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 DALA2023050903613Unknown · unknownCORROSION WAS FOUND ON FITTING END OF LONGERON 23 RH STA 1053 AFT CARGO COMPARTMENT. SUMMARY OF NRC 00185: LEVEL CORROSION II. FITTING (END LONGERON) ON LONGERON 23 RH STA 1053 AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-40-08-0G. (LP #2757963)SDR DALA2023050203395Unknown · unknownCORROSION ON AFT PRESSURE BULKHEAD DOME WEB FORWARD FACE LOW AREA STA Y=1053 BTW LONGERON 29L AND 28R AT AFT CARGO COMPARTMENT. ORIGINAL THICKNESS OF 0.063IN AND REMAINING THICKNESS OF 0.045IN,.THE AREA REWORKED IS OUT OF LIMITS PER B717-200 SRM 53-20-08-2R PRSDR DALA2023041803049Unknown · unknownIN REFERENCE NRC 0014: AFTER DOOR STOP #3 REMOVAL, CRACK WAS FOUND BELOW AFT EDGE OF AFT CARGO COMPARTMENT. SUMMARY OF NRC 00171: PAN OF AFT EDGE OF AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 8 REPAIR 8. PAR 4.A.(1). FIGURE 201. SDR DALA2022100406441None · noneLEFT HAND WING UPPER SURFACE HAS CORROSION AT XRS 310 STR 6. MAINTENANCE SMOOTHED AND BLENDED THE CORROSION ON THE LFT HAND WING AT XRS 315 STR 6 PER B717 SRM 57-10-01. MEASURED AREA AFTER BLENDOUT PER B717 SRM 57-10-01-1A-1 FIG 105 SHEET 3 AND FOUND AREA AT XSDR DALA2022091906177None · noneFOUND ROW 21 LEFT AND RIGHT OVER WINDOW EXIT SIGN LIGHTS INOPERATIVE DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE BATTERY PACK B5-230 IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD AND ALL LIGHTS ILLUMINATE. AIRCRAFT OK FOR SERVICE. (LP #9098652)SDR DALA2022031801804None · noneNLG RETRACT SCISSORS LINK BOLT COTTER KEY CUT INTO CENTER LT SUPPORT WEB IN RETRACT POSITION (FOUND ON FREE FALL). NO ALLOWABLE DAMAGE PER B717 SRM. REMOVED DAMAGED SUPPORT WEB. FABRICATED, DRILLED, AND INSTALLED STIFFENERS ON NEW SUPPORT WEB. TREATED, PRIMED,SDR DALA2021042802440Skin · corrodedCORROSION ON INNER SKIN STA 966-977 AT AFT CARGO DOOR CUTOUT. REPAIRED PER ER/A 591210-14 REV ORIG ON NON-ROUTINE CARD 271. (LP #1793130)SDR DALA2021042602400Door Frame · corrodedTHE AFT CARGO DOOR JAMB IS CORRODED ALONG LOWER EDGE. MARKED. REPLACED C2 DOOR JAMB PAN PER B717 SRM 51-41-00. AFT CARGO DOOR JAM PAN WAS TRIMMED, DRILLED, PAINTED, AND INSTALLED PER B717 SRM 53-20-15-2R. ALL WORK ABOVE ACCOMPLISHED BY B717 RII QUALIFIED INSP.SDR DALA2021033001873Battery Pack · inoperativeTHE OVERHEAD EMERGENCY LIGHTS AT ROW 15-18 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-120 REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7576411)SDR DALA2021021600833Battery · missingFOUND CARGO EMERGENCY EXTERIOR LIGHTS POWER SUPPLY BATTERY MISSING. REPLACED BATTERY PER B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #7614440)SDR DALA2021021600835Lens · missingTHE EMERGENCY LIGHT IN THE AFT TAIL COMPARTMENT IS MISSING THE LENS. MAINTENANCE INSTALLED THE LENS ON THE EMERGENCY VENTRAL LIGHT PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7614434)SDR DALA2021010600056Flashlight · inoperativeTHE EMERGENCY LIGHT BATTERY POWER SUPPLY IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY, REF B717 AMM 33-51-03.SDR DALA2019042502630Release Mech · inoperativeMAINTENANCE FOUND THE TAILCONE RELEASE MECHANISM DOOR TAPED SHUT WITH THE DECAL. DURING REMOVAL, THE TAIL CONE WAS DEPLOYED, BUT THE SLIDE DID NOT DEPLOY. MAINTENANCE THEN FOUND THE LANYARD BROKEN ON THE DEPLOYED TAIL CONE AND REPLACED THE TAIL CONE WITH A NEWSDR DALA2019041542428Door Frame · corrodedCORROSION ON LOWER DOOR JAMB FROM STA=954 TO 985 AT AFT CARGO COMPARTMENT (C2). NRC 00238: CORROSION LEVEL2, LOWER DOOR JAMB FROM STA=954 TO 985 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R-7.SDR DALA2019041542427Door Frame · corrodedCORROSION ON LOWER/RH FWD FACE AT DOOR JAMB VENTRAL DOOR. CORROSION LEVEL2, LOWER/RH FWD FACE AT VENTRAL DOOR JAMB WAS REPAIRED PER ETI-17-19-052 REV. 3 AND ER/A 577238-14 REV. ORIGINAL.SDR DALA2019041542426Hinge · damagedFREE PLAY DUE TO ELONGATED HOLES AT OUTBOARD FLAP HINGE LH WING (AI). LH OUTBOARD FLAP HINGE WAS REPAIRED PER ETI-17-19-059 REV 2. AND ER/A 577279-14 REV. ORIGINAL. FREE PLAY WAS CORRECTED.SDR DALA2019041432425Skin · crackedCRACK AT FUSELAGE SKIN STA 1076 LONG 14 LH. (FUS). NRC 00568: FUSELAGE SKIN STA 1076 LONG 14 LH WAS REPAIRED PER ETI-17-19-053 REV. 2 AND ER/A 577167-14 REV. ORIGINAL. ASSOCIATED ER/A 14-577167 ADDED FOR AC 9501. (LP #1028464)SDR DALA2019041532424Skin · crackedFOUND 2 CRACKS IN FUSELAGE SKIN AT STA 1022 LONG 14 RH. (FUS). NRC 00569: FUSELAGE SKIN STA 1022 LONG 14 RH WAS REPAIRED PER ETI-17-19-051 REV 3 AND ER/A 577210-14 REV. ORIGINAL. ASSOCIATED ER/A 14-577210 ADDED FOR AC 9501. (LP #1028458)SDR DALA2019041202396Skin · crackedCRACK AT FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14RH. (FUS). NRC 00571: FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14RH WAS REPAIRED PER ETI-17-19-056 REV. 2 AND ER/A 577171-14 REV. ORIGINAL. ASSOCIATED ER/A 00-577171 ADDED FOR AC 9501.SDR DALA2019041202395Cargo Track · corrodedEXCESSIVE CORROSION AT FWD CARGO COMPARTMENT RH TIE TRACK BETWEEN STA 588/655 IN REF NRC 00264. (CCD). NRC 00612: CORROSION LEVEL 2, TIE TRACK WAS REPLACED PER B717- 200 SRM 51-41-01 AND 51-41-02 0G.SDR DALA2019041002371Gusset · crackedCRACK ON GUSSET AFT FACE OF ENGINE PYLON SUPPORT BULKHEAD AND LONG 7LH AT PAX CABIN. NRC 00377: GUSSET WAS REPAIRED PER ETI-17-19-048 REV.2 AND ER/A 577138-14 REV. ORIGINAL. (LP #1024147)SDR DALA2019041002370Gusset · crackedCRACK ON GUSSET AFT FACE OF ENGINE PYLON SUPPORT BULKHEAD AND LONG 7RH AT PAX CABIN. NRC 00376: GUSSET WAS REPAIRED PER ETI-17-19-048 REV. 2 AND ER/A 577138-14 REV. ORIGINAL. ASSOCIATED ER/A 00-577138 ADDED FOR AC 9501. (LP #1024144)SDR DALA2019041002369Fitting · crackedCRACK ON RIGHT MAIN FRAME WING TO FUSELAGE FITTING, LONGERON NUMBER 22. NRC 00464: FITTING WAS REPLACED PER B-717-200 SRM 51-41-05-0G AND 51-41-01-0G. (LP #1023991)SDR DALA2019040902320Floor Support · corrodedCORROSION AT FLOOR SUPPORT ELEMENTS BETWEEN STA 1022/1076 AND X-22 (W2) IN REF NRC 00537. NRC 00574: CORROSION LEVEL 2, FLOOR SUPPORT WAS OUT OF LIMITS BETWEEN STA 1022/1076 AND X-22 AND WAS REPLACED PER B-717-200 SRM 51-41-01 AND DWG #9936656 REV. AM. (LP #10SDR DALA2019040902319Skin · corrodedCORROSION AT FUSELAGE SKIN SPLICE STA 1037 BETWEEN LONG 18/20RH. (W2). NRC 0538: CORROSION LEVEL 2, WAS DETERMINED TO BE OUT OF LIMITS PER B717-200 SRM 53-00-00-1A FIGURE 103 (SHEET1). SKIN SPLICE STA 1037 BETWEEN LONG 18/20RH WAS REPLACED PER B717-200 SRM 51-SDR DALA2019040802302Longeron · crackedCRACK ON LONGERON 5RH AT STA 1022. (CPAX). NRC 00494: LONGERON 5RH AT STA 1022 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1021073)SDR DALA2019040802299Longeron · crackedCRACK ON LONGERON 13RH AT STA 1037 (CPAX). NRC 00498: LONGERON 13RH AT STA 1037 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1020787)SDR DALA2019040802298Fitting · crackedCRACK ON INNER FITTING STA Y=954 AND BEAM #3. AFT CARGO COMPARTMENT(FYT). NRC 00604: INNER FITTING STA Y=954 AND BEAM #3 AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 DWG #3914025 REV. C AND B717-200 SRM 51-41-05-0G. (LP #1020512)SDR DALA2019040872297Longeron · crackedCRACK ON LONGERON 16LH AT STA 1022 (CPAX). NRC 00493: CRACK ON LONGERON 16LH AT STA 1022 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1019714)SDR DALA2019040872296Former · crackedCRACK ON KEEL BEAM FORMER RH SIDE STA Y=715 AND X=-37.(FYT). NRC 00594: FORMER RH SIDE STA Y=715 AND X=-37 WAS REPAIRED PER B717-200 SRM 51-70-11-2R REP 1. (LP #1019506)SDR DALA2019040872295Former · crackedCRACK ON KEEL BEAM FORMER LH SIDE STA Y=655 AND X=21.(FYT). NRC 00593: FORMER LH SIDE STA Y=655 AND X=21 WAS REPAIRED PER B717-200 SRM 51-70-11-2R REP 1. (LP #1019503)SDR DALA2019040872294Former · crackedCRACK ON KEEL BEAM FORMER RH SIDE STA Y=655 AND X=-21. FORMER RH SIDE STA Y=655 AND X=-21 WAS REPAIRED PER B717-200 SRM 51-70-11-2R REP 1. (LP #1019497)SDR DALA2019040602254Keelbeam · crackedCRACK ON KEEL BEAM FORMER RH SIDE STA Y=696 AND X=-30.(FYT). NRC 00591: FORMER RH SIDE STA Y=696 AND X=-30 WAS REPAIRED PER B717-200 SRM 51-70-11-2R REP 1.SDR DALA2019040602253Keelbeam · crackedCRACK ON KEEL BEAM FORMER LH SIDE STA Y=696 AND X=30.(FYT). NRC 00590: FORMER LH SIDE STA Y=696 AND X=30 WAS REPAIRED PER B717-200 SRM 51-70-11-2R REP 1. (LP #1018524)SDR DALA2019040402153Floor Panel · damagedHOLE ON FLOOR PANEL 211ANF AT COCKPIT (CPIL). NRC 00598: FLOOR PANEL 211ANF WAS FABRICATED, REPLACED, AND IDENTIFIED PER B717-200 SRM 53-20-50 2R REP.3. (LP #1015597)SDR DALA2019040302114Access Panel · corrodedCORROSION IN ACCESS #520FT ON SETTLEMENT AREA AND COUNTERSINK HOLES AT FUEL TANK LEFT. (AI). NRC 00565: CORROSION LEVEL 2, CORROSION ON FUEL ACCESS PLATE #520FT AT SETTLEMENT AND COUNTERSINK HOLES AREA WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26, WAS FOUNDSDR DALA2019040302116Longeron · crackedCRACK ON LONGERON 8RH AT STA 1022. (CPAX). NRC 00497: LONGERON WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1014057)SDR DALA2019040302115Longeron · crackedCRACK ON LONGERON 6RH AT STA 1022. (CPAX). NRC 00495: LONGERON WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1014048)SDR DALA2019040302113Access Panel · corrodedCORROSION ON COUNTERSUNK AND SETTLEMENT ON FUEL ACCESS PLATE #620FT AT FUEL TANK RIGHT. (AD). NRC 00577: CORROSION LEVEL 2, CORROSION ON FUEL ACCESS PLATE #620FT AT SETTLEMENT AND COUNTERSINK HOLES AREA WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26, WAS FOUNSDR DALA2019040302112Access Panel · corrodedCORROSION ON COUNTERSUNK AND SETTLEMENT ON FUEL ACCESS PLATE #520DB AT FUEL TANK LEFT. (AI). NRC 00576: CORROSION LEVEL 2, CORROSION ON FUEL ACCESS PLATE #520DB AT SETTLEMENT AND COUNTERSINK HOLES AREAS WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26, WAS FOUNSDR DALA2019040302111Access Panel · corrodedCORROSION IN ACCESSES 520CT AND 620CT ON SETTLEMENT AREA AND COUNTERSINK HOLES AT FUEL TANK. (AI) (AD). NRC 533: CORROSION LEVEL 2, ACCESS PLATES 520CT AND 620CT WERE REPLACED PER B-717 SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION III. (LP #1013646)SDR DALA2019040322110Cusp Web · corrodedCRACK ON CABIN FLOOR CUSP WEB AT STA 775 X=57 (CPAX). NRC 00302: CUSP WEB AT STA 775 X=57 WAS REPAIRED PER B717-200 SRM 53-00-55-2R FIG. 206. (LP #1012553)SDR DALA2019040322109Cusp Web · corrodedCORROSION OUT OF LIMITS AT PASSENGER CABIN CUSP WEB BETWEEN STA 862-870 X-54/X-60. IN REF NRC 00309. NRC 00581: CORROSION LEVEL 2, CUSP WEB WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4- FIG. 211, 51-41-02-0G, AND 51-41-05-0G. (LP #1012544)SDR DALA2019040322108Cusp Web · corrodedCORROSION OUT OF LIMITS AT PASSENGER CABIN CUSP WEB BETWEEN BS 889-896 X-54/X-60. IN REF NRC 00309. NRC 00582: CORROSION LEVEL 2, CUSP WEB BETWEEN STA 889-896 X-54/X-60 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 215. (LP #1012536 )SDR DALA2019040202073Seat Track · crackedCRACK ANGLE STA Y=715 AND X=-43 BELOW SEAT TRACK AT WING BOX. NRC 00345: ANGLE STA Y=715 AND X=-43 WAS REPLACED PER B717-200 SRM 51-41-05. (LP #1012333)SDR DALA2019040202072Pan · crackedCRACK PAN ON LOWER FWD CORNER AT FWD CARGO COMPARTMENT DOOR (CCD). NRC 00364: CRACK PAN ON LOWER FWD CORNER WAS REPAIRED PER B717-200 SRM 52-30-02-2R-1. (LP #1011692)SDR DALA2019033002042Fitting · crackedCRACK ON FITTING STA Y=737 AND X=-44 BELOW SEAT TRACK AT WING BOX. NRC 00344: FITTING STA Y=737 AND X=-44 WAS REPLACED PER SRM 51-41-05. (LP #1008181)SDR DALA2019033002041Pan · crackedCRACK PAN ON BEAM 5 CORNER AT FWD CARGO COMPARTMENT DOOR(CCD). NRC 00412: CRACK PAN ON BEAM 5 CORNER AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER SRM 52-30-02-2R-1. (LP #1007676)SDR DALA2019033002040Pan · crackedCRACK PAN ON UPPER AFT CORNER AT FWD CARGO COMPARTMENT DOOR(CCD). NRC 00239: CRACK PAN ON UPPER AFT CORNER AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER SRM 52-30-02-2R-1. (LP #1007668)SDR DALA2019032901984Fitting · crackedCRACK ON FITTING STA Y=737 AND X=44 BELOW SEAT TRACK AT WING BOX. NRC 00343: FITTING STA Y=737 AND X=44 WAS REPLACED PER SRM 51-41-05. (LP #1006757)
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