N921AT
Service difficulty reports · 236
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 = 'N921AT' 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 = 'N921AT' 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 DALA2018051403370Frame · crackedCRACK ON FRAME STA Y=1039 AND LONGER 17R AT AFT ACCESSORY COMPARTMENT. FRAME ON STA Y=1039 AND LONGER 17R WAS REPAIRED PER SRM 53-20-07 FIG. 201 REPAIR 4.SDR DALA201805143292Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 222UF. THE FLOOR PANEL WAS FABRICATED AND REPLACED IAW SRM 53-20-50-2R.SDR DALA201805143288Floor Panel · crackedCRACKED FLOOR PANEL 222DF. THE FLOOR PANEL WAS REPLACED SRM 53-20-50-2R.SDR DALA201805143287Gusset · crackedCRACKED GUSSET AT BS 1022, LONGERON 7R. REPAIRED IAW ER/A 568440-14, REV ORIG, AND ETI-17-18-080, REV 1.SDR DALA201805143286Gusset · crackedCRACKED GUSSET AT BS 1022, LONGERON 7L. REPAIRED IAW ER/A 568440-14, REV ORIG. AND ETI-17-18-080, REV 1.SDR DALA2018051003285Cusp Web · corrodedCORRODED RT CUSP WEB BETWEEN BS 385 & 391, X-44 TO X-60. REPAIRED IAW SRM 53-00-55 2R, FIG 217.SDR DALA2018051003284Fairing · crackedCRACKED FIXED FAIRING OF GEARED TAB INBOARD PUSH ROD ON THE LT ELEVATOR. REPAIRED IAW SRM 55-00-00-2R-1-.SDR DALA2018051003283Access Panel · crackedCRACKED ACCESS PANEL 370AL ON THE VERTICAL STABILIZER. REPAIRED IAW SRM 55-00-00-2R-2, & SRM 51-41-02-0G.SDR DALA2018051143282Frame Angle · crackedCRACKED FRAME ANGLE AT BS 1022 BETWEEN LONGERONS 16 - 16R. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA2018051003281Access Panel · corrodedCORROSION ON THE COUNTERSINK HOLES OF THE FUEL ACCESS PANEL 141AL, AT THE CENTER TANK. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.SDR DALA201805143280Cusp Web · crackedCRACKED LT CUSP WEB BS 665, X 44 TO X 54. REPAIRED IAW SRM 53-00-55-2R-4, FIG 221.SDR DALA201805143279Access Panel · corrodedCORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF THE FUEL ACCESS PANEL 520JB, LT WING. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.SDR DALA201805143278Access Panel · corrodedCORROSION FOUND ON THE COUNTERSINK HOLES OF THE FUEL ACCESS PANEL 520QB, LT WING. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.SDR DALA201805143277Cusp Web · crackedCRACKED RT CUSP WEB, BS 651 AND 655, X-54 TO X-60. REPAIRED IAW SRM 53-00-55-2R, FIG 221.SDR DALA201805143276Cusp Web · corrodedCORROSION FOUND ON THE RT CUSP WEB BETWEEN BS 427 TO 430, X-44 TO X-60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 211.SDR DALA201805143275Access Panel · damagedTHE FUEL ACCESS PANEL 141AL WAS FOUND DAMAGED OUT OF LIMITS IAW SRM 57-10-01-2R, PAR 5. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00.SDR DALA201805143274Floor Support · crackedFLOOR SUPPORT BS 737, X-56 WAS FOUND CRACKED. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA201805143273Floor Support · corrodedCORROSION ON THE FLOOR SUPPORT AT X 44 BETWEEN BS 160 - 198. THE CORROSION WAS REMOVED IAW SRM 51-10-04-0G, PAR. 26. FOUND TO BE OUT LIMITS IAW SRM 53-00-00-1A, FIG 103, SHEET 1. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-08.SDR DALA201805143272Cusp Web · crackedCRACKED CUSP WEB BETWEEN BS 218 TO 232. THE CUSP WEB WAS REPLACED IAW SRM 51-41-02-0G, AND DWG 9930538 RE. CC.SDR DALA201805143271Cusp Web · corrodedCORROSION FOUND ON THE RT CUSP WEB BETWEEN BS 427 TO 430, X-44 TO X-60. REPAIRED IAW SRM 53-00-55-2R, FIG 211.SDR DALA201805143270Web · corrodedCORROSION FOUND ON THE DOOR FRAME WEB BS 200, X=56. REPAIRED IAW SRM 53-00-00-2R, FIG 201.SDR DALA2018050903269Access Panel · corrodedCORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 620GB ON THE RT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00.SDR DALA2018050903268Doubler · corrodedCORROSION ON THE PRODUCTION DOUBLER. THE DOUBLER WAS REPLACED IAW DWG 9936534, ITEM 179, REV BW, AND SRM 51-41-02.SDR DALA201805143265Floorbeam · corrodedCORROSION ON THE FLOORBEAM BS 180, X-10 TO X-43. THE FLOORBEAM WAS REPLACED IAW SRM 53-10-51-0I-2, AND 51-41-01-0G.SDR DALA201805143264Floor Support · corrodedCORROSION ON FLOOR SUPPORT, X=7, BS 200 CABIN. THE FLOOR SUPPORT WAS REPLACED IAW SRM 53-10-51-0I-2, AND 51-41-01-0G.SDR DALA2018051403323Scuff Plate · crackedCRACKED SCUFF PLATE ON THE FWD R1 SERVICE DOOR. THE SCUFF PLATE WAS WELDED IAW ETI 17-18-089, REV ORIGINAL, AND ER/A 568360-14, REV ORIGINAL.SDR DALA2018051403322Access Panel · corrodedCORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 520DT ON THE LT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00.SDR DALA2018051403321Access Panel · corrodedCORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 620DB ON THE RT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00.SDR DALA201805153320Access Panel · corrodedCORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 620FT, RT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00.SDR DALA201805173100Cusp Web · crackedCRACKED LT CUSP WEB BS 647 AND 665, X 44 TO X 54. THE CUSP WEB WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 9910151, REV CH.SDR DALA201805173099Cusp Web · crackedCRACKED RT CUSP WEB, BS 670, X -54 TO X -60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 223.SDR DALA2018051703098Cusp Web · crackedCRACKED LT CUSP WEB BETWEEN BS 660 AND 665, X 54 TO X 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 203, AND 51-41-02-0G.SDR DALA2018051703097Frame Angle · crackedCRACKED FRAME ANGLE AT BS 1022, BETWEEN LONGERONS 16 - 17L. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA2018051703096Frame Angle · crackedCRACKED FRAME ANGLE AT BS 1022, BETWEEN LONGERONS 13 - 14R. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA2018051703095Longeron · crackedCRACKED LONGERON 17L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2, FIG 201.SDR DALA2018051703094Cusp Web · crackedCRACK ON THE LT CUSP WEB, BETWEEN BS 908 AND 912, X 54 TO X 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215.SDR DALA2018051703004Plate · corrodedCORROSION ON THE RT PLATE BETWEEN BS 1037 - 1053, X-57 TO X-60. THE PLATE WAS REPLACED IAW SRM 51-41-02-0G, AND DWG 9981474, REV L.SDR DALA2018050102956Doubler · wornWORN RT PRODUCTION DOUBLER Z=11 IN THE AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR. THE DOUBLER WAS REPAIRED IAW SRM 52-10-02-2R, PROCEDURE 16, REPAIR 16.SDR DALA2018050202978Pan · crackedRT WINDOW RING PAN CRACKED, FWD UPPER CORNER, BS 351. REPAIRED IAW SRM 56-20-02-2R1 FIG. 202.SDR DALA2018050102955Doubler · wornWEAR ON PRODUCTION DOUBLER LOWER SURFACE FROM BS 370 TO 416, THE FWD CARGO DOOR. THE DOUBLER WAS REPLACED IAW DWG 5910141, REV FE, AND SRM 51-41-02-0G.SDR DALA2018050102954Pan · crackedCRACKED LT WINDOW RING PAN FWD LOWER CORNER BS 832, 851, 889, AND 908. THE PAN WAS REPAIRED IAW SRM 56-20-02-2R1 FIG.202.SDR DALA2018040202117Lamp · inoperativeTHE LEFT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE LAMP IAW AMM 33-51. OPS CHECKED GOOD.SDR DALA2017110908081Lens · missingEMERGENCY EXIT DIFFUSER LENS MISSING ABOVE ROW 29.SDR DALA2017060804557Sign · inoperativeEMERGENCY EXIT SIGNS INOPERATIVE. LENS COVER IS MISSING. INSTALLED SIGN. OPERATIONAL CHECKED NORMAL.SDR DALA2016120209462Lens · unknownTHE FLIGHT ATTENDANT DISCOVERED THAT THE OVERWING EXIT PATH AT 29C EMERGENCY EXIT SIGN HAD A DAMAGED OR MISSING LENS/COVER. MAINTENANCE INSTALLED THE LENS/COVER AND THE OPERATIONAL CHECK WAS GOOD.SDR DALA2016103107969Support · corrodedVERTICAL SUPPORT AT BS 1028 AFT BULKHEAD IN AFT CARGO BAY CORRODED. REPLACED THE SUPPORT IAW DRAWING 5965788-15A.SDR DALA2016042503266Cam · dislodgedDURING A CHECK OF TAILCONE RELEASE MECHANISM, MAINTENANCE FOUND THE CAM ASSY FOR THE TAILCONE LATCH WAS DISLODGED. MAINTENANCE REINSTALLED THE CAM ASSY. THE TAILCONE WAS RIG CHECKED AFTER INSTALLATION AND FOUND OPERATIONAL. THE RII COMPLETED FOLLOWING MAINTSDR DALA2016042303186Longeron · corrodedAFT CARGO BAY- L23R CORRODED AT BS 1008. REPAIRED IAW SRM 53-00-05, REPAIR 2.SDR DALA2016042303185Longeron · corrodedL30 CORRODED AT STA 1038. REPAIRED IAW SRM 53-20-07, REPAIR 3, DWG 9912243.SDR DALA2016042303184Frame · corrodedAFT CARGO BAY- FRAME AT BS 1028 IS CORRODED FROM L28L TO L28R. REPAIRED FRAME SECTION IAW SRM 53-20-07, REPAIR 3.
Back to N921AT