N919AT

Service difficulty reports · 204

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 = 'N919AT' 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 DALA2019031401671Battery Pack · dischargedEMERGENCY LIGHTS AT SEAT 20 LT AND RT ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT SEAT 23 OVERHEAD. OPERATIONAL CHECK WAS GOOD PER AMM 33-51. (LP #5026121)Mar 14, 2019 · N919AT · Boeing 717200 · Emergency LightingSDR DALA2019030601508Light · inoperativeTHE EMERGENCY EXIT SIGN IN CENTER AISLE CEILING ABOVE OVER WING EXITS LIGHT WAS TOO DIM TO BE OF PROPER USE. FOUND SEVERAL LAMPS OUT IN EXIT SIGN IN CENTER AISLE IN CEILING ABOVE OVER WING EXITS AND RE-LAMPED IN REF WITH AMM 33-51. OPERATIONAL CHECK WAS GOOD. Jan 5, 2019 · N919AT · Boeing 717200 · Emergency LightingSDR DALA2018122007297Cover · brokenTHE RIGHT AFT OVERWING EXIT SIGN COVER IS BROKEN. MAINTENANCE REPLACED THE EXIT SIGN COVER AT THE RIGHT AFT OVERWING EXIT HATCH PER AMM 33-50.Dec 20, 2018 · N919AT · Boeing 717200 · Emergency LightingSDR DALA2018120316975Buffer Valve · leakingWHILE TAXIING IN, DURING APU START-UP, OILY FUEL FUMES ARE NOTICEABLE THROUGHOUT THE ENTIRE CABIN AND COCKPIT. SMELL DISSIPATES A MINUTE OR TWO AFTER APU RUNNING. C/W NO GO ODI CHECK STEPS 1 THRU 5 PER STEP 6 REMOVED L/H AND R/H BUFFER VALVES, R/H SHOWS NO OBVNov 30, 2018 · N919AT · Boeing 717200 · Pneumatic Distribution SystemSDR DALA2018112806863Pin · bentELECTRICAL PANEL LIGHTS INCORRECT. BURNING SMELL FROM OVHD PANEL. ELECTRICAL PANEL LIGHTS ARE CORRECT PER SSM 31-12-0. FOUND LEFT APU ANNUNCIATOR LIGHT FOR LEFT BUS DAMAGED WITH BENT PINS. REMOVED AND REPLACED INDICATOR LIGHT ASSY L2-1510 PER WDM 24-27. PERFORNov 27, 2018 · N919AT · Boeing 717200 · Flight Compartment LightingSDR DALA2018101506042Sign · damagedON CEILING AT ROW 1, THE EXIT SIGN IS MISSING HALF ALSO CLOSE NOT ILLUMINATED. MAINTENANCE REPLACED THE EXIT SIGN PER AMM 33-51-18. OPERATIONAL CHECK IS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP 4689852)Oct 14, 2018 · N919AT · Boeing 717200 · Emergency LightingSDR DALA2018060763860Lanyard · damagedTAILCONE DEPLOYMENT SYSTEM LANYARD FRAYED AND WORN. REPLACED TAILCONE LANYARD IAW AMM 53-52-01, AND 25-61-02.Jun 2, 2018 · N919AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2018060103769Bulkhead · puncturedFWD CARGO BULKHEAD, BS 218, RBL 15, Z=-20 HAD A PUNCTURE. REPAIRED THE BULKHEAD IAW ER/A 567762-14, REV ORIGINAL.May 31, 2018 · N919AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA201806013768Bulkhead · puncturedE & E BAY, AFT BULKHEAD, 12 INCHES RIGHT OF BL 0, 5 INCHES UP FROM BILDGE, THE BULKHEAD WAW PUNCTURED. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-00, REPAIR 2.May 25, 2018 · N919AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2018052963624Bulkhead · puncturedFWD CARGO BULKHEAD BS 218, LBL 33, Z=-30 HAD A PUNCTURE. ACCOMPLISHED A PERMANENT REPAIR TO FWD CARGO FWD BULKHEAD IAW SRM 53-00-00, REPAIR 2.May 25, 2018 · N919AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2017072405670Blower · failedAT GATE PRIOR TO PUSH BACK, A STRONG ELECTRICAL ODOR EMANATED FROM THE AFT LAVATORY AREA IN THE CABIN. MAINTENANCE FOUND THE LAVATORY BLOWER MOTOR CIRCUIT BREAKER HAD TRIPPED OPEN. MAINTENANCE REPLACED THE LAVATORY WASTE VENT SYSTEM BLOWER.Jul 19, 2017 · N919AT · Boeing 717200 · Waste Disposal SystemSDR DALA2016103107953Lens · damagedTHE FLIGHT ATTENDANT DISCOVERED THAT AN EMERGENCY EXIT SIGN DIFFUSER LENS WAS DAMAGED. MAINTENANCE REPLACED THE LENS AND THE OPS CHECKED GOOD.Oct 29, 2016 · N919AT · Boeing 717200 · Emergency LightingSDR DALA2016082806240Light · missingDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY EXIT IDENTIFIER IN THE FLOOR AT SEAT 19AB IN THE CABIN WAS MISSING, AND INOPERATIVE. MAINTENANCE INSTALLED THE FLUORESCENT STRIP FOR THE NOTED AREA AND THE OPS CHECK WAS GOOD.Aug 28, 2016 · N919AT · Boeing 717200 · Emergency LightingSDR DALA2016052704185Light · inoperativeEIGHT EMERGENCY LIGHTS INOPERATIVE. LIGHTS WERE REPLACED IAW 33-52-00.May 26, 2016 · N919AT · Boeing 717200 · Emergency LightingSDR DALA2016052604191Skin · corrodedCORROSION ON UPPER CENTER WING SKIN AFT EDGE FROM BS XCW=10, XCW=50 AT LT MLG WHEEL WELL. SM, MLG. CORROSION ON WING BOX SKIN WAS ATTENDED WITH ER/A 545162-14, REV ORIGINAL AND SRM 51-41-03, 51-41-01, 51-41-05, 51-10-04 PAR 14, 21, 26. OLYMPUS NDT 3DL, SONOMay 25, 2016 · N919AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016052404175Skin · corrodedCORROSION ON UPPER CENTER WING SKIN AFT EDGE FROM BS=10 TO XCW=50 AT RT MLG WELL CORROSION ON WING SKIN WAS ATTENDED WITH ER/A NR 545162-14, REV ORIGINAL 546475-14, REV ORIGINAL AND SRM 51-10-04, 51-41-03, 51-70-10, 51-70-11 AND 51-41-05.May 23, 2016 · N919AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016052004043Cargo Track · corrodedCORROSION ON RT TIE TRACK FROM BS 994 TO 1022 AT AFT CARGO COMPARTMENT, C2. TIE TRACK FROM BS 994 TO 1022 WAS REPLACED IAW SRM 53-20-51, FIG 1 AND 51-41-01, 51-41-02, 51-40-08, 51-10-04 PAR 15, 21, AND 37. ORIGINAL THICKNESS IS 0.090" MINIMUN REMAINING IS 0.0May 20, 2016 · N919AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016052004042Cargo Track · corrodedCORROSION ON RT TIE TRACK FROM BS 813 TO 889 AT AFT CARGO COMPARTMENT. C2, SM. RT TIE TRACK FROM BS 813 TO 889 WAS REPLACED IAW SRM 53-20-51, FIG 1 AND 51-41-01, 51-41-02, 51-40-08, 51-10-04 PAR 15, 21, AND 37. OLYMPUS 38 DL PLUS SONOPEN V260SM 25AUG16 AMX-PNMay 20, 2016 · N919AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016052004039Cargo Track · corrodedCORROSION ON LT TIE TRACK FROM BS 813 TO 889 AT AFT CARGO COMPARTMENT. C2, SM. LT TIE TRACK FROM BS 813 TO 889 WAS REPLACED, DRILLED, ADJUSTED, TREATED, PAINTED, INSTALLED, AND CIC APPLIED IAW SRM 53-20-51, FIG 1, ITEM 3, 51-40-08, 51-10-04, PAR 15, 21, 37, 5May 19, 2016 · N919AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016052004038Cargo Track · corrodedCORROSION ON LT TIE TRACK FROM BS 908 TO 1022 AT AFT CARGO COMPARTMENT. C2, SM. LT TIE TRACK FROM BS 908 TO 1022 WAS REPLACED, DRILLED, ADJUSTED, TREATED, PAINTED, INSTALLED, CIC APPLIED, AND REPAIR PARTS WERE INSTALLED IAW SRM 53-20-51, FIG 1, ITEM 9, 51-40-May 19, 2016 · N919AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016051904036Skin · crackedCRACKED EXTERNAL FUSELAGE SKIN BS 100 AND LONGERON 28R. FUSELAGE SKIN WAS PERFORMED IAW SRM 53-10-01, FIG 201.May 18, 2016 · N919AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051503930Skin · delaminatedDELAMINATED RT WING INBD SPOILER UPPER SURFACE BETWEEN BS XRS 189-214. RT WING INBD SPOILER UPPER SURFACE BETWEEN BS XRS 189-214 WAS REPAIRED IAW SRM 51-70-02, REPAIR 3. RT WING INBD SPOILER, PANEL WAS REMOVED AND INSTALLED TO FACILITATE OTHER ACTIVITIES IAWMay 14, 2016 · N919AT · Boeing 717200 · SpoilersSDR DALA2016051503929Frame · crackedCRACKED FRAME ANGLE BS 1087 BTW LONGERONS 13-14R AT AFT ACCESSORIES COMPARTMENT. FRAME ANGLE WAS REPLACED IAW AMM 21-22-01, 21-51-04, SRM 51-41-02, 51-41-05, DWG 9971140, REV F.May 14, 2016 · N919AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016051203888Skin · canningDENT WITH OIL CAN EFFECT ON EXTERNAL FUSELAGE, SKIN BS 1189 CANT TO 1200 CANT BETWEEN 6-7 O'CLOCK POSITION, SM, FS. FUSELAGE SKIN WAS REPAIRED IAW ER/A 545165-14, REV ORIGINAL.May 11, 2016 · N919AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051203887Bearing · wornFREEPLAY ON AILERON SECTOR BUSS AT LT WING. FREE PLAY ON AILERON SECTOR BUS WAS CORRECTED BY REPLACING BEARING ON BUS SECTOR IAW CMM 27-10-16. RII COMPLETED BY INSPECTION.May 11, 2016 · N919AT · Boeing 717200 · Aileron Control SystemSDR DALA2016051203890Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA ON LT WING FUEL ACCESS PANEL. DUE TO CORROSION OUT OF LIMITS FUEL ACCESS PANEL REPLACED IAW SRM 57-10-01 UNDER CONDITION III.May 10, 2016 · N919AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016051203889Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA ON RT WING FUEL ACCESS PLATE NR 620CB AND 620EB IN REF ORNRC 48, ZONE 000, CARD 53, ZONE 000. DUE TO CORROSION OUT OF LIMITS FUEL ACCESS PLATE NR 620CB AND 620EB WERE REPLACED IAW SRM 57-10-01 UNDER CONDITION III.May 10, 2016 · N919AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016051103849Hinge Fitting · damagedSCRATCHES ON BUSHINGS ON RT ELEVATOR HINGE FITTINGS BS XE=49. AYP, CARD 1, ZONE 340. UPPER BUSHING AT BS XE=49 ON RT ELEVATOR HINGE FITTING WAS CLEANED IAW PS 900-1-2-1 NR 001 AND DAMAGE WAS NOT FOUND. LOWER BUSHING AT BS XE=49 ON RT ELEVATOR HINGE FITTING WMay 10, 2016 · N919AT · Boeing 717200 · Elevator StructureSDR DALA2016051103848Hinge Fitting · wornFREEPLAY ON EYEBOLT NR 6 ON HINGE FITTING ON RT HORIZONTAL STAB. AYP, CARD 14, ZONE 340. EYEBOLT NR 6 ON HINGE FITTING ON RT HORIZONTAL STABILIZER WAS REPLACED IAW CMM 27-30-2 AND FREE PLAY WAS CORRECTED. RII COMPLETEDMay 10, 2016 · N919AT · Boeing 717200 · Horizontal Stabilizer StructureSDR DALA2016051103847Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA ON RT WING FUEL ACCESS PLATE NR 620JB, 620LB, 620MB, AND 620PB, AYP. DUE TO CORROSION OUT OF LIMITS FUEL ACCESS NR 620JB, 620LB, 620MB, AND 620PB WERE REPLACED IAW SRM 57-10-01 UNDER CONDITION III. TOOL USED, PN 1May 10, 2016 · N919AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016051103846Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA ON LT WING FUEL ACCESS NR 520CB, 520DB, 520EB, AND 520GB, AYP. CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON FUEL ACCESS 520CB, 520DB, 520EB, AND 520GB WAS REMOVED, COUNTERSINK HOLES AT FUEL ACCESS 520CB AND 520EMay 10, 2016 · N919AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016051103845Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA ON LT WING FUEL ACCESS PLATE NR 620DB AND 620HB, AYP, IN REF OR NRC 48, ZONE 000. FUEL ACCESS PLATES 620DB AND 620HB WERE REPAIRED UNDER CONDITION II IAW SRM 57-10-01.May 10, 2016 · N919AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016051103844Access Panel · corrodedCORROSION ON LT FUEL ACCESS PLATE COUNTERSINK NR 520CB AND 520EB. CORROSION ON LT FUEL ACCESS PLATE 520CB AND 520EB WAS REMOVED AND FUEL ACCESS WERE REPAIRED IAW SRM 57-10-01.May 10, 2016 · N919AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016050603719Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF RT WING FUEL ACCESS PLATE NR 620AT AND 620DT, AYP IN REF ORNRC 50, ZONE 000, CARD 55, ZONE 000. FUEL ACCESS 620AT WAS REPAIRED UNDER CONDITION II IAW SRM 57-10-01.May 5, 2016 · N919AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016050603714Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF RT WING FUEL ACCESS PLATE 620DT. CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS WAS REMOVED, COUNTERSINK HOLES AND SETTLEMENT AREA ON FUEL ACCESS 620DT WERE MEASURED THIS IS OUT OF LIMITS. AMay 5, 2016 · N919AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016050603713Hinge Fitting · damagedNICK ON LOWER HOUSING ON RT ELEVATOR HINGE FITTING XE=49. REPAIR WAS PERFORMED IAW ER/A 545166-14, REV ORIGINAL.May 5, 2016 · N919AT · Boeing 717200 · Elevator Tab, Attach FittingsSDR DALA2016050603712Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA ON LT WING FUEL ACCESS PLATE NR 520FT CARD 52, ZONE 000. DUE TO EXCESSIVE DAMAGE AT FUEL ACCESS 520FT THIS WAS REPLACED IAW SRM 57-10-01.May 5, 2016 · N919AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016050603711Support Fitting · crackedCRACKED FITTING SUPPORT ON BS 737, X=-44, AND Z=5 AT PASSENGER STRUCTURE WING BOX AREA, SM, CARD 23, ZONE 140. FITTING SUPPORT WAS REPLACED IAW DWG 3925812, REV A, SRM 51-41-02, 51-40-05, 51-10-04 PAR 15, 21.May 5, 2016 · N919AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2016050603708Tee Fitting · crackedCRACK ON TEE FITTING ON LOWER SECTION OF FWD CARGO DOOR BS 401 APPROXIMATELY C1, SM, CARD 12, ZONE 810. TEE FITTING WAS REPLACED IAW SRM 51-41-01 AND 51-41-02.May 5, 2016 · N919AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016050503659Skin · puncturedPUNCTURE AND CRACK ON UPPER SKIN, LT ELEVATOR, BS PROYECTION XE=13.213, APPROACH. SM VHS. UPPER SKIN LT ELEVATOR WAS REPAIRED IAW SRM 51-41-02, 41-41-08, 51-70-13, PAGE 201, SHT 1-3, REPAIR 2, RII COMPLETEDMay 4, 2016 · N919AT · Boeing 717200 · Elevator, Plate/SkinSDR DALA2016050503658Intercostal · crackedCRACKED INTERCOSTAL ON LT ELEVATOR INTERNAL STRUCTURE BS XE=13.213, SM, IN REF ORNRC 4, ZONE 300. CRACKED INTERCOSTAL WAS REPAIRED IAW SRM 51-41-02, 55-00-00, FIG 201. RII COMPLETED BY INSPECTION.May 4, 2016 · N919AT · Boeing 717200 · Rudder StructureSDR DALA2016050403608Access Panel · corrodedCORROSION ON RT FUEL ACCESS PLATE NR 620CT. FUEL ACCESS PLATE NR 620CT WAS REPLACED IAW SRM 57-10-01.May 3, 2016 · N919AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016050203476Pan · crackedCRACKS ON LOWER PAN BETWEEN STOP 1 AND 2 BS 373 APPROXIMATELY AT FWD CARGO COMPARTMENT DOOR. 1, SM CARD 11, ZONE 810. PAN BETWEEN STOP 1 AND 2 WAS REPAIRED IAW SRM 52-30-02, FIG 201.May 1, 2016 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016050203475Bracket · crackedCRACKED AFT BRACKET SUPPORT TOP AREA OF L1 DOOR. BRACKET WAS REPLACED IAW SRM 51-41-02 AND DWG 5961804, REV 2F.May 1, 2016 · N919AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016050203474Beam · crackedCRACK ON BEAM 1, AFT EDGE AT L1 DOOR. BEAM WAS REPAIRED IAW SRM 52-10-2, FIG 201, SHEET 3.May 1, 2016 · N919AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016050103469Floor Panel · crackedCRACKED FLOOR PANEL. FLOOR PANEL REPAIRED IAW SRM 53-20-50.Apr 30, 2016 · N919AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016050103465Frame · crackedCRACKED FRAME BS 1037 LONGERON 17R AT PAX CABIN. FRAME WAS REPAIRED IAW SRM 53-20-07, FIG 201, 51-41-03 PAR 11, AND 51-41-02, 51-41-05. RII INSPECTOR SGMR ID 796792.Apr 30, 2016 · N919AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016050103464Door Frame · crackedCRACK ON DOOR FRAME LT SIDE BETWEEN BS 35 TO BS 46 NOSE GEAR WHEEL WELL. THE DOOR FRAME WAS REPAIRED IAW SRM 53-14-4, FIG 201, 51-41-02, 51-41-03, 51-41-05, 51-20-09, AND 51-10-4 PAR 21 AND 15.Apr 30, 2016 · N919AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016050103463Door Frame · crackedCRACK ON DOOR FRAME RT SIDE BETWEEN BS 35 TO BS 46 AT NOSE GEAR WHEEL WELL. DOOR FRAME WAS REPAIRED IAW SRM 53-10-14, FIG 201, 51-41-02, 51-41-03, 51-41-05, 51-20-09, AND 51-10-4 PAR 21 AND 15.Apr 30, 2016 · N919AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016050103462Cusp Web · corrodedCORROSION OUT OFF LIMITS ON CUSP WEB UPPER/LWR SURFACE ON BS 874 . REPAIRED IAW SRM 53-00-55, FIG 212, SRM 51-10-04 PAR 15, 21, 37, 26, SRM 51-41-01, 51-41-02, AND 51-41-05.Apr 30, 2016 · N919AT · Boeing 717200 · Fuselage Miscellaneous Structure
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