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.
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
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 USAA960681Floor Beam · corrosionCLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND SEVERAL CORRODED AREAS 1 INCH BY 1 INCH STATION 1640 FLOOR BEAM. NEW CHORD SECTIONS INSTALLED, REPAIRED PER EA 58911 SRM 53-00-51 FIG 201 AND 203. (M)SDR AWXA960594Coffeemaker · failedPHX - FLT 0001 - AFT COFFEEMAKER CIRCUIT BREAKER OUT. FLIGHT ATTENDANT PUSHED IT BACK IN AND SMELLED ELECTRICAL SMOKE. REPLACED COFFEEMAKER. (M)SDR AWXA960586Light · loosePHX - FLT 2260 - DURING ROUTINE MAINTENANCE CEHCK, FOUND EMERGENCY LIGHT AT 3 CD INOP. RESECURED LIGHT. OPS CHECK GOOD. (M)SDR USAABB96038Fuel Control · failedSFO - FL 74 - ON CLIMB FROM SFO, LEFT ENGINE WOULD NOT DEVELOP CLIMB POWER WITHOUT EXCEEDING EGT LIMITS. FUEL FLOW WAS MUCH HIGHER ON THE LEFT ENGINE. FLIGHT RETURNED TO SFO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE EEC LIMITSDR USAABB96036Lights · inoperativeBDL - EXTERIOR EMERGENCY LIGHTS WOULD NOT TEST FROM THE NOSE LANDING GEAR TEST SWITCH. MAINTENANCE REPAIRED WIRING AT SWITCH S10035. (M)SDR USAABB96034Duct · leakingSFO - FLT 56 - CLIMBING THROUGH 10,000 FEET, CREW RECEIVED RIGHT ENGINE OVERHEAT LIGHT. CREW REDUCED POWER ON THE ENGINE AND LIGHT EXTINGUISHED. FLIGHT RETURNED TO SFO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE SIXTH STAGE HIGH PRESSURE DSDR USAABB96033B-Nut · looseSFO - FLT 60 - CLIMB THROUGH 10,000 FEET, CREW RECEIVED RIGHT ENGINE OVERHEAT LIGHT. CREW REDUCED POWER ON THE ENGINE AND LIGHT EXTINGUISHED. FLIGHT RETURNED TO SFO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE UPPER RIGHT 'B' NUT ON THE HPSOV SDR USAABB96031Door Seal · loosePHL - FLT 79 - AFTER TAKEOFF, RIGHT FORWARD DOOR ANNUNCIATOR LIGHT ILLUMINATED. AIRCRAFT WOULD NOT HOLD PRESSURIZATION. FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE DOOR SEAL LOOSE AND IN THE DOOR TRACK. SEAL WAS REINSTSDR USAABB96030Pseu · failedMCO - FLT 244 - AFTER TAKEOFF AND DURING GEAR RETRACTION, GREEN INDICATION LIGHTS EXTINGUISHED, DOOR LIGHT REMAINED ON, AND CREW RECEIVED EICAS MESSAGE 'GEAR DISAGREE'. CREW CYCLED THE GEAR. NO CHANGE IN THE SITUATION WAS APPARENT. FLIGHT RETURNED TO MCO ANDSDR USAABB96029Hyd Line · failedLAX - FLT 18 - DURING GEAR RETRACTION ON CLIMB, CREW RECEIVED INDICATION OF LOSS OF HYDRAULIC FLUID/PRESSURE FROM THE LEFT SYSTEM. FLIGHT RETURNED TO FIELD TO LAX AND WAS TOWED TO GATE DUE TO LOSS OF NOSE STEERING. MAINTENANCE REPLACED THE PRESSURE LINE TO TSDR USAABB96028Locked Sensor · failedCLT - FLT 8081 - AFTER TAKEOFF AND GEAR RETRACTION, CREW RECEIVED THE EICAS MESSAGES 'LDG GEAR MONITOR' AND GEAR DISAGREE'. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 SYSTEM NOSE GEAR LOCKED SENSOR AND ADJUSTED SDR USAABB96024Hyd Line · leakingPIT - FL 88 - AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. LEFT SIDE HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO. SYSTEM PRESSURE LIGHT ILLUMINATED AND CREW RECEIVED EICAS MESSAGE 'L HYD SYS PRESS'. TOWER ADVISED THAT SMOKE WAS COMING FROM THE LEFT SIDE SDR AWXA960371Yaw Dmpr Module · malfunctionedPHX - FLT 2610 - UNCOMMANED RUDDER ON CLIMB-OUT, RUDDER KICKED TWICE, ONCE UPON TURNBACK. APPROX 1 HOUR LATER LATER, RUDDER KICKED ONCE AT 500 FEET FROM TOUCHDOWN. CHECKED YAW DAMPER PER FIM 22-21-00, PAGE 101. NO FAULTS NOTED. CHECKED THE YAW DAMPER MODULSDR 96ZZZM1325Yaw Dmpr Module · malfunctionedPHX - FLT 2610 - UNCOMMANED RUDDER ON CLIMB-OUT, RUDDER KICKED TWICE, ONCE UPON TURNBACK. APPROX 1 HOUR LATER LATER, RUDDER KICKED ONCE AT 500 FEET FROM TOUCHDOWN. CHECKED YAW DAMPER PER FIM 22-21-00, PAGE 101. NO FAULTS NOTED. CHECKED THE YAW DAMPER MODULSDR AWXA960398Rt Cam Roller · failedPHX - FLT 2294 - AIRCRAFT ARRIVED WITH FLIGHT CREW COMPLAINING OF STIFF RUDDER PEDALS. WE CONFIRMED A TIGHT RATCHETY FEEL WHEN OPERATING PEDALS, ESPECIALLY WHEN LEFT PEDAL WAS PUSHED. RUDDER TRIM STICKS AND IS NOT RESPONSIVE TO PILOT INPUTS. FOUND THE SEAL SDR AWXA960429Battery Pack · inopPHX - FLT 2020 - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT CABIN SECTION OF EMERGENCY LGIHTS INOP AND BATTERY PACK AT L-2 DOOR NOT CHARGING. REMOVED AND REPLACED BATTERY PACK IN AFT SECTION. OPS GOOD. REMOVED AND REPLACED CHARGER AT L-2 DOOR. OPS GOOD. SDR AWXA960393Battery Pack · dischargedPHX - FLT 2020 - DURING ROUTINE MAINTENANCE CHECK, FOUND ENTRY AFT CABIN EMERGENCY LIGHTS INOP. SHOT IN WIRING KEPT FUSES IN THE CHARGER OPENING UP. DEACTIVATED SEAT ROWS AND RECONNECTED EACH SEAT INDIVIDUALLY UNTIL ROW WAS IDENTIFIED. REPAIRED WIRING CHAFESDR 96ZZZM1373Charger · inopPHX - FLT 2020 - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT CABIN SECTION OF EMERGENCY LIGHTS INOP AND BATTERY PACK AT L-2 DOOR NOT CHARGING. REMOVED AND REPLACED BATTERY PACK IN AFT SECTION. OPS GOOD. REMOVED AND REPLACED CHARGER AT L-2 DOOR. OPS GOOD. SDR AWXA960370Rt Unit · failedPHX - FLT 2610 - AIR TURNBACK - WEATHER WEAK MESSAGE ON SCREEN BUT WILL NOT PAINT BEYOND 30 MILES AND THEN RETURN IS NOT WHAT IS REALLY THERE. REMOVED AND REPLACED WEATHER RADAR R/T UNIT PER MM 34-41-00. OPS CHECK NORMAL. (M)SDR AWXA960418Battery · dischargedPHX - FLT 2611 - DURING ROUTINE MAINTENANCE CHECK, FOUND R-4 DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. CHARGED BATTERY. OPERATES GOOD. (X)SDR AWXA960271Actuator · failedPHX-ORD - AIR TURN BACK, EICAS MESSAGE GEAR DOORS AND GEAR DISAGREE DIPLAYED WITH GEAR HANDLE UP. DOOR AND GEAR AMBER LIGHTS ILLUMINATED ALL GREEN. DOWN LIGHT EXTINGUISHED WITH GEAR HANDLE OFF. RIGHT GEAR DOWN LIGHT ILLUMINATED. REMOVED AND REPLACED RIGHT SDR USAABB96017Windshield · failedDEN - FL 93 - EN ROUTE SAN AT FL 390, R1 WINDSHIELD SHATTERED. FLIGHT DIVERTED TO DEN AND LANDED WITH NO FURTHER INCIDENT. MX REPLACED THE WINDOW AND HEAT CONTROLLER, (P/N 6240664). (M)SDR USAABB96015Hp2 Duct · leakingSFO - FLT 56 - AFTER TAKEOFF FROM SFO, CREW RECEIVED OVETEMP LIGHT ON LEFT ENGINE. LIGHT EXTINGUISHED WHEN THROTTLE RETARDED. FLIGHT RETURNED TO SFO AND LANDED WITH NO FURTHER INCIDENTS. MX REPLACED THE HP2 AND P6 DUCTS DUE TO LEAKAGE. (M)SDR 96ZZZM883Hp6 Duct · leakingSFO - FLT 56 - AFTER TAKEOFF FROM SFO, CREW RECEIVED OVETEMP LIGHT ON LEFT ENGINE. LIGHT EXTINGUISHED WHEN THROTTLE RETARDED. FLIGHT RETURNED TO SFO AND LANDED WITH NO FURTHER INCIDENTS. MX REPLACED THE HP2 AND P6 DUCTS DUE TO LEAKAGE. REFERENCE USAABB96015SDR USAABB96013Actuator · failedCLT - FLT 1104 - EN ROUTE PIT/MIA, CREW RECEIVED EICAS MESSAGE: LT BLD DUCT LEAK. CREW ISOLATED THE LEAK. CREW THEN EXPERIENCED A RIGHT PACK OVERHEAT AND RECEIVED THE EICAS MESSAGE: RT PACK OFF. CREW PERFORMED AN EMERGENCY DESCENT AND DIVERTED THE FLIGHT SDR USAABB96012Duct Assembly · crackedSJU - FL 1970 - AFTER TAKEOFF, CREW REPORTED A PNEUMATIC LEAK ON THE LEFT ENGINE (EICAS MESSAGE - 'L ENG OVHT'). FLIGHT RETURNED TO SJU. MAINTENANCE CONFIRMED A BLEED PROBLEM AND TIGHTENED A CLAMP ON THE LEFT ENGINE DUCTING. FLIGHT TOOK OFF AND RETURNED A SSDR AWXA960173P1 Probe · failedPHX-JFK - LEFT ENGINE PROBE HEAT STATUS MESSAGE. FOUND BURNT PINS ON CONNECTOR D1498. REMOVED AND REPLACED P1 PROBE PER MM 73-21-04. RETERMINATED D1498. REMOVED AND REPLACED RELAYS K10478 AND K10308. PROBE LEAK CHECK GOOD. (M)SDR AWXA960172Clip · crackedFLT NR 3838 - PAE - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND FORWARD CARGO DOOR FORWARD END OF DOOR FRAME NR 3, FRAME CLIP FROM BOTTOM OF DOOR IS CRACKED IN RADIUS. REMOVED CRACKED FRAME CLIP AND FABRICATED PER SRM 51-30-01, ALODINED, PRIMED AND SDR AWXA960171Support · corrodedPAE - FLT NR 3838 - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND SUPPORT STRUCTURE T-FRAME HAS CORROSION, STATION 960, BL 0, WL 133. FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 53-40-12. (M)SDR AWXA960170Floorbeam · corrodedFLT NR 3838 - PAE - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD STATION 365, BL 0 TO RBL 60, WL 208. BLENDED CORROSION, FOUND OUT OF LIMITS. FABRICATED REPAIR CHORD AND ANGLES. ALODINED AND PRIMED PER SRM 53-00-5SDR AWXA960169Floorbeam · corrodedDURING ROUTINE SCHEDULED C-3 MX CHECK, FOUND CORROSION ON FLOORBEAM AT STATION 350, RBL 2-LBL 20, WL 208. REPAIR AREAS OF FLOORBEAM THAT ARE OUT OF LIMITS WITH REPAIR ANGLE AND FILLERS PER SRM 53-00-51. ALODINE, PRIME AND INSTALL WET WITH SEALANT. (M)SDR AWXA960168Seat Track · corrodedPAE - DLT NR 3838 - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK STATION 377, LBL 25, WL 208. REMOVED CORRODED SEAT TRACK STATION 377-428, LBL 25, WL 208 AND INSTALLED NEW PART PER SRM 53-00-52, SRM 51-20-01, SRM 51-40-08 AND SDR AWXA960167Seat Track · corrodedPAE - FLT NR 3838 - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK STATION 377, LBL 45, WL 208. REMOVED SEAT TRACK STATION 377 - STATION 428, LBL 45, WL 208 AND INSTALLED NEW PART PER SRM 53-00-52, SRM 51-20-01, SRM 51-40-08 ANDSDR AWXA960166Intercostal · corrodedPAE - FLT NR 3838 - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND CORROSION ON INTERCOSTAL STATION 350 - STATION 365, LBL 60 WL 208. REMOVED CORRODED INTERCOSTAL STATION 350-365, LBL 60, WL 208. (M)SDR AWXA960165Floor Beam · corrodedPAE - FLT 3838 - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM AT BS 350, RBL 2 - LBL 20, WL 208. PER ERR, BLENDED CORROSION ON BEAM. FABRICATED REPAIR ANGLE, ALODINED, PRIMED, AND INSTALLED PART WITH SEALANT PER ER 5-53-12-05SDR AWXA960164Seat Track · corrodedPAE - FLT 3838 - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK BS 373, RBL 25, WL 208. REMOVED CORRODED SEAT TRACK. FABRICATED AND INSTALLED SEAT TRACK IAW SRM 51-40-02. (M)SDR AWXA960162Skin · damagedPAE - FLIGHT 3838 - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND A TEMPORARY REPAIR INSTALLED AT BS 620, .5 INCH BELOW STRINGER 16L. REMOVED TEMPORARY REPAIR, FABRICATED EXTERNAL DOUBLER AND REPAIR PARTS PER ENGINEERING REPAIR NR 5-53-33-01 AND INSTASDR USAABB96008Tower Shaft Seal · failedSMF - FLT 68 - AFTER TAKEOFF FROM SFO, CREW NOTED LOSS OF OIL FROM LT ENGINE. CREW SHUT DOWN ENGINE. FLIGHT DIVERTED TO SMF AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE TOWER SHAFT SEALS. (X)SDR 96ZZZX1694Warning Light · illuminatedMIA - FLT 538 - LEFT EMERGENCY DOOR (L3) WARNING LIGHT CAME ON DURING CLIMB-OUT FROM MIA. AIRCRAFT RETURNED TO FIELD. MAINTENANCE PERFORMED DOOR FIM PROCEDURE. NO PROBLEMS WERE FOUND. DOOR WAS CHECKED OPERATIONALLY AND NO PROBLEMS WERE NOTED. AIRCRAFT WAS SDR USAABB96006Warning Light · illuminatedMIA - FLT 538 - LEFT EMERGENCY DOOR (L3) WARNING LIGHT CAME ON DURING CLIMB OUT FROM MIA. AIRCRAFT RETURNED TO FIELD. CORRECTIVE ACTION: PENDING. (X)SDR USAABB96004Battery Packs · dischargedPIT - FL 1767 - PRIOR TO DEPARTURE, EMERGENCY EXIT LIGHTS AT ROWS 22, 23 AND 25 AND R-3 AND R-4 DOORS WERE INOPERATIVE. MAINTENANCE REPLACED THE APPROPRIATE BATTERY PACKS. (M)SDR USAA960169Skin · dentedCLT - INSPECTION VISUALLY AND BY HFEC, FOUND A DENT 5.5 INCH BY 3.75 INCH BY .130 INCH DEEP IN THE FUSELAGE SKIN LOCATED AT BS 231.5, OUTBOARD CHORD ABOVE AOA VANE. REPLACED CHORD ANGLES AND REPAIRED W/SKIN FILLER AND DOUBLER AS PER EA 40596. (M)SDR USAA960168Skin · dentedCLT - INSPECTION VISUALLY FOUND A DENT 1 INCH DIAMETER BY .50 INCH DEEP (APPROXIMATELY 1.25 INCH BY .75 INCH) LOCATED AT BS 1738, S27L. INSTALLED DOUBLER AS PER USAIR EA 58015 AND BOEING SRM 53-00-01. (M)SDR USAA960167Skin · dentedCLT - INSPECTION VISUALLY FOUND A SHARP DENT 1 INCH DIAMETER .145 INCH DEEP, 3 INCHES FORWARD BS 1280 BETWEEN STRINGER 1280 BETWEEN STRINGER 24L AND STRINGER 25L. INSTALLED FLUSH PATCH REPAIR AS PER BOEING SRM 53-00-01. (M)SDR USAA960166Skin · corrosionCLT - INSPECTION VISUALLY FOUND AN EXFOLIATION LEVEL 2 CORROSION BETWEEN SKIN AND DOUBLER 4 INCHES OUTBOARD PYLON SKIN IN AREA OF HEAT SHIELD NR 2 PYLON. REPLACED PYLON SKIN OUTBOARD AS PER USAIR EA 40605, EA 40669 AND USAIR EO 05492R274. (M)SDR USAA960165Skin · corrosionCLT - INSPECTION VISUALLY FOUND EXFOLIATION LEVEL 2 CORROSION BETWEEN SKIN AND DOUBLER, 2 INCHES LOCATED INBOARD PYLON IN AREA OF HEAT SHIELD NR 2 PYLON. REPLACED PYLON SKIN INBOARD AS PER USAIR 40605 AND USAIR EO 5492R274. (M)SDR USAA960162Skin · corrodedCLT - INSPECTION VISUALLY FOUND AN 8 INCH BY 8 INCH CORROSION EXTERNAL DOUBLER NOT PER SRM LOCATED AT FS 1681.8 THROUGH 1701 BETWEEN STRINGER 17 AND STRINGER 19L. FABRICATED AND INSTALLED EXTERIOR DOUBLER AS PER USAIR EA 40578 AND BOEING SRM 53-60-10. (M)SDR USAA960010Skin · dentedCLT - INSPECTION VISUALLY AND BY HFEC FOUND AT FUSELAGE SKIN A DENT 5.5 INCH BY 3.75 INCH, .130 DEEP LOCATED AT BS 231.5, OUTBOARD CHORD ABOVE VANE. REPLACED CHORD ANGLES AND REPAIRED SKIN WITH FILLER AND DOUBLER AS PER USAIR EA NR 40596. (M)SDR USAA960009Skin · dentedCLT - INSPECTION VISUALLY FOUND A .0531 INCH DEEP DENT WITH .0065 GOUGE LOCATED AT FUSELAGE SKIN AT STRINGER 52R-55R, BETWEEN STATION 480-500. INSTALLED EXTERNAL DOUBLER AS PER USAIR EA NR 40595. (M)SDR USAA960008Skin · corrosionCLT - INSPECTION VISUALLY FOUND EXFOLIATION LEVEL 2 CORROSION BETWEEN SKIN AND DOUBLER OUTBOARD PYLON SKIN IN AREA OF HEAT SHIELD NR 1 PYLON. REPLACED SKIN NR 1 PYLON OUTBOARD SIDE PER USAIR EA NR 40605. (M)
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