N982AT
Service difficulty reports · 202
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 = 'N982AT' 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 = 'N982AT' 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 DALA2017071605454Spar Cap · distressedDISTRESS AT LT & RT SIDES OF VERTICAL STABILIZER LE SPAR CAP. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.SDR DALA2017071605453Spar Cap · cracked0.5 INCH CRACK WAS FOUND ON VERTICAL STAB. FRONT SPAR CAP RT SIDE. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.SDR DALA2017071605452Spar Cap · damagedELONGATED HOLES AT THE LT & RT SIDES OF VERTICAL STABILIZER L.E. FRONT SPAR CAP. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.SDR DALA2017071605451Fairing · damagedDURING INSPECTION, AN ELONGATED HOLE ON THE LE REMOVABLE FAIRNG LT SIDE WAS FOUND. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.SDR DALA2017071605447Frame · crackedCRACKED FRAME BS 1022, LONGERON 7R. REPAIRED IAW ETI 17-17-083, REV 1, AND ER/A 559502-14, REV ORIGINAL.SDR DALA2017071605446Frame · crackedCRACKED FRAME BS 1022 ON LONGERON 7L AT PASSENGER CABIN AREA. REPAIRED IAW ETI 17-17-083, REV 1, AND ER/A 559502-14, REV ORIGINAL.SDR DALA2017071505436Door Frame · corrodedCORROSION ON THE LT WEB DOOR FRAME BS 200, LONGERONS 17 AND 18L REPAIRED IAW ETI-17-17-093, REV. 2 AND ER/A 559514-14 REV. ORIGINAL.SDR DALA2017071205387Cargo Track · corrodedCORROSION ON THE RT CARGO TRACK BETWEEN BS 895 & 954, BS 994 & 1022 IN THE AFT CARGO BAY. THE SECTION OF CARGO TRACK WAS REPLACED IAW SRM 51-41-01, 51-41-02, AND 51-40-08.SDR DALA2017071205367Skin · corrodedCORROSION ON CTR FUEL TANK SKIN STA Y=742 BTW X=-20 TO X=-60 AT RT WHEELWELL SLANT PANEL AREA AMDS 5300-2003. REPAIR WAS ACCOMPLISHED PER ETI 17-17-087 REV 04 AND ER/A 559506-14 REV ORIGINAL.SDR DALA2017071205366Skin · corrodedCORROSION ON CENTRAL FUEL TANK SKIN BELOW SLANT PANEL STA Y=742 BTW X=18 TO X=25 LT WHEEL WELL AMDS 0593-2002. REPAIR WAS ACCOMPLISHED PER ETI 17-17-087 REV 04 AND ER/A 559506-14 REV ORIGINAL.SDR DALA2017071205365Skin · corrodedCORROSION ON CENTER FUEL TANK UPPER SKIN FROM Y=737 TO Y=756, X=22 TO X=60, ALSO Y=705-710, X=-56 TO X=-60 AT CABIN PAX WING BOX AREA AMDS 5300-2008. REPAIR WAS ACCOMPLISHED PER ETI 17-17-087 REV 04 AND ER/A 559506-14 REV ORIGINAL.SDR DALA2017071105332Cowling · crackedCRACK ON FIXED COWL APRON HINGE, LATCH ASSEMBLY AFT OF LOWER FAN COWL DOOR ENGINE LT. CRACK ON FIXED COWL WAS REPAIRED PER SRM 54-00-00 REP 1 HINGE, GUSSET, AND CLIP WERE REMOVED AND REINSTALLED PER SRM 51-41-02-0G AND 51-41-05-0G.SDR DALA2017070905290Frame Angle · crackedCRACKED FRAME ANGLE BS 1022 BELOW OF LONGERON 14L IN THE PAX CABIN. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-05, AND DWG 9912243, REV JS.SDR DALA2017070905288Access Panel · damagedELONGATE HOLES ON THE FUEL ACCESS PANEL 520CB. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.SDR DALA2017070905286Access Panel · damagedHOLES ELONGATED AT FUEL ACCESS PANEL 520GB. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, PAR 5, REPAIR 2, CONDITION II.SDR DALA2017070905285Strap · crackedCRACKED STRAP ON FRONT OF DOOR FRAME WEB BS 200 LONGERON 18L. THE STRAP WAS REPLACED IAW SRM 51-41-08, AND SRM 51-41-05.SDR DALA2017070905284Frame Angle · crackedCRACKED FRAME ANGLE BS 1022, LONGERON 14L. FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 9912243, REV JB.SDR DALA2017070805283Skin · crackedCRACK ON FUSELAGE SKIN BS 1076 BETWEEN LONGERONS 15 - 13L. REPAIRED IAW ETI-17-17-082, REV 2, AND ER/A 559501-14, REV ORIG.SDR DALA2017070805282Skin · crackedCRACK ON FUSELAGE SKIN BS 1087 BETWEEN LONGERONS 13 - 15L. REPAIRED IAW ETI-17-17-082, REV 2, AND ER/A 559501-14, REV ORIG.SDR DALA2017070805281Longeron · crackedCRACKED LONGERON 2R, BS 1133 IN THE AFT ACCESSORIES BAU AREA. A REPAIR SPLICE WAS INSTALLED SRM 53-00-05-2R.SDR DALA2017070805280Intercostal · crackedCRACK ON INTERCOSTAL IN THE CEILING AREA BETWEEN BS 617 - 636, BL 0 IN THE FWD CARGO BAY. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00-2R-1.SDR DALA2021122908130Skin · crackedTWO CRACKS WERE NOTED ON THE FUSELAGE SKIN, BETWEEN 1076 AND 1087, L-14L. ER/A 559501-14 SECTION I REPAIR WAS ACCOMPLISHED. FOLLOW ON ACTION FOR SECTION II IS REQUIRED. ACCOMPLISH ER/A 559501-14 SECTION II INSPECTION AT C-CHECK INTERVALS FROM SECTION I, NOT TOSDR DALA2017070705279Frame · crackedCRACKED FRAME ANGLE BS 1022, LONGERON 14R. THE DAMAGE WAS REMOVED AND A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW SRM 53-00-06-2R, AND DWG 9912243, REV JB.SDR DALA2017070505187Skin · debondedDISBONDED AREAS AT DENTS 6, 7, AND 18 ON RT WING AFT MOVABLE FLAP VAN. REPAIRED IAW SRM 57-53-01-2R, REPAIR 1, AND OPN 1031 CARD 2000-8149-02.SDR DALA2017070505214Seat Track · corrodedCORROSION ON RT SEAT TRACK RBL 22 BTW BS 822 & 937. SEAT TRACK WAS REPAIRED IAW SRM 53-20-52-2R, REPAIR 5.SDR DALA2017070505186Frame · crackedCRACKED FRAME ANGLE, BS 1168. A NEW FRAME ANGLE WAS INSTALLED IAW SRM 51-41-02, AND 51-41-05.SDR DALA2017070505185Frame · crackedCRACKED FRAME ANGLE BETWEEN LONGERONS 3R &3L, BS 1168. A NEW FRAME ANGLE WAS INSTALLED IAW SRM 51-41-02, AND 51-41-05.SDR DALA2017070505181Pan · crackedCRACKED PAN LOWER AREA INTERNAL STRUCTURE BS 408 FWD CARGO DOOR. REPAIRED IAW SRM 52-30-02-2R PROCEDURE 1, REPAIR 1, FIG 201.SDR DALA2017070505180Fitting · crackedCRACKED LOWER FITTING INTERNAL STRUCTURE BS 408 FWD CARGO DOOR. REPLACED IAW SRM 51-41-01, AND 51-41-05.SDR DALA2017070505179Skin · delaminatedDELAMINATION WAS FOUND BELOW DENTS NR 3 & 12 OF RT WING FLAP FORWARD MOVEABLE VANE LOWER SURFACE. REPAIRED SRM 57-53-01, FIG 201, REP 1.SDR DALA2017070405177Frame · crackedCRACK ON LT FORMER BS 694, LONGERON 26L. THE FRAME WAS REPAIRED IAW SRM 51-70-11, REP 1.SDR DALA2017070305155Intercostal · crackedCRACKED INTERCOSTAL BETWEEN BEAMS 4 AND 5, BS 181, FWD PASSENGER DOOR. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02, AND DWG 9955763, REV M.SDR DALA2017070305175Rub Strip · corrodedCORROSION ON RUBSTRIP OF FUEL ACCESS DOOR 520JB I. NEW RUB STRIP 520JB WAS REPLACED PER B717-200 SRM 57-10-01-2R REP 3 PAR 6. (LP #0098256)SDR DALA2017070205112Doubler · damagedWEAR AND NICKS ON PREVIOUS REPAIR DOUBLERS STA 907 LT/LWR ALSO STA 909 LT/UPPER AT PASSENGER CABIN RING PANS AREA. REPAIR DOUBLERS WERE REPLACED PER SRM 56-20-02 REPAIR 1 FIGURE 202.SDR DALA2017070105111Pan · crackedCRACK ON RT RING PAN (FWD UPPER CORNER) STA Y=756 AT PAX CABIN (CPAX). RING PAN WAS REPAIRED PER SRM 56-20-02-2R-1 REPAIR 1.SDR DALA2017070105110Longeron · crackedCRACKED LONG 6 RT ON STA 1022. AT PASSENGER CABIN AREA. LONG 6 RT ON STA 1022. WAS REPAIRED PER SRM 53-00-05-2R-2-, FIG 201.SDR DALA2017070105109Longeron · crackedCRACKED LONGERON 6 LT ON STA 1022 AT PASSENGER CABIN AREA. LONGERON WAS REPAIRED PER SRM 53-00-05-2R-2, FIG 201.SDR DALA2017070305156Access Panel · damagedELONGATE HOLES ON FUEL TANK ACCESS PANEL 620DB. THE ACCESS PANEL WAS OUT OF LIMITS FOR EXCESSIVE DAMAGES IAW SRM 57-10-01 AND WAS REPLACED.SDR DALA2017063005108Access Panel · corrodedCORROSION ON COUNTERSINK AREA ON FUEL TANK ACCESS 620CT AND 620FT. FUEL TANK ACCESS 620CT AND 620FT OUT OF LIMITS FOR EXCESSIVE DAMAGES PER SRM 57-10-01 AND WERE REPLACED. THE EFFECTIVITY WAS VERIFIED PER IPC 57-22-01-01.SDR DALA2017063005107Skin · corrodedCORROSION ON SETTLEMENT AREA ON FUEL TANK ACCESS 520CT AND 520DT. FUEL TANK ACCESS 520CT AND 520DT OUT OF LIMITS FOR EXCESSIVE DAMAGES PER SRM 57-10-01 AND WERE REPLACED. THE EFFECTIVITY WAS VERIFIED PER IPC 57-22-01-01.SDR DALA2017063005106Access Panel · corrodedCORROSION ON COUNTERSINK AREA ON FUEL TANK ACCESS 520FT. FUEL TANK ACCESS 520FT OUT OF LIMITS FOR EXCESSIVE DAMAGES PER SRM 57-10-01 AND WAS REPLACED. THE EFFECTIVITY WAS VERIFIED PER IPC 57-22-01-01.SDR DALA2017063005079Frame · crackedCRACK ON RT FORMERS Y=715 , Y= 694 AT UNDERWING CANTED KEEL , INTERNAL STRUCTURE. FRAMES WERE REPAIRED PER SRM 51-70-11-2R. HFEC INSPECTION WAS PERFORMED AND 01 CRACK OF 0.4" ON RT FORMER Y=694 AT UNDERWING CANTED KEEL, INTERNAL STRUCTURE AND 01 CRACK OF 0.5" SDR DALA2017062905077Door Frame · crackedCRACKED DOOR JAMB WEB STA Y=207 LONG 15L AT PAX CABIN. CRACKED DOOR JAMB WAS REPAIRED PER SRM 53-10-15-2R-1.SDR DALA2017062905051Pan · crackedCRACKED LT UPPER RING PAN STA 926 AT PASSENGER CABIN AREA. LT UPPER RING PAN STA 926 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR1 FIG 201.SDR DALA2017062905050Pan · crackedCRACKED LT LWR RING PAN STA 928 AT PASSENGER CABIN AREA. LT LWR RING PAN STA 928 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR 1 FIG 201.SDR DALA2017062905049Pan · crackedCRACKED LT LWR RING PAN STA 890 AT PASSENGER CABIN AREA. LT LWR RING PAN STA 890 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR 1 FIG 201.SDR DALA2017062905048Pan · crackedCRACKED LT UPPER RING PANS STA 869 AT PASSENGER CABIN AREA. LT UPPER RING PANS STA 869 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR 1 FIG 201.SDR DALA2017062905047Pan · crackedCRACKED LT LWR/UPPER RING PANS STA 831 AT PASSENGER CABIN AREA. LT LWR/UPPER RING PANS STA 831 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REP 1 FIG 201.SDR DALA2017062905046Pan · crackedCRACKED LT LWR RING PAN STA 637 AT PASSENGER CABIN AREA. LT LWR RING PAN STA 637 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REP 1 FIG 201.SDR DALA2017062905044Skin · crackedCRACKED SKIN BTW BEAM NR 1-2 AT HOUSING AREA FWD CARGO COMPARTMENT DOOR (C1). SKIN WAS REPAIRED PER SRM 52-30-01-2R-1, FIG 201.
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