N940AT
Service difficulty reports · 243
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 = 'N940AT' 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 = 'N940AT' 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 SWAA2013032514046Fitting · corrodedR1 DOOR JAMB FWD AND AFT CLIPS ATTACHED TO GIRT BAR LATCHES CORRODED. REMOVED AND REPLACED FITTING IAW SRM.SDR SWAA2013032614125Frame · corrodedFRAME CORRODED AT BS 1037, LONGERON 30. REPAIRED FRAME IAW SRM.SDR SWAA2013032614124Frame · corrodedFRAME CORRODED AT BS 1022, LONG 30. REPAIRED FRAME IAW SRM.SDR SWAA2013032213996Intercostal · crackedL1 DOOR INSIDE HANDLE AREA ANGLE CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW SRM.SDR SWAA2013032614123Cover Plate · crackedLEFT WING - BETWEEN STA NR 1 AND 2 - COVER PLATE CRACKED. REMOVED AND REPLACED PLATE IAW SRM.SDR SWAA2013010311113Cable · disconnectedGIRT BAR CONNECTING CABLE DISCONNECTED L1 DOOR. RECONNECTED GIRT BAR CABLE PER MM.SDR SWAA2012112609730Cover · missingSEAT 1D EMERGENCY EXIT LIGHT BULB COVER MISSING/ BULB INOP. RELAMPED AND REPLACED COVER. OPS CHECKED REF AMM.SDR SWAA2012071805961Tab · delaminatedRIGHT WING AILERON INBD TAB DELAMINATED. REMOVED AND REPLACED TAB IAW SRM.SDR SWAA2012071205715Tab · delaminatedRIGHT WING AILERON INBOARD TAB DELAMINATED. REPAIRED TAB IAW SRM.SDR SWAA2012060404574Light · inoperativeRIGHT EEPLS INOP AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.SDR ZZDA2011983Actuator · malfunctionedGEAR DOOR OPEN MESSAGE ON FINAL APPROACH. REMOVED AND REPLACED RT MLG DOOR ACTUATOR. REMOVED AND REPLACED LT AND RT MLG DOOR TORQUE TUBES; LEAK CHECK GOOD. ACCOMPLISHED ALL ADJUSTMENTS; TEST AND OPERATIONAL CHECKS REF AMM 32-34.SDR ZZDA2011866Socket · defectiveROW 24 E-PATH LIGHTS INOP. REMOVED AND REPLACED E-PATH LAMP SOCKET ASSEMBLY IAW AMM 33-51-04. REPAIRED 2 BROKEN SPLICES AFT OF ROW 23 IAW SWPM 20-10-03, OPS CHECK OF EMERGENCY LIGHTING SYSTEM NORMAL IAW AMM 33-51-00.SDR ZZDA2011470Slide · unserviceableL-1 DOOR PAX SLIDE PSI IN RED. REMOVED AND REPLACED L-1 DOOR SLIDE REF 717 MM 25-61.SDR ZZDA2011400Wire · damagedEMERGENCY LIGHTS ON THE LAST 7 ROWS OF SEATS INOP. REPLACED POWER SUPPLY WITH NO HELP. AT APPROX FS 813 REPAIRED WIRING AS REQUIRED REF WDM 33-51. REPLACED POWER SUPPLY AGAIN AND ALL OPS NORMAL REF MM 33-51.SDR ZZDA2011388Light · inoperativeL-1 DOOR EMERGENCY EXIT IDENTIFIER INOP/DAMAGED. REPLACED IDENTIFIER LIGHT ASSY PER MM 33-51.SDR ZZDA2011322Frame · corrodedAFT CARGO COMPARTMENT FRAME SECTION, STA 908, LONG L29L TO L29R, CORROSION. ACCOMPLISHED FRAME SECTION REPLACEMENT PER B717 SRM 53-20-07 FIG 201 REPAIR 3.SDR ZZDA2011321Skin · damagedEXTERIOR FUSELAGE SKIN, STA 237, LONG L17L, CREASED. ACCOMPLISHED FUSELAGE SKIN FILLER AND DOUBLER REPAIR PER B717 SRM 53-00-01 FIG 201 REPAIR 6.SDR ZZDA2011320Skin · crackedRIGHT MLG DOOR CENTER FWD EDGE SKIN, CRACKED. ACCOMPLISHED SKIN DOUBLER REPAIR PER B717 SRM 52-82-02 AND BOEING DWG SR09520012-4.SDR ZZDA2010624Door · openGEAR DOOR OPEN ALERT ILLUMINATED ON SHORT FINAL. LEFT GEAR DOOR DRAG ON RUNWAY. REMOVED AND INSTALLED LEFT GEAR DOOR REF B717 AMM 32-14-01, ALL CLEARANCE AND OPS CHECK GOOD.SDR ZZDA2010305Light · inoperativeLT WING EMERGENCY LIGHT INOPERATIVE. RELAMPED LT WING EMERGENCY LIGHT ASSEMBLY IAW B717 AMM 33-51, OPS CHECK NORMAL.SDR ZZDA2010280Sign · missingEXIT SIGN MISSING AT R1 EXIT DOOR. INSTALLED LENS/SIGN. REF AMM 33-51. OK FOR SERVICE.SDR ZZDA2009101Skin · dentedFUSELAGE SKIN HAS A DENT AT STA 226 AND L-18L. CUT OUT DAMAGED SKIN SECTION LT BETWEEN STA 193 AND 228 AND L-15L TO L-18L, FABRICATED SKIN SECTION, DOUBLERS AND FINGER DOUBLERS, AND INSTALLED REPAIR PARTS PER B717 SRM 53-00-01 REPAIR 6.SDR ZZDA2009100Shear Tie · crackedFUSELAGE INTERIOR FRAME SHEAR TIE CLIP IS CRACKED AT FS 1022 BETWEEN STR 15R AND 16R. FABRICATED NEW SHEAR TIE CLIP AND INSTALLED PER BOEING DRAWING 9912243.SDR ZZDA2009099Seat Track · wornCABIN SEAT TRACK WORN FROM STA 246 TO 265 RBL 22. CUT OUT DAMAGED SECTION OF SEAT TRACK AND INSTALLED SPLICE REPAIR AND NEW SECTION OF SEAT TRACK PER REF EA 17-53-01591IR AND DC9 SRM 53-05 FIG 4F-7001 INSTALLATION.SDR ZZDA2009098Attach Fitting · crackedFUSELAGE AFT SECTION FWD OF VERTICAL STABILIZER REAR SPAR ATTACH TANG STA Y=1178.225 AND LONG 2R TEAR STRAP IS CRACKED PASSING FASTENER HOLE. CUT OUT DAMAGED AREA OF TEAR STRAP ON AFT FUSELAGE SECTION FWD OF VERTICAL STAB REAR SPAR STA Y=1178.225 AND L2R, FABSDR ZZDA2009097Shear Tie · crackedFUSELAGE INTERIOR FRAME SHEAR TIE CLIP IS CRACKED AT FS 1022 BETWEEN STR 13R AND 14R. CUT OUT DAMAGED AREA OF CLIP, FABRICATED REPAIR ANGLE AND FILLER, AND INSTALLED ANGLE REPAIR AND FILLER ON FRAME SHEAR TIE CLIP PER REF BOEING REPAIR SKETCH CQT-CQT-09-0023-SDR ZZDA2009096Longeron · corrodedCABIN LONGERON CORRODED STA 160-220 LBL 7. BLENDED CORROSION BYL. REMOVED AND REPLACED FLOOR TRACK LONGERON.SDR ZZDA2009138Pan · corrodedAFT CARGO COMPARTMENT DOOR CUTOUT LOWER PAN HAS CORROSION. CUT OUT LOWER SECTION OF AFT CARGO DOOR CUTOUT LOWER PAN, FABRICATED AND INSTALLED NEW SECTION OF LOWER PAN AND SPLICES PER B717 SRM 53-20-15 REPAIR 7.SDR ZZDA2009095Cusp Web · crackedLT CABIN STA 660 STR 18L CUSP LINE WEB CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER B717 SRM 51-40-02.SDR ZZDA2009094Cusp Web · crackedRIGHT SIDE CABIN STA 389 STR 18R CUSP LINE WEB HAS CORROSION. CUT OUT DAMAGE, INSTALLED DOUBLER REPAIR ON RIGHT STA 389 STR 18R PER REF B717 SRM 51-70-10 FIG 201 SHEET 2.SDR ZZDA2009093Cusp Web · crackedAT CABIN FLOOR STA 680 AND LBL 48 CUSP WEB HAS A CRACK. CUT OUT DAMAGED WEB SECTION, FABRICATED AND INSTALLED DOUBLER REPAIR AT STA 680 LBL 48 PER REF B717 SRM 51-70-10 REPAIR 2.SDR ZZDA2009092Floor Support · damagedFLOOR SUPPORT WEB HAS A HOLE LOCATED 6FT AFT OF R1 DOOR AFT DOOR FRAME. CUT OUT DAMAGE SECTION AND INSTALLED TYPICAL WEB REPAIR PER REF B717 SRM 51-70-10 REPAIR 2 FIG 201.SDR ZZDA2009091Skin · dentedFUSELAGE SKIN HAS A DENT AT APPROX STA 237 AND LONG 18L. CUT OUT DAMAGE AREA ON LT FUSELAGE SKIN FROM STA 229 TO 245 BETWEEN L-16L TO 18L. FABRICATED AND INSTALLED SKIN REPAIR PER REF B717 SRM 53-00-01.SDR ZZDA2009090Floor Support · damagedCABIN FLOOR SUPPORT WEB HAS A HOLE LOCATED 6 INCHES I/B OF R1 DOOR THRESHOLD. CUT OUT DAMAGED SECTION OF WEB, FABRICATED AND INSTALLED DOUBLER REPAIR AND FILLER PER REF B717 SRM 51-70-10 REPAIR 2 FIG 201.SDR ZZDA2009089Cusp Web · corrodedFUSELAGE INTERIOR RT SIDE CUSP WEB HAS CORROSION BETWEEN FS 579 AND FS 598. INSTALLED NEW CUSP WEB AT FUSELAGE INTERIOR RT SIDE BETWEEN FS 579 AND 598. REF B717 SRM 51-40-02 AND SRM 51-40-05.SDR ZZDA2008131Engine · failedDEPARTING 12R THE LEFT ENGINE FAILED AT ABOUT 300' AGL. HIGH TGT NOTED. NO BIRDS SIGHTED. OVERWEIGHT LANDING AT 109K. FOUND NR 1 ENGINE FODDED DUE TO INTERNAL FAILURE. REMOVED AND REPLACED ENG IAW W/C 603 ON W/O 177916. ALL OPERATIONS NORMAL - AUTOLAND CSDR ZZDA2007298Pan · corrodedFWD CARGO DOOR LOWER PAN, CUT OUT HAS CORROSION. INSTALLED LOWER SECTION OF JAMB PAN BETWEEN STA 370 & 427 AND SPLICED REPAIR PER SRM 53-20-15 REPAIR 6.SDR ZZDA070622182Pump · inoperativeON TAKEOFF RECEIVED -A- RIGHT HYD PRESSURE LOW, RIGHT QUANTITY LOW, AND HYDRAULIC POWER OFF. THERMAL PLUG BLOWN, REMOVED AND REPLACED NR 2 EDP AND ELECTRIC AUX PUMP. SERVICED SYSTEM, ALL OPS NORMAL.SDR AT0400012Wire · brokenEMERGENCY LIGHTS AT ROW 3F INOPERATIVE. RETERMINATED BROKEN WIRE AT SEAT ROW 3 DISCONNECT IAW SWPM 20-31-00. FUNCTIONAL CHECK NORMAL IAW AMM 33-51-00.SDR AT0700027Bulkhead · bentFUSELAGE STA 37 BULKHEAD WEB AND FLANGE ARE BENT ON LEFT EDGE BETWEEN LONGERON 18L AND NLG WHEEL WELL CUTOUT. INSTALLED FRAME SECTION AND SPLICE AT FUSELAGE BS 37 BETWEEN LONGERON 18L AND MLG WHEEL WELL PER RES NUMBER 02-0547 AND B717 SRM 53-10. MATERIAL USESDR AT0100177Engine · malfunctionedON TAKE OFF CLIMB NR 1 ENGINE SURGE FOLLOWED BY ENGINE FLAME OUT. CORRECTIVE ACTION: REMOVED AND REPLACED NR 1 ENGINE. IAW 717 MM 72-00SDR AT0000488Power Supply · inoperativeFOUND DURING SERVICE CHECK EXTERIOR EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING TEST. CORRECTIVE ACTION: REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT BATTERY PACK/POWER SUPPLY. IAW 717 MM 33-50SDR AT0000332Light · inoperativeFOUND EMERGENCY PATH LIGHT LIGHTS INOPERATIVE AT SEAT 22 DEF. RE-CONNECTED PLUG AT SEAT 22 DEF IAW 717 MM 25-23-05.
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