Boeing 757-232
Service difficulty reports · 15,843
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 = '757232' 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 = '757232' 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 DU4R2006307Panel · corrodedCORROSION AND ON AFT CARGO COMPARTMENT TRANSITION PANEL BS 1540 - 1640. REPAIRED BY REMOVING AND REPLACING WITH P/N 146N5431-41IAW B757 SRM 51-40-02.SDR DU4R2006303Floor Support · corrodedCORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT BS 1440 - 1500 LBL 7. REPAIRED BY CUTTING OUT CORRODED AREA OF FLOOR SUPPORT BS 1440 - 1500 LBL 7. FABRICATED AND INSTALLED REPAIR 8.4" BY 7" BY 1" BY 1.4" FROM 7075-T6 .080 IAW B757 SRM 51-70-11.SDR DU4R2006305Floor Support · corrodedCORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT BS 1470 LBL 11. REPAIRED BY CUTTING OUT CORRODED AREA, FABRICATED AND INSTALLED REPAIR 9-1/8" BY 8-1/4" BY 1.4" FROM 7075-T6 .080 IAW B757 SRM 51-70-11.SDR DU4R2006306Intercostal · corrodedCORROSION AND ON AFT CARGO COMPARTMENT LOWER ANGLE OF VERTICAL INTERCOSTAL BS 1400 - 1420 S-28L. REPAIRED BY FABRICATING AND INSTALLING REPAIR 16.25" BY 3.0" FROM 7075-T6 .040 IAW B757 SRM 51-70-13.SDR DL757060182Scavenge Pump · failedDURING FLT AT 41,000 FT LEFT ENGINE OIL TEMP WAS IN AMBER BAND. OIL TEMP THEN WENT TO RED BAND, FOLLOWED ENGINE SHUTDOWN LIST PER QRH. DIVERTED FLT TO LAS. REPLACED SCAVENGE PUMP AND INTERNAL LUBE PUMP. REPLACED EJECTOR PUMP. RAN ENGINE AT T/O PER PFHB. SDR DU4R2006301Panel · corrodedCORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BS 1410 - 1530 LT. REPAIRED CORRODED TRANSITION PANEL BY REMOVING AND REPLACING TRANSITION PANEL P/N 654N0244-406 IAW B757 SRM 51-40-02.SDR DU4R2006300Floor Support · corrodedCORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT WEB UPPER SURFACE BS 1340 LBL-9. REPAIRED CORROSION BY FABRICATING AND INSTALLING WEB REPAIR 20" BY 2.5" FROM 7075-T6 .040 IAW B757 SRM 53-60-04.SDR DL757060175Unknown · unknownRUBBER/ELECTRIC SMELL WHILE AT ALTITUDE COMING FROM MID CABIN AREA ROWS 19 - 27. RAN SMOKE OR FUMES OR FIRE ELECTRICAL CHECKLIST SMELL DID NOT DISSIPATE UNTIL LATE IN THE DESCENT FOR EMERGENCY DIVERT. MTC REMOVED CEILING PANELS FROM MID AREA INSPECTED CABIN SDR DL75K060178Relay · malfunctionedON LIFTOFF LOST 1 PHASE L AC BUSS, RETURN TO LAX. INSPECTED TB5003 AND TB5012 CHECKED OK. FOUND C/B C313 ON P31 POPPED FOR L BUSS SECT 1, REPLACED C/B RAN BOTH ENGS C/B C313, OPS CHECKED NORMAL. CHECKED OUT WIRES FROM C313 TO TB 5003 AND TB5012 FOR CORRECT SDR DL757060171Control Module · inoperativeLEFT MAIN SHOWED UNSAFE AFTER DROPPING GEAR. AFTER COMPLETE WITH PROCEDURE LEFT DOWN AND LOCKED WITH JUST LEFT SIDE LIGHT MAIN GEAR ON. ALL LIGHTS TESTED GOOD. NEVER GOT LIGHT ON THE GEAR HANDLE OR AN EICAS THAT THE GEAR DISAGREE. REPLACED LANDING GEAR CONSDR DU4R2006294Support · corrodedLOWER WING TO BODY FAIRING STRUCTURE CORRODED RT BS 880. REMOVED CORRODED T-ANGLE, FABRICATED AND INSTALLED REPAIR T-ANGLE 36.800" FROM BAC1505-101029 IAW B757 SRM 51-40-02, 51-20-01, AMM 51-00-00-01 AND DPS 900-2 NR 5.SDR DU4R2006290Frame · dentedAFT PIT STA 1320 S-25R - S-26R FRAME DENTED. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTALLED FRAME REPAIR 26 X 5 INCHES FROM 7075-T6. 071 IAW B757 SRM 51-70-11 FIG 1 AND 51-40-02.SDR DU4R2006287Frame · bentFRAME AS STA 1440 , S-26L IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 10.5 X 2.5 INCHES FROM 7075-T6 .063 AND CLIP P/N 3.30 X 1.75 INCHES FROM BAC1518-769 IAW B757 SRM 51-70-11, 51-20-01 AND 51-40-02.SDR DU4R2006292Floor Panel · corrodedCORROSION ON FWD PIT FLOOR PANEL LT NR 5 BS 750 - 845. REMOVED CORROSION IAW B757 SRM 51-10-02 FOUND L00 PERCENT MATERIAL LOSS IAW B757 SRM 53-00-53. FABRICATED AND INSTALLED REPAIR FLOOR PANEL 94 X 18 INCHES FROM 2024-T3 .020 IAW B757 SRM 53-30-53 AND 51-20SDR DU4R2006282Frame · bentFRAME AS STA 1300, S-26L IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 11.40 X 2.50 INCHES FROM 7075-T6 .071 IAW B757 SRM 51-70-11 AND 51-20-1.SDR DU4R2006286Frame · bentFRAME AS STA 1240, S-26R IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 10.4 X 2.5 INCHES FROM 7075-T6 .080 IAW B757 SRM 51-70-11, 51-20-01 AND 51-40-02.SDR DU4R2006285Frame · bentFRAME AS STA 1480, S-26L IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 10 X 2.4 INCHES FROM 7075-T6 .063 IAW B757 SRM 51-70-11, 51-20-01 AND 51-40-02.SDR DU4R2006284Frame · bentFRAME AS STA 1320, S-26R IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 13 X 4 FROM 7075-T6 .071 AND CLIP P/N 140N2063-56 IAW B757 SRM 51-70-11 AND 51-40-02.SDR DU4R2006283Frame · bentFRAME AS STA 1340, S-26R IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 13 X 4 INCHES FROM 7075-T6 .071 AND CLIP IAW B757 SRM 51-70-11 AND 51-40-02.SDR DU4R2006278Skin · dentedC-2 DOOR INTERNAL SKIN HAS 2EA DENTS (WITH CREASE MARKS) AT STA 1400. MEASURED DENTS A=.400", Y= .029 A/Y RATIO 13. FABRICATED AND INSTALLED INTERNAL FLUSH REPAIR 3.8 DIAMETER FROM 2024-T3 .063 IAW B757 SRM 52-30-01 FIG 201.SDR DU4R2006279Skin · crackedC-2 DOOR INTERNAL SKIN LWR AFT CORNER HAS CRACK STA 1440. CUT OUT EDGE CRACK ON C-2 DOOR EXTERNAL SKIN AT LOWER AFT CORNER STA 1140. FOUND WITHIN LIMITS IAW B757 SRM 52-30-01 DETAIL IV. HFEC PER NTM PT6 51-00-19, NO CRACK INDICATION. TREATED IAW B757 SRM 5SDR DUR42006293Floor Panel · corrodedFWD CARGO COMPT PIT FLOOR PANEL RT NR 5 CORRODED AT BS 750 - 845. REMOVED CORROSION IAW B757 SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-53. FABRICATED AND INSTALLED REPAIR FLOOR PANEL 94 X 18 INCHES FROM 2024-T3 .020 IAW B757 SRM 51-40-05 ANSDR DU4R2006289Seat Track · gougedMAIN CABIN SEAT TRACK FROM STA 760 TO STA 880 LBL 45 INNER SURFACE HAS MULTIPLE GOUGES. REMOVED GOUGED SECTIONOF SEAT TRACK. CUT, DRILLED UP AND INSTALLED NEW SEAT TRACK SECTION 10 X 1.5 INCH FROM BAC1520-792 IAW B757 SRM 51-20-01, 51-40-2, 51-40-05, 51-40-0SDR DU4R2006281Frame · bentFRAME AS STA 1400, S-25L IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 22.5 X 3.75 INCHES FROM 7075-T6 .063, AND 2EA CLIPS P/N 140N2063-56 IAW B757 SRM 51-70-11 FIG 1, 51-20-2, 51-40-02.SDR DU4R2006280Frame · bentFRAME AS STA 1420, S-26L IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 11.625 X 3.75 INCHES FROM 7075-T6 .063, FILLER AND CLIP P/N 140N2063-56 IAW B757 SRM 51-70-11 FIG 1, 51-20-2, 51-40-02.SDR DL757060148Circuit Breaker · faultyEMERGENCY LIGHTS ALONG MAIN AISLE FLOOR ILLUMINATED WITH COCKPIT SW IN ARMED POS AND FLT ATTENDANT PANEL SW IN NORMAL POS. REPLACED C/B TO CHARGER.SDR DU4R2006291Floor Support · dentedFWD CARGO FLOOR SUPPORT HAS DENTS BETWEEN STA 580 & 600 AT LBL 2. CUT OUT DENTED SECTION. FABRICATED AND INSTALLED REPAIR 40.80 INCHES AND 2 EA SPLICES 10.00 X 1.10 X .75 AND 10.0 X 1.10 X .65 FROM BAC1517-2226 IAW B757 SRM 53-00-53, 51-70-11, 51-70-12, 51-2SDR DL757060138Slide · out of positionL1 ESCAPE SLIDE FELL OUT WHEN DOOR WAS OPENED. REPLACED L1 DOOR SLIDE PER M/M. SAFETY PIN REMOVED AND STOWED.SDR DL757060136Engine · fodDURING TAKEOFF SUSPECT LEFT ENGINE INGESTED FOD. ENGINE DID HAVE A COMPRESSOR STALL WITH AN INDUCED YAW AFFECT. EGT STARTED CLIMBING. FLT CREW FOLLOWED QRH PROCEDURES AND SHUT DOWN THE ENGINE AND RETURNED TO LIR. REPLACED ENGINE.SDR DL75K060126Door Seal · defectiveLOSS OF PRESSURIZATION AT FL380. CABIN ALT INDICATED 10K FT DIFF PRESS APPROX 6.5 PSID. MODE SELECTED IN AUTO 1 WITH NO AUTO INOP LIGHT. MANUAL AND AUTO 2 WORKED AT 10K FT. ON AFT CARGO DOOR, REPLACED MISSING UPPER AFT STOP AND DOOR SEAL.SDR DL757060125Relief Valve · malfunctionedCREW ON FLT 1148/12 SLC-BWI RADIOED THAT AT FL340 CABIN ALTITUDE WARNING SOUNDED AND CREW REALIZED CABIN ALTITUDE WAS 11K AND CLIMBING AT 1000FT/MIN. REPLACED LOWER PRESSURE RELIEF VALVE.SDR DU4R2006288Skin · dentedDENT LEFT SIDE FUSELAGE SKIN 7 FEET FWD OF L-2 DOOR. CUT OUT DENTED PORTION. FABRICATED AND INSTALLED REPAIR DOUBLER 9.5 X 9.5 INCHES FROM 2024-T3 .020 CLAD AND ID TAG IAW B757 SRM 53-00-01, 51-20-01, 51-40-02 AND 51-40-08 AND PROCESS STANDARD 900-5-1, NR 4.SDR DU4R2006275Floorbeam · corrodedCORROSION ON FLOORBEAM FWD SIDE AT BS 1640 RBL 14 TO LBL 14. REPAIRED FLOORBEAM BY CUTTING OUT CORRODED SECTION OF FLOORBEAM. FABRICATED AND INSTALLED REPAIR SECTION 57-7/8" X 2" X 46-1/4" FROM BAC1505-100617, 2 EA REINFORCEMENT STRAPS 11" X 1" AND 10-1/2" XSDR DL75K060109Panel · faultyINFLIGHT SLIGHT ELECTRICAL BURNING ODOR DETECTED -NO SMOKE SEEN. ANTI COLLISION RED LT CB POPPED. TURNED RED ANTI COLLISION SWITCH OFF, ODOR WENT AWAY. FOUND BLACK BURN MARKS ON BACK OF LIGHT PANEL ON J2 CONNECTION ON BACKSHELL ON PANEL. REPLACED PANEL. CHESDR DU4R2006277Seat Track · damagedMID CABIN BS 905 RBL 23 WL 208 SEAT TRACK HAS ELONGATED HOLE WHERE DOME NUT IS LOCATED. REPAIRED ELONGATED HOLE BY INSTALLING A FREEZE PLUG IAW DELTA B757 SRM 51-20-07 AS DIRECTED BY TIMCO RFTS 60006.SDR DU4R2006276Skin · damagedAFT CARGO DOOR HAS 2 EA NOTCHES ON LOWER AFT SIDE. REPAIRED AFT CARGO DOOR BY CUTTING OUT NOTCHED AREA, FABRICATING AND INSTALLING DOUBLER 7.3 X 7 INCHES FROM 2024-T3 .071 AND FILLER REPAIR IAW DELTA B757 SRM 52-30-01 FIG 206.SDR DL757060104Engine · malfunctionedAT FLT LVL 360 LOUD BANG FROM LEFT ENGINE. ENGINE SHUT ITSELF DOWN. PASSENGERS ON LEFT SIDE OF A/C SAW FLAMES FROM TAILPIPE OF LEFT ENGINE. REPLACED ENGINE.SDR DL75K060100Bolt · looseA 1L JUMPSEAT BELT CAME UNBOLTED DURING LANDING. SECURED LOOSE FASTENER, OPS OK.SDR DL757060083Hose · rupturedATB ON DEPARTURE LOST ALL LEFT HYD SYS FLUID. RETURNED TO AIRPORT. REPLACED RUPTURED HOSE.SDR DL757090117Torque Tube · corrodedRT INBD MAIN FLAP FAIL SAFE TORQUE TUBE HAS CORROSION ON INSIDE AREA, C/W AT SAA SAT ON N/R 104719 SAA JOB 82069520001.SDR DL757060078Fitting · corrodedMLG FORWARD TRUNNION ATTACH FITTINGS HAVE CORROSION PRESENT. REMOVED CORROSION BY OVERSIZING BORES AND INSTALLING OVERSIZED BUSHINGS.SDR DU4R2006256Frame · puncturedCIRCUMFERENTIAL FRAME AT BS 1460 JUST ABOVE STRINGER 26L HAS A PUNCTURE. FABRICATED AND INSTALLED REPAIR ANGLE IAW B757 SRM 53-00-07 FIG 201.SDR DL757060066Bulb · inoperativeEMERGENCY AISLE SIDE PATH LIGHTS INOP (2EA) SEAT ROW 21 AND AFT LAV FLOOR LEVEL. RELAMPED LIGHT.SDR DL757060061Skin · dentedTHE FUSELAGE SKIN WAS STRUCK BY GSE AND SUFFERED DENTS AND GOUGES BETWEEN STR 27L AND 27R AT BS 570 - 605. THE DAMAGED SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED PER ER/A 452483-14.SDR DL75K060055Windshield · failedCAPTS L1 WINDOW SHATTERED AT ALTITUDE. AIRCRAFT REMAINED PRESSURIZED. REPLACED L1 WINDOW PER MM. PRESSURIZED A/C. ALL CHECKS OK.SDR DL75K060056Windscreen · failedAIRCRAFT DIVERTED OFF FLT 2009/15 TPA-BDL DUE TO REPORT OF SMOKE/FIRE IN COCKPIT LOWER LEFT CORNER OF CAPTS WINDSHIELD. REPLACED WINDSHIELD.SDR DL75K060031Line · crackedCREW REPORTS ALL NORMAL AT CRUISE AND SUDDENLY OIL QTY AND OIL PRESSURE WENT TO ZERO. ALSO, LEFT ENGINE LOW OIL PRESS INDICATIONS ILLUM. CREW WAS GIVEN IMMEDIATE HANDLING INTO IAH SO CREW REPORTS ENGINE WINDMILLED FOR 10-12 MINUTES MAX. CONTRACT MTC NOW REPSDR DL75K060015Fcu · inoperativeI/R ON TAKEOFF ROLL AT 100+ KNOTS LOUD BANG FOLLOWED BY AC JOLT AND RT ENGINE FAILURE TAKEOFF REJECTED. RETURNED TO GATE. FOUND STATUS MESSAGE AOX OR FUEL CONTROL/EEC SVA OR FUEL CONTROL/EEC LCC/EEC SECONDARY FUEL CONTROL 351-27 AND SECONDARY 351-23. REPLACSDR DL757060012Brake Assy · failedNR 3 BRAKE ASSY FAILED, STATORS CAME FREE. REPLACED SAME.SDR DL757060010Engine · failedCREW SHUT ENGINE DOWN IN FLIGHT. EICAS L ENG STATOR, ENG FAILED W/ PWR REDUCTION. REPLACED STATOR VANE ACTUATOR.
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