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.

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.Jul 15, 2017 · N982AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR 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.Jul 15, 2017 · N982AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR 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.Jul 15, 2017 · N982AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR 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.Jul 15, 2017 · N982AT · Boeing 717200 · Vertical StabilizerSDR DALA2017071605447Frame · crackedCRACKED FRAME BS 1022, LONGERON 7R. REPAIRED IAW ETI 17-17-083, REV 1, AND ER/A 559502-14, REV ORIGINAL.Jul 15, 2017 · N982AT · Boeing 717200 · Fuselage Main, FrameSDR 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.Jul 15, 2017 · N982AT · Boeing 717200 · Fuselage Main, FrameSDR 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.Jul 14, 2017 · N982AT · Boeing 717200 · Fuselage Main, StructureSDR 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.Jul 11, 2017 · N982AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Jul 11, 2017 · N982AT · Boeing 717200 · Fuel StorageSDR 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.Jul 11, 2017 · N982AT · Boeing 717200 · Fuel StorageSDR 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.Jul 11, 2017 · N982AT · Boeing 717200 · Fuel StorageSDR 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.Jul 10, 2017 · N982AT · Boeing 717200 · Engine Cowling SystemSDR 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.Jul 8, 2017 · N982AT · Boeing 717200 · Fuselage Main, FrameSDR 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.Jul 8, 2017 · N982AT · Boeing 717200 · Wing, Plate/SkinSDR 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.Jul 8, 2017 · N982AT · Boeing 717200 · Wing, Plate/SkinSDR 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.Jul 8, 2017 · N982AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR 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.Jul 8, 2017 · N982AT · Boeing 717200 · Fuselage Main, FrameSDR 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.Jul 7, 2017 · N982AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR 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.Jul 7, 2017 · N982AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017070805281Longeron · crackedCRACKED LONGERON 2R, BS 1133 IN THE AFT ACCESSORIES BAU AREA. A REPAIR SPLICE WAS INSTALLED SRM 53-00-05-2R.Jul 7, 2017 · N982AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR 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.Jul 7, 2017 · N982AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR 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 TOJul 6, 2017 · N982AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR 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.Jul 6, 2017 · N982AT · Boeing 717200 · Fuselage Main, FrameSDR 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.Jul 5, 2017 · N982AT · Boeing 717200 · Trailing Edge FlapsSDR 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.Jul 4, 2017 · N982AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017070505186Frame · crackedCRACKED FRAME ANGLE, BS 1168. A NEW FRAME ANGLE WAS INSTALLED IAW SRM 51-41-02, AND 51-41-05.Jul 4, 2017 · N982AT · Boeing 717200 · Fuselage Main, FrameSDR 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.Jul 4, 2017 · N982AT · Boeing 717200 · Fuselage Main, FrameSDR 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.Jul 4, 2017 · N982AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017070505180Fitting · crackedCRACKED LOWER FITTING INTERNAL STRUCTURE BS 408 FWD CARGO DOOR. REPLACED IAW SRM 51-41-01, AND 51-41-05.Jul 4, 2017 · N982AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR 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.Jul 4, 2017 · N982AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2017070405177Frame · crackedCRACK ON LT FORMER BS 694, LONGERON 26L. THE FRAME WAS REPAIRED IAW SRM 51-70-11, REP 1.Jul 3, 2017 · N982AT · Boeing 717200 · Fuselage Main, FrameSDR 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.Jul 3, 2017 · N982AT · Boeing 717200 · Passenger/Crew DoorsSDR 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)Jul 2, 2017 · N982AT · Boeing 717200 · Wing Main, Frame StructureSDR 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.Jul 1, 2017 · N982AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR 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.Jul 1, 2017 · N982AT · Boeing 717200 · Passenger Compartment WindowsSDR 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.Jun 30, 2017 · N982AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017070105109Longeron · crackedCRACKED LONGERON 6 LT ON STA 1022 AT PASSENGER CABIN AREA. LONGERON WAS REPAIRED PER SRM 53-00-05-2R-2, FIG 201.Jun 30, 2017 · N982AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR 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.Jun 29, 2017 · N982AT · Boeing 717200 · Wing, Plate/SkinSDR 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.Jun 29, 2017 · N982AT · Boeing 717200 · Wing, Plate/SkinSDR 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.Jun 29, 2017 · N982AT · Boeing 717200 · Wing, Plate/SkinSDR 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.Jun 29, 2017 · N982AT · Boeing 717200 · Wing, Plate/SkinSDR 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" Jun 29, 2017 · N982AT · Boeing 717200 · Fuselage Main, FrameSDR 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.Jun 28, 2017 · N982AT · Boeing 717200 · Fuselage Main, StructureSDR 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.Jun 28, 2017 · N982AT · Boeing 717200 · Passenger Compartment WindowsSDR 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.Jun 28, 2017 · N982AT · Boeing 717200 · Passenger Compartment WindowsSDR 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.Jun 28, 2017 · N982AT · Boeing 717200 · Passenger Compartment WindowsSDR 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.Jun 28, 2017 · N982AT · Boeing 717200 · Passenger Compartment WindowsSDR 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.Jun 28, 2017 · N982AT · Boeing 717200 · Passenger Compartment WindowsSDR 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.Jun 28, 2017 · N982AT · Boeing 717200 · Passenger Compartment WindowsSDR 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.Jun 28, 2017 · N982AT · Boeing 717200 · Cargo/Baggage Doors
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