N817AW
Service difficulty reports · 262
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N817AW' AND registry_match = 'registration' 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 n_number = 'N817AW' AND registry_match = 'registration' 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 USAA2012042500006Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66+6 INCHES, -Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66+6 INCHES, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472816.SDR USAA2012042400018Floorbeam · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16", S23R, -Y1292. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16", S23R, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D534-72780.SDR USAA2012042400017Floorbeam · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+6 INCHES TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66+6 INCHES TO FR70, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D534-72780.SDR USAA2012042400016Floorbeam · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+16 INCHES TO FR69, S23R, -Y1162. REPLACED FLOORBEAM BETWEEN FR67+16 INCHES TO FR69, S23R, -Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D534-72780.SDR USAA2012042300027Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 6 INCHES TO FR70, S23L, Y765. REPLACED FLOORBEAM BETWEEN FR66 + 6 INCHES TO FR70, S23L, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING 53472780, 53472815 & 53472092.SDR USAA2012042300023Dummy Rail · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY AT FR16, Y503.2. REPLACED RAIL DUMMY AT FR16, Y503.2 IAW A319 SRM 51-72-11 & AIRBUS DRAWING 53112827 & 53112825.SDR USAA2012042300022Web · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR20 TO FR23, S23R, -Y1660. REPLACED WEB BETWEEN FR20 TO FR23, S23R, -Y1660 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112784 & D53112261.SDR USAA2012042000007Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL NR 261PF BETWEEN FR38 TO FR70 & BETWEEN Y1292 TO -Y292. REPLACED FLOOR PANEL NR 261PF IAW A319 SRM 53-02-00 PAR 8G & IRM 9701 REV G.SDR USAA2012050100016Angle · cracked2S CHECK - CRACK ON SEGMENT ANGLE OF RIGHT AFT EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 4. REPLACED SEGMENT ANGLE OF RIGHT AFT EMERGENCY EXIT DOOR 844 IAW EO 5210Y228.SDR USAA2012042400019Hinge Fitting · excess playS2 CHECK - EXCESSIVE PLAY ON RUDDER HINGE NR 1 AT VERTICAL STABILIZER RIB 2. REPLACED NR 1 RUDDER HINGE FITTING IAW A318 SRM 51-72-11 & AMM 55-36-41-400-001.SDR USAA2012043000018Channel · corroded2S CHECK - CORROSION ON CHANNEL AT RIGHT AILERON TRAILING BETWEEN WS 1228 TO WS 1287 & BETWEEN WING RIB 23 TO WING RIB 24. REPAIRED RIGHT AIRERON IAW A319 SRM 57-61-21.SDR USAA2011120900009Battery · dischargedEMERGENCY LIGHT TEST FAILED DUE TO BAD EPSU BATTERY LEFT MID CABIN. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) BATTERY LEFT MID CABIN. OPS CHECK GOOD.SDR USAA2011101400018Battery · dischargedAFT FLIGHT ATTENDANT STATION FLASHLIGHT REPORTED "NOT BLINKING". REMOVED AND REPLACED BATTERY FOR AFT FLIGHT ATTENDANT FLASHLIGHT, OPS CHECKED GOOD.SDR USAA2011090600021Light · brokenEMERGENCY LIGHT BROKEN AT SEAT 1C. REMOVED AND REPLACED EMERGENCY LIGHT AT 1C. OPS CHECKED GOOD.SDR USAA2010071291396Computer · faultyFLT 450 - PHX-SLC - EMERGENCY LANDING - IN FLIGHT, ECAM INDICATED LOSS OF BRAKE ANTI-SKID / NOSE WHEEL STEERING. UNSUCCESSFUL RESET. EMERGENCY LANDING AND AIRCRAFT TOWED TO THE GATE. REMOVED AND REPLACED CENTRALIZED FAULT DISPLAY INTERFACE UNIT (CFDIU) PER SDR USAA2010050390875Lens · missingFLT 436 - YEG-PHX - EMERGENCY LIGHTS - SEAT EMERGENCY EXIT LIGHT LENS AT 10C MISSING. REPLACED MISSING SEAT EMERGENCY LIGHT LENS AT 10C.SDR USAA2009081092058Unknown · odorFLT 607 - ORD - LAS - VIBRATION / BURNING SMELL - BURNING FELT VIBRATION IN FLIGHT DECK FLOOR AREA (15 MIN), LATER SLIGHT ELECTRIC MOTOR BURN ODOR. CYCLED BLOWER AND EXTRACT MOTORS, NO VIBRATIONS OR ODORS NOTED. COMPLIED WITH AEVC TEST WITH NO FAULTS NOTED. SDR USAA2009080592018Damper · low pressureSAL - BC6 - EES - NR 6157225 - LOW PRESSURE DAMPER AND EMERGENCY OPERATIONAL CYLINDER AT PASSENGER CREW DOOR 831. PERFORMED CHARGING OF DAMPER AND EMERGENCY OPERATIONAL CYLINDER AT PASSENGER CREW DOOR 831 IAW A319 AMM 52-10-00-614-050.SDR USAA2009073091950Damper · low pressureSAL - BC-6 - EES - LOW PRESSURE IN THE DAMPER AND EMERGENCY OPERATION CYLINDER AT THE PASSENGER / CREW DOOR 831. PERFORMED CHARGING OF DAMPER AND EMERGENCY OPERATION CYLINDER AT THE PASSENGER / CREW DOOR 831 IAW A319 AMM 52-10-00-614-001.SDR USAA2009073091949Damper · low pressureSAL - BC-6 - EES - LOW PRESSURE IN THE DAMPER AND EMERGENCY OPERATION CYLINDER AT THE PASSENGER/CREW DOOR 841. PERFORMED CHARGING OF DAMPER AND EMERGENCY OPERATION CYLINDER AT THE PASSENGER/CREW DOOR 841 IAW A319 AMM 52-10-00-614-001.SDR USAA2009080391986Cylinder · low pressureBC6-CHECK - SAL - EMERGENCY EQUIPMENT - LOW PRESSURE DAMPER AND EMERGENCY OPERATION CYLINDER AT PASSENGER / CREW DOOR L2 (832). SERVICED DAMPER AND EMERGENCY OPERATION CYLINDER AT PASSENGER / CREW DOOR L2 (832) PER MAINTENANCE MANUAL 52-10-00-314-050.SDR USAA2009080391985Cylinder · low pressureBC6-CHECK - SAL - EMERGENCY EQUIPMENT - LOW PRESSURE DAMPER AND EMERGENCY OPERATION CYLINDER AT PASSENGER / CREW DOOR L1 (842). SERVICED DAMPER AND EMERGENCY OPERATION CYLINDER AT PASSENGER / CREW DOOR L1 (842) PER MAINTENANCE MANUAL 52-10-00-314-050.SDR USAA2009081192073Support · wornSAL - BC-6 - MAJOR REPAIR - WEAR ON TORSION SUPPORT ASSEMBLY RIGHT WING. REPLACED TORSION SUPPORT ASSEMBLY RIGHT WING IAW A319 CMM 57-52-21 & AMM 27-54-61.SDR USAA2009081192072Support · wornSAL - BC-6 - MAJOR REPAIR - WEAR ON TORSION SUPPORT ASSEMBLY LEFT WING. REPLACED TORSION SUPPORT ASSEMBLY LEFT WING IAW A319 AMM 27-54-61.SDR USAA2009081092064Hinge Fitting · excess playSAL - BC-6 - MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 5 AT VERTICAL STABILIZER RIB 7. REPLACED RUDDER HINGE FITTING NR 5 AT VERTICAL STABILIZER RIB 7 IAW A319 SRM 51-72-11.SDR USAA2009081092063Hinge Fitting · excess playSAL - BC-6 - MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 4 AT VERTICAL STABILIZER RIB 6. REPLACED RUDDER HINGE FITTING NR 4 AT VERTICAL STABILIZER RIB 6 IAW A319 SRM 51-72-11.SDR USAA2009081092062Hinge Fitting · excess playSAL - BC-6 - MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 3 AT VERTICAL STABILIZER RIB 5. REPLACED RUDDER HINGE FITTING NR 3 AT VERTICAL STABILIZER RIB 5 IAW A319 SRM 51-72-11.SDR USAA2009081092061Hinge Fitting · excess playSAL - BC-6 - MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 2 AT VERTICAL STABILIZER RIB 4. REPLACED RUDDER HINGE FITTING NR 2 AT VERTICAL STABILIZER RIB 4 IAW A319 SRM 51-72-11.SDR USAA2009081092060Hinge Fitting · excess playSAL - BC-6 - MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 1 AT VERTICAL STABILIZER RIB 2. REPLACED RUDDER HINGE FITTING NR 1 AT VERTICAL STABILIZER RIB 2 IAW A319 SRM 51-72-11.SDR USAA2009072091890Girt Bar · obstructedLOGPAGE:8517000 - FLT 108 - PHX-LAS - EMERGENCY EQUIPMENT - AFTER TAKEOFF, DOOR 2L SLIDE ARMED INDICATION DISAPPEARED. FLIGHT ATTENDANT REPORT CABIN PRESSURE LIGHT ON DOOR 2L WAS FLASHING. CLEANED DEBRIS FROM GIRT BAR AREA AT DOOR L2. NO DAMAGE TO DOORS EVISDR AWXA200600899Sill · corrodedSAL - MAJOR REPAIR - NR 5910947 - DURING BC4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON SILL BEAM LOCATED ON FRAME 66-1" AT Y-1310 IN THE PAX CABIN AT THE LOWER R2 CUTOUT. CORROSION WAS REMOVED AND RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM SDR AWXA200600901Support Angle · crackedSAL - MAJOR REPAIR - NR 5911063 - DURING BC4 CHECK DISCOVERED CRACK ON SUPPORT ANGLE LOCATED LT PYLON OUTBOARD SIDE FROM PYLON STA 537 TO PYLON STA 608. MAINTENANCE REMOVED AND INSTALLED NEW SUPPORT ANGLE EXTRUSION FROM PYLON STA 537 TO PYLON STA 608 IAW AIRBSDR AWXA200600974Floorbeam · corrodedNR 5910965 - DURING BC-4 CHECK, DISCOVERED LEVEL 2 GALVANIC CORROSION ON FLOOR BEAM LOCATED ON FR 68 Y765. MAINTENANCE REPLACED BEAM FR 66 TO FR 70+3 INCH IAW SRM A319 51-72-11.SDR AWXA200600973Floorbeam · corrodedNR 5910893 - DURING BC-4 CHECK, DISCOVERED LEVEL 2 GALVANIC CORROSION ON FLOOR BEAM IN PAX CABIN ON FRAME 67-5 INCH Y1292. MAINTENANCE REPLACED FLOOR BEAM IAW SRM A319 51-72-11 FROM FR 66 TO FR 68.SDR AWXA200600972Floorbeam · corrodedNR 5910894 - DURING BC-4 CHECK, DISCOVERED LEVEL 2 GALVANIC CORROSION ON FLOOR BEAM LOCATED IN PAX CABIN, FR 66 Y1292. MAINTENANCE REPLACED FLOOR BEAM IAW SRM 51-72-11 FROM 64 TO FR 66 Y1292.SDR AWXA200600971Floorbeam · corrodedNR 5910888 - DURING BC-4 CHECK, DISCOVERED LEVEL 2 GALVANIC CORROSION ON FLOOR BEAM LOCATED IN PAX CABIN AT FR 66 - Y1292. MAINTENANCE REPLACED FLOOR BEAM FROM FR 64 TO FR 66 - Y1292 IAW SRM A319-51-72-11.SDR AWXA200600969Floorbeam · corrodedNR 5910964 - DURING BC-4 CHECK, DISCOVERED LEVEL 2 GALVANIC CORROSION ON FLOOR BEAM AT CABIN FLOOR STRUCTURE FR 20 - Y275. MAINTENANCE REPAIRED FLOOR BEAM FROM FR 17+120 INCH TO FR18+5 INCH - Y275 IAW SRM A319 53-11-14.SDR AWXA200600968Fitting · corrodedNR 5910917 - DURING BC-4 CHECK, DISCOVERED LEVEL 2 GALVANIC CORROSION ALONG CENTRAL FITTING AT R1 DOOR THRESHOLD AREA BETWEEN FR 16 AND FR 20 Y1860. MAINTENANCE REPLACED CENTRAL FITTING AT R1 DOOR THRESHOLD AREA BETWEEN FR 16 TO FR 20 Y1860 IAW SRM A319 51-72SDR AWXA200600967Fitting · corrodedNR 5910916 - DURING BC-4 CHECK, FOUND LEVEL 2 GALVANIC CORROSION ALONG CENTRAL FITTING AT L1 DOOR THRESHOLD AREA BETWEEN FR 16 AND FR 20 Y1860. MAINTENANCE REPLACED CENTRAL FITTING ON L1 FROM FR 16 TO FR 20 Y1860 IAW SRM A319 51-72-11.SDR AWXA200600966Hinge Pin · corrodedNR 5911011 - DURING BC-4 CHECK, DISCOVERED LEVEL 2 GALVANIC CORROSION ON LT WING SPOILER NR 3 CENTER IB HINGE PIN. MAINTENANCE REPLACED PIN ON SPOILER NR 3 CENTER IB HINGE LOCATED AT LT WING IAW AMM 27-64-43.SDR AWXA200600964Seat Track · corrodedNR 5910511 - DURING BC-4 CHECK, FOUND LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK Y1292 FR 36+3 INCH, FR 38+3 INCH AND FR 40. MAINTENANCE REPLACED SEAT TRACK FROM FR 36 TO FR 41 IAW A319 SRM 51-72-11 AND 51-42-11.SDR AWXA200600892Dummy Rail · corrodedSAL - MAJOR REPAIR - DURING BC4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON DUMMY RAIL AT CABIN FLOOR STRUCTURE LOCATED AT FR 20 -3.5" AT Y-1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED NEW SEASDR AWXA200600884Floorbeam · corrodedSAL - DURING BC4 CHECK, DISCOVERED CORROSION ON FLOORBEAM AT CABIN FLOOR STRUCTURE FROM FS 15+8IN TO FS 16 Y765. SEAT TRACK WAS REPLACED BETWEEN FS 12 TO FS 24 Y765 IAW SRM A319 51-72-11.SDR AWXA200600979Stop Fitting · corrodedNR 5910755 - DURING BC-4 CHECK, DISCOVERED LEVEL 2 GALVANIC CORROSION ON STOP FITTING LOCATED AT LOWER SILL SURROUNDING STRUCTURE FR 27+11 INCH, STR 38R, FWD CARGO COMPARTMENT. MAINTENANCE REPLACED STOP FITTING LOCATED ON LOWER SILL SURROUNDING STRUCTURE FR 2SDR AWXA200600978Stop Fitting · corrodedNR 5910746 - DURING BC-4 CHECK, DISCOVERED LEVEL 2 GALVANIC CORROSION ON STOP FITTING LOCATED AT LOWER SILL SURROUNDING STRUCTURE FR 24A+9 INCH, STR 38R, FWD CARGO COMPARTMENT. MAINTENANCE REPLACED STOP FITTING LOCATED AT LOWER SILL SURROUNDING STRUCTURE FR 2SDR AWXA200600977Stop Fitting · corrodedNR 5910747 - DURING BC-4 CHECK, DISCOVERED LEVEL 2 GALVANIC CORROSION ON STOP FITTING LOCATED AT LOWER SILL SURROUNDING STRUCTURE FR 25+1 INCH, STR 38R, FWD CARGO COMPARTMENT IAW SRM A319-51-72-11.SDR AWXA200600975Stop Fitting · corrodedNR 5910754 - DURING BC-4 CHECK, DISCOVERED LEVEL 2 GALVANIC CORROSION ON STOP FITTING LOCATED AT LOWER SILL SURROUNDING STRUCTURE FR 27+8 INCH, STR 38R FWD CARGO COMPARTMENT. MAINTENANCE REPLACED STOP FITTING LOCATED LOWER SILL SURROUNDING STRUCTURE FR 27+8 ISDR AWXA200600965Floor Panel · perforatedNR 5910654 - DURING BC-4 CHECK, FLOOR PANEL NR 151VG AFT CARGO COMPARTMENT FOUND WITH PERFORATION AND DELAMINATION OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 151VG IAW IRM 9701 REV F.SDR AWXA200600963Seat Track · corrodedNR 5910477 - DURING BC-4 CHECK, DISCOVERED LEVEL 2 GALVANIC CORROSION ON SEAT TRACK FR 39+4" Y765. MAINTENANCE REPLACED SEAT TRACK FROM FR 36 TO FR 41 Y765 IAW SRM A319 51-72-11.SDR AWXA200600962Seat Track · corrodedNR 5910497 - DURING BC-4 CHECK, DISCOVERED LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK Y1292 - 4 POINT - FR 43+4 INCH, FR 44+6 INCH, FR 45+8 INCH, FR 46-4 INCH. MAINT REPLACED SEAT TRACK LOCATED ON FR 41 TO FR 47 Y1292 IAW SRM A319 51-71-11.
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