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 DALA2016050103461Cusp Web · corrodedCORROSION ON RT CUSP WEB UPPER, LWR SURFACE BETWEEN BS 397-405 AND 465 TO 477, SM, IN REF OR NRC 37, ZONE 200, CARD 57, ZONE 200. CUSP WEB BS 397 TO 405 AND 465 AND 465 TO 477 WERE REPAIRED IAW SRM 53-00-55, FIG 219 AND FIG 216 AND 51-41-02, 51-41-01, 51-41-05Apr 30, 2016 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016043003459Intercostal · crackedCRACK ON INTERCOSTAL ON RT ELEVATOR HINGE FITTING AREA XE=204 ACCESS 340UB. SM, CRACK ON INTERCOSTAL ON RT ELEVATOR HINGE FITTING AREA BS XE=204 ACCESS 340UB, WAS REPAIRED IAW SRM 55-00-00, FIG 201.Apr 29, 2016 · N919AT · Boeing 717200 · Horizontal Stabilizer StructureSDR DALA2016103107956Cusp Web · corrodedCORROSION OUT OF LIMITS ON RT CUSP WEB UPPER & LOWER SURFACE BS 447 - 452. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 FIG. 215 AND 51-10-04 PAR 21-15 AND 37, 51-40-02.Apr 28, 2016 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016042903430Cusp Web · corrodedCORROSION ON RT CUSP WEB UPPER, LOWER SURFACE BETWEEN BS 486 TO BS 501. AREA WAS REPAIRED IAW SRM 53-00-55, FIG 216 AND 51-10-04, PAR 15, 21, 37 UT WAS ACCOMPLISHED NDT SPM 04-00-07, PAR 5, FIG 3, ORIGINAL THICKNESS ON WEB IS 0.020" REMAINING IS 0.010". THERApr 28, 2016 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016042703388Cusp Web · out of limitsOUT OF LIMITS LT CUSP WEB UPPER AND LOWER SURFACE BETWEEN BS 525 TO 526 AND 530 TO 531, X 60 TO X 54. REPAIRED IAW SRM 53-00-55, FIG 216 51-10-04 PAR 15, 21, AND 37.Apr 26, 2016 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016042703387Cusp Web · crackedCRACK ON RT CUSP WEB, BS 645. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 215, SRM 51-41-05, 51-41-02, SRM 53-20-51, 51-10-04, PAR 15, 21.Apr 26, 2016 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016042503196Cusp Web · puncturedPUNCTURE ON LT CUSP WEB BS 715, BETWEEN X 54 - 44. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 219, SHEET 1 AND 51-10-04, PAR 15, 21.Apr 24, 2016 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016042503194Frame · crackedCRACK ON FRAME BS 256 LONGERON 18L. FRAME WAS REPLACED IAW DWG 9911524, REV N AND SRM 51-40-5, 51-40-2, AND 51-10-04, PAR 15 AND 21.Apr 24, 2016 · N919AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016042503193Pan · crackedCRACK ON LWR FWRD CORNER WINDOW RING PAN BS 560 LONGERON 14 LT AT PAX CABIN. SM, CARD 21, ZONE 201. DAMAGE WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, 51-41-02, 51-41-05, 51-20-09, AND 51-10-04, PAR 15 AND 21. CRACK LENGTH: 0.093.Apr 24, 2016 · N919AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016042503192Pan · crackedCRACK ON UPPER/AFT WINDOW RING PAN STA 851. DAMAGE WAS REPAIRED IAW SRM 56-20-02. REPAIR 1, 51-41-02, 51-41-05, 51-20-09, AND 51-10-04 PAR 15 AND 21.Apr 24, 2016 · N919AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016042503191Pan · crackedCRACK ON LOWER/FWD WINDOW RING PAN BS 636. DAMAGE WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, 51-41-02, 51-41-05, 51-20-09, AND 51-10-04, PAR 15 AND 21.Apr 24, 2016 · N919AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016042403189Skin · damagedBLEND OUT ON UPPER FUSELAGE SKIN BS 858 BETWEEN LONG 5-6R. AREA WAS REPAIRED IAW SRM 53-02-01, FIG 202, SHEET 3 AND 51-10-04, PAR 15, 21. HFEC WAS PERFORMED AND CRACKS WERE NOT FOUND. PERFORM GENERAL VISUAL INSPECTION INITIAL AND REPETITIVE EA 8,000 CYCLES IApr 23, 2016 · N919AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2015012000370Cusp Web · crackedLEFT CUSP WEB BS 655-715, CRACKED IN 3 PLACES. INSTALLED SERVICEABLE CUSP WEB IAW SRM 51-10-02.Jan 19, 2015 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2014112006181Power Supply · inoperativeDURING SERVICE CHECK, FOUND F/A PANEL EMERGENCY SWITCH NOT WORKING IN ARM POSITION. REPLACED OVERWING EVAC BATTERY POWER SUPPLY IAW AMM 33-51-06-00-801.Nov 19, 2014 · N919AT · Boeing 717200 · Emergency LightingSDR DALA2014112006180Lamp · inoperativeDURING SERVICE CHECK, NOTED THE EXTERIOR EMERGENCY ILLUMINATION SYS WAS INOPERATIVE. REPLACED THE LAMPS.Nov 19, 2014 · N919AT · Boeing 717200 · Emergency LightingSDR DALA2014081904595Charger · malfunctionedDURING PILOT WALK AROUND, NOTED THE RT OVERWING EXTERIOR EMERGENCY LIGHT WAS ILLUMINATED. MAINTENANCE FOUND THE LIGHT TO GO OUT WHEN THE EMERGENCY LIGHT SWITCH WAS TURNED ON. THE AFT CARGO EMERGENCY CHARGER RACK WAS REPLACED AND OPS CHECKED NORMALLY.Aug 15, 2014 · N919AT · Boeing 717200 · Emergency LightingSDR SWAA2014061028903Frame · crackedLEFT MLG FWD CUT OUT FRAME CRACKED AT UPPER OTBD END. REPAIRED FRAME IAW SRM.Jun 4, 2014 · N919AT · Boeing 717200 · Fuselage Main, StructureSDR SWAA2014060628757Charger · inoperativeEMERGENCY BATTERY PACK INOPERATIVE AT BS 230 ABOVE SEAT NR 20. R & R BATTERY CHARGER IAW AMM.May 28, 2014 · N919AT · Boeing 717200 · Emergency LightingSDR SWAA2014051427967Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 211ALF DELAMINATED. R & R PANEL IAW MM.Apr 25, 2014 · N919AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2014051427966Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 221DF DELAMINATED. R & R PANEL IAW MM.Apr 25, 2014 · N919AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2014051427965Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 221CF DELAMINATED. R & R PANEL IAW SRM & DWG.Apr 25, 2014 · N919AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2014051427964Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 221 FF DELAMINATED. R & R PANEL IAW SRM & DWG.Apr 25, 2014 · N919AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2014051427963Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 221EF DELAMINATED. R & R PANEL IAW SRM.Apr 25, 2014 · N919AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2014051427962Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 221KF DELAMINATED. R & R PANEL IAW SRM & DWG.Apr 25, 2014 · N919AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2014051427961Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 221JF DELAMINATED. R & R PANEL IAW SRM & DWG.Apr 25, 2014 · N919AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2014043027524Lens · crackedMAIN CABIN CEILING PANEL NR 1 EMERGENCY LIGHT LENS CRACKED. R & R LENS IAW AMM.Apr 25, 2014 · N919AT · Boeing 717200 · Emergency LightingSDR SWAA2014051427951Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 222APF DELAMINATED. R & R PANEL IAW SRM & DWG.Apr 24, 2014 · N919AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2014050527704Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 222ATF DELAMINATED. REPAIRED PANEL IAW SRM.Apr 24, 2014 · N919AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2014050527703Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 222AVF DELAMINATED. REPAIRED PANEL IAW SRM.Apr 24, 2014 · N919AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2014050627721Support · corrodedR1 DOOR EMER EVAC SLIDE FWD GIRT BAR FITTING MOUNTING SUPPORT CORRODED. R & R SUPPORT IAW SRM.Apr 21, 2014 · N919AT · Boeing 717200 · Emergency EquipmentSDR SWAA2014051628070Fitting · looseLEFT MLG STRUT DOOR LANDING ROD FITTING LOOSE. R & R FITTING IAW SRM & AMM.Apr 18, 2014 · N919AT · Boeing 717200 · Landing Gear DoorsSDR SWAA2014050727778Cover · crackedEMPENNAGE LT AFT UPPER VENT COVER LOUVER CLIP CRACKED. R & R COVER ASSEMBLY IAW SRM & DWG.Apr 17, 2014 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2013082119404Battery · dischargedAFT FLASHLIGHT INOPERATIVE. R&R BATTERY IAW SIP.Aug 20, 2013 · N919AT · Boeing 717200 · Emergency EquipmentSDR SWAA2013052416473Light · inoperativeRIGHT EEPLS INOP AT ROW 3. RELAMPED IAW MM.May 23, 2013 · N919AT · Boeing 717200 · Emergency LightingSDR SWAA2013052416469Light · inoperativeRIGHT EEPLS INOP AT ROW 10. RELAMPED IAW MM.May 23, 2013 · N919AT · Boeing 717200 · Emergency LightingSDR SWAA2013020112233Support · corrodedC-1 BARRIER DOOR UPPER HINGE ATTACH STRUCTURE IS CRACKED. REMOVED DAMAGED C1 BARRIER DOOR UPPER ATTACH SUPPORT. LOCATED, DRILLED, DEBURRED & INSTALLED NEW SUPPORT P/N 5926003-82 PO 2229152 IAW B717 SRM 51-41-01, 51-40-08.Jan 31, 2013 · N919AT · Boeing 717200 · Cargo/Baggage DoorsSDR SWAA2013012811893Access Panel · crackedLEFT WING FUEL TANK ACCESS PANEL 520CB DOME NUT CHANNEL HAS A CRACK. REMOVED AND REPLACED DOME NUT CHANNEL AT LEFT WING FUEL TANK ACCESS PANEL 520CB IAW B717 SRM 57-10-01.Jan 23, 2013 · N919AT · Boeing 717200 · Wing, Plate/SkinSDR SWAA2013013012143Angle · crackedRIGHT EMERGENCY EXIT SURROUND CRACKED AT FWD UPPER CORNER. REPAIRED ANGLE IAW SRM.Jan 14, 2013 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2013013012147Angle · crackedMAIN CABIN NR 2 EMERGENCY WINDOW STOP ANGLE AT UPPER RIGHT SIDE, CRACKED (RT SIDE OF FUSELAGE). REMOVED AND REPLACED STOP ANGLE AT UPPER RIGHT SIDE NR 3 EMERGENCY WINDOW IAW B717 SRM 51-41-02.Jan 13, 2013 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2013012811892Cusp Web · corrodedCUSP WEB RIGHT SIDE STA 408-427 CORRODED. REPAIRED WEB IAW SRM.Jan 13, 2013 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2013020112237Angle · crackedRIGHT VENT BOX STRUCTURE CRACKED AT STA 1200 CANTED FRAME. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.Jan 12, 2013 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2013013112190Cusp Web · crackedRIGHT CUSP WEB STA 655-674 CRACKED. REMOVED AND REPLACED WEB IAW SRM.Jan 12, 2013 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2013013112189Tie Down · crackedD-RING TIE DOWN FITTING CRACKED - STA 950 BETWEEN L30 AND L29L 80-101. REMOVED AND REPLACED STRIP TIE DOWN STA 950 BETWEEN L30 AND L29R P/N 2957315-1 PO 22291145 IAW B717 SRM 51-41-01.Jan 12, 2013 · N919AT · Boeing 717200 · Cargo CompartmentsSDR SWAA2013013012146Skin · canningRIGHT WING TRAILING EDGE I/B FLAP UPPER SURFACE SKIN OIL CANNING. REMOVED AND REPLACED WEDGE IAW SRM.Jan 12, 2013 · N919AT · Boeing 717200 · Trailing Edge FlapsSDR SWAA2013012912092Cusp Web · corrodedCUSP WEB LEFT SIDE STA 541-560 AREAS CORRODED. REPAIRED CUSP WEB IAW SRM.Jan 12, 2013 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2013012511853Seat Track · corrodedSEAT TRACK AT STA 588-898 LBL 54 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED SEAT TRACK IAW SRM.Jan 12, 2013 · N919AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2013012311748Seat Track · corrodedSEAT TRACK CORRODED BETWEEN BS 237 TO BS 588, RBL 54. REMOVED AND REPLACED SEAT TRACK IAW SRM.Jan 12, 2013 · N919AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2013011611504Mechanism · looseTAIL CONE EMERGENCY RELEASE; LEFT LOWER RELEASE PIN MECHANISM IS LOOSE AT FRAME ATTACHMENT. TIGHTENED TAIL CONE EMERGENCY RELEASE LEFT LWR RELEASE PIN MECHANISM IAW B717 SRM 51-41-01.Jan 12, 2013 · N919AT · Boeing 717200 · Emergency EquipmentSDR SWAA2013011611503Pin · looseTAIL CONE EMERGENCY RELEASE CABLE PULLEYS AT 8:00, 9:30, AND 11:00 POS.'S ON THE 1225 CANTED FRAME LOOSE GUIDE/SECURITY PINS. SECURED PINS IAW MM.Jan 12, 2013 · N919AT · Boeing 717200 · Emergency EquipmentSDR SWAA2013011611502Mechanism · looseTAIL CONE EMERGENCY RELEASE; RIGHT LOWER RELEASE PIN MECHANISM IS LOOSE AT FRAME ATTACHMENT. TIGHTENED TAIL CONE EMERGENCY RELEASE RIGHT LWR RELEASE PIN MECHANISM IAW B717 SRM 51-41-01.Jan 12, 2013 · N919AT · Boeing 717200 · Emergency Equipment
Back to N919AT