Boeing 757-225

Service difficulty reports · 1,988

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 = '757225'
  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 USAABB02200Battery · inoperativeSJU - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M)Dec 4, 2002 · N604AU · Boeing 757225 · Emergency LightingSDR USAABB02198Controller · malfunctionedFLL - FLT 58 - IN CRUISE AT FL350, CREW RECEIVED THE CABIN ALTITUDE WARNING AS CABIN PRESSURE WAS INDICATING 10,000 FEET. CREW DESCENDED AT FL200, WHERE THE CABIN ALTITUDE WAS 8,500 FEET. FLIGHT CONTINUED TO FLL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANov 30, 2002 · N602AU · Boeing 757225 · Cabin Pressure ControllerSDR USAABB02197Battery · dischargedTPA - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROW 1 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M)Nov 29, 2002 · N605AU · Boeing 757225 · Emergency LightingSDR AWXA200201218Door Frame · crackedDURING C-09 CHECK A .6250 INCH CRACK WAS FOUND ON FORWARD CARGO DOOR CUTOUT FRAME WEB AT ATTACHMENT HOLE FOR UPPER GUIDE TRACK FITTING, BS 560. MAINTENANCE REMOVED THE CRACKED SECTION OF FORWARD CARGO DOOR FRAME WEB BS 560; FABRICATED A REPAIR PLATE AND SPLICENov 24, 2002 · N913AW · Boeing 757225 · Fuselage Main, StructureSDR AWXA200201217Door Frame · crackedDURING C-09 CHECK A .250 INCH CRACK WAS FOUND ON FORWARD CARGO DOOR CUTOUT FORWARD FRAME WEB AT ATTACHMENT HOLE FOR NR6 DOOR STOP, BS 560. MAINTENANCE REMOVED THE CRACKED SECTION OF FORWARD CARGO DOOR FRAME WEB BS 560; FABRICATED A REPAIR PLATE AND SPLICE PLATNov 24, 2002 · N913AW · Boeing 757225 · Fuselage Main, StructureSDR AWXA200201216Door Frame · crackedDURING C-09 CHECK 2 EACH .3750 INCH CRACKS WERE FOUND ON AFT CARGO DOOR CUTOUT FRAME WEB AT THE LOWER DOOR STOP FITTING HOLE, BS 1440. MAINTENANCE REMOVED THE CRACKED SECTION OF AFT CARGO DOOR FRAME WEB BS 1440; FABRICATED A REPAIR PLATE AND SPLICE PLATE; AND Nov 24, 2002 · N913AW · Boeing 757225 · Fuselage Main, StructureSDR AWXA200201215Door Frame · crackedDURING C-09 CHECK A .250 INCH CRACK WAS FOUND ON AFT CARGO DOOR SURROUND CUTOUT WEB AT THE LOWER DOOR STOP FITTING HOLE, BS 1380. MAINTENANCE REMOVED THE CRACKED SECTION OF AFT CARGO DOOR FORWARD FRAME WEB; FABRICATED A NEW SECTION OF FRAME WEB; AND INSTALLED Nov 24, 2002 · N913AW · Boeing 757225 · Fuselage Main, StructureSDR AWXA200201226Frame · crackedLCQ - MAJOR REPAIR - DURING C-09 CHECK A 3" VERTICAL CRACK WAS FOUND ON FRAME IN THE AFT CARGO COMPARTMENT AT BS 1600, LBL 20. MAINTENANCE CUTOUT CRACKED SECTION OF FRAME AT BS 1600, LBL 20; FABRICATED REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B757Nov 22, 2002 · N913AW · Boeing 757225 · Fuselage Main, FrameSDR AWXA200201225Frame · corrodedLCQ - MAJOR REPAIR - DURING C-09 CHECK CORROSION WAS FOUND ON TOP OF FRAME IN THE AFT CARGO COMPARTMENT AT BS 1640, LBL 15. MAINTENANCE CUTOUT CORRODED SECTION OF FRAME AT BS 1640, LBL 15; FABRICATED 2 EACH CHANNELS AND A FILLER; INSTALLED REPAIR PARTS IAW B75Nov 22, 2002 · N913AW · Boeing 757225 · Fuselage Main, FrameSDR AWXA200201223Frame · crackedLCQ - MAJOR REPAIR - DURING C-09 CHECK A 3/4" CRACK WAS FOUND ON AFT CARGO COMPARTMENT FRAME AT BS 1400, BETWEEN STRINGERS 25 L/H AND 26 L/H. MAINTENANCE CUTOUT DAMAGED SECTION OF FRAME AT BS 1400, BETWEEN STRINGERS 24 L/H AND 27 L/H; FABRICATED 2 EACH CHANNELNov 22, 2002 · N913AW · Boeing 757225 · Fuselage Main, FrameSDR AWXA200201222Frame · crackedLCQ - MAJOR REPAIR - DURING C-09 CHECK A 1 1/4" CRACK WAS FOUND ON AFT CARGO COMPARTMENT FRAME AT BS 1420, BETWEEN STRINGERS 26 L/H AND 27 L/H. MAINTENANCE CUTOUT DAMAGED SECTION OF FRAME AT BS 1420, BETWEEN STRINGERS 26 L/H AND 27 L/H; FABRICATED 2 EACH CHANNNov 22, 2002 · N913AW · Boeing 757225 · Fuselage Main, FrameSDR AWXA200201221Frame · corrodedLCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION AND A DENT WERE FOUND ON TOP FLANGE OF FRAME IN THE AFT CARGO COMPARTMENT AT BS 1560, LBL 9. MAINTENANCE CUTOUT CORRODED SECTION OF FRAME AT BS 1560, LBL 9; FABRICATED 2 EACH CHANNELS AND A FILLER; INov 22, 2002 · N913AW · Boeing 757225 · Fuselage Main, FrameSDR USAABB02194Light · inoperativeCLT - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M)Nov 21, 2002 · N600AU · Boeing 757225 · Emergency LightingSDR AWXA200201214Floorbeam · corrodedMAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AROUND A HILOC ON CABIN FLOORBEAM AT BS 1661, LBL 57.5. MAINTENANCE REMOVED HILOC AND CORROSION ON CABIN FLOORBEAM AT BS 1661, LBL 57.5, AND FOUND MATERIAL LOSS OUT OF LIMITS. CUTOUT DAMAGED SENov 21, 2002 · N913AW · Boeing 757225 · Fuselage Main, Floor BeamSDR AWXA200201212Frame · crackedDURING C-09 CHECK, A .250 INCH CRACK WAS FOUND ON THE NR 2 ENGINE PYLON FRAME CUTOUT FOR PANEL 443GL AT FORWARD LOWER CORNER INBOARD SIDE OF PYLON. MAINTENANCE PERFORMED A HFEC INSPECTION OF CRACK AT NR2 ENGINE PYLON FRAME CUTOUT; STOP DRILLED CRACK AND PERFONov 21, 2002 · N913AW · Boeing 757225 · Nacelle/Pylon, Frame/Spar/RibSDR AWXA200201213Floorbeam · corrodedDURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON CABIN FLOORBEAM UPPER FLANGE AT BS 1661, LBL 24. MAINTENANCE REMOVED CORROSION ON CABIN FLOORBEAM UPPER FLANGE AT BS 1661, LBL 24, AND FOUND MATERIAL LOSS OUT OF LIMITS. CUTOUT DAMAGED SECTION OF FLOORBEAMNov 20, 2002 · N913AW · Boeing 757225 · Fuselage Main, Floor BeamSDR AWXA200201210Pan · corrodedMAJOR REPAIR, DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF AFT CABIN FLOOR SUB PAN AT BS 1681-BS 1720. MAINTENANCE BLENDED OUT CORROSION ON AFT CABIN FLOOR SUB PAN BS 1681-BS 1720 AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED 6 EACH ANov 20, 2002 · N913AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR AWXA200201224Structure · crackedDURING C-09 CHECK A 1 INCH CRACK WAS FOUND ON RT WING TO BODY FAIRING LOWER FLAP TRACK STRUCTURE BS 1170. MAINTENANCE REMOVED RT WING TO BODY FAIRING LOWER FLAP TRACK STRUCTURE BS 1170; FABRICATED A NEW REPLACEMENT STRUCTURE. INSTALLED REPAIR PART SRM.Nov 19, 2002 · N913AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR AWXA200201220Stringer · corrodedLCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT STRINGER AT BS 1290, STR 28 L/H. MAINTENANCE CUTOUT CORROSION DAMAGE ON STRINGER 28 L/H AT BS 1290; FABRICATED A NEW SECTION OF STRINGER, AND STRINGER SPLICE ANGLNov 19, 2002 · N913AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR AWXA200201219Stringer · crackedLCQ - MAJOR REPAIR - DURING C-09 CHECK CORROSION WAS FOUND ON STRINGER 29 L/H, AT BS 1680. MAINTENANCE CUTOUT 4" SECTION OF CORRODED STRINGER AND FOUND CORROSION ON SKIN; CLEANED CORROSION OFF SKIN AND FOUND MATERIAL LOSS OUT OF LIMITS; CUTOUT CORRODED SECTIONNov 19, 2002 · N913AW · Boeing 757225 · Fuselage Main, Longeron/StringerSDR AWXA200201209Floorbeam · corrodedMAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOORBEAM AT RIGHT INBOARD EDGE OF CUSP, BS 1681. MAINTENANCE REMOVED CUSP ATTACH ANGLE FROM RIGHT CUSP AREA BS 1640 TO BS 1720, THRESHOLD WEB AND SUPPORT STRUCTURE, INTERCOSTALS FROM Nov 19, 2002 · N913AW · Boeing 757225 · Fuselage Main, Floor BeamSDR AWXA200201211Bear Strap · corrodedLCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT LOWER CORNER OF THE AFT CARGO DOOR BODY SKIN CUTOUT (BEAR STRAP) BS 1440, STR 26 R/H. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; PERFORMED HFEC INSPECTION ANov 11, 2002 · N913AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR USAA020440Skin · crackedCLT - FOUND INNER SKIN CRACKED .250 INCH, ABOVE LOWER HINGE BOX, L4 DOOR INNER SKIN 1661. INSTALLED REPAIR DOUBLER ON INNER DOOR SKIN PER EA 86643. (M)Nov 1, 2002 · N604AU · Boeing 757225 · Service DoorsSDR USAA020441Skin · crackedCLT - FOUND SKIN CRACKED .75 INCH, INBOARD TRAILING EDGE FLAP RIGHT WING ABOVE NR 6 FLAP TRACK LINKAGE. INSTALLED REPAIR STRAP AFTER DAMAGE AREA TRIMMED PER EA 86716. (M)Nov 1, 2002 · N604AU · Boeing 757225 · Trailing Edge FlapsSDR AWXA200201051Governor · fluctuatesFLT 0488 - ON TAKEOFF ROLL, AUTO THROTTLES AND EPR MISMATCHED, ADJUSTED NR 2 ENGINE TO 1.58. AFTER LIFT OFF RT EPR JUMPED TO 1.70, AFTER REDUCING RT ENGINE EPR DROPPED TO 1.24 FLUX FROM 1.65 TO 1.25. CONTINUED TO FLUX AFTER DISCON AUTO THROT. RETURNED TO PHX LOct 24, 2002 · N913AW · Boeing 757225 · Turbine GovernorSDR USAABB02184Light · inoperativeCLT - FOUND L3 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M)Oct 23, 2002 · N618AU · Boeing 757225 · Emergency LightingSDR USAABB02178Battery · dischargedMCO - FOUND THE EMERGENCY LIGHT AT ROW 14 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AT ROW 14. OPERATIONAL CHECK GOOD. (M)Oct 21, 2002 · N609AU · Boeing 757225 · Emergency LightingSDR USAA020401Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 1 INCH, STATION 480 LBL 40 6 INCHES BELOW FLOOR LEVEL. REPAIR ANGLE INSTALLED PER SRM 51-70-11. (M)Oct 17, 2002 · N604AU · Boeing 757225 · Fuselage Miscellaneous StructureSDR USAABB02177Light · inoperativeLAX - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 6 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M)Oct 15, 2002 · N605AU · Boeing 757225 · Emergency LightingSDR USAA020400Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 10 INCHES, BL 0 BETWEEN STATION 440 AND 460 FLOOR LEVEL. FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 51-10-02. (M)Oct 15, 2002 · N604AU · Boeing 757225 · Fuselage Miscellaneous StructureSDR USAA020399Intercostal · crackedCLT - FOUND INTERCOSTAL WITH 2 INCH CRACK, STATION 440 BL 0 BELOW FLOOR LEVEL. FABRICATED AND INSTALLED NEW WEB SECTION PER SRM 51-10-02. (M)Oct 15, 2002 · N604AU · Boeing 757225 · Fuselage Miscellaneous StructureSDR USAA020396Intercostal · crackedINTERCOSTAL HAS 10 INCH CRACK BL 0 BETWEEN STA 540 AND 560. INSTALLED NEW INTERCOSTAL.Oct 13, 2002 · N604AU · Boeing 757225 · Fuselage Miscellaneous StructureSDR USAA020398Intercostal · crackedCLT - FOUND CHORD WITH MULTIPLE CRACKS, MAXIMUM WIDTH .125 INCH, UPPER CHORD OF INTERCOSTAL AT BL 0, BS 1420-1440. FABRICATED AND INSTALLED NEW ANGLE AND SHIM PER SRM 53-00-51. (M)Oct 10, 2002 · N604AU · Boeing 757225 · Fuselage Miscellaneous StructureSDR USAA020442Intercostal · crackedCLT - FOUND CHORD CRACKED .125 INCH, UPPER CHORD INTERCOSTAL AT BL 0, BS 1420-1440. FABRICATED AND INSTALLED NEW ANGLE PER SRM 53-00-51. (M)Oct 9, 2002 · N604AU · Boeing 757225 · Fuselage Miscellaneous StructureSDR USAABB02173Light · inoperativeFOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 6, INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY.Oct 8, 2002 · N605AU · Boeing 757225 · Emergency LightingSDR USAABB02167Sign · inoperativeBDL - FOUND THE L4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M)Sep 27, 2002 · N608AU · Boeing 757225 · Emergency LightingSDR USAABB02164Battery · dischargedBOS - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 4, 9, 23 AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M)Sep 24, 2002 · N601AU · Boeing 757225 · Emergency LightingSDR USAABB02163Actuator · failedPHL - FLT 1535 - UPON GEAR RETRACTION, CREW RECEIVED THE EICAS MESSAGES 'GEAR DISAGREE' AND 'GEAR DOORS', AND THE ASSOCIATED AMBER LIGHTS. CREW RECYCLED THE GEAR, AND HAD THE SAME INDICATIONS. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINSep 22, 2002 · N603AU · Boeing 757225 · Landing Gear ActuatorSDR AWXA200200970Web · crackedLCQ - MAJOR REPAIR - DURING C-06 CHECK A 1/2" CRACK WAS FOUND EMANATING FROM LIGHTNING HOLE ON CABIN FLOOR WEB AT LBL 24, BS 660 - 680. MAINTENANCE CUTOUT DAMAGED PORTION OF WEB, FABRICATED A REPAIR DOUBLER, AND INSTALLED REPAIR PART IAW B757-200 SRM 51-70-13,Sep 20, 2002 · N907AW · Boeing 757225 · Fuselage Main, Floor BeamSDR AWXA200200983Structure · wornDURING C-06 CHECK THE RUDDER FEEL CENTERING AND TRIM QUADRANT RIG HOLE EXCEEDS SPECIFIED HOLE DIAMETER (SPECIFIED SIZE .312, ACTUAL SIZE .380). MAINTENANCE OVERSIZED THE HOLE TO .395, FABRICATED A BUSHING AND REAMED HOLE TO .312, INSTALLED REPAIR IAW AWA E.R.Sep 18, 2002 · N907AW · Boeing 757225 · Rudder Tab Control SystemSDR AWXA200200971Seat Track · corrodedLCQ - MAJOR REPAIR - DURING C-06 CHECK INTERGRANULAR CORROSION WAS FOUND ON R/H OUTBOARD SEAT TRACK BS 440. MAINTENANCE CUTOUT DAMAGED SECTION OF SEAT TRACK BS 440 TO BS 640. FABRICATED A NEW SECTION OF SEAT TRACK, AND INSTALLED REPAIR PART IAW B757-200 SRM 51Sep 16, 2002 · N907AW · Boeing 757225 · Fuselage Main, Floor BeamSDR USAABB02155Battery · dischargedBDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M)Sep 15, 2002 · N608AU · Boeing 757225 · Emergency LightingSDR AWXA200200978Panel · crackedDURING C-06 CHECK A 1 INCH CRACK WAS FOUND ON NR 2 ENGINE PYLON LOWER TRAILING EDGE PANEL, AT THE INBOARD FORWARD END. MAINTENANCE REMOVED THE LOWER TRAILING EDGE PANEL. FABRICATED A NEW LOWER TRAILING EDGE PANEL, AND INSTALLED REPAIR PART IAW B757-200 SRM 51-Sep 15, 2002 · N907AW · Boeing 757225 · Nacelle/Pylon, Plate/SkinSDR USAABB02160Hydraulic Line · leakingCLT - FLT 1892 - ON GEAR EXTENSION FOR LANDING, CREW NOTED LOSS OF HYDRAULIC QUANTITY ON THE LEFT SYSTEM. CREW PERFORMED A TOWER FLYBY TO ENSURE THE GEAR DOWN AND LOCKED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEASep 14, 2002 · N607AU · Boeing 757225 · Hydraulic System, MainSDR AWXA200200977Angle · crackedDURING C-06 CHECK A 1 INCH CRACK WAS FOUND ON UPPER FLOOR BEAM ANGLE IN THE FORWARD CARGO COMPARTMENT, BS 672. MAINTENANCE REMOVED THE CRACKED ANGLE FROM BS 660 TO BS 680. FABRICATED A NEW ANGLE, AND INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, FIG. 8, PG.Sep 14, 2002 · N907AW · Boeing 757225 · Fuselage Main, Floor BeamSDR AWXA200200979Structure · contaminatedDURING C-06 CHECK X-RAY INDICATED MOISTURE WAS TRAPPED IN THE LT WING INBOARD AFT FLAP. MAINTENANCE REMOVED DAMAGED SKIN PLIES TO ACCESS HONEYCOMB; REMOVED DAMAGED AREA AND MOISTURE; REINSTALLED SKIN PER B757-200 SRM 51-70-04, PG. 4-31.Sep 12, 2002 · N907AW · Boeing 757225 · Trailing Edge FlapsSDR AWXA200200976Intercostal · crackedDURING C-06 CHECK A 3/4 INCH CRACK WAS FOUND ON CABIN UPPER INTERCOASTAL ANGLE BS 445. MAINTENANCE REMOVED THE DAMAGED INTERCOASTAL ANGLE AT BS 445. FABRICATED A NEW INTERCOASTAL ANGLE, AND INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, FIG. 8, PG. 39-40.Sep 12, 2002 · N907AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR USAABB02151Wire · damagedCLT - FOUND EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. MAINTENANCE REPAIRED WIRING AND REPLACED THE BATTERY PACK AT M370. (M)Sep 7, 2002 · N600AU · Boeing 757225 · Light System WiringSDR AWXA200200869Altimeter · brokenPHX - ABORTED TAKEOFF - FLT 0085 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR BWI THE CAPTAINS ALTIMETER OFF FLAG WAS IN VIEW, NO FLAG IN STANDBY ALTIMETER, FLAG APPEARED AT 90 KTS AND DISAPPEARED AT 80 KTS. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE COULD NOSep 7, 2002 · N913AW · Boeing 757225 · Altimeter, Barometric/EncoderSDR USAABB02147Fan · faultyON PREFLIGHT IN SJU, CREW NOTED A SLIGHT SMOKE SMELL IN THE LT WHEEL WELL. ON TAKEOFF, THE SMELL WAS NOTED AGAIN, BUT DISSIPATED. THE SMELL RETURNED AND THE FLIGHT DIVERTED TO GSO. MAINTENANCE OPERATED THE PACKS FROM VARIOUS SOURCES THROUGH FULL TEMPERATURESep 3, 2002 · N607AU · Boeing 757225 · Air Distribution Fan
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