N893AT

Service difficulty reports · 171

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 = 'N893AT' 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 DALA2023020600881Not Reported · not reportedCRACK ON INTERCOSTAL OF CPAX FLOOR SUPPORT AT STA 636 AND X=0. SUMMARY OF NRC 00168: CRACK ON INTERCOSTAL OF CPAX FLOOR SUPPORT AT STA 636 AND X=0 WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1. (LP #2613685)Feb 4, 2023 · N893AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023020200822Not Entered · not enteredCRACKED INTERCOSTAL ON INTERNAL STRUCTURE OF THE L1 PAX DOOR (FWD UPPER SIDE). SUMMARY OF NRC 00314: CRACKED INTERCOSTAL ON INTERNAL STRUCTURE OF THE L1 PAX DOOR (FWD UPPER SIDE) WAS REPAIRED PER B717-200 SRM 52-10-02-2R-8 REPAIR 8. (LP #2608676)Jan 31, 2023 · N893AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2023020200821Not Entered · not enteredCRACK ON INTERCOSTAL IN L1 PASSENGER DOOR INTERNAL STRUCTURE AFT SIDE. SUMMARY OF NRC 00316: CRACK ON INTERCOSTAL IN L1 PASSENGER DOOR INTERNAL STRUCTURE AFT SIDE WAS REPAIRED PER B717-200 SRM 52-10- 02-2R-7 REPAIR 7. (LP #2608672)Jan 31, 2023 · N893AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2022082905782None · noneSHIP 9553 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC WHILE DUE TO THE #1 ENGINE BEING DIFFICULT TO CONTROL DURING CLIMB. THE ENGINE WAS NOT SHUT DOWN. THE LANDING AT THE SCHEDULED ARRIVAL AIRPORT WAS UNEVENTFUL. MAINTENANCE COULD NOT FIND ANY SOUAug 26, 2022 · N893AT · Boeing 717200 · Fuel Control/Turbine EnginesSDR DALA2022022501229None · noneDURING CCK AT QRO, A 0.500 INCH LONG CRACK AFFECTING SKIN 5936436-102 (M/F 0.050 INCH THICK 2024-T3 CLAD SHEET) AND A 1.800 INCH LONG CRACK AFFECTING INNER DOUBLER 5936436-39 (M/F 0.025 INCH THICK 7075-T6 CLAD SHEET) WERE FOUND AT STA 1022, BETWEEN L13R-L13R. Feb 23, 2022 · N893AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2022022301182None · noneCRACKS ON SCUFF PLATE AT AFT CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00160: SCUFF PLATE WAS REPAIRED PER ER/A 542149- 14TR REV.B SECTION I: PERMANENT REPAIR. (LP #2130791)Feb 22, 2022 · N893AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2022022201132None · noneCORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0008: CORROSION LEVEL 2, LOWER DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPAIRED PER B-717 SRM 53-20-15-2R AND SRM 51-41-02-0G AND 51-41-05-0G PAR. 8 FIG. 12 AND 13. (LP #2130516)Feb 21, 2022 · N893AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2022021601014None · noneCRACKED LONGERON 2 RH ON STA Y=1133 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00099: LONGERON 2 RH ON STA Y=1133 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R-2 FIG. 201. (LP #2123109)Feb 15, 2022 · N893AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2022021601013None · noneCRACKED LONGERON 2 LH ON STA Y=1133 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00100: LONGERON 2 LH ON STA Y=1133 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R-2 FIG. 201. (LP #2123104)Feb 15, 2022 · N893AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2021052702915Pseu · failedSHIP 9553 - THE CREW DECLARED AN EMERGENCY FOR A PSEU FAILURE WITH ASSOCIATED SLAT OVER SPEED WARNING. CORRECTIVE ACTION: MAINTENANCE REPLACED THE PSEU AND THE LEFT SLAT CHANNEL B PROXIMITY SENSOR. (LP #7568504)May 26, 2021 · N893AT · Boeing 717200 · Leading Edge Slat Control SystemSDR DALA2021020800703Battery Pack · inoperativeTHE TAILCONE SLIDE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENACE REPLACED THE EMERGENCY LIGHTS BATTERY, B5-116, PER B717 AMM 33-51. (LP #7593826)Feb 6, 2021 · N893AT · Boeing 717200 · Emergency LightingSDR DALA2020123104353Battery Pack · inoperativeALL FOUR UPPER OVER WING EMERGENCY EXIT SIGNS HAVE INOPERATIVE LIGHTS. MAINTENANCE REPLACED THE BATTERY PACKS AT ROW 19EDC AND 20DC, IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD.Dec 23, 2020 · N893AT · Boeing 717200 · Emergency LightingSDR DALA2020021101065Gasket · damagedRIGHT WHEELWELL SLANT PANEL LEAKING. GASKET IS DAMAGED. MAINTENANCE REPLACED THE SLANT PANEL GASKET REF B717 AMM 53-32-02. LEAK CHECK IS GOOD. (LP #1484805)Feb 11, 2020 · N893AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2019121107219Lens · missingTHE MID CABIN OVERHEAD EMERGENCY SIGN LENS IS MISSING. MAINTENANCE INSTALLED A NEW LENS. EEPL ARE OK FOR SERVICE PER B717 AMM 33-51. (LP #5371965)Dec 10, 2019 · N893AT · Boeing 717200 · Emergency LightingSDR DALA2019031101605Power Supply · inoperativeAFT EQUIPMENT BAY EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY PER AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #5551070)Mar 9, 2019 · N893AT · Boeing 717200 · Emergency LightingSDR DALA2018082085143Lever · out of adjustTAILCONE DEPLOYMENT FAILED TEST USING INTERNAL RELEASE HANDLE. READING LESS THAN MINIMUM REQUIREMENT. MAINTENANCE ADJUSTED BOTH BOTTOM AND UPPER RIGHT LATCH LEVERS IAW AMM 53-52-01 830-802. THE TAILCONE OPERATION NOW TESTS PROPERLY IAW AMDS W/C 5352-2001.Aug 18, 2018 · N893AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2018031701755Skin · crackedCRACKED FUSELAGE SKIN BS 1022, BETWEEN LONGERONS 14R TO 15R. THE SKIN & DOUBLER WERE REPAIRED IAW ETI-17-18-047, REV 3, AND ER/A 566828-14, REV ORIGINAL.Mar 16, 2018 · N893AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018031501732Channel · corrodedWEAR ON THE CORNERS OF THE FWD CARGO DOOR BARRIER. LOWER FORWARD AND LOWER AFTER CORNERS OF DOOR BARRIER CHANNEL WERE BLENDED AND UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1, AND 2. FOUND OUT OF LIMITS AND LOWER AFTER EDGE OF DOOR BARRIERMar 14, 2018 · N893AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018031501712Skin · dentedDENT ON RT FLAP LOWER MOVEABLE VANE LOWER SKIN -5" FROM OUT EDGE. RT FLAP LOWER MOVEABLE VANE LOWER SKIN WAS REPAIRED PER SRM 57-53-01-2R PROCEDURE 1 PAR 4 AND SRM 51-70-02.Mar 14, 2018 · N893AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2018031201613Door Frame · crackedCRACKED RT NLG DOOR FRAME BEAM BS 40. THE RT NLG DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2, FIG 201. HFEC INSPECTION WAS ACCOMPLISHED AFTER THE DAMAGE WAS REMOVED. NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001.Mar 11, 2018 · N893AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018031001602Skin · crackedCRACKED FUSELAGE SKIN, BS 1189.604 LONGERON L22R. THE SKIN WAS REPAIRED IAW SRM 53-00-00-2R-1, FIGURE 201.Mar 9, 2018 · N893AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017121800027Life Vest · out of positionMAINTENANCE FOUND THAT THE LIFE VESTS WERE BLOCKING THE EMERGENCY EXIT DOOR AFTER THE REVENUE FLIGHT ARRIVED. THE LIFE VESTS WERE REPOSITIONED TO THEIR PROPER LOCATION PER B717 AMM 25-62. (LP #4135006)Dec 15, 2017 · N893AT · Boeing 717200 · Life JacketSDR DALA2017060704556Shaft · brokenDURING A CHECK OF TAILCONE RELEASE MECHANISM, MAINTENANCE FOUND THAT THE RELEASE SHAFT WAS BROKEN. MAINTENANCE REPLACED THE CAM LATCH/LOCK ASSEMBLY. THE TAILCONE WAS ADJUSTED AND RIGGED AFTER INSTALLATION AND FOUND OPERATIONAL. THE RII WAS COMPLETED FOLLOWING Jun 6, 2017 · N893AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2017032902519Light · out of adjustLT AFT EMERGENCY LIGHT INOPERATIVE. ADJUSTED LT AFT EXTERIOR EMERGENCY LIGHT PER B717 AMM 35-54. CHECKS OK.Mar 28, 2017 · N893AT · Boeing 717200 · Emergency LightingSDR DALA2016110908367Power Supply · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN THE TAIL COMPARTMENT INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO NORMAL OPERATIONAL CONDITION.Nov 9, 2016 · N893AT · Boeing 717200 · Emergency LightingSDR DALA2016110408243Lens · damagedMAINTENANCE DISCOVERED THAT THE EMERGENCY EXIT SIGN DIFFUSER COVER OVER DOOR L1 WAS DAMAGED. MAINTENANCE REPLACED THE LENS AND THE OPS CHECKED GOOD.Nov 3, 2016 · N893AT · Boeing 717200 · Emergency LightingSDR DALA2016071305265Power Supply · inoperativeDURING SERVICE CHECK, FOUND SEVERAL CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED TWO CABIN EMERGENCY POWER SUPPLIES AND BATTERIES IAW AMM 33-51.Jul 12, 2016 · N893AT · Boeing 717200 · Emergency LightingSDR DALA2016060804423Oven · smokeCREW REPORTED THE FORWARD GALLEY OVEN SMOKING FROM TOP VENT. CABIN CREW PULLED OVEN CIRCUIT BREAKER AND SMOKE SUBSIDED. MAINTENANCE FOUND PLASTIC INSIDE OVEN HAD BEEN BURNING. THE OVEN WAS REPLACED IAW AMM. COMPLIED WITH NO GO ODI PREVENTION FOR SMOKE IN CABJun 6, 2016 · N893AT · Boeing 717200 · Buffet/GalleysSDR DALA2016060604375Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS FOR THE FWD OVERWING HATCH WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Jun 5, 2016 · N893AT · Boeing 717200 · Emergency LightingSDR DALA2016030901775Pan · crackedPASSNEGER COMPARTMENT BETWEEN BS 794 AMD BS 813 FWD BOTTOM WINDOW PAN AFT OF BS 794 IS CRACKED AS MARKED IN CORNER LT SIDE. REPLACED PASSENGER COMPARTMENT WINDOW PAN LT BS 794 AND BS 813 IAW SRM 51-41-02 AND DWG 5936019, SHEET 1.Mar 8, 2016 · N893AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016030901774Pan · crackedPASSENGER CABIN RT WINDOW PAN, BS 756 UPPER FWD CORNER CRACKED. REPLACED PASSENGER CABIN RT WINDOW PAN BS 756 IAW SRM 51-41-02 AND DWG 5936019, SHEET 3.Mar 8, 2016 · N893AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016030901773Skin · corrodedCENTER WING BOX UPPER SKIN IS CORRODED IN SEVERAL LOCATIONS AROUND FASTENER HEADS BETWEEN BS 715 THROUGH BS 737, RBL 43 THROUGH RBL 59, VIEW FROM UNDER CABIN FLOOR BOARDS. REPAIRED CENTER WING BOX UPPER SKIN AT BS 715 THROUGH BS 737, RBL 43, RBL 59 IAW PRI 54Mar 8, 2016 · N893AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016030901772Fuel Cell · damagedCENTER WING BOX FUEL TANK UPPER SKIN BS 708, RBL 50: 2 FASTENERS HOLES ELONGATED. REPAIRED CENTER WING BOX FUEL TANK UPPER SKIN AT BS 708, RBL 50, 2 FASTENER HOLES IAW PRI 540750-14, REV 0, PRI 540753-14, REV 0- REV 2 AND ER/A 540753-14, REV ORIGINAL ASSOCIATEMar 8, 2016 · N893AT · Boeing 717200 · Fuel StorageSDR DALA2016030901771Skin · corrodedCENTER WING BOX UPPER SKIN IS CORRODED IN SEVERAL LOCATIONS AROUND FASTENER HEADS, BETWEEN BS 696 THROUGH 715 RBL, 43 THROUGH RBL 59, VIEW FROM UNDER CABIN FLOOR BOARDS. REPAIRED CENTER WING BOX UPPER SKIN AT BS 696 THROUGH 715, RBL 43 THROUGH RBL 59 IAW PRI 5Mar 8, 2016 · N893AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016030901770Skin · corrodedCENTER WING BOX UPPER SKIN IS CORRODED IN SEVERAL LOCATIONS AROUND FASTENER HEADS BETWEEN STA 674 THROUGH 696, RBL 43 THROUGH RBL 59, VIEW FROM UNDER CABIN FLOOR BOARDS. REPAIRED CENTER WING BOX UPPER SKIN BS 674 THROUGH 696, RBL 43 THROUGH RBL 59 IAW PRI 540Mar 8, 2016 · N893AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016030901769Skin · corrodedCENTER WING BOX UPPER SKIN IS CORRODED IN SEVERAL LOCATIONS AROUND FASTENER HEADS BETWEEN BS 674 THROUGH 696, LBL 43 THROUGH LBL 59, VIEW FROM UNDER CABIN FLOOR BOARDS. REPAIRED CENTER WING BOX UPPER SKIN BS 674 THROUGH 696, LBL 43 THROUGH LBL 59 IAW PRI 5407Mar 8, 2016 · N893AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016030901768Skin · corrodedCENTER WING BOX UPPER SKIN IS CORRODED IN SEVERAL LOCATIONS AROUND FASTENER HEADS BETWEEN BS 715 THROUGH 737, LBL 43 THROUGH LBL 59, VIEW FROM UNDER CABIN FLOORBOARDS. REPAIRED CENTER WING BOX UPPER SKIN BS 715, THROUGH 737, LBL 43, THROUGH LBL 59 IAW PRI 540Mar 8, 2016 · N893AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016030901767Skin · corrodedCENTER WING BOX UPPER SKIN IS CORRODED IN SEVERAL LOCATIONS AROUND FASTENER HEADS BETWEEN BS 696 THROUGH 715, LBL 43 THROUGH LBL 59. VIEW FROM UNDER CABIN FLOOR BOARDS. REPARIED CENTER WING BOX UPPER SKIN BS 696 THROUGH 715, LBL 43 THROUGH LBL 59 IAW PRI 540Mar 8, 2016 · N893AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016030901766Frame · crackedFWD CARGO COMPARTMENT AFT BULKHEAD AREA RT SIDE BS 674 BETWEEN LONGERONS 23R AND 24R WING FRONT SPAR FWD FACE SUPPORT PLATE CRACKED IN RADIUS. REPLACED FWD CARGO COMPARTMENT AFT BULKHEAD AREA RT SIDE BS 674 BETWEEN LONGERON 23R AND 24R WING FRONT SPAR FWD FACMar 8, 2016 · N893AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016030901765Frame · crackedFWD CARGO COMPARTMENT AFT BULKHEAD AREA LT SIDE BS 674 BETWEEN LONGERONS 23L AND 24L WING FRONT SPAR FWD FACE SUPPORT PLATE CRACKED IN RADIUS. REPLACED FORWARD CARGO COMPARTMENT AFT BULKHEAD AREA LT SIDE BS 674 BETWEEN LONGERON 23L AND 24L WING FRONT SPAR FWDMar 8, 2016 · N893AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016030901763Cusp Web · damagedCUSP WEB FROM BS 656-715, RT SIDE HAS A CRACK AND SEVERAL FASTENER HOLES TORN. REPAIRED THE CUSP WEB IAW SRM 53-00-55, PAGE 298, REPAIR 4.Mar 8, 2016 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016030901762Cusp Web · damagedBS 655-715, LBL 59, CUSP WEB DAMAGE AT INBD EDGE COMMON TO SEAT TRACK. REPAIRED CUSP WEB AT BS 655-715, RBL 59, LT SIDE IAW SRM 53-00-55, PAGE 298, REPAIR 4.Mar 8, 2016 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016030502576Longeron · corrodedAFT CARGO BAY BILGE AREA, BS 889.50, LONGERON 30 AREA FRAME IS CORRODED TOP SURFACE IN BOTTOM CURVED FLANGE AS MARKED.Mar 4, 2016 · N893AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016030501683Shear Tie · corrodedAFT CARGO BAY BILGE AREA, BS 889.5 BETWEEN LONGERON 30 AND 29L AREA SHEAR TIE IS CORRODED IN CORNER AS MARKED. REMOVED CORROSION ON AFT CARGO BS 889.5 SHEAR TIE BETWEEN LONGERON 30 AND 29L, REMOVED CORROSION IAW SRM 51-10-01. DAMAGE FOUND TO BE OUT OF LIMITSMar 4, 2016 · N893AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016030401631Structure · crackedTAIL SECTION INTERIOR UPPER RT SIDE BS 1200 CANT AFT END OF VENT BOX CRACKED AT PREVIOUS REPAIR. REPAIRED CRACKED VENT BOX AT BS 1200 RT SIDE IAW ER/A 540752-14, REV 0, NO DEVIATIONS.Mar 3, 2016 · N893AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016030401630Structure · crackedTAIL SECTION INTERIOR UPPER LT SIDE BS 1200 CANT AFT END OF VENT BOX CRACKED.Mar 3, 2016 · N893AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016030401629Cargo Track · corrodedAFT CARGO BAY AREA BS 954 BETWEEN LONGERON 28R AND 27R. TRACK IS CORRODED TOP SURFACE. BLENDED OUT CORROSION. .042 REMAINING FOUND TO BE OUT OF LIMITS IAW 53-20-52 SRM. FABRICATED NEW TRACK IAW DWG 5936663-535, ALODINED, PRIMED AND INSTALLED TOP COAT IAW SMar 3, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016030401628Door Sill · corrodedAFT CARGO DOOR LOWER SILL HAS MUTIPLE AREAS OF CORROSION. BLENDED OUT CORROSION. ORIGINAL .050 REMAINING .031, LOSS .019 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15. REPAIRED LOWER SILL IAW SRM 53-20-15, REPAIR 7.Mar 3, 2016 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016030401626Frame · crackedLEFT WW UPPER FWD OTBD FRAME CRACKED. STOP DRILLED CRACK AT LT WHEEL WELL UPPER FWD OTBD FRAME AND COMPLETED REPAIR IAW SRM 53-20-02. REPAIR 3, RESTORED FINSHES. DOOR FIT AND FAIR AND LANDING GEAR RETRACTION FUNCTIONAL CHECKS ACCOMPLISHED ON JC 3230-2001 & Mar 3, 2016 · N893AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016030301624Threshold · corrodedAFT CARGO BAY BILGE AREA BS 954 TO BS 977 DOOR THRESHOLD WEB IS CORRODED 20 EA AREAS TOP SURFACE MARKED. BLENDED CORROSION FOUND TO BE 100 PERCENT MATERIALS LOSS. REPLACED WEB IAW SRM 51-40-02 AND DWGS NR 5910158.Mar 2, 2016 · N893AT · Boeing 717200 · Fuselage Miscellaneous Structure
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