Boeing 757-251

Service difficulty reports · 4,707

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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 = '757251'
  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 9511805520Door Warning · malfunctionedDURING TAKEOFF ROLL DTW-MEM, LEFT AFT DOOR WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF WITHOUT INCIDENT. OPERATIONAL CHECK OK, NO TROUBLE FOUND.Aug 2, 1995 · N520US · Boeing 757251 · Door Warning SystemSDR 9511165511Fuel Control · malfunctionedDURING TAKEOFF THE NR 1 ENGINE DID NOT REACH FULL TAKEOFF POWER, THE THROTTLES WERE CLOSED, BUT THE ENGINE DID NOT REDUCE TO IDLE. THE NR 1 ENGINE WAS SHUTDOWN AND THE MESSAGES LT ENG SEC CONT AND LT ENG PRI CONT WERE RECEIVED. THE LEFT FUEL CONTROL UNIT WASJul 21, 1995 · N511US · Boeing 757251 · Fuel Control/Turbine EnginesSDR 9511115502Telephone Box · malfunctionedAT ALTITUDE, THERE WAS A STRONG ELECTRICAL SMOKE SMELL IN THE FIRST CLASS SECTION. THE SMELL WAS ISOLATED TO AN AIRPHONE UNDER-SEAT AUDIO BOX. THE AIRPHONE CIRCUIT BREAKER WAS PULLED AND THE BOX WAS REMOVED AND PLACED IN A PLASTIC BAG IN THE COCKPIT. BOTH CJul 18, 1995 · N502US · Boeing 757251 · Communications SystemSDR 9510755529Steering · malfunctionedDURING INITIAL TAKEOFF POWER APPLICATION AFTER EPR WAS SET, THE AIRCRAFT TURNED HARD RIGHT ON THE RUNWAY. FULL LEFT RUDDER DID NOT CONTROL THE TURN, ALL ENGINE INDICATIONS WERE NORMAL. TAKEOFF WAS ABORTED. NO ASYMMETRY WAS NOTICED DURING TAXI OUT OR IN. RUJul 15, 1995 · N529US · Boeing 757251 · Landing Gear Steering SystemSDR 9510465522Outflow Act · malfunctionedDURING CLIMB, BOTH AUTO PRESSURE CONTROLLERS WERE INOPERATIVE WITH CABIN AUTO INOPERATIVE STATUS MESSAGE. AIRCRAFT RETURNED TO MSP. REPLACED OUTFLOW VALVE ACTUATOR. SYSTEM CHECK WAS NORMAL.Jul 8, 1995 · N522US · Boeing 757251 · Pressure Regulator/Outflow ValveSDR 9509465533Smoke Detector · failedDURING CLIMB, THE SMOKE LIGHT CAME ON FOLLOWED BY EQUIPMENT OVERHEAT FIVE MINUTES LATER. DECISION WAS MADE TO RETURN WHEN THE FLIGHT INSTRUMENTS WENT DIM. EQUIPMENT OVERHEAT LIGHT WENT OUT WHEN ALTERNATE SYSTEM WAS USED. THE AIRCRAFT RETURNED TO MSP AND LANJun 15, 1995 · N533US · Boeing 757251 · Smoke DetectionSDR 9509425530Retract Mech · malfunctionedLEADING EDGE SLAT DISAGREE LIGHT CAME ON DURING APPROACH. AIRCRAFT MADE A GO-AROUND AND EMERGENCY EQUIPMENT WAS REQUESTED BY THE CREW. USED ALTERNATE FLAP PROCEDURE AND LANDED WITHOUT INCIDENT. MAINTENANCE IS IN PROGRESS.Jun 13, 1995 · N530US · Boeing 757251 · Leading Edge Slat Control SystemSDR 9509345509Floorbeam · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD BS 345 AT LBL 22 TO RBL 25. REPAIRED BEAM (P/N 141N5111) PER EA 55-98496.Jun 9, 1995 · N509US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9508835529Seal · looseA BUMPING NOISE WAS REPORTED NEAR DOOR 4R AFTER TAKEOFF, AIRCRAFT RETURNED TO SFO. FOUND THE INNER (NOISE) DOOR SEAL OUT OF THE SEAL RETAINER AND PROTRUDING OUTSIDE OF DOOR 4R. REINSTALLED SEAL, NO DAMAGE FOUND.Jun 3, 1995 · N529US · Boeing 757251 · Passenger/Crew DoorsSDR 9509115528Bracket · crackedDURING PERIODIC CHECK, FOUND A 3.75 INCH CRACK IN THE NR 1 ENGINE FAN COWL SUPPORT BEAM ANGLE STA 105. REPAIRED ANGLE PER EA 55-98490.May 28, 1995 · N528US · Boeing 757251 · Nacelle/Pylon StructureSDR 9508755522Bleed Valve · failedDURING CLIMB, THE NR 2 COMPRESSOR STALLED TWICE. TWO LOUD BANGS AND A BRIGHT FLASH WERE OBSERVED. NO ABNORMAL ENGINE INDICATIONS WERE OBSERVED. AIRCRAFT WAS RETURNED TO MEM WHERE TROUBLESHOOTING FOUND THE 2.5 BLEED VALVE SEIZED. THE ENGINE WAS REPLACED.May 28, 1995 · N522US · Boeing 757251 · Compressor Bleed ValveSDR 9509105528Floor Beam · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE FS 365 FLOOR BEAM UPPER CHORD FASTENER HOLES RBL 0 - 19. REPAIRED BEAM PER EA 55-98483.May 27, 1995 · N528US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9509075528Floor Beam · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE FS 377 FLOOR BEAM UPPER CHORD FASTENER HOLES LBL 6 - 23. REPAIRED BEAM PER EA 55-98485.May 25, 1995 · N528US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9509045528Floor Beam · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE FS 365 FLOOR BEAM UPPER CHORD FASTENER HOLES RBL 8 AND RBL 16. REPAIRED PER EA 55-98483.May 24, 1995 · N528US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9509035528Floor Beam · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE FS 1640 FLOOR BEAM UPPER CHORD RBL 12 - 59. REPAIRED BEAM PER EA 55-98486.May 24, 1995 · N528US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9508195503Fuel Control · malfunctionedDURING TAXI AND AFTER BOTH ENGINES STABILIZED, THE LEFT ENGINE SHUTDOWN BY ITSELF. RECEIVED LOW OIL PRESSURE WARNING AND LEFT ENGINE PIRMARY CONT MESSAGE. THE FUEL CONTROL WAS THEN SHUTOFF AND THERE WAS A TAILPIPE FIRE. AIRCRAFT WAS RETURNED TO GATE WHERE TMay 21, 1995 · N503US · Boeing 757251 · Fuel Control/Turbine EnginesSDR 9508325527Skin · crackedDURING PERIODIC CHECK, FOUND A ONE INCH CRACK IN THE NR 1 ENGINE NACELLE STRUT SKIN PANEL, NACELLE STA 115. REPAIRED PANEL P/N 311N3450-11, -13, -15 PER EA 55-98479.May 17, 1995 · N527US · Boeing 757251 · Nacelle/Pylon, Plate/SkinSDR 9508135527Floorbeam · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE FLOORBEAM UPPER CHORD FS 365. REPAIRED PER EA 55-98478.May 16, 1995 · N527US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9507915519Engine · failedON TAKEOFF, THE RIGHT ENGINE SPOOLED UP SLOWER THAN THE LEFT ENGINE. A POP WAS HEARD AND THE TAKEOFF WAS ABORTED. EGT STAYED AT APPROXIMATELY 535, OTHER PARAMETERS WERE NORMAL. AIRCRAFT RETURNED TO THE GATE. ENGINE CHANGE IS IN PROGRESS.May 14, 1995 · N519US · Boeing 757251 · Engine (Turbine/Turboprop)SDR 9507715518Skin · crackedDURING PERIODIC CHECK, FOUND CRACK IN THE NR 1 ENGINE NACELLE STRUT SKIN AT THE CUTOUT FOR ACCESS PANEL 433AL. REPAIRED PER EA 55-98206. MFG PART NUMBER 311N3450-15.May 8, 1995 · N518US · Boeing 757251 · Nacelle/Pylon, Plate/SkinSDR 9507655518Floorbeam · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE FLOORBEAM UPPER CHORD FS 345 FROM LBL 10 TO LBL 24. REPAIRED PER EA 55-98208.May 7, 1995 · N518US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9507595516Support · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN SEAT TRACK SUPPORT FS 365, RBL 45.5. REPAIRED PER EA 55-98202. MFG PART NUMBER 141N5131-4.Apr 28, 1995 · N516US · Boeing 757251 · Fuselage, Seat/Cargo Attach FittingsSDR 9506975530Circuit Breaker · trippedON TAKEOFF, THE LEADING EDGE SLAT DISAGREE MESSAGE AND LEADING EDGE LIGHTS ILLUMINATED. DURING FLAP RETRACTION, THE FLAP NEEDLES STOPPED AT FLAPS 1/2 POSITION AND DID NOT COME UP USING THE ALTERNATE PROCEDURES. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCApr 28, 1995 · N530US · Boeing 757251 · Leading Edge Slat Control SystemSDR 9506335533Apu · failedTHE APU FAILED DURING CRUISE AND RESTART ATTEMPTS WERE UNSUCCESSFUL. THE RIGHT IDG WAS ON MEL, SO THE AIRCRAFT DIVERTED TO ATL. REPLACED THE RIGHT IDG, PERFORMED BITE ON APU, NO FAULTS WERE DETECTED. APU OPERATIONAL CHECK WAS NORMAL.Apr 22, 1995 · N533US · Boeing 757251 · Airborne Auxiliary Power Unit (APU) SystemSDR 9505945526Skin · crackedDURING PERIODIC CHECK, THE NR 1 ENGINE NACELLE STRUT SKIN PANEL WAS FOUND WITH A CRACK COMING OUT OF THE 433AL ACCESS PANEL. CRACKS WERE APPROXIMATELY 0.75 INCH LONG IN THE SKIN, DOUBLER, AND TRIPLER. INSTALLED REPAIR PER NWA EA 55-98174. MFG PART NUMBER 31Apr 13, 1995 · N526US · Boeing 757251 · Nacelle/Pylon, Plate/SkinSDR 9505665518Eec Stator · failedDURING CRUISE, RECEIVED 'R ENG SEC CONT' MESSAGE AND LOST OIL TEMPERATURE INDICATIONS. AIRCRAFT DIVERTED TO DTW. RIGHT EEC STATOR WAS REPLACED AND THE AIRCRAFT CHECK OK FOR SERVICE.Apr 13, 1995 · N518US · Boeing 757251 · Fuel Control/Turbine EnginesSDR 9506265526Floor Beam · corrodedDURING PERIODIC CHECK, THE FS 365 FLOOR BEAM UPPER CHORD WAS FOUND WITH TYPICAL CORROSION. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER NWA EA 55-98176.Apr 11, 1995 · N526US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9506255526Floor Beam · corrodedDURING PERIODIC CHECK, THE FS 377 FLOOR BEAM UPPER CHORD WAS FOUND WITH TYPICAL CORROSION. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER NWA EA 55-98175.Apr 11, 1995 · N526US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9505455523Oven · malfunctionedON TAKEOFF, THE FLIGHT ATTENDANT REPORTED SMOKE FROM THE AFT GALLEY CENTER OVEN. AIRCRAFT RETURNED TO MSP, NO EMERGENCY WAS DECLARED. CHECKED FOR EVIDENCE OF FOOD OR PAPER, NONE FOUND. PULLED AND COLLARED OVEN CIRCUIT BREAKERS. REPLACED OVEN IN DCA, OPERATApr 7, 1995 · N523US · Boeing 757251 · Buffet/GalleysSDR 9506425517Threshold · corrodedDURING PERIODIC CHECK, THE AFT CARGO THRESHOLD BEAM CHORD WAS FOUND CORRODED AROUND NUTPLATE HOLES AT FS 1380 TO 1440, RBL 20. REMOVED CORROSION AND INSTALLED REPAIR PER NWA EA 55-98173. (MFG PART NO. 146N8522-51)Apr 6, 1995 · N517US · Boeing 757251 · Fuselage Miscellaneous StructureSDR 9505485517Floorbeam · corrodedDURING PERIODIC CHECK, THE FS 345 FLOORBEAM UPPER CHORD WAS FOUND WITH TYPICAL CORROSION. REMOVED CORROSION AND INSTALLED REPAIR PER NWA EA 55-97822.Apr 6, 1995 · N517US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9505475517Floorbeam · corrodedDURING PERIODIC CHECK, THE FS 324 FLOORBEAM UPPER CHORD WAS FOUND WITH TYPICAL CORROSION AT LBL 15, WL 208. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER NWA EA 55-97821.Apr 6, 1995 · N517US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9505355517Floor Beam · corrodedDURING PERIODIC CHECK, THE FS 365 FLOORBEAM UPPER CHORD WAS FOUND WITH TYPICAL CORROSION AROUND THE NUTPLATE HOLES. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER NWA EA 55-97820.Apr 2, 1995 · N517US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9504955534Floor Support · corrodedDURING PERIODIC CHECK, THE AFT CARGO FLOOR SUPPORT STRINGERS WERE FOUND CORRODED AROUND NUTPLATES BETWEEN FS 1445 AND 1500, LBL 11 AND RBL 3. REMOVED CORROSION AND INSTALLED REPAIR PER NWA EA 55-97818.Mar 25, 1995 · N534US · Boeing 757251 · Fuselage Miscellaneous StructureSDR 9505035534Skin · damagedDURING PERIODIC CHECK, THE NR 1, NR 2, NR 10, NR 11, AND NR 12 SPOILER UPPER SKIN PANELS WERE FOUND WITH NUMEROUS AREAS OF DAMAGE AND DELAMINATION (2 INCH DIAMETER TYPICAL). INSTALLED REPAIRS PER SRM 57-70-01, FIG. 201 AND NWA EA 55-97817.Mar 24, 1995 · N534US · Boeing 757251 · SpoilersSDR 9504725515Floor Beam · gougedDURING PERIODIC CHECK, THE FLOOR BEAM AT FS 377.7, RBL 4 WAS DAMAGED AND WAS REPAIRED PER SRM 53-00-51, FIG 201 AND NWA EA 55-97863.Mar 14, 1995 · N515US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9503995504Acm · malfunctionedTAKEOFF WAS ABORTED AT 50 KTS DUE TO LOUD WHINE IN THE COCKPIT. COCKPIT TEMPERATURE WAS 85 DEGREES, WITH LEFT AIR CYCLE MACHINE MALFUNCTION. PLACARDED LEFT PACK INOPERABLE PER MEL 21-51-1. REPAIRED LEFT AIR CYCLE MACHINE PER MM 21-51-03, P. 201 IN BOS, SYSTMar 14, 1995 · N504US · Boeing 757251 · Cabin Cooling SystemSDR 9504185515Floor Beam · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FUSELAGE LATERAL FLOOR BEAM UPPER CHORD AT FS 365, LBL 24.75. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER NWA EA 55-096485.Mar 13, 1995 · N515US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9504155532Skin · damagedDURING PERIODIC CHECK, THE FUSELAGE BELLY SKIN BETWEEN FS 660 - 670 AROUND STRINGER 27R WAS FOUND WITH TYPICAL NICK AND GOUGE DAMAGE CAUSED BY CARGO NETS. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 AND NWA EA 55-93840.Mar 13, 1995 · N532US · Boeing 757251 · Fuselage Main, Plate/SkinSDR 9504215515Door Sill · corrodedDURING PERIODIC CHECK, THE AFT CARGO DOOR LOWER SILL INNER CHORD WAS FOUND CORRODED ON THE TOP AND BOTTOM SIDES AROUND THE NUTPLATE HOLES. REMOVED CORROSION AND INSTALLED REPAIR PER NWA EA 55-97802.Mar 10, 1995 · N515US · Boeing 757251 · Fuselage Miscellaneous StructureSDR 9503735514Indicator Bulb · failedEXECUTED A GO-AROUND AT MSP DUE TO THE RIGHT MAIN GEAR GREEN LIGHT WOULD NOT COME ON. ACFT LANDED WITHOUT INCIDENT. REPLACED INDICATOR BULB, SYSTEM CHECKED NORMAL.Mar 10, 1995 · N514US · Boeing 757251 · Landing Gear Position and WarningSDR 9504195515Longeron · corrodedDURING PERIODIC CHECK, THE AFT CARGO COMPARTMENT FLOOR STRINGERS AT BS 1510 AND 1330 WERE FOUND WITH TYPICAL CORROSION. REMOVED CORROSION AND INSTALLED REPAIRS PER NWA EA 55-96724 AND 55-96725.Mar 7, 1995 · N515US · Boeing 757251 · Fuselage Main, Longeron/StringerSDR 9503245507Circuit Breaker · trippedDURING TAKEOFF AS TAKEOFF POWER WAS APPLIED, THE NR 1 THRUST LEVER WAS UNABLE TO REACH FULL TAKEOFF. THE TAKEOFF WAS ABORTED. THE LEFT REVERSER INTERLOCK CIRCUIT BREAKER WAS RESET AND THE SYSTEM CHECKED OK.Feb 27, 1995 · N507US · Boeing 757251 · Power LeverSDR 9503055527Cooling Fan · failedA STRONG ELECTRICAL BURNING SMELL WAS NOTICED IN THE COCKPIT. FOLLOWED COCKPIT OPERATING PROCEDURE AND SMELL WAS EVACUATED, SOURCE WAS UNKNOWN. FOUND THE FORWARD EQUIPMENT COOLING SUPPLY FAN CIRCUIT BREAKER POPPED, AND WAS UNABLE TO RESET. REPLACED FORWARD Feb 24, 1995 · N527US · Boeing 757251 · Air Distribution FanSDR 9504175532Skin · damagedDURING PERIODIC CHECK, THE FUSELAGE BELLY SKIN BETWEEN FS 1355 - 1410, STR 24L - 26L WAS FOUND WITH NICKS AND GOUGES CAUSED BY CARGO NETS. REMOVED DAMAGED SKIN AND INSTALLED REPAIR PER SRM 53-00-01, FIG 205 AND NWA EA 55-93836.Feb 14, 1995 · N532US · Boeing 757251 · Fuselage Main, Plate/SkinSDR 9504165532Skin · damagedDURING PERIODIC CHECK, NUMEROUS NICKS AND SCRATCHES WERE FOUND ON THE FUSELAGE BELLY SKIN BETWEEN FS 1340 - 1360, STR 26R. DAMAGE WAS CAUSED BY CARGO NETS. INSTALLED REPAIR DOUBLER PER SRM 53-00-01, FIG 204 AND NWA EA 55-93835.Feb 10, 1995 · N532US · Boeing 757251 · Fuselage Main, Plate/SkinSDR 9501755520Idg · malfunctionedAT THE START OF TAKEOFF, THE LEFT GENERATOR DRIVE LIGHT FLICKERED AND THE LEFT GENERATOR CONTROL LIGHT ILLUMINATED; ABORTED TAKEOFF. PLACED THE LEFT IDG ON MEL 24-00-1. REPLACED THE LEFT INTEGRATED DRIVE GENERATOR AT MSP. SYSTEM CHECK ON RUN-UP WAS NORMAL.Feb 5, 1995 · N520US · Boeing 757251 · AC Generator-AlternatorSDR 9501775508Stringer · corrodedDURING PERIODIC CHECK, THE AFT CARGO FLOOR SUPPORT STRINGER AT FS 1510, RBL 11 AND RBL 7 WAS FOUND CORRODED AT THE NUTPLATES. REMOVED CORROSION AND REPAIRED PER NWA EA 55-93725Feb 1, 1995 · N508US · Boeing 757251 · Fuselage Main, Longeron/StringerSDR 9501765508Stringer · corrodedDURING PERIODIC CHECK, THE AFT CARGO FLOOR SUPPORT STRINGER AT FS 1330, RBL 11 AND RBL 7 WAS FOUND CORRODED AT THE NUTPLATES. REMOVED CORROSION AND REPAIRED PER NWA EA 55-96620.Feb 1, 1995 · N508US · Boeing 757251 · Fuselage Main, Longeron/StringerSDR 9501675508Chord · corrodedDURING PERIODIC CHECK, THE AFT CARGO LOWER DOOR SILL INNER CHORD WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER NWA EA 55-93722.Jan 30, 1995 · N508US · Boeing 757251 · Fuselage Miscellaneous Structure
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