Boeing 757-2Y0
Service difficulty reports · 830
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 = '7572Y0' 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 = '7572Y0' 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 U2RA2012072348603Skin · misrepairedSKIN MISREPAIRED AT BS 490, BETWEEN S22-23R.SDR U2RA2012072348602Skin · dentedFUSELAGE SKIN AT BS 450, BETWEEN S25-26R HAS DENT FOUND TO BE OUT OF SRM LIMITS.SDR U2RA2012072348601Sill · corrodedCORROSION FOUND AROUND FASTENER HOLES ABOVE AND BELOW ANGLE ON THE LT EMERGENCY EXIT SILL PLATE AT BS 1320 - 1360.SDR U2RA2012072347801Skin · gougedUPPER FUSELAGE FORWARD AREA, FUSELAGE SKIN AND RIVET HEAD GOUGED AT BS 339 S7R.SDR FDEA201207202626Crease Beam · corrodedMAIN CABIN AREA, STRINGER 17L CREASE BEAM BS 730-760 CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL IV. R & R IAW SRM 51-40-02 AND DWG 143N8322. MAJOR REPAIR.SDR FDEA201207202625Stringer · corrodedSTRINGER 17R BS 660-760, CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL IV. INSTALLED STRINGER IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201207192619Floorbeam · corrodedMAIN CABIN SEC 41, AREA AT BS 377.7 FLOORBEAM CORRODED. BLENDED CORROSION IAW SRM 51-10-02. CHECKED LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III, D=.029 W=.6 L=1.3 ORIGINAL MATERIAL THICKNESS, .150 AFTER BLEND .121 FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAMSDR FDEA201207032458Crease Beam · corrodedAT BS 1440 INNER CREASE BEAM CORRODED ON RT SIDE.SDR U2RA2012072448601Floorbeam · corrodedFLOORBEAM CORRODED AROUND FASTENER HOLES AT BS1600, BETWEEN LBL24 AND RBL24. REPAIRED IAW EA PD57-53-170.SDR U2RA201206148602Fitting · galledNR 1 ENGINE 1/B SIDE LOAD FITTING TWO FASTENER HOLES GALLING AND ELONGATED.SDR U2RA201206148601Floor Support · crackedFORWARD CARGO FLOOR SUPPORT WEB CRACKED UPPER AFT SECTIONS BS 657 AT LBL 7.55SDR U2RA2012041648602Longeron · crackedMAIN PASSENGER CABIN AREA, CRACK FOUND IN STRINGER S10L AT BS 625 EXTENDING FROM RIVET HOLE. CRACK LENGTH IS 0.125" LONG.SDR U2RA2012041648601Longeron · crackedMAIN PASSENGER CABIN AREA, 3 EA CRACKS FOUND IN STRINGER S7L AT BS 625, EACH CRACK IS 0.125" LONG.SDR U2RA2012040548601Stringer · crackedMAIN CABIN AT BS 1701, STRINGER 11R WAS FOUND TO BE CRACKED. CRACK LENGTH 1".SDR U2RA2012032348602Stringer · crackedMAIN CABIN AT BS 1701, STRINGER 16R FOUND TO BE CRACKED. CRACK LENGTH IS APPROX 1.5" LONG.SDR U2RA2012032348601Intercostal · crackedINTERCOSTAL IN MAIN PASSENGER CABIN WAS FOUND TO BE CRACKED AT AFT LOWER END AT BS 1600 RBL 24. CRACK LENGTH IS 1.5" LONG.SDR U2RA2012021648602Intercostal · crackedE & E COMPARTMENT INTERCOSTAL CRACKED AT AFT END, BS 440 - 410 AT S23L.SDR U2RA2012021648601Cusp Web · corrodedMAIN CABIN, CORROSION FOUND ON THE CUSP WEB BETWEEN BS 1620 TO 1640 AT RBL 54.SDR FDEA201202010422Shear Tie · crackedUPON REMOVAL OF WING TO BODY SUPPORT, FOUND SHEAR TIE CRACKED AT STA 1300, STR 20L. REMOVED SHEAR TIE IAW SRM 51-40-02. FABRICATED NEW SHEAR TIE IAW DWG NR 140N2002-1059 AND SRM 51-30-01 AND 51-40-5. INSTALLED SHEAR TIE IAW SRM 51-40-02.SDR U2RA20120105080Stiffener · crackedFORWARD CARGO COMPARTMENT AT BS 845 AND RBL 19, STIFFENER FOUND CRACKED.SDR U2RA20110105079Floor Support · corrodedAFT CARGO FLOOR SUPPORT CHANNEL LOCATED AT BS 1510 AND LBL 15 FOUND TO BE CORRODED UNDER NUTPLATES.SDR U2RA486DHN078Floor Support · corrodedAFT CARGO COMPARTMENT AT BS 1350 LBL 7.5, FLOOR SUPPORT WAS FOUND TO BE CORRODED.SDR U2RA20111213077Frame · dentedDENT FOUND ON TOP OF FRAME AT BS 690 S24L.SDR U2RA2011120300076Intercostal · corrodedBS 1681 S17R, AFT LOWER WEB INTERCOSTAL FOUND TO BE CORRODED.SDR U2RA2011112948675Angle · corrodedAFT CARGO COMPARTMENT - SPLICE ANGLES HAS SEVERAL AREAS OF CORROSION, BS1340 - 1345 RBL 2.7, LBL 2.90, LBL 7.55 AND LBL 10.95.SDR U2RA2011112948674Floor Support · corrodedAFT CARGO COMPARTMENT, FLOOR SUPPORT "Z" CHANNEL FOUND TO BE CORRODED UNDER NUT-PLATES AT BS 1335 LBL 10.SDR U2RA20111108036Skin · damagedFUSELAGE SKIN APPROX BS 600 AT S5R, DAMAGED, DAMAGE FOUND TO BE OUT OF SRM LIMITS.SDR U2RA486DHN071Skin · dentedFUSELAGE SKIN BS 460, BETWEEN S23R AND S24R, DENTED. REPAIRED IAW SRM 53-00-01/REPAIR 2.SDR U2RA20111017070Attach Fitting · corrodedR4 DOOR WEB & ATTACHING SUPPORT FOR FLOORBEAM AT BS1640 - 1681 REPLACED DUE TO CORROSION.SDR U2RA20111014069Fitting · corrodedBS 1720 RBL 53, HEAVY CORROSION ON CORNER FITTING BELOW AFT PRESSURE BULKHEAD.SDR U2RA20111014068Beam · crackedMAIN PASSENGER CABIN PRESSURE RESISTANT BEAM CRACKED AT FASTENER HOLE AT STA BS 1681 BL 0.SDR U2RA20111014067Floorbeam · corrodedBS377 LBL45 - 62, HEAVY CORROSION ABOVE AND BELOW FLOORBEAM, AREA DAMAGE CUT-OUT 85 INCHES.SDR U2RA20111014066Channel · corrodedAFT CARGO ZEE CHANNEL FRAME SUPPORT, CORRODED AT BS 1320 RBL 10.SDR U2RA201110140066Floorbeam · corrodedBS377 LBL 45-62, HEAVY CORROSION ABOVE AND BELOW FLOORBEAM. AREA DAMAGE CUT-OUT 85 INCHES.SDR FDEA201110074363Lens · brokenLENS CAP ASSY ON EMERGENCY LIGHT UNARMED ANNUNCIATOR BROKEN. R & R EMERGENCY LIGHT UNARMED ANNUNCIATOR LENS CAP ASSY, DIODE/FUSE CARD AND DRAWER ASSY. OPS CHECKED GOOD WITH EMERGENCY LIGHTS ARMED/UNARMED. AMM 33-16-02-2.SDR U2RA20111004003Intercostal · crackedINTERCOSTAL AFT SIDE OF FLOORBEAM AT BS 1320 LBL45 BELOW SEAT TRACK IS CRACKED.SDR U2RA20111004001Support · corrodedBS 336, LBL 53 FWD OF L1 DOOR HAS CORROSION, AROUND NUTPLATES AND HOLE DRILLED IN RADIUS WITH GOUGE INSIDE.SDR U2RASill · corrodedMAIN CABIN, L1 DOOR LOWER SILL HAS CORROSION, APPROX 10 INCHES FROM FORWARD FRAME.SDR U2RA486DHN062Cusp Web · corrodedBS 376 AT RBL 66, CUSP HAS CORROSION ON BOTTOM SIDE.SDR U2RA486DHN061Skin · puncturedAFT CARGO COMPARTMENT, PUNCTURE IN BELLY FUSELAGE SKIN BTW BS 1661 - 1681.5 AT LBL 11, APPROX NR 10 SIZE HOLE.SDR U2RA486DHN060Floor Support · corrodedAFT CARGO, FLOOR SUPPORT "Z" CHANNEL AT BS 1510, LBL 2.9 HAS CORROSION UNDER NUT PLATES.SDR U2RA478DHN035Frame · damagedFUSELAGE STATION BS 1280 BETWEEN S4L & SA2L, FRAME DAMAGED.SDR U2RA478DHN034Floor Support · crackedSTATION BS 750 AT LBL 10, FORWARD CARGO COMPARTMENT, FLOOR SUPPORT CRACKED. CRACK LENGTH 1.250 INCHESSDR U2RA478DHN033Channel · crackedSTATION BS 345 - BS 355 AT RBL 24.75, "U" CHANNEL CRACKED. CRACK LENGTH IS 2 INCHES.SDR U2RA478DHN032Fitting · corrodedSTATION BS 1720 AT RBL 55, HEAVY CORROSION ON CORNER FITTING AT AFT PRESSURE BULKHEAD (APB).SDR U2RA478DHN031Sill · corrodedBS 1645 AT RBL 60, HEAVY EXFOLIATION CORROSION ON R-4 DOOR SILL.SDR U2RA20110823001Angle · corrodedFORWARD CARGO LT BS 508 - 660, TRANSITION ANGLE CORRODED TOP AND BOTTOM.SDR U2RA478DHN030Channel · corrodedMAIN CABIN AT FUSELAGE STATION BS326 AND LBL12, FLOOR CHANNEL CORRODED.SDR U2RA20110816001Floor Support · corrodedAFT CARGO COMPARTMENT, FLOOR SUPPORT, LT SIDE WEB AT FUSELAGE STATION 1530 - 1640, HAS CORROSION ON NUTPLATE UNDER WEB.SDR U2RA486DHN053Support Angle · corrodedMAIN PASSENGER CABIN, R & R ANGLE BETWEEN STATION BS 1701 - 1702, RT SIDE OF BL 0 DUE TO CORROSION AT FASTENER HOLE.
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