N910AT

Service difficulty reports · 150

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 = 'N910AT' 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 SWAA2014061629099Floor Support · corrodedMAIN CABIN FLOOR SUPPORT CORRODED AT BS 200, RBL 22. REPAIRED SUPPORT IAW SRM & DWG.Jun 8, 2014 · N910AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2014061629098Seat Track · corrodedSEAT TRACK CORRODED BETWEEN BS 898 TO 1022, RBL 54. R & R SEAT TRACK IAW SRM.Jun 4, 2014 · N910AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2014061629097Handle · looseEMERGENCY EXIT PULL HANDLE LOOSE AT BS 1140, LONGERON 27L. SECURED HANDLE IAW MM.Jun 1, 2014 · N910AT · Boeing 717200 · Emergency ExitsSDR SWAA2014061629096Longeron · crackedLONGERON CRACKED AT BS 1045, LONGERON 2L. R & R LONGERON IAW SRM.Jun 1, 2014 · N910AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR SWAA2013102221368Handset · faultyELECTRICAL SMOKE ODOR IN AFT LAVATORY, AFT FLIGHT ATTENDANT`S HANDSET. R & R HANDSET IAW AMM.Oct 20, 2013 · N910AT · Boeing 717200 · Interphone/Passenger Announcement (PA) SystemSDR SWAA2013100720924Connector · disconnectedR1 DOOR EMERGENCY EVAC SLIDE Y CONNECTOR DISCONNECTED. RECONNECTED CONNECTOR IAW AMM.Oct 5, 2013 · N910AT · Boeing 717200 · Equipment/Furnishings WiringSDR SWAA2013062017427Lens · missingBUSINESS CLASS CEILING EMERGENCY EXIT SIGN MISSING. INSTALLED LENS PER MM.Jun 20, 2013 · N910AT · Boeing 717200 · Emergency LightingSDR SWAA2013030413310Sign · looseOVERHEAD BUSINESS EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER AMM.Feb 25, 2013 · N910AT · Boeing 717200 · Emergency LightingSDR SWAA2013021512698Skin · corrodedAFT FUSELAGE SKIN HAS CORROSION AT STA 880 STR 28R. REPAIR IAW B717 SRM.Feb 8, 2013 · N910AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR SWAA2013021412664Cusp Web · crackedMAIN CABIN RIGHT FLOOR CUSP WEB CRACKED AT FS 653 RBR 60. REMOVED DAMAGED DIM 1 1/2" X 3" AT STA 653 CUSP WEB IAW B717 SRM 53-00-55 FIG 203. FABRICATED DOUBLER DIM 6 1/2"X 5 1/2" FROM 7075.T6.032 PO 90015254 IAW B717 SRM 51-40-08 & 53-00-Feb 7, 2013 · N910AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2013021412663Cusp Web · crackedMAIN CABIN FLOOR RIGHT CUSP WEB CRACKED AT FS 674 RBL 46. CUT OUT AREA 36"X 14.9", FABRICATED REPAIR CUSP WEB DIM 36"X14.9 FROM 7075T6.020 PO 90015141, DOUBLER DIM 15.5"X3. 5/8" FROM 7075T6 .032 PO 90015519 IAW B717 SRM 53-00-55 REPAIRFeb 5, 2013 · N910AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2013021112555Battery · dischargedAFT ATT SEAT EMERGENCY FLASHLIGHT BATTERY INOP. REMOVED AND REPLACED AFT ATT SEAT FWD EMERGENCY FLASHLIGHT BATTERY IAW B717 25-60-01. OPERATIONAL CHECK COMPLIED WITH. GOOD IAW B717 M/M 25-60-01Feb 5, 2013 · N910AT · Boeing 717200 · Emergency EquipmentSDR SWAA2013021112554Cusp Web · crackedMAIN CABIN FLOOR LEFT SIDE CUSP WEB CRACKED AT FS 676 LBL 46. CUT OUT DAMAGE DIM 4.5"X8" AND FAB REPAIR USING P/N 7075T6 .020" PO 90015962 DIM 4.5"X 8" (FILLER) DOUBLER USING 7075T6.032" PO 90014133 DIM 6.5" X 12", ALODINED + PRIMED PFeb 5, 2013 · N910AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2013022213006Door Frame · corrodedFORWARD PIT CARGO DOOR JAMB HAS CORROSION IN A FEW AREAS. FABRICATED SPLICES 2024T3 P/O 90015407 LOCATED & DRILLED NEW PAN IAW B717 SRM 51-40-08 & 53-20-15 REPAIR 6.Feb 1, 2013 · N910AT · Boeing 717200 · Fuselage Main, StructureSDR SWAA2013022112944Beam · crackedL1 DOOR UPPER BEAM IS CRACKED AT AFT CORNER. REMOVED FITTING FOR ACCESS AT L1 DOOR UPPER BEAM. FABRICATED DOUBLER REPAIR IAW B717 SRM 51-10-04.Feb 1, 2013 · N910AT · Boeing 717200 · Passenger/Crew DoorsSDR SWAA2013022112943Beam · crackedL1 DOOR UPPER BEAM IS CRACKED AT FWD CORNER. REMOVED FITTING FOR ACCESS AT L1 DOOR UPPER BEAM. FABRICATED DOUBLER REPAIR IAW B717 SRM 51-10-04.Feb 1, 2013 · N910AT · Boeing 717200 · Passenger/Crew DoorsSDR SWAA2013021912809Skin · crackedRIGHT NLG STRUT DOOR, AFT HINGE CUTOUT CRACKED. STOP DRILLED CRACK IAW B717 SRM 53-10-01 REPAIR 6 FIG 201. VERIFIED STOP DRILLED CRACK IAW B717 NDTM PT. 6 06-10-01. FABRICATED DOUBLER FROM 2024T3 .071 P/O 90013533 IAW B717 SRM 53-10-01 REPAIR 6 FIG 201 51-4Feb 1, 2013 · N910AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR SWAA2013021512697Angle · crackedL1 DOOR INTERIOR HAS CRACKED VERTICAL ANGLE JUST AFT OF DOOR HANDLE. REMOVED VERTICAL ANGLE L-1 DOOR STA 180 AND INSTALLED IAW B717 SRM.Feb 1, 2013 · N910AT · Boeing 717200 · Passenger/Crew DoorsSDR SWAA2013021412662Support Fitting · crackedMAIN CABIN ABOVE WING CENTER SECTION LBL 25 SEAT TRACK SUPPORT FITTING IS CRACKED AT LOWER LEG FS 737. REMOVED AND REPLACED SUPPORT LBL 25 STA 737 P/N 3925819-1, PO 2300968 IAW B717 SRM 51-41-05, LOCATED & DRILLED NEW SUPPORT IAW B71Feb 1, 2013 · N910AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2013021412661Cusp Web · corrodedMAIN CABIN - CUSP WEB HAS CORROSION AT STA 446-465 RIGHT SIDE. REMOVED CORROSION AT STA 446-465 CUSP WEB IAW B717 SRM 51-10-04. ORIG MAT .020 REMAINING .000 LOSS OF .020 FOUND TO BE OUT OF LIMITS IAW B717 SRM 53-00-00 FIG 103 CUT OUT DAMAGE DIM 1" X 4.Feb 1, 2013 · N910AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2013021312623Support · crackedINTERNAL FUSELAGE LEFT STA 200 L15L WEB SUPPORT CRACKED. CUT OUT DAMAGE AREA LEFT STA 200 L15L, FABRICATE REPAIR DOUBLER FROM 7075T6 0.50" PO 900143440 FILLER FROM 7075T6 0.040" PO 90014579 AND INSTALLED IAW B717 SRM 53-10-15 51-41-02,Feb 1, 2013 · N910AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2013021312622Cusp Web · corrodedMAIN CABIN - CUSP WEB HAS CORROSION AT STA 503-522 RIGHT SIDE. REMOVED CORROSION AT STA 503-522 RIGHT CUSP WEB IAW B717 SRM 51-10-04. ORIG MAT .020 REMAINING .000 LOSS OF .020 FOUND TO BE OUT OF LIMITS IAW B717 SRM 53-00-00 FIG 103. REMOVED DAMFeb 1, 2013 · N910AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2013021112550Support Fitting · crackedMAIN CABIN ABOVE WING CENTER SECTION LBL 45 SEAT TRACK SUPPORT FITTING IS CRACKED AT LOWER LEG FS 737. REMOVED AND REPLACED SUPPORT TRACK AT FS 737 LBL 45 P/N 3925812U1 PO 790191430 IAW B717 SRM 51-41-02, 51-41-05, 51-40-08, 51-10-0Feb 1, 2013 · N910AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2013021112549Support Fitting · crackedMAIN CABIN ABOVE WING CENTER SECTION, RBL 45 SEAT TRACK SUPPORT FITTING IS CRACKED AT LOWER LEG FS 737. REMOVED AND REPLACED SUPPORT SEAT TRACK FROM P/N 392581U1 PO 90014681 AT FS 737 RBL 45 IAW B717 SRM 51-41-02, 51-41-05, 51-40-Feb 1, 2013 · N910AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2013022112981Connector · corrodedRIGHT WING AILERON ROTARY TRANSDUCER CONNECTOR CORRODED. REMOVED AND REPLACED AILERON ROTARY TRANSDUCER CONNECTOR ON RIGHT WING IAW B717 WDM 22-12-11.Jan 31, 2013 · N910AT · Boeing 717200 · Flight Control System WiringSDR SWAA2013022012890Bracket · crackedAFT ACCESSORY COMP - EMERGENCY EXIT PULL - LWR BRACKET CRACKED. REMOVED BRACKET AT THE AFT ASSY COMP EMERGENCY EXIT HANDLE IAW B717 SRM 51-41-02, FABBED BRACKET FROM 2024-T3 .040 PO# 90015161, 2" X 6" IAW B717 SRM 51-30-08, BAC DRAWING 9951070 AND BAC MESSAGEJan 31, 2013 · N910AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2013021912820Frame · crackedLEFT FRAME HAS A CRACK IN RADIOS BELOW FLOOR LEVEL. REMOVED AND REPLACED FRAME AT LEFT FS 715. FRAME P/N SA 95530034-11 PO 2300928 IAW B717 SRM 51-41-05 & 51-41-02, 51-40-08.Jan 31, 2013 · N910AT · Boeing 717200 · Fuselage Main, FrameSDR SWAA2013021912819Floor Panel · delaminatedMAIN CABIN FLOOR 222 ACF AT STA 696 TO STA 737 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED PANEL 222ACF AT STA 696 TO STA 737 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X40" IAW B717 SRM 53-20-50 REPAJan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021912818Floor Panel · delaminatedMAIN CABIN FLOOR 222 AGF AT STA 737 TO STA 813 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED PANEL 222AMF AT STA 813 TO STA 889 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X76" IAW B717 SRM 53-20-50 REPAIJan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021912817Floor Panel · delaminatedMAIN CABIN FLOOR 222 ATF AT STA 889 TO STA 954 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED PANEL 222ATF AT STA 889 TO STA 954 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X 65" IAW B717 SRM 53-20-50 REPJan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021912816Floor Panel · delaminatedMAIN CABIN FLOOR 222 WF AT STA 313 TO STA 389 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED PANEL 222WF AT STA 313 TO STA 389 RBL 22 TO 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X76" IAW B717 SRM 53-20-50 REPAIR 3 ANJan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021912815Floor Panel · delaminatedMAIN CABIN FLOOR 222FF AT STA 408 TO STA 446 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED PANEL 222FF AT STA 408 TO STA 446 RBL 22 TO RBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X38" IAW B717 SRM 53-20-50 REPAIR 3Jan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021912814Floor Panel · delaminatedMAIN CABIN FLOOR 222LF AT STA 465TO STA 541 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED PANEL 222LF AT STA 465 TO STA 541 RBL 22 TO RBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X76" IAW B717 SRM 53-20-50 REPAIR 3 Jan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021912813Floor Panel · delaminatedMAIN CABIN FLOOR 222 RF AT STA 541 TO STA 636 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED PANEL 222RF AT STA 541 TO STA 636 RBL 22 TO RBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X76" IAW B717 SRM 53-20-50 REPAIRJan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021912812Floor Panel · delaminatedMAIN CABIN FLOOR 222 ABF AT STA 674 TO STA 696 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED PANEL 222ABF AT STA 674 TO STA 696 RBL 22 TO RBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X22" IAW B717 SRM 53-20-50 REPAIJan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021912804Floor Panel · delaminatedMAIN CABIN FLOOR 222 UF AT STA 313 TO STA 389 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED FLOOR PANEL 222UF AT STA 313 TO STA 389 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM: BZZ7002TYPE3 PO 79019147 DIM: 21"X76" IAW B717 SRM 53-20-50 REPJan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021912803Floor Panel · delaminatedMAIN CABIN FLOOR 222BF AT STA 389 TO STA 465 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED FLOOR PANEL 222BF AT STA 389 TO STA 465 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM: BZZ7002TYPE3 PO 79019147 DIM: 21"X76" OAW B717 SRM 53-20-50 REPJan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021912802Floor Panel · delaminatedMAIN CABIN FLOOR 222 JF AT STA 465 TO STA 541 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED FLOOR PANEL 222JF AT STA 465 TO STA 541 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM: BZZ7002TYPE3 PO 79019147 DIM: 21"X76" IAW B717 SRM 53-20-50 REPJan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021912801Floor Panel · delaminatedMAIN CABIN FLOOR 222PF AT STA 541 TO STA 617 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED FLOOR PANEL 222PF AT STA 541 TO STA 617 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM: BZZ7002TYPE3 PO 79019147 DIM: 21"X76" IAW B717 SRM 53-20-50 REPAJan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021912800Floor Panel · delaminatedMAIN CABIN FLOOR 222 AAF AT STA 674 TO STA 696 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED FLOOR PANEL 222AAF AT STA 674 TO STA 696 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM: BZZ7002 TYPE 3 PO #79019147 DIM: 21"X22" IAW B717 SRM 53-20-5Jan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021912799Floor Panel · delaminatedMAIN CABIN FLOOR 222 AMF AT STA 813 TO STA 889 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED FLOOR PANEL 222AGF AT STA 737 TO STA 813 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM: BZZ7002TYPE3 PO #79019147 DIM: 21"X76" OAW B717 SRM 53-20-50 Jan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021812734Floor Panel · delaminatedMAIN CABIN FLOOR PANELS 222 AVF AT STA 889 TO STA 954 RBL 22 TO RBL 44 DELAMINATED. REMOVED & REPLACED FLOOR PANEL PER SRM.Jan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021812737Floor Panel · delaminatedMAIN CABIN FLOOR 222 AEF AT STA 696 TO STA 737 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED & REPLACED PANEL PER SRM.Jan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021812736Floor Panel · delaminatedMAIN CABIN FLOOR 222 AHF AT STA 737 TO STA 813 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED & REPLACED PANEL PER SRM.Jan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021812735Floor Panel · delaminatedMAIN CABIN FLOOR 222 APF AT STA 813 TO STA 889 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED & REPLACED PANEL PER SRM.Jan 31, 2013 · N910AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013021512695Longeron · crackedAFT ACCESSORY COMPARTMENT - AT STA 1133 LONG 2R CRACKED. REPAIR LONGERON & SPLICE IAW B717 SRM.Jan 31, 2013 · N910AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR SWAA2013021212604Rub Strip · corrodedWING TO BODY FAIRING RUB STRIP HAS CORROSION UNDER FILLET PANEL 160SL 26-013. REMOVED CORRODED RUB STRIP UNDER FILLET FAIRING 150SL IAW B717 MM 53-53-01. TREATED AND PRIMED NEW RUB STRIP IAW B717 SRM 51-10-04. INSTALLED SERVICEABLE RUB STRIP UNDERJan 31, 2013 · N910AT · Boeing 717200 · Aerodynamic FairingsSDR SWAA2013021212603Finger Doubler · corrodedAFT PIT RIGHT SIDE INTERNAL REPAIR FINGER DOUBLER HAS CORROSION AT FS 1010 LONGERON 24R. REMOVED CORRODED FINGER DOUBLER AND FABRICATED NEW FINGER DOUBLER FROM 7075-T6 .025 PO 90015477 B717 SRM 53-03-01 FIG 213 51-10-04 & 51-41-08 AND INSTALLEDJan 31, 2013 · N910AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR SWAA2013021912798Longeron · corrodedAFT PIT BILGE, LONGERON 28R HAS AREAS OF CORROSION FS 958 TO FS 927. REMOVED CORROSION AT STA 908 INTERCOSTAL IAW B717 SRM 51-10-04. ORIG MAT .063 REMAINING .039 LOSS OF .024 FOUND TO BE OUT OF LIMITS IAW B717 SRM 53-00-00 FIG 103. FABRICATED NEW INTERCOSTAJan 30, 2013 · N910AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR SWAA2013021512694Shear Tie · corrodedAFT PIT BILGE AREA, LOWER SHEAR TIE CORRODED AT FS 1038 RBL 2. REMOVED CORROSION SHEAR TIE FABRICATED NEW IAW B717 SRM.Jan 30, 2013 · N910AT · Boeing 717200 · Fuselage Internal Mounting Structure
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