Boeing 757-224
Service difficulty reports · 3,824
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 = '757224' 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 = '757224' 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 CALA0100317Actuator · wornINSPECTION FOUND HORIZONTAL STABILIZER ACTUATOR GIMBAL WORN BEYOND LIMITS. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 27-41-10.SDR CALA0100218Hydraulic Line · leakingTHE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. OVERRIDE WAS USED AND THE GEAR RETRACTED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MAIN GEAR TRUCK PRESSURE LINE LEAKING. THE LINE WAS REPLACED USSDR CALA0100214Smoke Detector · false indicationBOTH CARGO FIRE BOTTLES WERE DISCHARGED AND AIRCRAFT WAS RETURNED TO GLA DUE TO A FIRE WARNING IN THE AFT CARGO COMPARTMENT. THE AIRCRAFT LANDED SAFELY AND THE L-1 AND L-2 DOOR SLIDES WERE DEPLOYED TO EVACUATE THE PASSENGERS AS A PRECAUTIONARY MEASURE. THE EMESDR CALA0100154Skin · crackedINSPECTION FOUND A 9 INCH CRACK IN LT WING LEADING EDGE BETWEEN SLAT NR 3 & 4, WS 459.5. THE CRACK WAS REPAIRED IAW ECRA 5721-01009 AND A DIP WAS ISSUED TO REINSPECT EVERY 1000 HOURS AND TO ACCOMPLISH A PERMANENT REPAIR WITHIN 1800 HOURS OR NEXT C4 CHECK.SDR CALA0100153Skin · crackedINSPECTION FOUND A 9 INCH CRACK IN RT WING FIXED LEADING EDGE UPPER SURFACE BETWEEN SLAT NR 7 AND NR 8. THE CRACK WAS REPAIRED IAW ECRA 5721-01009 AND A DIP WAS ISSUED TO REINSPECT EVERY 1000 HOURS AND TO ACCOMPLISH A PERMANENT REPAIR WITHIN 1800 HOURS OR NEXSDR CALA0100020Wire · shortedINSPECTION FOUND EMERGENCY EXIT LIGHT AT R-4 DOOR INOPERATIVE. MAINTENANCE FOUND A SHORTED WIRE. THE WIRE WAS REPAIRED IAW WDM 33-51-15.SDR CALA0001547Floorbeam · corrodedINSPECTION FOUND T-CAP BEAM CORRODED AT STA 1640 FROM LBL 30 TO RBL 30. REPAIRED IAW SRM 53-00-51.SDR CALA0001433Charger · inoperativeEMERGENCY LIGHTS ON WITH SWITCH IN ARMED POSITION. REMOVED AND REPLACED CHARGER PER MM 33-51-11.SDR CALA0001462Bearing · failedR1 GALLEY DOOR BINDS WHEN OPENING. REPLACED BEARING AND HANDLE MECHANISM PER MM 52-11-13.SDR CALABearing · failedR1 GALLEY DOOR BINDS WHEN OPENING. REPLACED BEARING AND HANDLE MECHANISM PER MM 52-11-13.SDR CALA0001392Oven · overheatedA VERY STRONG ACRID ODOR BEGAN TO FILL THE CABIN APPROXIMATELY 45 MINUTES INTO FLIGHT AFTER DEPARTING FROM MCO. THE ELECTRICAL SMOKE CHECKLIST WAS ACCOMPLISHED. THE UTILITY BUSSES WERE TURNED OFF AND THE ODOR/SMOKE LESSENED, BUT DID NOT GO AWAY. THE AIRCRAFSDR CALA0001272Charger · inoperativeINSPECTION FOUND THE R-3 DOOR EMERGENCY EXIT SIGN INOPERATIVE. THE BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07 AND OPERATION CHECKED GOOD.SDR CALA0001263Idg · lack of lubeTHE L GEN OFF LIGHT ILLUMINATED (EICAS) EN ROUTE WHILE THE NR 2 IDG WAS ON PLACARD. THE AIRCRAFT WAS DIVERTED TO KTN. THE APU AUTO SHUTDOWN WHILE AT 32,000 FT. APU RESTART WAS SUCCESSFUL AFTER DESCENT TO 22,000 FT. THE AIRCRAFT LANDED SAFELY. MAINTENANCE SDR CALA0000914Megaphone · inoperativeINSPECTION FOUND FORWARD FLIGHT ATTENDANT SEAT MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REMOVED AND REPLACED.SDR CALA0000339Oven · inoperativeSMOKE APPEARED IN THE AFT CABIN SHORTLY AFTER TAKEOFF FROM SDQ. THE CIRCUIT BREAKER FOR THE NR 3 OVEN IN AFT GALLEY WAS PULLED AND THE SMOKE CEASED. THE AIRCRAFT WAS RETURNED TO SDQ WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 OVEN AT FAULT.SDR CALA0000178Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 1640, LBL 28 TO LBL 34. THE AREA WAS REPAIRED IAW ECRA 5321-01082.SDR CALA0000131Warning System · activatedTHE LAV SMOKE LIGHT ILLUMINATED AND ALL LAV DETECTORS ACTIVATED WHILE EN ROUTE FROM SFO TO EWR. SMOKE WAS SEEN IN BOTH THE COCKPIT AND CABIN. THE AIRCRAFT WAS DIVERTED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE NR 1 AND NR 2 ENGINE CHISDR CALA0000104Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 310-324, RBL 41. THE FLOOR SUPPORT WAS REPLACED IAW BOEING DRAWING 141N5160.SDR CALA0000103Angle · corrodedINSPECTION FOUND LAV SUPPORT ANGLE CORRODED AT STA 683-700, LBL 26. THE SUPPORT ANGLE AND MOUNT WERE REPLACED IAW BOEING DRAWING 143N5130 AND SRM 53-10-00.SDR CALA0000102Floorbeam · corrodedINSPECTION FOUND TOP CAP OF FLOORBEAM CORRODED ATSTA 720, LBL 60 TO RBL 60. THE TOP CAP OF FLOORBEAM WAS REPLACED IAW TRAMCO ENGINEERING DRAWING 95-030.SDR CALA0000101Beam · corrodedINSPECTION FOUND SEAT TRACK SUPPORT BEAM CORRODED AT STA 720-780, LBL 25. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-00-51.SDR CALA0000100Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT STA 660-680, LBL 25. THE INTERCOSTAL WAS REPLACED IAW BOEING DRAWING 143N5130.SDR CALA0000099Intercostal · corrodedINSPECTION FOUND INTERCOSTALS CORRODED AT STA 680-700, RBL 54 AND RBL 15. THE INTERCOSTALS WERE REPLACED IAW BOEING DRAWINGS 143N5434 AND 143N5130.SDR CALA0000098Floor Panel · crackedINSPECTION FOUND A .5 INCH CRACK IN FLIGHT DECK FLOOR PANEL AT ENTRYWAY AREA, STA 297, LBL17. THE FLOOR PANEL WAS REPAIRED IAW BOEING DRAWING 141N5810 AND ECRA 5321-01080.SDR CALA0000097Beam · corrodedINSPECTION FOUND SUPPORT BEAM CORRODED AT STA 683RBL 54-60 AND RBL 15-45. THE SUPPORT BEAMS WERE REPLACED IAW BOEING DRAWINGS 143N5845 AND 143N5530.SDR CALA0000094Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER FLANGE CORRODED AT STA 680 FROM LBL 24 TO RBL 15. THE CORROSION WAS REMOVRD IAW SRM 51-30-51 AND ECRA 5321-01078.SDR CALA0000096Skin · chafedINSPECTION FOUND LT O/B FLAP PANEL CHAFED IN THREE PLACES ON THE UPPER PANEL AFT OF NR 3 AND NR 4 SPOILERS. THE FLAP PANEL WAS REPAIRED IAW SRM 51-70-10 AND ECRA 5731-01023.SDR CALA0000095Skin · chafedINSPECTION FOUND RT O/B FLAP UPPER PANEL CHAFED BY NR 10 SPOILER BOLT. THE FLAP PANEL WAS REPAIRED IAW SRM 51-70-10 AND ECRA 5731-01023.SDR CALA9901589Charger · inoperativeINSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE AT ROWS 15-25. THE BATTERY CHARGER WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-51-07.SDR CALA9901453Compressor · leakingSEVERAL EICAS MESSAGES AND TAT PROBE CAME ON DURING TAKEOFF ROLL. A STRONG SMELL ENTERED THE CABIN AND THE PACKS OVERHEATED AFTER LIFT OFF. ALSO, A RUMBLING NOISE WAS HEARD. THE SMELL IN CABIN KEPT GETTING STRONGER AND AT 11,000 FEET THE CAPTAIN DECIDED TO SDR CALA9901438Panel · crackedINSPECTION FOUND A 6 AND 7 INCH CRACK IN RT WING FIXED L/E PANEL AT WS 421-471. REPAIRED IAW ECRA 5720-01668. A DIP WAS INITIATED TO REINSPECT THE AREAS EVERY 1000 HOURS AND ACCOMPLISH A PERMANENT REPAIR WITHIN 18 MONTHS OR NEXT C-CHECK.SDR CALA9901437Panel · crackedINSPECTION FOUND A 10 AND 6 INCH CRACK IN LT WING FIXED LEADING EDGE PANEL AFT OF NR 4 L/E SLAT, WS 421-471. A FIBERGLASS REPAIR WAS INSTALLED IAW ECRA 5720-01668. A DIP WAS ISSUED TO ACCOMPLISH A PERMANENT REPAIR WITHIN 18 MONTHS OR NEXT C-CHECK.SDR CALA9901424Intercostal · corrodedINSPECTION FOUND INTERCOSTAL ON FLOOR STRUCTURE CORRODED AT BS 1620-1640. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW BOEING DRAWINGS 146N5300 AND 143N5554-6.SDR CALA9901423Seat Track · corrodedINSPECTION FOUND I/B SEAT TRACK CORRODED AT BS 377-400, LBL 25 AND O/B SEAT TRACK WAS CORRODED AT BS 377-440, LBL 45. THE SEAT TRACKS WERE REPLACED IAW SRM 53-10-00 AND BOEING DRAWING 141N5130.SDR CALA9901370Skin · dentedIMPACT DAMAGE (1)ON LEFT SIDE FUSELAGE STATION 610 BETWEEN STRINGERS 15 AND 16 LEFT. REPAIRED PER SRM 53-00-01 FIG 208.SDR CALA9901303Panel · delaminatedINSPECTION FOUND LT WING FIXED LEADING EDGE PANEL DELAMINATED AT WS 150. THE PANEL WAS REPAIRED IAW SRM 51-70-08, 57-41-01, AND 51-40-2.SDR CALA9901302Skin · damagedINSPECTION FOUND IMPACT DAMAGE TO SKIN AT BS 600-620, S15L-16L. REPAIRED IAW ECRA 5331-01068.SDR CALA9901301Skin · crackedINSPECTION FOUND A 1.2 CRACK IN RT O/B T/E FLAP O/B LOWER SKIN. THE SKIN WAS REPAIRED IAW ECRA 5753-01086.SDR CALA9901300Seat Track · corrodedINSPECTION FOUND LT O/B SEAT TRACK CORRODED AT BS 377.7-440, LBL 45. THE SEAT TRACK WAS REPLACED IAW DRAWING 141N5130.SDR CALA9901299Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT STA 333, RBL 2. REPAIRED IAW ECRA 5322-01003.SDR CALA9901298Floorbeam · corrodedINSPECTION FOUND FLOORBEAMS CORRODED AT STA 277.7, RBL 43-48, STA 365, RBL 6.12-10.25, AND STA 377.7, LBL 22. THE FLOORBEAMS WERE REPAIRED IAW ECRA 5321-01071.SDR CALA9901297Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 720, RBL 24.75. THE SEAT TRACK WAS REPAIRED IAW DRAWING NR 140N2069.SDR CALA9901296Floorbeam · corrodedINSPECTION FOUND TOP CHORD OF FLOORBEAM CORRODED AT STA 720 BETWEEN RBL 1.0 AND RBL 53. THE FLOORBEAM CHORD WAS REPAIRED IAW ECRA 5321-01066.SDR CALA9901286Deck · corrodedINSPECTION FOUND SHEAR DECK CORRODED AT STA 1720, BL 0 AND LBL 49. REPAIRS WERE ACCOMPLISHED IAW ECRA 5321-01069.SDR CALA9901279Skin · damagedINSPECTION FOUND IMPACT DAMAGE TO FORWARD CARGO DOOR AFT LOWER DOOR SKIN. THE AREA WAS REPAIRED IAW ECRA 5231-01020.SDR CALA9901278Seat Track · corrodedINSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA 532, LBL 24.75. THE SEAT TRACK WAS REPLACED IAW DRAWING 141N5130.SDR CALA9901275Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT STA 700-680, RBL 54. A NEW INTERCOSTAL WAS INSTALLED IAW DRAWING NR 143N5845.SDR CALA9901124Skin · gougedINSPECTION FOUND A GOUGE IN FUSELAGE SKIN PANEL AT STA 456, STRINGER 27-28R. THE SKIN WAS REPAIRED IAW ECRA 5331-01066.SDR CALA9901123Shear Web · corrodedINSPECTION FOUND SHEAR WEB CORRODED AT STA 1681, LBL 16.4, LBL 40.0, AND BL 0 TO LBL 10.7. THE AREAS WERE REPAIRED IAW ECRA 5321-01062 AND ECRA 5321-01063.SDR CALA9901122Skin · gougedINSPECTION FOUND LT O/B FLAP I/B UPPER PANEL GOUGED BY SPOILER HINGE FITTING BOLTS AT FLAP STA 425.5. THE PANEL WAS REPAIRED IAW ECRA 5731-01017.
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