N927AT
Service difficulty reports · 218
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 = 'N927AT' 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 = 'N927AT' 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 DALA2022100506465None · noneDURING THE SERVICE CHECK, THE OVER WING AFT LOWER EMERGANCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENACE REPLACED THE BATTERY PACK AT LOCATION B5-119 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #9128858)SDR DALA2022091206032None · noneDOOR 1 RIGHT GIRT BAR SEEMED TO COME LOOSE FROM SLIDE. PIN CAME LOOSE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE RE-HOOKED THE PIN REF B717 AMM 52-11. VISUAL INSPECTION OK. (LP #923SDR DALA2022060303885Sign · missingTHE EMERGENCY EXIT SIGN COVER IS MISSING AT STA 600. MAINTENANCE INSTALLED THE SIGN COVER LENS. (LP #2261915)SDR DALA2022041302581Frame · corrodedAFTER CORROSION REMOVAL IN FRAME CLIP STA Y=927 LONGERON 29 LH / 29RH, OT=0.050", RT=0.011" WAS FOUND OUT OF LIMITS PER B717-200 SRM 53-00-00-A01. PAR 4.C. (REF. NRC 00080) . SUMMARY OF NRC 00163: CORROSION LEVEL 2, CLIP STA Y=927 LONGERON 29 LH / 29RH WAS REPSDR DALA2022040802420Channel · crackedA CRACK WAS FOUND ON CHANNEL AT STA Y=737 AND X=55 AT RH PASSENGER CABIN. SUMMARY OF NRC 00107: CHANNEL ON STA Y=737 AND X=55 AT RH PASSENGER CABIN WAS REPAIRED PERMANENTLY PER ER/A 598274-14 REV. ORIGINAL SEC.I AND PRI REV. 2. INSPECTION REQUIREMENT WILL BE USDR DALA2022040702383Channel · corrodedCORROSION ON FRAME CHANNEL STA Y=908 BTW LONGERON 29 LH / 29 RHAT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00079: CORROSION LEVEL 2, FRAME CHANNEL STA Y=908 BTW LONGERON 29 LH / 29 RH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3.SDR DALA2022040602326Frame · crackedCRACK ON FRAME STA=1130 BTW STRINGERS 2 AND 3 RH SIDE AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00115: PERMANENT REPAIR WAS PERFORMD ON FRAME STA=1130 BTW STRINGERS 2 AND 3 RH SIDE AT AFT ACCESSORY COMPARTMENT PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIRSDR DALA2022010600094None · noneCAPT WINDSHIELD SHOWED SPARKS TOP LEFT. MAINTENANCE FOUND CAPT WINDSHIELD TEMP SENSOR WIRES TOUCHING SPRING. ADJUSTED WIRES. CAPTS WINDSHIELD HEAT CHECKS GOOD. A/C OK FOR SERVICE. (LP #8297415)SDR DALA2021033001875Lens · missingTHE CABIN CEILING EMERGENCY LIGHT LENS MISSING AT ROW 12. MAINTENANCE INSTALLED LENS COVER. (LP #7578966)SDR DALA2021011900345Battery Pack · inoperativeTHE FRONT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. THE LIGHTS DIRECTLY OVER THE EXITS AND THEY WERE FOUND ON THE SERVICE CHECK. MAINTENANCE REPLACED THE BATTERY PACK B5-230, PER B717 AMM 33-51. OPERATIONAL TEST WERE GOOD.SDR DALA2019111806742Sign · missingTHE EMERGENCY EXIT SIGN ABOVE DOOR 1L IS MISSING AND INOPERATIVE. MAINTENANCE INSTALLED A NEW LENS COVER. EMERGENCY LIGHT EXIT SIGN NOW CHECKS GOOD AT DOOR 1L IAW B717 AMM 33-51. (LP #1361214)SDR DALA2019072804457Battery Pack · dischargedTHE EMERGENCY CEILING LIGHTS AT ROW 10 THRU 13 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-227 REF AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #6005927)SDR DALA2019062803917Lens · missingEMERGENCY EXIT COVER DIFFUSER LENS MISSING AT LOCATION 600. MAINTENANCE REPLACED THE COVER WHICH WAS FOUND ON THE FLOOR. OPERATIONS IS NORMAL AND THE AIRCRAFT IS OKAY TO CONTINUE SERVICE. (LP #1143587)SDR DALA2018121007120Tire · failedSHIP 9572 - THE CREW RETURNED THE AIRCRAFT BACK TO DTW DUE TO VIBRATIONS ON ROTATION. TOWER ALSO REPORTED TIRE DEBRIS WAS LEFT ON THE RUNWAY. THE LANDING GEAR RETRACTED NORMALLY AND ALL OTHER INDICATIONS WERE GOOD, BUT AN EMERGENCY WAS DECLARED. CORRECTIVE ACTSDR DALA2018111986670Battery Pack · inoperativeMULTIPLE EMERGENCY LIGHTS OUT IN THE CABIN. MAINTENACE REPLACED BATTERY PACKS B5-118 AND B5-119 REF B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #4722813)SDR DALA2018041602535Scuff Plate · crackedCRACKED AND ELONGATED HOLES AT AFT CARGO COMPARTMENT SCUFF PLATE. AFT CARGO COMPARTMENT SCUFF PLATE WAS REPAIRED PER ER/A 542149-14MA REV A.SDR DALA2018041502477Frame · corrodedCORROSION ON FRAME BS 1022, BETWEEN LONGERONS 27L TO 27R. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R. HFEC INSPECTION WAS ACCOMPLISHED ON FRAME AFTER TRIM OUT AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001.SDR DALA2018041202369Web · crackedCRACK ON WEB OF VENT LOUVER STA Y=1200 AND 1:00 POSITION APPROX AT AFT ACCESSORY COMPT. WEB OF VENT LOUVER STA Y=1200 AND 1 HRS POSITION WAS REPAIRED PER SRM 53-00-00-2R FIG 201.SDR DALA2018041102328Angle · crackedCRACK ON SPLICE AND ANGLE ON INNER SKIN LT WING L/E STA XOS:296. SPLICE AND ANGLE WERE REPLACED ON INNER SKIN LT WING L/E STA XOS:296 PER SRM 51-41-02-0G, 51-41-05-0G, 57-40-01, AND DWG 9919326 REV E.SDR DALA2018041002316Longeron · crackedCRACKED LONGERON 2R, BS 1134 IN THE AFT ACCESSORY COMPARTMENT AREA. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R, FIG 201.SDR DALA2018040902284Rub Strip · damagedCORROSION, DISBONDED, AND CRACKED RUB STRIPS AT LH FILLET PANELS FROM BS 560 TO 917. THE RUB STRIPS WERE REPLACED IAW SRM 53-20-70-01, AND SRM 51-20-05.SDR DALA2018040802282Skin · crackedCRACKED FUSELAGE SKIN BS 1076, BETWEEN LONGERONS 13R - 14R. THE SKIN WAS REPAIRED IAW ER/A 567482-14 ,REV. ORIGINAL AND ETI-17-18-063 REV. 3.SDR DALA2018040802281Frame Angle · crackedCRACKED FRAME ANGLE, BS 1023, LONGERON 7R. THE FRAME ANGLE WAS REPAIRED IAW ETI-17-18-068, REV 2, AND ER/A 567515-14, REV ORIGINAL.SDR DALA2018040802280Door Frame · crackedCRACKED DOOR FRAME WEB BS 207, LONGERON 11L. THE DAMAGED AREA WAS REPAIRED SRM 53-10-15-2R, PROCEDURE 1.SDR DALA2018040702315Access Panel · corrodedCORROSION OUT OF LIMITS IAW NRC 00520. CORROSION ON FUEL ACCESS PANEL 520EB, LT WING. THE FUEL ACCESS PANEL WAS REPLACED IAW AMM 28-00-00 AND JIC CARD 2040-0010 JOB 001-0295.SDR DALA2018040602231Floor Panel · delaminatedDELAMINATED FLOOR PANELS #211ARF, 211AQF, AND 222APF AT COCKPIT/PAX CABIN. NRC 00711: FLOOR PANELS #211ARF, 211AQF, AND 222APF WERE FABRICATED, REPLACED, IDENTIFIED PER B-717 SRM 53-20-50-2R-3. FLOOR PANELS WERE INSTALLED PER JIC NUMBER 2040-0058. (LP #0496238SDR DALA2018040602625Door · crackedCRACK ON BUTTE DOOR INBOARD TRAILING EDGE LOWER CORNER LT WING. THE BUTTE DOOR WAS REPAIRED IAW SRM 57-00-00-2R, REPAIR 1.SDR DALA2018040602230Seal Depressor · wornWEAR ON THE SEAL DEPRESSOR AND DEPRESSOR SPLICE BS 994, BETWEEN LONGERONS 24R - 25R. REPAIRED IAW SRM 53-20-15-2R-4.SDR DALA2018040602229Slat Track · wornWEAR ON THE SLAT TRACK DOOR NR 8 AT THE LT WING. SLAT TRACK DOOR WAS REPLACED IAW ER/A 540095-14MA, REV A, SECTION II.SDR DALA2018040502191Rub Strip · damagedCORROSION AND DISBONDED RUB STRIPS AT RH FILLET PANELS FROM BS 560 TO 917 IAW AMDS 5331-2003. THE RUB STRIPS WERE REPLACED IAW SRM 51-20-70-0I, AND SRM 51-20-05-0G, PAR 7.SDR DALA2018040502190Strap · crackedCRACKED PYLON TO FUSELAGE STRAP, BS 1178 BETWEEN LONGERONS 16 - 17R. THE STRAP WAS REPLACED IAW SRM 51-41-01-0G, SRM 51-41-05-0G, AND DWG 5966498, REV T.SDR DALA2018040402174Former · crackedCRACKED FORMER ON STA Y=679,Y=694, AND Y=715 RH SIDE AT CANTED KEEL INTERNAL STRUCTURE. (FUS). NRC 00573: FORMERS WERE REPAIRED PER B717 SRM 51-70-11 REPAIR 1. (LP #0492941)SDR DALA2018040402175Fitting · crackedCRACKED RT FITTING BS 664, RBL 19. THE FITTING WAS REPLACED IAW SRM 51-41-02-0G AND SRM 51-41-05-0G.SDR DALA2018040402173Beam · crackedCRACKED BEAM NR 1 BS 206. THE BEAM WAS REPLACED IAW SRM 51-41-02-0G, 51-41-04-0G, 51-41-05-0G, DWG 9911582 REV T, AND 9911579 REV L.SDR DALA2018040302140Channel · crackedCRACKED CHANNELS ON FLOOR PANELS #222AF, 223EF, AND 222ZF. (CPAX). NRC 00605: FLOOR PANELS WERE REPAIRED PER B717 SRM 53-20-50-2R-5. HFEC INSPECTION WAS ACCOMPLISHED ON CHANNELS ON FLOOR PANELS #222AF, 223EF, AND 222ZF NO CRACKS WERE FOUND AFTER STOP DRILLS PESDR DALA2018040302142Seat Track · corrodedCORRODED SEAT TRACK RBL 44, BETWEEN BS 237, AND 240. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-20-52-2R-1, FIG 201, REPAIR 1.SDR DALA2018040302141Stop Fitting · crackedCRACK ON STOP FITTING AT THE AFT ENTRY DOOR FRAME, LONGERON 14R. THE STOP FITTING WAS REPLACED IAW SRM 51-41-01-0G, AND 51-41-02.SDR DALA2018040302139Former · crackedCRACKED FORMER BS 679. THE FORMER WAS REPAIRED IAW SRM 51-70-11, REPAIR 1.SDR DALA2018040302138Frame Angle · crackedCRACK ON THE FRAME ANGLE BS 1021, LONGERON 14L. REPAIRED IAW SRM 53-00-06-2R.SDR DALA2018040302137Floorbeam · crackedCRACKED FLOORBEAM ANGLE BS 120 LBL 50 & RBL 50. REPLACED THE ANGLE IAW SRM 51-41-02-0G, 51-41-05-0G, 51-41-08-0G, AND DWG 9911559, REV A.SDR DALA2018040302136Frame · crackedCRACKED FRAME ANGLE BS 1021, LONGERON 16L. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 9912243, REV JS.SDR DALA2018040302135Intercostal · crackedCRACKED INTERCOSTAL BETWEEN BS 617 - 636. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00-2R, REPAIR 1.SDR DALA2018040202172Floor Panel · delaminatedDELAMINATION ON FLOOR PANELS #221AF, 221BF, 221CF, 221DF, AND 221KF AT PAX CAB (CPAX)(W1). NRC 00611: FLOOR PANELS #221AF, 221BF, 221CF, 221DF, AND 221KF AT PAX CAB WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SRM 53-20-50-2R-3. FLOOR PANELS WERE INSTALSDR DALA2018040202112Floor Panel · delaminatedDELAINATION ON FLOOR PANELS #221VF, 222CF 222DF, 222GF, 222JF, 222QF, AND 222PF AT PAX CAB (CPAX) (FWD PANELS). NRC 00613: FLOOR PANELS #221VF, 222CF, 222DF, 222GF, 222JF, 222QF, AND 222PF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SRM 53-20-50-2R-3. SDR DALA2018040202624Skin · dentedDENTS ON LOWER SKIN ON THE RT FWD FLAP MOVEABLE VANE. LOWER FLAP VANE SKIN WAS REPAIRED IAW SRM 57-53-01-2R, PROCEDURE 1, REPAIR 1, PARAGRAPH 4.SDR DALA2018040202623Skin · dentedDENT ON UPPER SKIN, 16 INCHES FROM ROOT TO TIP AND 12 INCHES FROM TRAILING EDGE TO LEADING EDGE, ON THE RT AFT FLAP MOVEABLE VANE. THE UPPER SKIN WAS REPAIRED IAW SRM 57-53-01-2R, PROCEDURE 1, REPAIR 1, PARAGRAPH 4.SDR DALA2018040202114Access Panel · crackedCRACKED FUEL TANK ACCESS PANEL 520CB ON THE LT WING. THE ACCESS PANEL WAS REPLACED.SDR DALA2018040202113Angle · crackedCRACKED VERTICAL ANGLE AT BS 737, BELOW THE SEAT TRACK RBL 44. THE ANGLE WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 9923417, REV B.SDR DALA2018040202111Floor Panel · crackedCRACKED FLOOR PANEL 221EF. THE FLOOR PANEL WAS FABRICATED, AND REPLACED IAW SRM 53-20-50-2R-3.SDR DALA2018040202110Cusp Web · crackedCRACKED CUSP WEB, BS 675, BETWEEN RBL 44 TO 46. REPAIR IAW SRM 53-00-55-2R-4, FIG 221.
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