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 DL757080391Skin · scratchedSCRATCH IN FUSELAGE SKIN, FS440, STR6L TO 7L. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER AND TRIPLER.SDR DL757080385Tire · blownBLOWN TIRE NR 7, REPLACED NR 7 WHEEL ASSY PER MM.SDR DL757080384Manifold · brokenRT ENG OIL QTY AT ZERO AND OIL PRESSURE DROPPING WITH OIL PRESS LIGHT FLICKERING AT CRUISE. MX FOUND THE MAIN BEARING BREATHER MANIFOLD BROKEN. REPLACED SAME, RAN ENGINE LEAK CHECKS GOOD.SDR DL757080352Skin · dentedDURING HMV, SEVERAL DENTS AND TWO EXISTING SKIN REPAIRS WERE FOUND BETWEEN STA 1621 AND STA 1661, S19R TO S23R. THE DENTS AND EXISTING REPAIR DOUBLERS WERE REMOVED AND A SINGLE REPAIR WAS INSTALLED AND APPROVED BY BOEING VIA FAA FORM 8100-9 FOR STATIC STRENGTSDR DL757080322Skin · dentedDURING HMV, THE FUSELAGE SKIN AT STA 1690 BETWEEN S-14R AND S-15R WAS FOUND DENTED. THE DENT WAS CUT OUT AND REPAIRED PER BOEING INSTRUCTIONS.SDR DL757080321Bulb · inoperativeEMERGENCY LIGHT OUTSIDE R4 DOOR INOP. RELAMPED.SDR DL757080320Connector · damagedTWO RED EMERGENCY LIGHT AT 26FED INOP. REPLACED CONNECTOR UNDER SEAT 26F, OP OK.SDR DL757080316Fan · fumesAT CRUISE, CREW HAD FUMES IN COCKPIT ELEC FUMES. CREW DIVERTED INTO NAS, DECLARED EMERGENCY. EICAS MSG EQUIP COOLING FAN AND ECS MSG FWD EQUIP SUP FAN 1. REPLACED SUPPLY FAN NR 1, OPS CHECKED OK PER MM. REMOVED MCO A PLAC.SDR DL757080291Skin · misrepairedDURING HMV AT SAA, THE FUSELAGE SKIN AT STA 628 AND S-25L WAS FOUND WITH AN EXISTING REPAIR THAT DID NOT MEET SRM REQUIREMENTS. THE REPAIR DOUBLER WAS REMOVED AND A BOEING DESIGNED REPAIR WAS INSTALLED.SDR DL757080285Fitting · damagedDURING HMV AT SAA, TWO OF THE NR 1 ENGINE PYLON SIDE LOAD FITTING FASTENER HOLES WERE OVERSIZED TO CLEAN UP TOOLING DAMAGE. THE HOLES WERE REAMED UP TO TRANSITION FIT HOLE SIZES FOR OVERSIZE FASTENERS APPROVED BY BOEING.SDR DL757080287Skin · damagedTOOLING MARKS WERE FOUND AT THE AIRPHONE ANTENNA SKIN AT FS 1515 BETWEEN S-28R AND S-29R. THE ANTENNA IS NO LONGER IN USE. BECAUSE THE ANTENNA HAD BEEN SUBJECT TO AN STC, THE ANTENNA WAS REMOVED, AND THE FASTENER PATTERN CUTOUT. AN EXTERNAL REPAIR DOUBLER SDR DL757080280Control Panel · malfunctionedCREW REPORTS BOTH PACKS FAILED AT FL 40. PERFORMED EMERGENCY DESCENT. MASKED DROPPED AND WERE USED BY APPROXIMATELY 78 PAX AND CREW. REPLACED COCKPIT CABIN CONTROL PANEL FOR MANUAL CONTROL PROBLEM. PERFORMED BITE ON BOTH L/AUTO PRESSURE CONTROLLERS OK. PRSDR DL757080258Skin · damagedDURING HMV AT SAA, A CREASE WAS FOUND IN THE FUSELAGE SKIN AT STA 1420, S-28R. THE CREASE EXCEEDED THE ALLOWABLE SRM LIMIT. A REPAIR WAS ACCOMPLISHED PER BOEING INSTRUCTIONS. STARTING AT 12,000 CYCLES AFTER REPAIR INSTALLATION AND EVERY 12,000 CYCLES THEREASDR DL757080226Seat Track · crackedCAPT SEAT LOOSE DURING FLIGHT. FOUND AFT LEFT SEAT TRACK STOP FITTING CRACKED REPLACED SEAT TRACK.SDR DL757080225Line · leakingLEFT HYD FAILURE AFTER T/O STT, AA MTC FOUND THE RT RETRACT ACT PRESSURE LINE LEAKING. AA MTC REPLACED SAME LEAK CHECKED GOOD. AA MTC ALSO CHECKED THE CASE DRAIN FILTERS AND DIFFERENTIAL PRESSURE POP OUTS ALL OK.SDR DL757080335Gate · corrodedFOUND CORROSION ON LOWER GATE OF L2 DOOR. REPLACED GATE IAW MM 52-11-38.SDR DL757080214Slide · unwanted deployR-4 DOOR WAS IN THE ARMED POSTION CABIN SERVICE OPENED DOOR FROM OUTSIDE AND BLEW THE DOOR ASSIST BOTTLE AND DROPPED THE SLIDE ONTO THE TRUCK. THE SLIDE DID NOT FULLY DEPLOY BECAUSE THE TRUCK PREVENTED THE SLIDE FROM DROPPING ENOUGH TO DEPLOY.SDR DL757080205Bulb · inoperativeDURING A SVC CK AD 5 FOUND EXTERIOR EMERGENCY LIGHTS INOP AT R-2 DOOR - 4L DOOR - 4R DOOR, AND LT FUSELAGE BEHIND WING AREA INOP. RELAMPEDSDR DL757080195Skin · puncturedFUSELAGE SKIN PUNCTURED AFT OF STA 620 ABOVE STER 16L. ADJACENT SKIN REPAIR REMOVED AND BOTH CUTOUTS REPAIR WITH A DOUBLER.SDR DL757080332Doubler · corrodedCORROSION ON TRANSITION PANEL SPLICE DOUBLER STATION 1530 LT SIDE IS OUT OF LIMITS. REPAIRED DOUBLER IAW SRM 51-40-05 AND SRM 51-20-01.SDR DL757080183Filter · unknownAFTER TAKEOFF, THE LEFT ENGINE OIL PRESS FLUX TO YELLOW BAND, THEN OIL QTY WENT TO ZERO. OIL PRESS THEN WENT TO RED. CREW THEN SHUT ENGINE DOWN. FOUND SCAVENGE LINE CHIP DETECTOR LAYING IN COWL. INSP CHIP DET POP OUT CHK VLV. FOUND SMALL PIECE OF SAFETY SDR DL757080337Stringer · corrodedSTRINGER 520R REPAIR SPLICE AT STA 1644-1654 IS CORRODED SEVERAL PLACES WITH A MISDRILLED HOLE. FABRICATED SPLICE IAW SRM 51-10-02.SDR DL757080340Panel · corrodedCORROSION EXIST ON FWD CARGO RT CATWALK PANEL STA 620 RBL 29. REPLACED WITH FABRICATED PANEL IAW SRM 51-40-02.SDR DL757080351Slide · no testRIGHT OFF WING SLIDE FAILED OPS TEST FOR MANUAL DEPLOYMENT OF CARRIER. READJUSTED CARRIER HOOK LOCK AND PERFORMED OPS TEST FOR MANUAL DEPLOYMENT OF CARRIER IAW MM 25-65-08.SDR DL757080350Floor Panel · corrodedFWD CARGO FLOOR PANEL 121BF HAS CORROSION ON UPPER AND LOWER SURFACE. FABRICATED FLOOR PANEL IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-40-02.SDR DL757080347Floor Support · corrodedCORROSION ON FLOOR SUPPORT AFT CABIN STA 1650-1670 RBL 60. REMOVED AND REPLACED SUPPORT IAW SRM 51-40-02.SDR DL757080345Slide · no testLEFT OFF WING SLIDE FAILED AMNUAL BACK-UP SYSTEM TEST. REPLACED BOTTLE BACK-UP CABLE IAW MM 25-65-06.SDR DL757080343Floor Panel · corrodedAFT CARGO FLOOR PANEL 161AF HAS CORROSION AND REPAIR DOUBLER BUCKLED. FABRICATED AND INSTALLED FLOOR PANEL IAW 53-60-53.SDR DL757080342Floor Panel · corrodedAFT CARGO FLOOR PANEL 153AF HAS CORROSION. FABRICATED FLOOR PANEL IAW SRM 53-60-53 FIG 1 AND INSTALLED.SDR DL757080341Floorbeam · damagedMAIN CABIN FLOOR SUPPORT STA 329 RBL 23 HAS ELONGATED FASTENER HOLE. REFABRICATED FLOOR SUPPORT IAW DWGJ141N5150.SDR DL757080336Floor Panel · corrodedAFT CARGO PANEL 153CF CORRODED, PUNCTURED. FABRICATED PANEL IAW SRM 53-60-53.SDR DL757080331Sill · corrodedCORROSION AROUND SEVERAL FASTENER HOLES AT AFT CARGO ENTRY DOOR LOWER SILL UPPER SURFACE. REMOVED CORR IAW SRM 51-10-02 AT AFT CARGO ENTRY DOOR LOWER SILL "T" CHORD. INSTALLED "T" CHORD IAW SRM 51-40-02.SDR DL757080344Floorbeam · corrodedCORROSION ON MAIN CABIN FLOORBEAM STA 1640 RBL 2. REMOVED DAMAGE IAW SRM 53-00-51. FABRICATED AND INSTALLED BEAM IAW SRM 53-00-51.SDR DL757080349Intercostal · corrodedAFT CARGO PIT WEB INTERCOSTAL BETWEEN STA 1480-1500 LBL 27 CORRODED. FABRICATED NEW INTERCOSTAL IAW SRM 53-60-04 AND INSTALLED IAW SRM 51-40-02.SDR DL757080339Structure · corrodedAFT CARGO PIT BS 1480, LBL 29; AREA CORRODED. REMOVED CORROSION IAW SRM 51-40-02, MEASURED AREA IAW NDTM PT 4, 51-00-00. CHECKED GOOD. TREATED AND PRIMED AREA IAW SRM 51-00-01.SDR DL757080338Frame · corrodedSURFACE CORROSION ON FRAME AT FS 690 RBL 13. FABRICATED "U" CHANNEL IAW B757 DRAWING 453N1853 AND SRM 51-70-11. INSTALLED IAW SRM 51-40-02.SDR DL757080334Floor Panel · crackedFWD CARGO FLOOR PANEL 121BF CORRODED UPPER AND LOWER SURFACES AND CRACKED IN CUTOUT. REPAIRED IAW SRM 53-30-53 FIG/SHT 7 AND SRM 51-20-01.SDR DL757080333Splice · corrodedAFT CARGO PIT-STA 1500, LBL 28 HAS SEVERE CORROSION. REPAIRED IAW SRM 53-00-03 FIG 201 AND DRAWING NR 146N3110.SDR DL757080156Coffeemaker · smokeAT CRUISE ALT 39000, FLT ATTENDANTS REPORTED SMOKE IN THE WASTE CAN AREA OF THE REAR GALLEY. REPORTED NO VISIBLE FLAMES. MADE AN EMERGENCY LANDING AT BWI. UPON ARRIVAL AT THE GATE AN INSPECTION OF THE TRASH CAN REVEALED A COFFEE GROUND BAG HAD IGNITED. FIRSDR DL757080348Floor Support · corrodedCORROSION ON FLOOR SUPPORT AFT CABIN STA 1650-1670 RBL 60. FABRICATED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02.SDR DL757080346Seat Track · corrodedMAIN CABIN STA 365-440; SEAT TRACK AT RBL 24 HAS SECTION OF SEVERE COROSION. FABRICATED AND REPLACED SEAT TRACK SECTION IAW SRM 53-10-52.SDR DL757080097Fan · odorODOR IN AREA 2C/D 3C/D AND ODOR STOPPED WHEN RECIRC FANS OFF CAME BACK WHEN TURNED ON. ALSO ODOR IN ROW 24 AREA. REMOVED AND REPLACED LT RECIRC FAN IAW MM.SDR DL757080093Oil System · lowON APPROACH INTO LGA AS WE WERE CONFIG FROM 20 TO 25 FLAPS, TE FLAP DISAGREE EICAS MSG. PERFORMED NON-NORMAL CHECKLIST AND AFTER SELECTING 20 WITH ALT SW POSITION AND ALTN SELECTED FOR POWER TE CAUTION LIGHT WENT OUT. LANDED AT JFK WITH 20 FLAPS. T/S PER FSDR DL757080092Bolt · looseWHILE WORKING ELEVATOR ASSY MESSAGE, FOUND APU DOOR HINGE BOLT LAYING ON TOP OF HORIZONTAL STABILIZER. REINSTALLED BOLT IN DOOR HINGE.SDR DL757080071Unknown · unknownPER THE CREW, AT CRUISE ALTITUDE, 380 LEFT ENGINE ROLLED BACK AND QUIT. CREW TRIED TO IN-FLIGHT START WITH NO JOY. REPLACED FUEL CONTROL AND FUEL PUMP PER MM. REPLACED EEC PE MM. INSPECTED PMG WIRING AND CONNECTORS. INSPECTED AND BLEW OUT PB SENSE LINE. SDR DL757080024Skin · puncturedFUSELAGE SKIN PUNCTURED BY JETWAY AT STA 609-619 BETWEEN STR 17L AND 18L. THE SKIN WAS ALSO FOUND DENTED AT STA 609 BETWEEN STR 15L AND 16L, STA 613 BETWEEN S16L AND 17L AND AT STA 609-619 AT STR 19L. ALL DAMAGE LOCATIONS WERE CUTOUT AND A SKIN REPAIR WAS INSDR DL757080014Skin · corrodedFUSELAGE SKIN, FRAME AND STRINGER FOUND CORRODED AT STA 1440 STR 28R. A SKIN DENT WAS ALSO FOUND AT STA 1425. DAMAGE WAS CUTOUT, STRINGER AND BEAR STRAP WERE SPLICED AND SKIN REPAIRS WERE INSTALLED.SDR DL757080013Warning Light · false activationT/E FLAP DISAGREE MSG ACCOMPLISHED 20 DEGREE FLAP LANDING IAW QRH. CK'D FSEU NO FAULTS. RAN FLAPS/SLATS SEVERAL TIMES ALL OPS NML.PER MCC CK'D AND LUBED ALL TRANSMISSIONS AND TORQUE LIMITERS. FOUND BOTH INBOARD TRANSMISSIONS LOW SERVICED FULL. LUBED ALL JASDR DL757080006Sill · crackedFUSELAGE/C2 DOOR OPENING/LOWER SILL BEAM/INNER CAP, CRACKED FLANGE REPAIR. THE INNER CHORD OF THE LOWER SILL BEAM AT THE C2 DOOR OPENING WAS DAMAGED BY CARGO LOADING EQUIPMENT RESULTING IN A ONE FOOT TEAR IN THE OUTER FLANGE OF THE CHORD. THE REPAIR CONSISTSSDR DL757080001Nut · wornAT LANDING WHEN FLAPS LEVER PLACED TO 5, GOT TE FLAP DISAGREE CAUTION AND FLAPS LOCKED AT 1. FOUND RT INBD FLAP OUTBD JACKSCREW DISCONNECTED FROM TRANSMISSION AT U JOINT. U JOINT PARTS FOUND IN FAIRING. REPLACED TRANSMISSION, U JOINT PARTS, AND DAMAGED FAIR
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