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 DU4R2006430Transition Panel · corrodedCORROSION AFT PIT ON LT TRANSITION PANEL NUMEROUS AREAS FROM BS 1530 TO 1640. REMOVED CORRODED TRANSITION PANEL AND INSTALLED NEW PANEL P/N 146N5431-41 IAW B757 SRM 51-40-08 AND 51-40-02.SDR DU4R2006432Door Frame · corrodedCORROSION LT AC BAY DOOR HINGE FRAME FROM BS 900 TO 1040. FABRICATED AND INSTALLED REPLACEMENT BEAM 38 X 1.625 X 2.875 X 1.5 INCHES FROM BAC1505-10047 IAW B757 SRM 51-20-01 AND 51-40-02.SDR DU4R2006428Floor Support · corrodedCORROSION ON FLOOR SUPPORT STRUCTURE UPPER WEB FROM BS 1320 - 1340 ABOVE S-30, RBL 9. REMOVED CORRODED WEB. FABRICATED AND INSTALLED REPLACEMENT WEB 20.875 X 2.75 INCHES FROM 7075-T6 .032 IAW B757 SRM 53-00-04 DETAIL 11 FIG 101, 51-40-02, 51-20-01 AND 53-60-SDR DL757060356Spar · damagedTHE NR 2 PYLON INBOARD MID SPAR CHORD HAS 3 ELONGATED HOLES. HOLES WERE OVERSIZED TO CLEAN UP THE DAMAGE AND BUSHED TO ORIGINAL SIZE AND LOCATION.SDR DU4R2006429Web · corrodedCORROSION ON AFT PIT FLOOR STRUCTURE WEB FROM BS 1320 - 1340 LT LBL 9. REMOVED CORRODED WEB. FABRICATED AND INSTALLED REPLACEMENT WEB 20.875 X 2.75 INCHES FROM 7075-T6 .032 IAW B757 SRM 53-00-04 DETAIL 11 FIG 101, 51-40-02, 51-20-01 AND 51-10-02.SDR DU4R2006424Floorbeam · corrodedFOUND CORROSION, AFT PIT, ON FLOOR SUPPORT ANGLE LWR SIDE BS 1510 LBL 7. FABRICATED AND INSTALLED REPAIR ANGLE 10 X .75 X .75 INCH FROM 7075-T6 .080 IAW B757 SRM 53-60-53 PG 221 & 222.SDR DU4R2006423Floorbeam · corrodedFOUND CORROSION AFT PIT ON FLOOR SUPPORT ANGLE LWR SIDE BS 1510, LBL 3. FABRICATED AND INSTALLED REPAIR ANGLE 10 INCHES LONG FROM 7075-T6 .080 IAW B757 SRM 53-60-53 PG 221 AND 222.SDR DU4R2006422Floorbeam · corrodedFOUND CORROSION AFT PIT ON FLOOR SUPPORT ANGLE LWR SIDE BS 1510, RBL 7. FABRICATED AND INSTALLED REPAIR ANGLE 8.75 INCHES LONG FROM 7075-T6 .080 IAW B757 SRM 53-60-53 PG 221 AND 222.SDR DL757060549Skin · crackedA CRACK WAS FOUND IN A PREVIOUS FUSELAGE SKIN BLENDED AREA. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.SDR DL757060545Skin · crackedAN EXISTING FUSELAGE SKIN BLENDED AREA WAS FOUND WITH A CRACK AT THE CENTER OF THE BLEND OUT. THE CRACKED AREA OF SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.SDR DUR42006417Skin · dentedFOUND CREASE 28" AFT OF L-4 DOOR AT SILL LEVEL. CUT OUT CREASED AREA IAW B757 SRM 53-00-01 FIG 201. HFEC FOR CRACKS IAW D6-34N301-6-51-00P6. FABRICATED AND INSTALLED REPAIR DOUBLER X 4.75" FROM 2024-T3 0.090" IAW B757 SRM 53-00-01 FIG 201 REPAIR 3.SDR DUR42006416Frame · dentedFOUND FRAME DENTED AT S-25L IN AFT PIT BS 1480. CUT OUT DENTED AREA IAW B757 SRM 51-70-11. FABRICATED AND INSTALLED FORMED SECTION REPAIR 210.50" BY 4.75" FROM 7075-0 .050" HEAT TREATED TO TPS-1002 IAW B757 SRM 51-20-01 AND 51-70-11.SDR DUR42006413Floor Support · corrodedFOUND CORROSION AROUND NUTPLATES ON FLOOR SUPPORT RBL NR 10, NR 45 SEVERAL AREAS FROM BS 1400 TO BS 1440. FABRICATED AND INSTALLED REPAIR SUPPORT 102-1/8" FROM BAC1517-2226 IAW B757 SRM 53-00-53 AND 53-87-01-801.SDR DL757060335Skin · dentedTHE FUSELAGE SKIN IS DENTED 3.25 INCH LONG AT BS 589 BETWEEN S22L AND S23L, NEAR A PREVIOUS REPAIR. DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.SDR DU4R2006403Panel · corrodedFOUND CORROSION ON RT TRANSITION STRIP BETWEEN BS 645 AND 765 (FWD CARGO). FABRICATED AND INSTALLED REPAIR DOUBLER 6-1/4" BY 2.5" BY 1-1/4" BY 3/4" FROM 7075 T6 .071 AND FILLER 2.5" BY 2.8" BY 1/4" FROM 7075-T6 .063" IAW B757 AMM 53-88-01-801.SDR DU4R2006401Floor Support · corrodedFOUND CORROSION ON FLOOR SUPPORT AT BS 1340 LBL 16 ABOVE S-29L (AFT PIT). FABRICATED AND INSTALLED DOUBLER REPAIR 5-3/4" FROM 301 .032 HD AND REPAIR SUPPORT 17" FROM BAC1517-2226 7075-T65 IAW B757 SRM 51-20-01 AND B757 MM 53-87-01-801.SDR DL757071121Floorbeam · corrodedDURING HMV AT YVR, THE STA 365 PASSENGER FLOORBEAM WAS FOUND CORRODED AT RBL 33.SDR DL757060392Floorbeam · corrodedTHE BS 365 FLOORBEAM WAS CORRODED ON THE UPPER CHORD AT RBL 33. REPAIR ANGLES WERE INSTALLED.SDR DU4R2006408Skin · puncturedFOUND PUNCTURED HOLE IN EXTERNAL FUSELAGE SKIN BS 1927 LBL 5.5, ABOVE APU. CUT OUT AND REMOVED PUNCTURED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER 4.25" IN DIAMETER FROM 2024-T3 .020 IAW B757 SRM 53-80-01, 51-70-10 FIG 203.SDR DU4R2006402Frame · corrodedFOUND CORROSION ON FRAME ANGLE BS 1360 BETWEEN S-27L AND S-25L (AFT PIT). FABRICATED AND INSTALLED CHANNEL REPAIR 31" BY 3" FROM 2024-T3 .050" IAW B757 SRM 51-20-01, 51-40-02 AND BOEING DRAWING 453N1801.SDR DU4R2006438Intercostal · corrodedCORROSION ON FLOOR STRUCTURE AT L4 DOOR BETWEEN BS 1640 TO 1681. FABRICATED AND INSTALLED 2 EACH INTERCOSTAL WEBS 21.75 X 3.5 X 1.8 INCHES FROM 7075-T6 .071" IAW B757 SRM 51-30-01, 51-40-05 AND 51-40-02.SDR DU4R2006411Cusp Web · corrodedFOUND CORROSION AT CABIN FLOOR STRUCTURE RBL 65 BS 996. FABRICATED AND INSTALLED REPAIR STIFFENER 3-3/4" BY 3-7/8" FROM 7075-T6 .090" IAW B757 SRM 53-40-13, 51-40-02 PG, 6, 7, AND 51-20-01.SDR DU4R2006410Intercostal · corrodedFOUND CORROSION IN AFT PIT ON FRAME UPPER ANGLE BS 1560, S-26R TO S-23R (UPPER SURFACE). CUT OUT CORRODED "C" CHANNEL. FABRICATED AND INSTALLED REPAIR "C" CHANNEL 34" BY 1.25" FROM 2024-T4 .050" IAW B757 SRM 51-30-1, 51-20-01 AND 51-40-02.SDR DU4R2006407Floor Support · corrodedFOUND CORROSION ON FLOOR STRUCTURE AT R-4 DOOR BETWEEN BS 1640 AND BS 1681. REMOVED CORRODED FLOOR SUPPORT. FABRICATED AND INSTALLED FORMED SECTION REPAIRS 3.5" BY 2.25" BY 1" AND 3-9/16" BY 1-5/8" BY 11/16" FROM 7075-T6 .080" AND 1-3/4" BY 5/8" AND 1-3/8" BSDR DU4R2006404Intercostal · corrodedFOUND CORROSION ON WEB AT FWD END AT SKIN BELOW FLOOR SUPPORT RBL 2.90 FROM BS 1400 TO 1420 (AFT CARGO). REMOVED CORRODED INTERCOSTAL. FABRICATED AND INSTALLED REPAIR INTERCOSTAL 19-3/8" FROM 7075-T6 .040" FROM B757 SRM 51-10-02, 51-20-01 AND 51-40-02.SDR DU4R2006400Panel · corrodedFOUND CORROSION ON NUMEROUS AREAS OF TRANSITION ANGLE FROM BS 1200 TO 1310 RT. DRILLED AND INSTALLED NEW TRANSITION PANEL IAW B757 SRM 53-00-53 FIG 101.SDR DL757060322Window · crackedDURING FLIGHT, R-1 WINDOW BEGAN TO ARC AND DELAMINATE. FOLLOW POM PROCEDURES AND TURNED OFF WINDOW HEAT. R-1 WINDOW THEN SPIDER WEB CRACKED. REPLACED R-1 WINDOW, OPS CHECK GOOD.SDR DU4R2006425Frame · corrodedFOUND CORROSION, AFT PIT, ON ATTACH ANGLE FOR FLOOR AND SIDEWALL PANELS (ALSO MISDRILLED HOLES, LOOSE FASTENERS) BS 1640 S-22R TO S-22L. FABRICATED AND INSTALLED REPAIR ATTACH ANGLE 3.5 X 1.5 INCH AND 2 EA ATTACH ANGLES 1.5 X 2.5 INCH FROM 2024-T3 .050 IAW B7SDR DL75K060295Jackscrew · lack of lubeTRAILING EDGE FLAPS DISAGREE WHEN FLAP LEVER MOVED FROM 15 TO 20. RAN CHECKLIST, LANDED WITH 20 FLAPS. LANDING WEIGHT 181.0. PSEU NO FAULTS. NO FAULTS ON FSEU. LUBED JACKSCREWS. RAN FLAPS OPS OK.SDR DUR42006415Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM BETWEEN R-1 AND L-1 DOORS BS 345. FABRICATED AND INSTALLED REPLACEMENT UPPER CAP 11 FEET BY 2" FROM BAC1505-100617 7075-T73 IAW B757 SRM 53-10-51 PG 217.SDR DUR42006414Intercostal · corrodedFOUND CORROSION IN AFT PIT ON WEB BS 1600 TO 1620 INBD OF S-28L. FABRICATED AND INSTALLED INTERCOSTAL 19-5/8" BY 7-1/2" FROM 7075-T6 .040 IAW B757 SRM 51-20-01 AND 51-40-02.SDR DU4R2006409Floorbeam · corrodedFOUND CORROSION ON FLOOR FRAME UPPER SURFACE, BS 700 INBD OF L2 DOOR AND UNDER CENTER FLOOR PANEL. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER 14-1/2" BY 1-1/4" FROM 2075-T6 .063 AND 13" BY 1" BY 1/2" FROM 7075-T6 .080 IAW B757 SRM 53-00-5SDR DU4R2006439Seat Track · corrodedCORROSION ON LEFT O/B SEAT TRACK BS 1027. FABRICATED AND INSTALLED SEAT TRACK BS 898 TO BS 1075 177 INCHES FROM BAC1520-541 IAW B757 SRM 51-40-02 AND 53-00-52.SDR DU4R2006418Floorbeam · corrodedFOUND CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 720 INBD OF L2 DOOR AND UNDER CENTER FLOOR PANEL. FABRICATED AND INSTALLED FLOORBEAM REPAIR 12.25" BY 1.75" BY .9" FROM 7075-T6 .080" AND 15.25" BY 1.8" BY 1" FROM 7075-T6 .063" IAW B757 SRM 53-30-51D FIG 20SDR DU4R2006406Intercostal · corrodedFOUND CORROSION ON WEB OUTBD OF S-28R FROM BS 1600 TO 1620. REMOVED CORRODED INTERCOSTAL. FABRICATED AND INSTALLED REPAIR INTERCOSTAL 19-5/8" BY 7-1/2" FROM 7075-T6 .040" FROM B757 SRM 51-10-02, 51-20-01 AND 51-40-02.SDR DU4R2006405Intercostal · corrodedFOUND CORROSION ON WEB OUTBD OF S-28L FROM BS 1400 TO 1420. REMOVED CORRODED INTERCOSTAL. FABRICATED AND INSTALLED REPAIR INTERCOSTAL 19-1/2" BY 7" FROM 7075-T6 .040" FROM B757 SRM 51-10-02, 51-20-01 AND 51-40-02.SDR DU4R2006441Gate · corrodedCORROSION ON L-1 DOOR LOWER GATE. REMOVED AND REPLACED L-1 DOOR LOWER GATE P/N 141N6120-29 IAW B757 SRM 51-40-02.SDR DU4R2006419Gate · corrodedFOUND L-4 DOOR LOWER GATE CORRODED. REMOVED AND REPLACED GATE ASSY ON L-4 DOOR IAW BOEING CMM 52-11-25 AND BOEING SRM 51-20-01.SDR DU4R2006420Frame · dentedFOUND AFT PIT FRAME 1460 FRAME DENTED AND GOUGED AT S-25L. CUT OUT DENT FROM FRAME STA. 1460. FORMED AND INSTALLED FRAME REPAIR 12.0" BY 1.0" BY .25" FROM 7075-T6 .063" IAW B757 SRM 53-00-07 PG 201-203, 51-20-01 AND 51-40-02 AND 51-70-11 FIG 1.SDR DL757071120Floor Panel · gougedDURING HMV AT YVR, A PASSENGER FLOOR DECK PLATE AT STA 1684, RBL 60 WAS FOUND GOUGED.SDR DL757060355Floor Panel · gougedTHE UPPER SURFACE OF THE DECK PLATE IS GOUGED AT BS 1684, RBL 60. THE GOUGE WAS BLENDED SMOOTH AND A REPAIR DOUBLER INSTALLED.SDR DL757071118Skin · crackedDURING HMV AT YVR, A CRACK WAS FOUND IN THE NR 2 PYLON O/B SKIN AT STA 133.5.SDR DL75K060245Outflow Valve · leakingAT FL410 - CABIN ALT WARNING, CABIN ALT EXCEEDED 10,000 FT. OUTFLOW VALVE CLOSED. ALL BLEEDS AND PACKS NORM. RECIRC FAN ON. C/W QRH PROCEDURES. DIVERTED TO MCO. BITE OF CABIN PRESSURE CONTROLLERS 1 AND 2 SHOW NO FAULTS. AMM TASK 05-51-24-702-001 HAS EXCSDR DL757060234Pseu · malfunctionedAFTER RISING LDG GEAR HANDLE EICAS CAUTION GEAR DISAGREE AND ADVISORY MSG GEAR DOORS ANNUNCIATED WITH GEAR AND DOOR LIGHTS AT GEAR HANDLE. GEAR LOWERED NORMALLY WITH GOOD DOWN AND LOCKED INDICATIONS. PSEU BITE - 072, 069, 239, 241, 406, 171, 170, AND MORE SUSDR DL757060268Fitting · misalignedAN ATTACH HOLE IN THE LT PYLON WING ATTACH LINK FITTING IS MISALIGNED. INSTALLED A TAPERED RADIUS FILLER TO PROPERLY ALIGN FASTENER.SDR DU4R2006357Skin · canningDOOR SKIN CORNER OIL CANNED BEYOND LIMITS. FABRICATED AND INSTALLED DOUBLER 8.5" BY 6.5" FROM 2024-T3 .071 AND FILLER 5.3" BY 3.75" FROM 2024-T3 .063 IAW B757 SRM 52-30-01 FIG 101, 52-30-01 PG 201 AND PROCESS STANDARD 900-5-1 NR 4, PG 4, 5 & 6.SDR DU4R2006356Intercostal · crackedCRACKED INTERCOSTAL UPPER CHORD FLANGE AT PANEL HOLES, BETWEEN BS 540-560, AIRCRAFT CENTER LINE BL-0 WL-208.10. REMOVED CRACKED FLOOR SUPPORT ANGLE, FABRICATED AND INSTALLED ANGLE 19-1/2" BY 1" BY 1" FROM 7075-T6 .032 IAW B757 SRM 53-00-51 FIG 201 REPAIR 4, 5SDR DU4R2006354Intercostal · corrodedCORROSION AFT CARGO INTERCOSTAL WEB BS 1500 TO BS 1520 LBL 2. REMOVED CORRODED INTERCOSTAL. FABRICATED AND INSTALLED INTERCOSTAL WEB REPAIR 19-3/4" BY 7-3/4" FROM 7075-T6 .040 IAW B757 SRM 51-40-02, 51-20-01.SDR DU4R2006348Skin · crackedFWD CARGO DOOR EXTERNAL SKIN CRACKED AFT LOWER CORNER. CUT OUT CRACKED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER 5.85" BY 5.75" FROM 2024-T3 .071 IAW B757 SRM 52-30-01.SDR DU4R2006352Floor Support · corrodedCORROSION NOTED ON AFT CARGO COMPARTMENT FLOOR SUPPORT BS 1670 LBL 55. CUT OUT CORRODED SECTION OF SUPPORT. FABRICATED AND INSTALLED FLOOR SUPPORT ANGLES 7.1" BY 1.8" BY 2.9" FROM 7075-T6 .090 AND 7.1 BY FROM 7075-T6 .071 IAW B757 SRM 51-70-11, 51-20-01.
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