Boeing 757-232
Service difficulty reports · 15,843
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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 DL757951773Floorbeam · corrodedAT HMV FOUND FLOORBEAM CORRODED, FS 324 BETWEEN RBL 16 AND RBL 64. REMOVED DAMAGED SECTION OF CHORD, FABRICATED REPAIR PARTS PER SRM 53-10-08 FIG 201. INSTALLED T-CAP SECTION PER SRM 53-10-08 FIG 201.SDR DL757951814Skin · crackedAT HMV, FOUND NR 2 ENG STRUT CRACKED AT OVAL ACCESS HOLE AT FWD END OF STRUT RT SIDE ABOVE FWD ENG MOUNT. REPAIRED PER SRM 54-51-01 FIG 203.SDR DL757951813Former · dentedAT HMV, FOUND RT FORMER DENTED AT STA 1540 ABOVE FIXED FLOOR PANEL. CUT OUT DAMAGED AREA AND INST REPAIR DOUBLER PER SRM 51-70-11 PAGE 1 TO 5.SDR DL757951740Door · dentedDURING HMV VISIT, HANGAR INSPECTION FOUND THAT THE OUTER SKIN WAS DENTED JUST FORWARD OF CENTER LATCH. THE DENT WAS REPAIRED PER SRM 52-40-01.SDR DL757951739Door · dentedDURING HMV VISIT IN ATLANTA, HANGAR INSPECTION FOUND THAT THE APU ACCESS DOOR HAD A DENT IN THE OUTER SKIN. THE SKIN WAS REPAIRED PER SRM 52-40-01.SDR DL757951727Skin · dentedAT HMV, FOUND LOWER FUSELAGE SKIN DENTED BEYOND LIMITS AT FS 1595 BETWEEN STRINGERS 24L AND 23L. REPAIRED PER SRM 53-00-01 PG 212-214.SDR DL757951683Skin · holeAT HMV, BELLY SKIN AT FS 1330 HAS PUNCTURE DAMAGE AT FUSELAGE STATION 1330 ABOVE STRINGER 25L. REPAIRED PER SRM 53-00-01 FIG 208.SDR DL757951757Te Wedge · crackedTHE UPPER SKIN OF THE TRAILING EDGE WEDGE OF THE NR 5 L/E SLAT IS DELAMINATED AT ISS 109.00. THE DELAMINATION MEASURES 1 INCH ALONG THE EDGE OF THE PANEL AND PROGRESSES 0.25 INCH FORWARD FROM THE EDGE OF THE PANEL. DAMAGE FOUND AT LETTER CHECK, REPAIRS WERE SDR DL757952160Radome · damagedRECEIVED RADOME INTO SHOP WITH TWO INCH GOUGE AT 4 O'CLOCK, TWENTY FOUR INCHES FROM AFT EDGE. REMOVED DAMAGED SKIN AND CORE. REPLACED SKIN AND CORE AS PER SRM 53-10-72. APPLIED ERROSION BOOT AND PAINT AS PER PS 900-9-1-11, NR 05. FINAL INSPECTED AND SENT TSDR DL757951681Weight · crackedAT HMV, THE LWR L/E AT THE O/B END OF THE I/B WEIGHT ON THE RT AILERON WAS FOUND CRACKED. THIS WAS REPAIRED PER SRM 57-60-01.SDR DL757951643Skin · lightning strikeFOUND DURING LETTER CHECK, LIGHTNING STRIKES AT TOP OF CROWN AT STA 1040. INSTALLED BLIND FLUSH HEAD RIVET AT STA 1020 AND STA 1060 APPROX 14 INCHES RT OF CENTERLINE PER SRM 53-00-01 PG 221. EDDY CURRENT INSP C/W TEMP AT 2,500 FLT CYCS 53-00-01.SDR DL757951642Skin · lightning strikeFOUND DURING LETTER CHECK, LIGHTNING STRIKE AT 12 O'CLOCK AT STA 940 TO 950 AND L2-L3 STRINGERS. INSTALLED BLIND FLUSH HEAD RIVET AT STATION 940, APPROX 14 INCHES LT SIDE OF CENTERLINE IAW SRM 53-00-01. EDDY CURRENT INSP, C/W FLUSH TEMP OVERSIZE FASTENER INSSDR DL757951844Te Wedge · delaminatedDURING SHOP INSPECTION, RT WING NR 10 L/E SLAT WAS FOUND WITH DELAMINATION TO THE T/E WEDGE. REPLACED WEDGE PER SRM 57-43-02.SDR DL757951607Channel · damagedFOUND DURING LETTER CHECK, DOOR CHANNEL HAS HOLE 12 INCHES AFT OF AFT DOOR CORNER, AFT B/B. REMOVED DAMAGE AND MFG DOUBLER PER SRM 51-70-11, INSTALLED DOUBLER PER SRM 51-70-11.SDR DL757951726Wedge · wornLOWER AFT EDGE IS WORN ON NR 4 SLAT. REPLACED WEDGE PER SRM 57-43-02 REF AD 90-23-06. FOUND AND REPAIRED DURING HMV.SDR DL757951680Floorbeam · corrodedAT HMV, CORROSION WAS FOUND ON FLOORBEAM BL0 TO RT FUSELAGE SKIN STA 324. REMOVED CORR AND CK LIMITS PER SRM 53-10-8 FIG 101. DRILLED REPAIR SPLICE ANGLES PER SRM 53-10-8 AND INSTALLED PER SAME.SDR DL757951600Floorbeam · corrodedAT HMV, THE FLOORBEAM WAS FOUND TO BE CORRODED AT STA 760 FROM LBL 15 TO RBL 15. THE CORROSION WAS REMOVED AT BL0 TO RBL 15 WITHIN LIMITS PER SRM 53-00-51 FIG 101. CORR REM AT LBL 5 TO BL 0 NOT IN EXCESS OF .040 DEPTH. REPAIR FABRICATED PER SRM 53-30-51 FIGSDR DL757951599Floorbeam · corrodedAT HMV, THE CABIN FLOORBEAM UPPER CAP WAS FOUND TO BE CORRODED FROM LBL 10 TO 16. REPAIRED PER SRM 53-30-51 FIG 202.SDR DL757953030Skin · damagedON INITIAL SHOP INSPECTION, MAINTENANCE FOUND 2 SMALL HOLES APPROX 1 INCH IN DIAMETER ON BOTTOM SKIN, LOCATED 4 INCHES FROM T/E. REPAIR WAS ACCOMPLISHED PER SRM 57-70-01 FOR NR 6 SPOILER PANEL.SDR DL757951682Skin · damagedAT HMV, PERM REPAIR OF NR 2 ENG NACELLE STRUT SKIN I/B WAS SCHEDULED. THE DAMAGE WAS ROUTED OUT, INSP FOR CRACKS (NONE DETECTED), AND DOUBLER AND TRIPLER WERE FABRICATED AND INSTALLED PER SRM 54-51-01.SDR DL757951534Radome · puncturedFOUND DURING LETTER CHECK, RADOME HAS 2 PUNCTURES ON LT SIDE. REPAIRED PER SRM 53-10-72.SDR DL757951533Skin · lightning strikeFOUND DURING LETTER CHECK, 2 LIGHTNING STRIKES 1 PREVIOUSLY PAINTED OVER UPPER FUS CROWN AREA 6 FEET FWD VERT STAB. REPAIRED PER SRM 53-00-01. TIME LIMITED REP MUST BE REINSPECTED PRIOR TO 2,500 CYCLES AND REPLACED PRIOR TO 12,OOO CYCLES, E/C INSPD OK AT THISDR DL757951498Strap · crackedFOUND DURING LETTER CHECK E/E COMPT STRAP CRACKED FWD OF STA 380 RT SIDE OF NOSE GEAR WELL. REPAIRED PER SRM 53-10-51.SDR DL757951839Radome · damagedRADOME HAD A BIRD STRIKE ON CENTER OF NOSE. AFTER INSPECTION RADOME DELAMINATION AND MOISTURE ABOVE LIMITS. REBUILD RADOME COMPLETE PER SRM 53-10-72. CUT RADOME OFF ABOVE BASE RING AND REBUILD IN 757 MOLD SYSTEM. PAINT PER SP 900-9-1-11, NR 05, TRANSMISSIVSDR DL757951487Floorbeam · corrosionDEFERRED NR CARD C/N 7648, DFW - 3-30-95 - J1 CHECK NR 164. CORROSION AROUND NUTPLATES ON FLOORBEAM STA 720 BETWEEN LBL 45.5 AND CENTERLINE. REPAIRED PER SRM 53-30-51.SDR DL757951415Skin · dentedAT LETTER CHECK, DUE PERMANENT REPAIR PER SRM 53-31-001 STA 654 WL 214.0 LT SIDE FUSELAGE SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-00-1.SDR DL757951394Floorbeam · corrodedAT HMV, FLOORBEAM AT STA 324 RBL 61 WAS FOUND TO BE CORRODED. THE DAMAGED AREA WAS BLENDED OUT AND REPAIR ANGLE WAS FABRICATED AND INSTALLED PER SRM 53-10-08 FIG 202. AREA WAS TREATED PER SRM 51-10-08.SDR DL757951402Coffee Maker · shortedDURING CRUISE HAD BURING ODOR IF AFT GALLEY, DEACTIVATED POWER ODOR DISSIPATED. FOUND ODOR COMING FROM NR 2 AFT COFFEE MAKER. REPLACED DISPENSER, OPERATION NORMAL.SDR DL757951363Skin · delaminatedAT HMV, AN AREA OF DELAMINATION WAS FOUND AT LOWER I/B EDGE OF THE RT AILERON. THE AILERON WAS REPAIRED IN THE SHOP PER SRM 57-60-01.SDR DL757951362Floorbeam · corrodedAT HMV, THE STA 680 FLOORBEAM WAS FOUND TO BE CORRODED AROUND HOLES LBL TO RBL0. THE CORROSION WAS CLEANED AND IN LIMITS, EXCEPT BETWEEN RBL 3 THRU RBL 9. A REPAIR WAS FABRICATED FOR RBL 3 TO RBL 9 PER SRM 53-30-51 AND INSTALLED PER SAME.SDR DL757951417Nose Cowl · delaminatedAT HMV, INSPECTION FOUND THE UPPER SECTION OF OUTER SKIN OF NR 2 ENGINE NOSE COWL DELAMINATED. REPAIRED PER SRM 54-11-01.SDR DL757951416Skin · delaminatedTHE NR 2 ENGINE NOSE COWL, UPPER SECTION OF OUTER SKIN DELAMINATED. REPAIRED PER MM 54-11-01. FOUND AT LETTER CHECK.SDR DL757951361Stringer · crackedAT HMV, STRINGER 23L WAS FOUND CRACKED JUST FORWARD OF THE STA 540 FRAME. THE DAMAGED PORTION WAS REMOVED AND A SPLICE FABRICATED AND INSTALLED PER SRM 53-00-03 FIG 201.SDR DL757951576Skin · delaminatedDURING INSPECTION, LEFT WING SLAT PANEL WAS FOUND WITH SKIN DELAMINATED AT THE INBOARD EDGE UNDER DOUBLER. REPAIRED PER SRM 51-70-10.SDR DL757951395Le Skin · wornAT HMV, THE I/B AFT FLAP LEADING EDGE WAS FOUND TO BE WORN AT O/B END UNDER FAIRING. THE DAMAGE WAS REPAIRED PER SRM 57-53-01.SDR DL757951308Door · crackedTHE RT APU COWL DOOR SKIN CRACKED AROUND LATCH CUTOUT, LOCATED 2ND FROM THE AFT END NR 62. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER PER MM 52-48-05.SDR DL757951324Control · faultyON LANDING WITH SPOILERS UNARMED AND THROTTLES AT REVERSE, HAD RIGHT ROLLING MOVEMENT ON ROLLOUT. TROUBLESHOT SPOILER SYSTEM COULD NOT FIND PROBLEMS. FLIGHT DATA RECORDED SHOWED LEFT ENGINE REVERSER DEPLOYED 5 SECONDS AFTER THE RIGHT REVERSER DEPLOYED, THIS SDR DL757951222Floor Panel · corrodedDURING LETTER CHECK INSP, CORROSION FOUND AFT CARGO FLOOR LEFT SIDE AFT OF CARGO DOOR. REMOVED FLOOR PANEL AND CANTED WALL PANEL. REMOVED CORRODED AREA, MANUFACTURED REPLACEMENT SECTION. STARTED INSTALLATION OF REPLACEMENT SECTION, INSTALLED DOUBLER, INSTALSDR DL757951820Radome · delaminatedRECEIVED RADOME IN SHOP FOR DELAMINATION. INSPECTED RADOME AND FOUND EXCESSIVE MOISTURE. REMOVED INSIDE SKIN TO DRY MOISTURE. REPLACED DAMAGE CORE, REPLACED INSIDE SKIN AS PER SRM 53-10-72 ERROSION PROTECTION AND PAINT APPLIED AS PER PS 900-9-1-11, NR 05. SDR DL757951152Skin · lighting strikesFOUND DURING LETTER CHECK INSPECTION SEVERAL LIGHTNING STRIKES UPPER FUSELAGE IN AREA OF UPPER ANTI-COLLISON LIGHT FS 420 FS 580 FS 620 FS 690 REPAIRED FS 580 620 690 PER SRM 53-00-01 PERMANENT REPAIR FS 420 HAS TEMP REPAIR OF BLIND FASTENER PER SRM 53-00-01.SDR DL757951150Skin · lighting strikeFOUND DURING LETTER CHECK, SEVERAL LIGHTNING STRIKES UPPER FUSELAGE BELOW SKY RADIO ANTENNA AND ALONG STRINGER 3L. REPAIRED PER SRM 53-00-01 FIG 207.SDR DL757951983Radome · damagedRECEIVED RADOME INTO SHOP AND UPON INSPECTION, FOUND EXCESSIVE MOISTURE IN CORE OF RADOME. REMOVED INSIDE SKIN TO DRY OUT CORE OF RADOME AS PER SRM 53-10-72. REPLACED INSIDE SKIN PER SRM 53-10-72. APPLIED EROSSION BOOT AND PAINT AS PER PS 900-9-1-11 NR 05. SDR DL757951100Intercostal · crackedFOUND ON F-1 LETTER CHECK, INTERCOASTAL STRAP CRACKED BELOW FLOOR BEAMS FS 365 LEFT TUNNEL INSIDE E/E COMPT. REPAIRED PER SRM 53-10-51.SDR DL757951093Pneumatic System · contanimatedSHORTLY AFTER TAKEOFF HAD SMOKE AND ODOR ENTER CABIN. RETURNED ATL. FOUND PNEUMATIC SYSTEM CONTANIMATED. A WATER BASED SOLUTION WAS DRAINED FROM GROUND AIR CONNECTION. RAN BOTH ENGINES AND PACKS AFTER 1 HOUR HAD NO ODOR. RETURNED TO SERVICE.SDR DL757951041Engine · failedDURING CLIMB-OUT, HAD OIL TEMP ENTER YELLOW BAND, THEN HAD SMELL OF OIL IN CABIN AND FLT DECK, ALONG WITH LOSS OF OIL QTY. RETURNED TPA. REPLACED NR 1 ENGINE FOR RETURN TO SERVICE. ROUTED ENGINE TO SHOP.SDR DL757951154Floor Beam · corrodedDURING HMV, INSPECTION FOUND FLOOR BEAM CORRODED AT STA 377 LBL 54 AT FASTENER HOLES. REPAIRED PER SRM 53-10-51.SDR DL757951037Actuator · faultyDURING CRUISE, HAD SVA FAILSAFE MSG, NR 2 ENGINE FLAMED-OUT. LANDED RDU. RAN ENGINE PER PFHB TEST 14 SVA, TEST NORMAL. FERRIED AC TO ATL. REPLACED STATOR VANE ACTUATOR, RETURNED TO SERVICE.SDR DL757951628Radome · delaminatedRADOME WAS ROUTED TO SHOP FOR REPAIRS DUE TO DELAMINATION AND MOISTURE ENTRAPMENT. REWORKED RADOME PER SRM 53-10-72.SDR DL757950967Wedge · damagedAT HMV, LEFT WING NR 1 SLAT WAS FOUND WITH DELAMINATION ON THE TRAILING EDGE WEDGE. REPLACED WEDGE PER SRM 57-43-02.SDR DL757951075Skin · lightning damageDURING HMV, INSPECTION FOUND UPPER FUSELAGE SKIN AREA AT STATION 520 STRINGER 10L TO BE BURNISHED BEYOND LIMITS, .25 INCH LIGHTNING STRIKE. REPAIRED PER SRM 53-00-01.
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