose clamp on PRSOV, secured per M/M 20-11-00, All Operations checked per F.I.M. 26-11-00SDR 02080601Control Unit · inoperativeAT 16000 FEET, COMPRESSOR STALL; AT 14000 FEET, 3 BANGS, AT 10000 FEET, NO BANGS, AT 7000 FEET, NO RESPONSE IN RT ENGINE UPON POWER UP, AT 7000 FEET, OIL PRESSURE LOSS INDICATED (2PSI) AT 7000 FEET, LOSS RT. ENG. IDG, SHUTDOWN RT ENGINE. AIRCRAFT CONTINUED DSDR 2002F00777Engine · surgesDURING THROTTLE MOVEMENT ENGINE PARAMETERS SURGED WITH EEC ENGAGED. WITH EEC NOT ENGAGED, ENGINE STILL SURGED, BUT NOT AS MUCH. ENGINE FLUCTUATED WITH EEC ON OR OFF. PERFORMED TEST 13 TAKEOFF POWER, ALL PARAMETERS ON BOTH ENGINES ARE NORMAL WITHIN LIMITS IAWSDR 2002F00881Eec · faultyFLIGHT NUMBER 218, LEFT EPR GAUGE WOULD NOT GO TO COMMANDED EPR DURING DESCENT/CRUISE. MAINTENANCE REMOVED AND REPLACED LEFT EEC PER M/M 73-21-07, OK FOR SERVICE.SDR 02062001Wire · brokensix emergency lights on floor between rows 5 and 6 INOP. Found and repaired broken wire as per WDM 33-51-21, ops ok.SDR 02052001Door · out of adjustON TAXI-OUT, FLIGHT ATTENDANT EMERGENCY OXYGEN MASKS DEPLOYED WITHOUT COMMAND. OXYGEN GENERATOR(S) WAS/WERE NOT ACTIVATED. INSPECTION REVEALED OXYGEN MASK DOOR SPRING WEAK. OXYGEN MASKS WERE REPACKED AS PER M/M 35-21-01. DOOR WAS TEMPORARILY SECURED WITH TSDR 02051302Lamp · burned outAft Red Emergency light, for seat 8ABC INOP. Re-lamped light at 8ABC per M/M 33-13-00; Ops Check Good.SDR 02051301Smoke DetectorAt FL350, Aft Cargo Fire Light illuminated, first fire extinguisher discharged, light extinguished, on approach second fire extinguisher was discharged. Investigation revealed No sign of Heat or Fire; Light bulbs in smoke detectors burnt out. re-lamped smoke dSDR 02051001Radar · failedRADAR FAILED DURING CLIMB. MSG RT AND WINDSHEAR SYS, ALSO STATUS MSG WXR SYS CYCLED C/B'S, UNABLE TO RESET. AIRCRAFT RETURNED TO BASE, AN UNEVENTFUL LANDING WAS ACCOMPLISHED.SDR 2002F00467Warning System · false activationFLIGHT NUMBER 669, DURING CRUISE RIGHT ENGINE OVERHEAT EICAS MESSAGE AND LIGHT/AURAL WARNING AT FL 370. FLIGHT CREW PERFORMED CHECKLIST, SHUT OFF BLEED VALVE AND BROUGHT POWER TO IDLE THRUST. LIGHT AND EICAS MESSAGE WENT AWAY 30 SECONDS LATER. MAINTENANCE RSDR ANCF200200008Window · crackedDURING CLIMB AFTER 15000 FT, A LOUD BANG WAS HEARED IN THE COCKPIT THE BANG WAS PRODUCED BECAUSE THE WINDOW CRACKED IN THE UPPER AND LOWER RIGHT HAND CORNER. WAS ACCOMPLISHED INSPECTION CHECK IAW AMM 56-11-00 PAGE 607 AND NO FOUND CRACK, WAS FOUND DELAMINSDR CA020222001Access Panel · missing(CAN) WHEN AIRCRAFT LANDED CREW SELECTED REVERSERS, THE NR 2 ENGINE, RT THRUST REVERSER WOULD NOT STOW. DURING THE WALK AROUND, THE CREW FOUND THE NR 2 ENGINE THRUST REVERSER DUCT ACCESS PANEL (P/N LJ76673) RIPPED OFF AND DAMAGE TO THE THE RT TRANSLATING SDR CA020221009Clamp · loose(CAN) WHEN REACHING FL330 , THE CABIN ALTITUDE LIGHT CAME NI AND THE RT PACK INOP LIGHT CAME N. WE STARTED DESCENT, THE CABIN STABILIZED AT FL 250. THE RT PACK WAS RESETTED AND FOUND OK. THE CREW STAYED AT THAT LEVEL FOR THE REMAINDER OF THE FLIGHT . MAINTENASDR CA011211007Fitting · cracked(CAN) ELBOW HYDRAULIC FITTING CRACKED AT OUTLET PORT OF LT ELECTRICAL HYDRAULIC PUMP.SDR CA011211022Rod · broken(CAN) AIRCRAFT ARRIVED WITH NR 1 BRAKE TORQUE ROD ASSEMBLY BROKEN IN HALF AND HYDRAULIC LINE TO BRAKE WAS BROKEN.SDR NOCA0501Fire · detectedAIRCRAFT EXPERIENCED NORMAL LANDING AT MIA. WHILE A/C WAS TAXIING TO GATE RAMP AGENT REPORTED SEEING A BRAKE FIRE ON THE RIGHT SIDE. THE FIRE WAS IMMEDIATELY EXTINGUISHED. THE CREW WAS ADVISED AND REPORTED THE HIGHEST TEMPERATURE RECORDED WAS 3 ON BRAKE NR SDR ANCF200100015Transmitter · failedLT ENGINE PARAMETERS FLUCTUATED AT TAKEOFF AND CLIMB. CREW DECIDED TO RETURN TO EDR. THE EPR TRANSMITTER LT ENGINE WAS REPLACED IAW AMM 77-11-00, REPLACED LT ENGINE IAW EWO 75-72-43-77 TEST SATISFACTORY IAW AMM 71-00-00 PAGE 404.SDR 2001F00432Engine · vibrationA/C AT FL330 EXPERIENCED RIGHT ENGINE VIBRATION. THROTTLE RETARDED AND VIBRATION REMAINED 1.2 AND 3.1 AT EPR 1.71. CREW REPORTED LEFT ENGINE VIBRATION DURING DESCENT. A/C REQUESTED DIVERSION TO ORF. VIBRATION RETURNED TO NORMAL RANGE ON DESCENT AT FLIGHT LSDR CA010704016Shaft · failed(CAN) DURING CRUISE PILOT REPORTED ENGINE OIL PRESSURE DROP AND QTY DROP, VIBS STARTED TO INCREASE AND THE FLIGHT CREW ELECTED TO SHUT DOWN THE ENGINE IN ACCORDANCE WITH QRH PROCEDURES. AIRCRAFT DIVERTED AND RETURNED TO GANDER. MAINTENANCE INSPECTED THE LP COUSDR CA010704023Spring · broken(CAN) RUDDER PEDAL HAS A LACK OF NORMAL RESISTANCE WHEN DISPLACED. INSPECTION FOUND THAT ONE OF THE FEED BACK SPRINGS WAS BROKEN, SPRING WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR ANCF200100011Harness · chafedLEFT ENGINE FIRE WARNING WITH EICAS MESSAGE “LT ENGINE FIRE”, FIRE INDICATION STOPPED WHEN FIRE SWITCH PULLED. CORRECTIVE ACTION:THE FIRE DETECTOR HARNESS WERE CHECKED AND FOUND CHAFING, IT WAS ISOLATED, THE TURBINE OVERHEAT SWITCH S10140 WAS FOUND GROUNDED ASDR CA010531009Shaft · sheared(CAN) DURING CRUISE FLIGHT CREW REPORTED R/H ENGINE HYDRAULIC PRESSURE LOW LIGHT CAME ON WITH ECIAS MESSAGE "R/H ENG EDP". AIRCRAFT DIVERTED AND LANDED. R/H EDP FOUND SHAFT SHEARED, PUMP REPLACED, FILTERS REPLACED AND SYSTEM FLUSHED AS PER AMM 29-11-00 AND 29-SDR 20010316SG003Warning System · activatedUPON CLIMBING THROUGH 9,000 FEET, LOWER EICAS MESSAGE, FLT DATA ACC ILLUMINATED. AIRCRAFT ACCOMPLISHED UNSCHEDULED LANDING AT ORGINATION STATION. REASON FOR RETURN IS THAT JUST PRIOR TO DEPARTURE THE CVR HAD BEEN PLACED ON MEL STATUS. ACCOMPLISHED TEST PROCSDR 20010207SG001Gcu · malfunctionedDURING CRUISE, EICAS MESSAGE ''LT GEN OFF'' DISPLAYED AND ''GEN OFF'' LIGHT ILLUMINATED. GENERATOR RESET, NO HELP. EICAS MESSAGE ''L AC BUT OFF'' REMAINED DISPLAYED. CREW SMELLED BURN ODOR IN THE FLT COMPT, NO SMOKE. UNSCHEDULED LANDING PERFORMED WITHOUT FSDR ANCF200100001Blade · failedDURING T/O IN MIA, AFTER LIFTOFF SOME BIRDS WERE INGESTED BY RIGHT ENGINE, ENGINE FAILED. AIRCRAFT RETURNED TO MIA WITHOUT FURTHER PROBLEM.CORRECTIVE ACTIONACCOMPLISHED AS PER EWO 75-72-4226PERFORMED FIM PROCEDURE AFTER BIRD STRIKE IAW FIM 71-00-00, THEN PERFOSDR ANCF200000004Control Panel · smokeDURING CRUISE SMOKE WAS PRESENT FROM THE LEFT VOR/DME SELECTOR PANEL, PERFORMED CHECK LIST AND SITUATION WAS CONTROLLED.CORRECTIVE ACTION:WAS UNCLOGGED EQUIPMENT COOLING LINE OF VOR CONTROL PANEL AND REPLACED VOR CONTROL PANEL IAW AMM 34-51-02 PAGE 201SDR 20010207SG020Skin · corrodedNR 2 ENGINE COMMON NOZZLE EXHAUST COLLECTOR LOWER SUPPORT STRUT SKIN CORRODED ON UPPER TRAILING EDGES. REMOVED CORROSION BY BLENDING, TREATED WITH ALODINE AND PRIMED USING BMS 10-11 TYPE 1 PRIMER. (M)SDR CA001212007Structure · missing(CAN) AIRCRAFT IN CLIMB PHASE OF TAKEOFF. CREW REPORTED THAT WHEN THEY MOVED THE FLAP/SLAT HANDLE FROM POSITION 1 TO FULLY RETRACTED THAT A NOISE WAS HEARD. UPON CARRYING OUT A VISUAL INSPECTION, IT WAS OBSERVED THAT A PORTION APPROXIMATELY 800 SQUARE INCHES SDR CA001123009Selector Knob · failed(CAN) THRU 10,000 FEET CABIN ALTITUDE EICAS WARNING. QRH ACTIONED. AIRCRAFT RETURNED TO YYZ WITHOUT INCIDENT. CABIN PRESSURE SELECTOR REPLACED.SDR CA001107005Tube · worn(CAN) DURING C-CHECK INSPECTION, FOUND CARGO FIRE EXTINGUISHING TUBE RUBBED THROUGH BY CONTACTING APU BLEED AIR DUCT. CAUSE OF PROBLEM IS THE APU DUCT VIBRATION WITH CLOSE TOLERANCE. FIX IS INCORPORATION OF SB 57-26A0040.SDR CA000830016Door Seal · obstructed(CAN) AIRCRAFT RETURNED TO BASE AFTER NOT BEING ABLE TO MAINTAIN CABIN PRESSURIZATION ABOVE 23,000 FEET,. DURING GRD PRESSURIZATION CHECK FOUND HEAVY AIR LEAK FROM L/H PRSOV AND C1 CARGO. C1 CARGO FOUND NET OVER CARGO DOOR SEAL, NET REPOSITIONED. PRSOV LOCKED SDR CA000830017Cable · damaged(CAN) LOG BOOK DEFECT REPORTED BY FLIGHT CREW ON ARRIVAL . NR2 ENGINE THROTTLE BINDING. FOUND THRUST REVERSER FEEDBACK PUSH PULL CABLE DAMAGED CAUSING THE T/R FEEDBACK CAM TO BEND. FORWARD THRUST FEED AND SENSE C/O, NO FAULT FOUND, T/R LOCKED OUT AS PER MEL.SDR CA000802010Coupling · contaminated(CAN) UNABLE TO ACHIEVE TAKEOFF POWER, WITHOUT RETURNING AT THE DATE, CREW DID A SUCCESSFUL POWER RUN AND A/C DEPARTED. SAME THING HAPPENED ON THE NEXT LEG. AFTER INVESTIGATION, MAINTENANCE FOUND COUPLING BETWEEN ENGINE AND FRAME FFG CABLE CONNECTOR CONTAMINATSDR CA000621031Fan Blade · damaged(CAN) NOT AN SDR - DEPARTING FROM YYZ DURING CLIMB AND CRUISE LEFT ENGINE VIBRATION WENT TO 2.4 UNITS. AIRCRAFT DIVERT TO YMX.MAINTENANCE REPLACED ALL THE ANNULUS FILLER AND CLEANED ALL THE BLADE ROOT. VIBRATION SURVEY CARRIED OUT AND VIBRATION WITHIN LIMITS. SDR CA000404027Sensor · failed(CAN) AFTER TAKEOFF NR 3 EMERGENCY DOOR LIGHT ON EICAS. A/C RETURNED TO GATE. DOOR PROPERLY INSTALLED AND PROX SENSORS ADJUSTED. A/C TOOK OFF AND AT 6 PSID SAME MESSAGE ON EICAS A/C RETURNED TO BLOCKS. FOUND WIRE SPLICES ON SENSOR WIRES FULL OF WATER DUE CONDESDR N8TA00012701Bleed Valve · inoperativeDURING TAKEOFF (80 KNOTS), LEFT PAC ICAS MESSAGE CAME ON FOLLOWED BY LT ENGINE BLEED MESSAGE. TAKEOFF ABORTED. CHANGED PSROV. OPS CHECKED NORMAL. (X)SDR N8TA00010701Handle · corrodedR4 DOOR EXTERIOR HANDLE PAN ASSY DEEPLY GOUGED AND HOLE NEAR HANDLE. CORROSION FOUND BETWEEN INNER AND OUTER SHAFTS. (M)SDR CA991210025Line · loose(CAN) DURING CRUISE LH HYD QTY DECREASED TO ZERO QTY PRESSURE LIGHT ON AND SYS DEACTIVATED. FOUND PRESSURE LINE JUST BEFORE FILTER MODULE AND BRACKET BROKEN. LINE TIGHTENED. PUMP SEIZED AND REPLACED. UNDER INVESTIGATION. PMUP WENT DRY AND THEN FAILED, UNIT FROSDR NOCA1199Lamp · inoperativeDURING INSPECTION, EMERGENCY EXTERIOR LIGHTS AT 4L AND 4R INOPERATIVE. RELAMPED 4L AND 4R EMERGENCY EXTERIOR LIGHTS. OPS CHECK NORMAL. (M)SDR NOCA1099Flashlight · inoperativeDURING INSPECTION, EMERGENCY FLASHLIGHT AT R4 DOOR FLIGHT ATTENDANT JUMP SEAT FOUND INOPERATIVE. FLASHLIGHT AT R4 DOOR REPLACED, OPS CHECK OK. (M)SDR CA991116013Flow Valve · failed(CAN) AIRCRAFT RETURNED DUE UNABLE TO PRESSURIZE. AFT CABIN DOOR SEAL FOUND ADRIFT. LEFT PACK UNDER MEL UNABLE TO PRESSURZIZE. REPLACED RIGHT PACK FLOW CONTROL VALVE.SDR NOCA0999Bulb · failedDURING INSPECTION, FOUND E-PATH FLOOR LIGHT AT SEAT 12 ABC INOP. RELAMPED E-PATH LIGHT AT SEAT 12 ABC. OPS CHECK NORMAL. (M)SDR CA990916003Coupling · broken(CAN) DURING FLIGHT, CREW OBSERVED RT HYDRAULIC LOW PRESSURE AND QUANTITY LOW. AIRCRAFT LANDED. HIGH PRESSURE QUICK DISCONNECT ON NR 2 ENGINE BROKEN IN TWO PIECES. FITTING REPLACED.SDR CA990707069Lens · broken(CAN) ON APPROACH WHEN GEAR LOWERED, NO GREEN LIGHT FOR THE LT MLG, ALT GEAR LOWERING CARRIED OUT AND AC LANDED OK. LT GREEN LENS ASSY BROKEN. REPLACED.
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