Boeing 757-225
Service difficulty reports · 1,988
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 = '757225' 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 = '757225' 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 USAA010611Skin · corrodedCLT - FOUND INNER SKIN SURFACE CORRODED APPROXIMATELY 10 SQUARE INCHES, BS 555 TO 572, STRINGER 28R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER AND TRIPLER PER EA 69643. (M)SDR USAA010605Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 3 INCH BY 2 INCH AREA OF CORROSION, BS 1320, RBL 22. REMOVED DAMAGED T-CAP, INSTALLED NEW T-CAP PER TYPICAL REPAIR 53-15-01 AND EA 69751. (M)SDR USAA010608Frame · corrodedCLT - FOUND FRAME CORRODED APPROX 1 INCH, BS 540, STRINGER 25L. REMOVED DAMAGE, INSTALLED FRAME DOUBLER REPAIR PER EA 69565A. (M)SDR USAA010614Frame · crackedCLT - FOUND FRAME CRACKED .75 INCH, BS 520, BETWEEN S24L AND S25L. DAMAGED REMOVED, INSTALLED FRAME REPAIR DOUBLER PER EA 69565A. (M)SDR USAA010613Frame · damagedCLT - FOUND FRAME CHORD BURNED APPROXIMATELY .75 INCH, BS 255, RBL 43, WL 180. DAMAGE REMOVED, INSTALLED DOUBLER WITH FILLER REPAIR PER SRM 53-00-07 FIG 201, AND EA 69684. (M)SDR USAA010574Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED APPROXIMATELY 10 SQUARE INCHES AT SCREW HOLES, BS 365, RBL 15 TO RBL 62. DAMAGE REMOVED, REPLACED T-CAP PER TYPICAL REP 53-15-01. (M)SDR USAA010575Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED APPROX 10 INCHES, BS 345, BL 0 TO LBL 45. DAMAGE REMOVED, REPLACED T-CAP PER TYPICAL REPAIR 53-15-01. (M)SDR USAA010579Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 6 INCH BY 6 INCH AREA, BS 1681, BL 0 TO RBL 55. REMOVED DAMAGE, REPLACED BEAM AND FLOOR PAN PER SRM 53-00-51. (M)SDR USAA010580Stringer · crackedCLT - FOUND STRINGER CRACKED 2 INCHES, BS 640, 16L. DAMAGE AREA REMOVED, INSTALLED STRINGER SPLICE AND DOUBLER PER SRM 53-00-03. (M)SDR USAA010576Floor Support · corrodedCLT - FOUND FLOOR SUPPORT BEAM CORRODED, BS 1715, RBL 46. REMOVED DAMAGE, REPLACED BEAM AND ANGLES PER SRM 51-10-2. (M)SDR USAA010578Web · corrodedCLT - FOUND DOOR SILL WEB CORRODED 1 INCH BY 4 INCH AREA, BS 1671 LBL 56.5. FABRICATED AND INSTALLED NEW WEB PER SRM 51-10-02. (M)SDR USAA010581Web · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 660, 14L. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED NEW WEB PER BAC DRAWING 143N8339 AND SRM 51-10-00. (M)SDR USAA010597Frame · corrodedCLT - FOUND FRAME CORRODED 2 INCHES BY 12 INCH AREA, BS 1701, BETWEEN STRINGERS 27L AND 28L. DAMAGE REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER PER EA 67935. (M)SDR USAA010577Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED APPROXIMATELY 24 SQUARE INCHES, BS 1661, LBL 55 TO RBL 55. DAMAGE REMOVED, REPLACED T-CAP PER EA 69718. (M)SDR USAABB01026Engine · malfunctionedSFO - FLT 56 - AFTER TAKEOFF APPROX 1000 FEET AGL, CREW HEARD LOUD BANG AND NOTED NUMEROUS WARNINGS ON THE LEFT ENGINE, AS WELL AS LIGHT SMOKE IN THE COCKPIT. ENGINE WAS SHUT DOWN. FLIGHT RETURNED TO SFO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTISDR USAABB01028Sign · inoperativeCLT - FOUND L4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE IDENTIFIER ASSEMBLY. (M)SDR USAABB01027Light · inoperativeCLT - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 18. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M)SDR USAA010532Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED IN SIX LOCATIONS EACH ONE IS 1 INCH BY 1 INCH AREA, BS 377.7, LBL 63 TO RBL 63. REMOVED DAMAGE AND INSTALLED REPAIR FILLER AND DOUBLER PER 53-00-51 FIG 205. (M)SDR USAA010516StrapCLT - FOUND STABILIZING STRAP WITH PREVIOUSLY INSTALLED DOUBLER, 6 SQUARE INCH AREA, BS 365 TO 377, LBL 25. REMOVED AND REPLACED DOUBLER PER 53-10-51 FIG 202. (M)SDR USAA010515Angle · crackedCLT - FOUND FAIL/SAFE ANGLE CRACKED .5 INCH, BS 600 STRINGER 16R. CRACK REMOVED, INSTALLED DOUBLER PER SRM 53-70-11. (M)SDR USAABB01024Light · inoperativeBDL - FOUND AFT AISLE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M)SDR USAA010385Web · corrodedCLT - FOUND TRANSITION ANGLE WEB CORRODED 4 INCHES, STATION 1340/1360 AT STRINGER 27 RIGHT. REMOVED AND REPLACED TA WEB, SRM 51-40-02. (M)SDR USAA010350Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 4 INCHES. T-CAP REPLACED, REPAIR ANGLES AND DOUBLERS INSTALLED PER TR 53-15-01. (M)SDR USAA010349Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 2 INCHES, STATION 365 LBL 10 TO RBL 65. T-CAP REPLACED/REPAIRED ANGLES PER EA 89244/69275. (M)SDR USAA010348Channel · corrodedCLT - FOUND HAT CHANNEL CORRODED 2 INCHES BY 4 INCHES, STATION 310 TO 324, RBL 42. INSTALLED NEW PART PER SRM 51-30-02. (M)SDR USAA010351Skin · delaminatedCLT - FOUND RIGHT ELEVATOR SKIN DELAMINATED 3.1 INCH BY .5 INCHES, OUTBOARD EDGE OF LOWER SKIN PANEL, 5 INCHES FORWARD T/E. COMPOSITE WET LAYUP REPAIR PER SRM 51-70-17. (M)SDR USAABB01019Battery · dischargedSFO - FOUND ALL FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED ALL THE BATTERIES (10 EACH). (M)SDR USAABB01017Girt Bar · dislodgedCLT - DURING A TEST OF THE R3 DOOR EMERGENCY ESCAPE SLIDE, THE GIRT BAR POPPED OUT OF THE FLOOR BRACKETS. (M)SDR USAA010346Strap · crackedCLT - FOUND STABILIZER STRAP CRACKED 2 INCHES, STATION 365 TO STATION 377, RBL 20. REMOVED AND REPLACED STABILIZER STRAP PER SRM 53-10-51. (M)SDR USAA010324Stringer · corrodedCLT - FOUND STRINGER CORRODED 8 INCHES, BETWEEN STATION 1320/1340. REPAIR ANGLES PER TR 53-10-01 PART B. (M)SDR USAA010329Strap · crackedCLT - FOUND STRAP CRACKED 2 INCHES, STATION 1380, RBL 46. REPAIR PLATE PER SRM 53-10-51. (M)SDR USAA010332Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .5 INCH, STATION 1320-1340, BL 0 UPPER CHORD. INSTALLED WEB AND FILLER PER SRM 51-00-10 AND 53-60-51. (M)SDR USAA010334Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 2 INCHES, STATION 1320, LBL FLOOR. FABRICATED NEW WEB PER REPAIR DOCUMENT 52-60-51. (M)SDR USAA010333Angle · crackedCLT - FOUND ANGLE CRACKED .25 INCH, STATION 1320 CABIN FLOOR SUPPORT. FABRICATED AND INSTALLED PER BOEING DWG 140N2502. (M)SDR USAA010328Angle · crackedCLT - FOUND OUTER CHORD ANGLE CRACKED 1 INCH, STATION 1300 BETWEEN STRINGER 21L-20L. FABRICATED AND INSTALLED NEW CHORD ANGLE PER SRM 51-10-00. (M)SDR USAA010327Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 690 STRINGER 7R. REMOVED DAMAGE INSTALLED DOUBLER, ANGLE RADIUS PER EA 69303. (M)SDR USAA010326Web · crackedCLT - FOUND SUPPORT WEB CRACKED 1.3 INCH, STATION 660, STRINGER 14L. INSTALLED DOUBLER PER SRM 51-70-11. (M)SDR USAA010330Web · crackedCLT - FOUND SUPPORT WEB CRACKED 1.3 INCHES, STATION 660, STRINGER 14R. INSTALLED DOUBLER PER SRM 51-70-11. (M)SDR USAA010325Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, STATION 640 PLUS 4 INCHES STRINGER 16L. INSTALLED NEW STRINGER SECTION PER SRM 53-00-03. (M)SDR USAA010331Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .5 INCH, BS 1671, RBL 12. FABRICATED NEW ANGLE PER SRM 53-60-51 AND 51-40-00. (M)SDR AWXA0001482Radome · puncturedLAS - 3/5/01 - ON DESCENT INTO LAS PASSING THROUGH 18,000 FT THE CREW HEARD A LOUD BANG AND AIR RUSHING SOUND FROM THE NOSE AREA AND FELT VIBRATION IN THE FLOOR. AN UNEVENTFUL LANDING WAS MADE IN LAS. UPON INSPECTION THE RADOME WAS FOUND TO HAVE A LARGE DENTSDR USAA010269Seat Track · corrodedCLT - FOUND SEAT TRACK CORRODED 1 INCH BY 1 INCH, INBOARD FLANGE RBL 24 STATION 1320. INSTALLED NEW SEAT TRACK AND DOUBLER. (M)SDR USAA010293Angle · corrodedCLT - FOUND TRANSITION ANGLE CORRODED 20 INCHES, STATION 1340 STATION 1360 WS 27R. REPAIRED PER SRM 51-40-02. (M)SDR USAA010286Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .5 INCH, BS 1671 AT RBL 12. INSTALLED NEW ANGLE 51-40-00. (M)SDR USAA010190Angle · crackedCLT - FOUND ANGLE CRACKED .25 INCH, STATION 1260, RBL 22 CABIN FLOOR SUPPORT. REMOVED CRACK AND FABRICATED PER SRM 53-60-01. (M)SDR USAA010220Flange · crackedCLT - FOUND WEB FLANGE CRACKED, TOP FLANGE WEB, AFT NUT PLATE HOLE STATION 480-500. FABRICATED NEW UPPER CHORD ANGLE PER BOEING DWG 284N1020-33 AND SRM 53-00-51 AND 51-10-00. (M)SDR USAA010174Angle · crackedCLT - FOUND ANGLE CRACKED .25 INCH, STATION 1320, RBL 46 CABIN FLOOR SUPPORT. INSTALLED PART PER SRM 51-10-02. (M)SDR USAA010175Skin · corrodedCLT - FOUND SKIN CORRODED 1 INCH BY 1 INCH, STATION 1300 INNER SKIN IN FRONT UNDER CARGO FLOOR. REPAIRED DOUBLER PER SRM 53-00-01 FIG 203 AND EA 69182. (M)SDR USAA010284Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 1 INCH, STATION 1420 AND STATION 1440 BL 0. INSTALLED NEW WEB FILLER. (M)SDR USAA010289Flange · crackedCLT - FOUND FLANGE CRACKED .5 INCH, STATION 480 AND STATION 500 RBL 9. FABRICATED FLANGE AND INSTALLED PER SRM 53-30-51. (M)
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