Boeing 757-222
Service difficulty reports · 15,539
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 = '757222' 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 = '757222' 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 FDEA201407121722Skin · scratchedFUSELAGE EXTERIOR SKIN RT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND A SCRATCH AT BS 560 - 580 BETWEEN STRINGER 26 - 27. SCRATCH REMOVED BY HAND CLEAN AND TREATED PER SRM 51-10-02 AND 51-20-01 REV 111. REPAIR CLASSIFIED AS MINOR.SDR FDEA201407121728Skin · scratchedFUSELAGE EXTERIOR SKIN RT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND SCRATCH AT BS 600 - 620 BETWEEN STRINGER 26 - 27. SCRATCH REMOVED BY HAND CLEAN AND TREATED PER SRM 51-10-02 AND 51-20-01 REV 111. REPAIR CLASSIFIED MINOR.SDR FDEA201407121727Skin · scratchedFUSELAGE EXTERIOR SKIN RT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND SCRATCH AT BS 600 -620 BETWEEN STRINGER 27 - BL0. SCRATCHES REMOVED BY HAND CLEAN AND TREATED PER SRM 51-10-02 REV 111 AND 51-20-01 REV 111. REPAIR CLASSIFIED MINOR.SDR FDEA201407121726Skin · dentedFUSELAGE EXTERIOR SKIN RT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND SCRATCH WITH DENT AT BS 600 - 620 BETWEEN STRINGER 26 - 27. SCRATCH WITH DENT REMOVED BY HAND CLEAN AND TREATED PER SRM 51-10-01 AND 51-20-01 REV 111. REPAIR CLASSIFIED MINOR.SDR FDEA201407121725Skin · scratchedFUSELAGE EXTERIOR SKIN RT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND A SCRATCH AT BS 580 - 600 BETWEEN STRINGER 27 - 28. SCRATCH REMOVED BY HAND CLEAN AND TREATED PER SRM 51-10-02 AND 51-20-01 REV 111. REPAIR CLASSIFIED MINOR.SDR FDEA201407121724Skin · scratchedFUSELAGE EXTERIOR SKIN LT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND A SCRATCH AT BS 560 - 580 BETWEEN STRINGER 28 - BL0. SCRATCH REMOVED BY HAND CLEAN AND TREATED PER SRM 51-10-02 AND 51-20-01 REV 111. REPAIR CLASSIFIED MINOR.SDR FDEA201407121723Skin · scratchedFUSELAGE EXTERIOR SKIN RT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND A SCRATCH AT BS 560 - 580 BETWEEN STRINGER 26 - 27. SCRATCH REMOVED BY HAND CLEAN AND TREATED PER SRM 51-10-02 AND 51-20-01 REV 111. REPAIR CLASSIFIED MINOR.SDR FDEA201407121741Skin · damagedEXISTING REPAIR FINDINGS. FUSELAGE EXTERIOR SKIN THERE IS DOME NUT RIVET HOLE ENLARGED AT STATION 610, STRINGER 28L - 28R, FOR CTR RA RECEIVER ANTENNA. ACCOMPLISH NEW REPAIR ON FUSELAGE SKIN BS 577. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201407111713Skin · scratchedFUSELAGE EXTERIOR SKIN RT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND A SCRATCH AT BS 560 - 580 BETWEEN STRINGER 26 - 27. ACCOMPLISH NEW REPAIR ON FUSELAGE SKIN BS 577. REPAIR CLASSIFIED AS MAJORSDR FDEA201407111710Skin · scratchedFUSELAGE EXTERIOR SKIN RT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND A SCRATCH AT BS 560 - 580 BETWEEN STRINGER 26 -27. ACCOMPLISH NEW REPAIR ON FUSELAGE SKIN BS 577. REPAIR CLASSIFIED AS MAJORSDR FDEA201407111709Skin · scratchedFUSELAGE EXTERIOR SKIN RT SIDE ADJACENT TO EXISTING REPAIR. FOUND SCRATCH AT BS 560 - 580 BETWEEN STRINGER 26 - 27. ACCOMPLISH NEW REPAIR ON FUSELAGE SKIN BS 577. REPAIR CLASSIFIED AS MAJORSDR FDEA201407111706Tee Fitting · wornWHILE REMOVING LT STUB SNRM N00618 FOUND TEE WITH WORN HOLE AT THE WING TO BODY STRUCTURE AT STATION 984, STRINGER 17L. SUPPORT TEE REMOVED & NEW FABRICATED SUPPORT TEE FABRICATED PER BOEING DRAWING 149N7210 SHT 5 REV B. REPAIR CLASSIFIED AS MAJORSDR FDEA201407111698Skin · scratchedFUSELAGE EXTERIOR SKIN RT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND NUMEROUS NICKS & SMALL SCRATCHES AT BS 580 - 600 STRINGER 28 - BL0. NUMEROUS NICKS AND SMALL SCRATCHES REMOVED BY HANDCLEAN AND TREATED PER SRM 51-10-02 AND 51-20-01 REV 111. REPAIRSDR FDEA201407111697Skin · scratchedFUSELAGE EXTERIOR SKIN RT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND NUMEROUS NICKS & SMALL SCRATCHES AT BS 580 - 600 BETWEEN STRINGER 26 - 28. NUMEROUS NICKS AND SMALL SCRATCHES REMOVED BY HANDCLEAN AND TREATED PER 51-10-02 REV 111 AND 51-20-01 REV 1SDR FDEA201407111695Skin · scratchedFUSELAGE EXTERIOR SKIN RT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND NUMEROUS NICKS & SMALL SCRATCHES AT BS 560 - 580 BETWEEN STRINGER 28 - BL0. REMOVED BY HANDCLEAN AND TREATED PER SRM 51-10-02 AND 51-20-01 REV 111. REPAIR CLASSIFIED AS MINOR.SDR FDEA201407111694Skin · scratchedFUSELAGE EXTERIOR SKIN RT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND NUMEROUS NICKS & SMALL SCRATCHES AT BS 560 - 580 BETWEEN STRINGER 26 - 28. ACCOMPLISH NEW REPAIR ON FUSELAGE SKIN BS 577. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201407111712Skin · scratchedFUSELAGE EXISTING SKIN RT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND A SCRATCH AT BS 580 - 600 BETWEEN STRINGER 27 - 28. SCRATCH REMOVED BY HAND CLEAN AND TREATED AS PER SRM 51-10-02 AND 51-20-01 REV 111. REPAIR CLASSIFIED MINOR.SDR FDEA201407111711Skin · scratchedFUSELAGE EXTERIOR SKIN RT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND A SCRATCH AT BS 580 - 600 BETWEEN STRINGER 26 - 27. SCRATCH AT STA 580-600 BETWEEN STR 26R-27R REMOVED BY HAND CLEAN AND TREATED PER SRM 51-20-01 AND 51-10-02 REV 111. REPAIR CLASSISDR FDEA201407111708Skin · scratchedFUSELAGE EXTERIOR SKIN LT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND NUMEROUS NICKS & SMALL SCRATCHES AT BS 580 - 600 BETWEEN STRINGER 28 - BL 0. NUMEROUS NICKS AND SMALL SCRATCHES REMOVED BY HAND CLEAN PER SRM 51-10-02 AND 51-20-01 REV 111. REPAIR CSDR FDEA201407111707Skin · scratchedFUSELAGE EXTERIOR SKIN RT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND A SCRATCH AT BS 560 - 580 BETWEEN STRINGER 27 - BL0. SCRATCH REMOVED BY HAND CLEAN AND TREATED PER SRM 51-10-02 AND 51-20-01 REV 111. REPAIR CLASSIFIED MINOR.SDR FDEA201407111699Skin · scratchedFUSELAGE EXTERIOR SKIN LT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND NUMEROUS NICKS & SMALL SCRATCHES AT BS 560 - 580 BETWEEN STRINGER 28 - BL0. ACCOMPLISH NEW REPAIR ON FUSELAGE SKIN BS 577. REPAIR CLASSIFIED AS MAJORSDR FDEA201407111693Skin · scratchedFUSELAGE EXTERIOR SKIN LT SIDE EXISTING REPAIR. AFTER DOUBLER REMOVAL FOUND SCRATCHES AT BS 600 - 620 BETWEEN STRINGER 27 - BL 0. SCRATCHES REMOVED BY HAND CLEAN AND TREATED PER SRM 51-10-02 AND 51-20-01 REV 111. REPAIR CLASSIFIED MINOR.SDR FDEA201407111696Skin · damagedEXISTING REPAIR FINDINGS FUSELAGE EXTERIOR EXISTING REPAIR EXTERIOR DOUBLE & TRIPLER HAVE NUMEROUS NICKS, SCRATCHES & TOOL MARKS AT STATION 560 - 620 STRINGER 28L - 26R. ACCOMPLISH NEW REPAIR ON FUSELAGE SKIN BS 577. REPAIR CLASSIFIED AS MAJORSDR CALA2014071191451Floorbeam · corrodedFORWARD PAX AREA BS 377.7 RBL 54 TO 56 FLOORBEAM HAS UPPER SURFACE CORROSION. REPAIRED FWD PAX COMP BS 377.7 RBL 54 TO 56 BY INSTALLATION OF REPAIR STRAP & TAPERED FILLERS. THIS IS A CAT A REPAIR.SDR CALA2014071191450Floorbeam · corrodedCABIN STATION 1680 LBL 50 FWD SIDE OF T CAP UPPER & LOWER SURFACE IS CORRODED. REPLACED CABIN FLOORBEAM STATION 1680 LBL 60 TO RBL 60 IAW SRM 51-40-02, DWG 146N5091, EA 130412IR & ECRA 5360-01298.SDR CALA2014071191449Rudder · damagedLIGHTNING STRIKE INSPECTION FOUND RUDDER DAMAGE ON TE. TE DAMAGE 20 INCHES FROM TOP WITH 1 INCH BY .5 INCH DAMAGE REPAIRED. REINSTALLED STATIC WICK.SDR FDEA201407101685Skin · damagedEXISTING REPAIR FINDING FUSELAGE EXTERIOR EXISTING REPAIR EXTERIOR DOUBLER & TRIPLER HAVE NUMEROUS NICKS, SCRATCHES & TOOL MARKS AT STATION 1639 - 1701 STRINGER 15R - 19R. CRACK HOLE ON EXISTING FUSELAGE SKIN & STRAP REPAIR AT R4 DOOR CUTOUT, BETWEEN STA 16SDR FDEA201407091674Floorbeam · corrodedCABIN FLOOR BS 365.25 RBL 71 - LBL 71, BEAM UPPER CHORD CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DET III, REPAIRED FLOORBEAM UPPER CHORD AT STA 365.25 LBL13.75 - RBL 71 IAW SRM 53-00-51 FIG 201 REPAIR 8. THIS IS A CATESDR CALA2014071191453Smoke Detector · inoperativeSMOKE DETECTOR ON FIRST CLASS LAVATORY INOPERATIVE. REPLACED SMOKE DETECTOR.SDR CALA2014071191452Wire · damagedFUEL PNL HAS NO POWER, FOUND CONTROL PNL BREAKER POPPED IN MAIN EE BAY. RESET BREAKER, OPENED PNL, PNL WORKED MOMENTARILY THEN POPPED BREAKER. SMOKE WAS EVIDENT WHEN PNL WAS SWITCHED TO BATTERY POWER USING BATTERY SWITCH ON FUEL PNL. REMOVED FUEL CONTROL PNSDR FDEA201407091677Crease Beam · corrodedCORROSION AT CABIN CREASE BEAM INNER CHORD STATION 730, BY DOOR L2. ORIGINAL CREASE BEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL IV. R & R CREASE BEAM SECTION IAW SRM 51-40-02, PG 1, SRM 51-40-05 & DWG 143N8322, BS 686 - 760, LBL 58. MAJSDR FDEA201407091673Seat Track · damagedSEAT TRACK, BS 418 - 440, RBL 45, NICKED, GOUGED & CORRODED. CHECKED LIMITS IAW SRM 53-00-52, FLAG NOTE G & FOUND TO BE OUT OF LIMITS. PROFILED NEW SEAT TRACK, BATCH 0002645495, PN BAC1520-792A, IAW SRM 51-40-05 & DWG 141N5131. LOCATED & DRILLED IAW SRM 51-SDR FDEA201407071648Splice Plate · gougedAFT CARGO COMPARTMENT, STATION 1520, STRINGER 23R - 25R FRAME SPLICE PLATE HAS GOUGE MARKS. GOUGED SPLICE PLATE AT STA 1520, STR 23R-25R, REMOVED AND REPLACED WITH NEW SPLICE PLATE FABRICATED AS PER DWG 146N1042 SHT 4 REV B AND INSTALLED IAW DWG 146N1017 SHT SDR CALA2014071191454Skin · tornL4 DOOR ASSEMBLY INNER SKIN TORN AFT SIDE AT SECOND FROM BOTTOM LIGHTING HOLE. REMOVED & REPAIRED L4 DOOR ASSEMBLY INNER SKIN AFT SIDE FROM BOTTOM LIGHTING HOLE.SDR FDEA201407071647Stringer Splice · corrodedAFT CARGO COMPARTMENT STATION 1618 STRINGER 20L, STRINGER SPLICE CORROSION AFTER ACCESS. REPAIR CARRIED OUT IAW EA F-5310-T0310628 PART 1. LOCAL FABRICATION TO REPLACE CORRODED THROUGH STRINGER CHANNEL SPLICE. REPAIR IS MAJOR.SDR CALA2014071191431Power Supply · inoperativeFOUND EMER BULLNOSE LIGHT L1065 INOPERATIVE. REPLACED POWER SUPPLY M732, TESTED GOOD.SDR FDEA201407041622Skin · scratchedCABIN L2 DOOR OUTER SKIN FOUND SCRATCHES. COMPLIED WITH EA F-5210-T0310189. REPAIR CLASSIFIED AS MAJOR.SDR CALA2014071191432Nut · splitNUMBER 1 MLG TIRE TIE BOLT NUT SPLIT. REPLACED WHEEL & TIRE IAW AMM 32-45-01 PG 406.SDR CALA2014071191430Frame · dentedDENT ON AFT CARGO COMPARTMENT MAIN FRAME UPPER SURFACE AT BS 1500 JUST BETWEEN & ABOVE STRINGER 26L & 27L. TRIMMED OUT DAMAGE AREA OF FRAME FLANGE AT AFT CARGO BS 1500 FRAME. FABRICATED, LOCATED, DRILLED & INSTALLED J SECTION REPAIR DOUBLER IAW SRM 53-00-07 SDR CALA2014070391397Unknown · malfunctionedELEVATOR FEEL STATUS MSG PROG TEXT OK FOR SERVICE IAW FIM 27-31-00 FIG 105 BLOCK 11. CONFIRMED RT & CTR FILTER MODULES RED INDICATORS ARE NOT OUT. PRESSURIZED ALL THREE HYD SYS, NO EICAS MSGS. WHEN ARRIVED BACK TO GATE, NO ELEVATOR FEEL EICAS MSG DISPLAYED.SDR FDEA201407021609Strap · corrodedEMPENNAGE APU AIR INLET DOOR CUT OUT MIDDLE STRAP FOUND CORROSION AT STATION 1825 STRINGER 3R - 6R AFTER APU AIR INLET DOOR HOUSING REMOVED. CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-80-15 TABLE 101 ALLOWABLE DAMAGE 1 REV 112 & REPAIR CARRIED OUT AS SDR FDEA201407021607Seat Track · corrodedCABIN STATION 688 - 710 RBL 24.75 SEAT TRACK BOTTOM FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-10-02 REV 112. REWORKED AREA CLEANED UP DEPTH OF 0.065" FOUND EXCEED 0.040" LIMIT AS PER SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 REV 112. SEAT TRACK REPAIR SDR FDEA201407021605Rib · wornLEFT WING INBD TE AFT FLAP INBD RIB FOUND WORN AT AFT FLAP STATION 78.30, IAW SRM 57-53-02 IDENTIFICATION 1 FIG 1 SHEET 4 OF 8. RIB REMOVED AND REPLACED WITH NEW RIB IAW DWG 113N2800 SHT 4 REV B AND SRM 51-40-02 REV 112. REPAIR IS MAJOR.SDR CALA2014070291398Wire · shortedFOUND CB E 1 P 6 PANEL POPPED FOR LT ENG SPAR VLV. REMOVED CONNECTOR FROM LT SPAR VLV ACTUATOR, CB STILL POPPED. FOUND W3384-1009 -18 SHORTED IN PYLON HYD BAY FWD END, 2 INCHES AFT OF A PREVIOUS SHIELDED SPLICE REPAIR. REPAIRED WIRE IAW SWPM 20 10 13, LT NASDR FDEA201407021603Light · inoperativeL1 DOOR SLIDE EMER LIGHT INOPERATIVE. RELAMPED L1 DOOR SLIDE LIGHT IAW MM 33-51-06-2-1. OPERATIONS CHECKED GOOD.SDR FDEA201406301592Skin Panel · damagedRIGHT WING INBD MAIN FLAP LOWER MID ACCESS PANEL FOUND WITH 16 EACH ELONGATED SCREW HOLES. REPAIR CARRIED OUT AS PER EA F-5750-T0308417 PART 1. REPAIR IS MAJOR.SDR CALA2014063091377Lanyard · missingMAIN CABIN R1 DOOR EMER ESCAPE SLIDE FOUND MISSING RETAINING LANYARD FROM UPPER FWD RETAINING PIN. R & R SLIDE IAW AMM 25-66-01.SDR CALA2014063091373Bleed Air Sys · malfunctionedCREW REPORT APU BLEED AIR INOPERATIVE ON GATE. APU ELEC OK. CYCLED BLEED SWITCH WITH NORMAL PRESS EACH TIME. RAN PACK MAINTAINED 28 PSI. TAXI CREW INDICATING NORMAL ENG STARTS IAW JRH 2-5-00SDR FDEA201406281572Fitting · damagedDURING COMPLYING EO F-7120-7-5000 PT1, FIG 1 SHEET 1 STEP 7, AFTER REMOVAL OF NR 1 PYLON AFT ENG MOUNT FWD & AFT SHEAR BOLT FLANGE BUSHINGS, FOUND BUSHING HOLES TWO EACH OUT OF DWG TOLERANCE. REPAIR CARRIED OUT AS PER EA F-5450-T0309191 PART 1 [ PYLONS STRUCTSDR FDEA201406281571Fitting · damagedDURING COMPLYING EO F-7120-7-5000 PT 1, FIG 1 SHEET 1 STEP 7, AFTER REMOVAL OF NR 2 PYLON AFT ENG MOUNT FWD & AFT SHEAR BOLT FLANGE BUSHINGS, HOLES TWO EACH OUT OF DWG TOLERANCE. REPAIR CARRIED OUT AS PER EA F-5450-T0309191 PART 1 [ PYLONS STRUCTURES - SB-757
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