# Service difficulty reports: N893AT

A list on [N893AT](https://openairdocs.org/aircraft/N893AT.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 171 reports

- [SDR DALA2026101605700](https://openairdocs.org/sdr/DALA2026101605700.md): Lanyard · unsecure · Oct 15, 2026 · N893AT · Boeing 717200 · Emergency Equipment
  > WIRE HANGING OFF GIRT BAR R1 SERVICE DOOR, REINSTALLED 1R DOOR SLIDE LANYARD ASSY PER AMM 25-61. (9539936) (AIRCRAFT GROUNDED).
- [SDR DALA2026091405131](https://openairdocs.org/sdr/DALA2026091405131.md): Light · inoperative · Sep 12, 2026 · N893AT · Boeing 717200 · Emergency Lighting
  > FWD UPPER EMERGENCY EXIT LIGHT INOP. REPAIRED PER B717 AMM 33-51. (9539800) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026050502828](https://openairdocs.org/sdr/DALA2026050502828.md): Door Frame · ground damage · Apr 30, 2026 · N893AT · Boeing 717200 · Fuselage Main, Structure
  > BELT LOADER DAMAGE TO AFT CARGO DOOR JAM FWD EDGE. REPAIRED DOOR JAM SEAL DEPRESSOR ON AFT CARGON FORWARD CARGO DOOR JAM IAW B717 SRM 53-20-15 (1571106) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502817](https://openairdocs.org/sdr/DALA2026050502817.md): Skin · ground damage · Apr 30, 2026 · N893AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > BELT LOADER DMG TO AFT CARGO DOOR JAMB, AFT EDGE. CORRECTIVE ACTION: REPAIRED PER PRI 634141-14. (1571522) (AIRCRAFT GROUNDED)
- [SDR DALA2026020900919](https://openairdocs.org/sdr/DALA2026020900919.md): Fmu · faulted · Feb 2, 2026 · N893AT · Boeing 717200 · Fuel Controlling System
  > ON TAKEOFF AROUND 700 - 1000 FT, HEARD A BANG AND RECEIVED LT ENG COMP STALL MESSAGE. MSG CLEARED 30 SECONDS LATER, RAN QRH AND ALL ENGINE INDICATIONS APPEARED NORMAL THE REMAINDER OF THE FLIGHT. R & R LT ENG FMU. ALL TESTS PASSED. LT ENG POWER ASSURANCE
- [SDR DALA2026012700606](https://openairdocs.org/sdr/DALA2026012700606.md): Compressor · stalled · Jan 24, 2026 · N893AT · Boeing 717200 · Turbine Engine Compressor Section
  > RETURNED TO BDL DUE TO LEFT ENGINE COMPRESSOR STALL. PERFORMED BORESCOPE INSPECTION OF THE ENTIRE LT ENGINE, NO DEFECTS FOUND. REPLACED N2 SPEED PROBE AND RETURNED TO SERVICE.(6589972)
- [SDR DALA2026010500069](https://openairdocs.org/sdr/DALA2026010500069.md): Eec · faulted · Jan 1, 2026 · N893AT · Boeing 717200 · Engine Fuel and Control
  > ATB TO DTW DUE TO LEFT ENGINE COMPRESSOR STALL ON CLIMB OUT. PERFORMED BORO INSP NO DAMAGED FOUND. REPLACED EEC, OPS CHECK NORMAL. (8071484)
- [SDR DALA2025121009010](https://openairdocs.org/sdr/DALA2025121009010.md): Relay · faulted · Dec 7, 2025 · N893AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY LIGHTS FLICKER ON AND OFF DURING FLGHT. REMOVED AND REPLACED RELAY R2-5133 PER B717 WDM 24-51-01. (8071400)
- [SDR DALA2025121009017](https://openairdocs.org/sdr/DALA2025121009017.md): Battery Pack · faulted · Dec 6, 2025 · N893AT · Boeing 717200 · Emergency Lighting
  > SEAT ROWS 23-29 CEILING EMER LIGHTS GO OFF AFTER SHORT TIME. REMOVED AND REPLACED BATTERY FOR PACK B5-231 PER B717 AMM 33-51. (8071402)
- [SDR DALA2025121009016](https://openairdocs.org/sdr/DALA2025121009016.md): Relay · faulted · Dec 5, 2025 · N893AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY LIGHTS FLICKER ON & OFF. REMOVED & REPLACED RELAY R2-5133 REF AIPC 24-50-22-01 ITEM 40, WDM 33-51-11. OPS CHECK NORMAL AT THIS NORMAL AT THIS TIME. (7961086)
- [SDR DALA2025121009014](https://openairdocs.org/sdr/DALA2025121009014.md): Light · no discrepancy · Dec 4, 2025 · N893AT · Boeing 717200 · Emergency Lighting
  > ONCE AIRBORNE, ALL EMERGENCY LIGHTS CAME OM AND WOULD NOT RESET ROW 25/22 EMER LIGHTS ARE OUT & EXIT LIGHT OUT AT EMER EXIT. EMER LIGHTD WENT OUT WHEN LDG GEAR CAME DOWN, CAME BACK ON AFTER LAND. PERFORMED EMERGENCY LIGHTING SYSTEM OPS CHK. OPS CHK GOOD. OK
- [SDR DALA2025111808417](https://openairdocs.org/sdr/DALA2025111808417.md): Slide · deflated · Nov 12, 2025 · N893AT · Boeing 717200 · Escape Slide
  > SLIDE IN TAIL CONE FOUND DEFLATED IN TAIL COMPARTMENT. REMOVED TAIL CONE SLIDE IAW AMM 25-61-02. INSTALLED NEW TAIL CONE SLIDE IAW WC 2561-9006 (7585377)
- [SDR DALA2025111208303](https://openairdocs.org/sdr/DALA2025111208303.md): Warning Message · false activation · Nov 11, 2025 · N893AT · Boeing 717200 · Rudder Control System
  > ATO- APPROX 85KTS DUE TO RUDDER RESTRICTED MESSAGE. PERFORMED RUDDER THROW LIMIT FUNCTIONAL TESTS AND RUDDER INSPECTIONS. NO DEFECTS NOTED, OPS NORMAL. (7585374)
- [SDR DALA2025041502918](https://openairdocs.org/sdr/DALA2025041502918.md): Pseu · failed · Apr 12, 2025 · N893AT · Boeing 717200 · Landing Gear Position and Warning
  > SHIP 9553 -MISC/DE- THE CREW DECLARED AN EMERGENCY WITH ATC DUE TO THE "PROXIMITY SWITCH ELECTRONIC UNIT FAIL" MESSAGE ILLUMINATING. THE FLIGHT LANDED WITHOUT FURTHER ISSUE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE PSEU AND THE OPERATIONAL CHECK WAS GOOD. (
- [SDR DALA2025020500881](https://openairdocs.org/sdr/DALA2025020500881.md): Door Frame · corroded · Feb 5, 2025 · N893AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON AFT CARGO DOOR JAMB AT AFT CARGO BIN. SUMMARY OF NRC 00064: CORROSION LEVEL 2. THE AFT CARGO DOOR JAMB AT AFT CARGO BIN WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #0796316)
- [SDR DALA2025020300802](https://openairdocs.org/sdr/DALA2025020300802.md): Cargo Track · corroded · Feb 1, 2025 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION WAS FOUND ON THE AFT CARGO COMP TIE TRACK LOCATED BETWEEN Y=995 TO Y=1022. SUMMARY OF NRC 00133: CORROSION LEVEL 2. THE TIE TRACK LOCATED BETWEEN Y=995 TO Y=1022 WAS FABRICATED PER DWG S2922357 AND REPLACED PER B717 SRM 51-41-01-OG. (LP #0790027)
- [SDR DALA2024021201856](https://openairdocs.org/sdr/DALA2024021201856.md): Battery Pack · inoperative · Feb 12, 2024 · N893AT · Boeing 717200 · Emergency Lighting
  > DOOR 1L & 1R EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT STA B5-118 REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #9376629)
- [SDR DALA2023031601913](https://openairdocs.org/sdr/DALA2023031601913.md): Unknown · unknown · Mar 15, 2023 · N893AT · Boeing 717200 · Elevator, Plate/Skin
  > DAMAGE T: HOLE CAUSED BY TOOLING DAMAGE ON ELEVATOR RH BTW XHR 214 AND XHR 218.762, AND 13 INCHES FWD APROX OF ELEVATOR TRAILING EDGE. SUMMARY OF NRC 00680: ELEVATOR RH BTW XHR 214 AND XHR 218.762, AND 13 INCHES FWD APROX OF ELEVATOR TRAILING EDGE WAS REPAIRED
- [SDR DALA2023031401848](https://openairdocs.org/sdr/DALA2023031401848.md): Unknown · unknown · Mar 12, 2023 · N893AT · Boeing 717200 · Elevator, Plate/Skin
  > DENT ON ELEVATOR RH BTW XHS 55 AND XHS 76, AND 12.5 INCHES FWD APROX OF ELEVATOR TRAILING EDGE. SUMMARY OF NRC 00679: DENT ON ELEVATOR RH BTW XHS 55 AND XHS 76, AND 12.5 INCHES FWD APROX OF ELEVATOR TRAILING EDGE WAS REPAIRED PER B717-200 SRM 51-70-13-2R-1. AL
- [SDR DALA2023031401847](https://openairdocs.org/sdr/DALA2023031401847.md): Unknown · unknown · Mar 11, 2023 · N893AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 18RH AT R1 PASSENGER DOOR (AFT EDGE). SUMMARY OF NRC 00479: CORROSION LEVEL: 2. LONGERON 18RH AT R1 PASSENGER DOOR (AFT EDGE) WAS REPAIRED PER ER/A 605807-14 REV ORIGINAL SECTION I, PERMANENT REPAIR AND PRI 605807-14 REV 4. ASSOCIATED ER/
- [SDR DALA2023030701659](https://openairdocs.org/sdr/DALA2023030701659.md): None · none · Mar 5, 2023 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH/LH TRACKS (RH) FROM STA Y=813 TO STA Y=896 AND (LH) TRACK FROM STA Y=813 TO STA Y=947 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00682: CORROSION LEVEL 2. RH/LH TRACKS (RH) FROM STA Y=813 TO STA Y=896 AND (LH) TRACK FROM STA Y=813 TO STA Y=947 AT
- [SDR DALA2023030801719](https://openairdocs.org/sdr/DALA2023030801719.md): None · none · Mar 3, 2023 · N893AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUR (4) CRACKS WERE DISCOVERED ON THE FUSELAGE SKIN. SUMMARY OF NRC 00157: PERMANENT REPAIR ON FUSELAGE SKIN WAS ACCOMPLISHED PER ER/A 566828-14 REV. B SECTION III: DAMAGE TOLERANCE PERMANENT REPAIR AND PRI 566828-14, REV. 3 AND ACCOMPLISH SECTION IV: GENERAL
- [SDR DALA2023030701657](https://openairdocs.org/sdr/DALA2023030701657.md): None · none · Mar 3, 2023 · N893AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON FINGER DOUBLER ADJACENT TO L-26LH, STA Y=1010 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00673: CORROSION LEVEL 2. FINGER DOUBLER ADJACENT TO L-26LH, STA Y=1010 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-03-01-2R PROCEDURE 1 REPAIR 1
- [SDR DALA2023030201556](https://openairdocs.org/sdr/DALA2023030201556.md): None · none · Mar 1, 2023 · N893AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 30, BTW STA Y:946 AND STA Y:974 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00255: CORROSION LEVEL 2: LONGERON 30 BTW STA Y:946 AND STA Y:974 AT AFT CARGO COMPARMENT WAS PERMANENTLY REPAIRED PER B-717-200 SRM 53-20-05 REPAIR 1 PAR. 4 FIG. 201
- [SDR DALA2023022501419](https://openairdocs.org/sdr/DALA2023022501419.md): None · none · Feb 23, 2023 · N893AT · Boeing 717200 · Fuselage Internal Mounting Structure
  > RE-WRITE TO NRC #00493: DUE TO INADEQUATE STEERING OF THE RELATED STATIONS. THIS NRC IS TO CLARIFY THE CORRECT LOCATION FOR EACH STRUCTURAL ELEMENT. CORROSION ON FLOOR STRUCTURE SUPPORTS ALONG FWD DIAPHRAGM AT CPAX BTW STA. Y=157 TO Y=200; AND BTW BL (X)=45 (-
- [SDR DALA2023022501418](https://openairdocs.org/sdr/DALA2023022501418.md): None · none · Feb 23, 2023 · N893AT · Boeing 717200 · Fuselage Floor Panel
  > AFTER REMOVAL OF FORWARD JAM PAN SEALS,CRACK WAS FOUND ON THE FWD SEAL. SUMMARY OF NRC 00626: REPAIR DOUBLER WAS INSTALLED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 REPAIR 1 AND SRM 51-41-02-0G. (LP #2642198)
- [SDR DALA2023022501417](https://openairdocs.org/sdr/DALA2023022501417.md): None · none · Feb 23, 2023 · N893AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR STRUCTURE SUPPORTS ALONG FWD DIAPHRAGM AT CPAX, BTW STA Y=200 TO Y=237 AND BL (-X)=55. SUMMARY OF NRC 00518: CORROSION LEVEL 2. FLOOR STRUCTURE SUPPORTS ALONG FWD DIAPHRAGM AT CPAX, BTW STA Y=200 TO Y=237 AND BL (-X)=55 WERE REPLACED PER B71
- [SDR DALA2023022401416](https://openairdocs.org/sdr/DALA2023022401416.md): None · none · Feb 23, 2023 · N893AT · Boeing 717200 · Fuselage Main, Keel
  > CRACKS (3 EA) ON FRAMES AT LH CANTED KEEL STA Y=674, Y=696, AND Y=715, (-X)=27. SUMMARY OF NRC 00319; FRAMES (3 EA) AT LH CANTED KEEL STA Y=674, Y=696, AND Y=715, (-X)=27. WERE REPAIRED PER B717-200 SRM 51-70-11-2R REPAIR 1. (LP #2642292)
- [SDR DALA2023022401413](https://openairdocs.org/sdr/DALA2023022401413.md): None · none · Feb 23, 2023 · N893AT · Boeing 717200 · Fuselage Main, Keel
  > CRACKS (2 EA) ON FRAMES AT RH CANTED KEEL STA Y=696 AND Y=715, (X)=27. SUMMARY OF NRC 00320: FRAMES (2 EA) AT RH CANTED KEEL STA Y=696 AND Y=715, (X)=27. WERE REPAIRED PER B717-200 SRM 51-70-11-2R REPAIR 1. (LP #2642050)
- [SDR DALA2023022201323](https://openairdocs.org/sdr/DALA2023022201323.md): None · none · Feb 20, 2023 · N893AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON CUSP WEB BETWEEN STA Y=200 TO STA Y=218 AND BL (-X)=55. SUMMARY OF NRC 00519: CUSP WEB WAS FABRICATED PER DWG 9936535 REV CS AND CUSP WEB BETWEEN STA Y=200 TO STA Y=218 AND BL (-X)=55 WAS REPLACED PER B-717-200 SRM 51-41-02-0G PAR 4, 51-41-05-0G P
- [SDR DALA2023022201322](https://openairdocs.org/sdr/DALA2023022201322.md): None · none · Feb 19, 2023 · N893AT · Boeing 717200 · Nacelle/Pylon Structure
  > CORROSION ON L-22LH, Y STA 845 AT FILLET FAIRING STRUCTURE. SUMMARY OF NRC 00277: CORROSION LEVEL 2. LONGERON STA 845 STR 22LH WAS REPLACED PER DWG 5911420 REV: AE AND B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2636166)
- [SDR DALA2023022201321](https://openairdocs.org/sdr/DALA2023022201321.md): None · none · Feb 19, 2023 · N893AT · Boeing 717200 · Fuselage Main, Frame
  > SECONDARY NRC, IN REF NRC 00618: CORROSION ON MEMBRANE ON WEB BTW STA Y=180 - 200 UNDER OF FLOOR SUPPORT RH. SUMMARY OF NRC 00650: CORROSION LEVEL 2. REPAIR OF MEMBRANE ON WEB BTW STA Y=180 - 200 UNDER OF FLOOR SUPPORT RH WAS PERFORMED PER B-717 SRM 53-00-55-2
- [SDR DALA2023022001259](https://openairdocs.org/sdr/DALA2023022001259.md): None · none · Feb 19, 2023 · N893AT · Boeing 717200 · Fuselage Main, Frame
  > SECONDARY NRC IN REF NRC #00493: SEVERAL DINGS ON DIAPHRAGM AT STA Y=176, BTW (-X)=15 TO (-X)=42. SUMMARY OF NRC 00660: DINGS ON DIAPHRAGM AT STA Y=176, BTW (-X)= 15 TO (-X)=42 WERE REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2. (LP #2636349)
- [SDR DALA2023022001257](https://openairdocs.org/sdr/DALA2023022001257.md): None · none · Feb 18, 2023 · N893AT · Boeing 717200 · Fuselage Main, Frame
  > A.A. A.D. CRACK WAS FOUND OF 0.437" LENGTH ON FRAME STA Y=715 RH SIDE IN REF CARD 5310-01436-04D JOB #074-0004 STEP: 13. SUMMARY OF NRC 00329: FRAME STA Y=715 RH SIDE WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G IN REF. A.A. WORK CARD: 5310-01436-03B.
- [SDR DALA2023022001256](https://openairdocs.org/sdr/DALA2023022001256.md): None · none · Feb 18, 2023 · N893AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT X=20 STA Y=236 PASSENGER CABIN (W1). SUMMARY OF NRC 00531: CORROSION LEVEL 2. FLOOR SUPPORT X=20 STA Y=236 PASSENGER CABIN (W1) WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2633854)
- [SDR DALA2023022001255](https://openairdocs.org/sdr/DALA2023022001255.md): None · none · Feb 17, 2023 · N893AT · Boeing 717200 · Escape Slide
  > WEAR ON CABLE TAIL CONE ASSEMBLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY NRC 00290: CABLE TAIL CONE ASSEMBLY WAS REPLACED PER B717-200 AMM 53-52-01. (LP #2633730)
- [SDR DALA2023021701233](https://openairdocs.org/sdr/DALA2023021701233.md): None · none · Feb 16, 2023 · N893AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON RH CUSP WEB BTW STA Y=385 AND Y=399, BL (-X)=55 AT CPAX. SUMMARY OF NRC 00649: CORROSION LEVEL 2. RH CUSP WEB BTW STA Y=385 AND Y=399, BL (-X)=55 WAS CUT PER B-717-200 SRM 53-00-55-2R REPAIR 4 FIG.212 SHEET 1 AND 51-41-05-0G. (LP #2632222)
- [SDR DALA2023021701232](https://openairdocs.org/sdr/DALA2023021701232.md): None · none · Feb 16, 2023 · N893AT · Boeing 717200 · Fuselage Floor Panel
  > IN REF NRC #00492: CORROSION ON RH CUSP WEB BTW STA Y=385 AND Y=399, BL (-X)=55 AT CPAX. SUMMARY OF NRC 00649: CORROSION LEVEL 2. RH CUSP WEB BTW STA Y=385 AND Y=399, BL (-X)=55 WAS CUT PER B-717-200 SRM 53-00-55-2R REPAIR 4 FIG 212 SHEET 1 AND 51-41-05-0G. (L
- [SDR DALA2023021701230](https://openairdocs.org/sdr/DALA2023021701230.md): None · none · Feb 16, 2023 · N893AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON INTERCOSTAL FROM STA Y=1002 TO Y=1022 ON PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00584: INTERCOSTAL FROM STA Y=1002 TO Y=1022 ON PASSENGER CABIN FLOOR STRUCTURE WAS REPLACED AND REPAIRED PER B717-200 SRM 53-00-00-2R REPAIR 2, 51-41-02-0G, AND
- [SDR DALA2023021501184](https://openairdocs.org/sdr/DALA2023021501184.md): Unknown · unknown · Feb 15, 2023 · N893AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON SUPPORT WEB AT STA 579 TO 598 L17 RH FWD CARGO COMPARTMENT. SUMMARY OF NRC 00331: CORROSION LEVEL 2. SUPPORT WEB AT STA 579 TO 598 L17 RH FWD CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2629599)
- [SDR DALA2023021501183](https://openairdocs.org/sdr/DALA2023021501183.md): Unknown · unknown · Feb 14, 2023 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH CENTER SEAT TRACK X=44 FROM STA Y=200 TO Y=256. SUMMARY OF NRC 00523: CORROSION LEVEL 2. LH CENTER SEAT TRACK AND SPLICE WAS REPLACED ON X=44 FROM STA Y=200 TO Y=256 PER B717-200 SRM 53-20-52-2R-PROCEDURE 5. (LP #2629217)
- [SDR DALA2023021501181](https://openairdocs.org/sdr/DALA2023021501181.md): None · none · Feb 13, 2023 · N893AT · Boeing 717200 · Fuselage Main, Frame
  > SECONDARY NRC, IN REF NRC 00488 CORROSION ON LH CUSP WEB BTW STA Y=560 - 579 AND BTW Y=609 TO 617. SUMMARY OF NRC 00612: CUSP WEB LH BTW STA Y=560 TO 579 AND BTW Y=609 TO 617 WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REP. 4 AND 51-41-02-0G. (LP #2
- [SDR DALA2023021501177](https://openairdocs.org/sdr/DALA2023021501177.md): None · none · Feb 12, 2023 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH INBD SEAT TRACK -X=22 FROM STA Y=200 TO Y=256. SUMMARY OF NRC 00524: CORROSION LEVEL 2. RH INBD SEAT TRACK -X=22 FROM STA Y=200 TO Y=256 WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #2625411)
- [SDR DALA2023021401128](https://openairdocs.org/sdr/DALA2023021401128.md): Unknown · unknown · Feb 10, 2023 · N893AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON ANGLE AT L1 DOOR JAMB (LWR SIDE) BTW STA Y=157 TO 186, BL -X=55 AT CPAX. SUMMARY OF NRC 00476: CORROSION LEVEL 2. ANGLE AT L1 DOOR JAMB (LWR SIDE) BTW STA Y=157 TO 186, BL -X=55 AT CPAX WAS REPLACED PER B717-200 SRM 53-10-51-0I-2 AND 51-41-02-0G.
- [SDR DALA2023021401124](https://openairdocs.org/sdr/DALA2023021401124.md): Unknown · unknown · Feb 9, 2023 · N893AT · Boeing 717200 · Fuselage Floor Panel
  > CRACK ON FWD PAN OF FWD CARGO DOOR BTW BEAM 2 AND 3. SUMMARY OF NRC 00294: FWD PAN OF FWD CARGO DOOR BTW BEAM 2 AND 3 WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #2622016)
- [SDR DALA2023021401123](https://openairdocs.org/sdr/DALA2023021401123.md): Unknown · unknown · Feb 9, 2023 · N893AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON INTERCOSTAL ON L1 DOOR INTERNAL STRUCTURE (BEHIND OPEN/CLOSURE HANDLE). SUMMARY OF NRC 00315: INTERCOSTAL ON L1 DOOR INTERNAL STRUCTURE (BEHIND OPEN/CLOSURE HANDLE) WAS FABRICATED AND REPLACED PER DWG 9955763 REV. M, B717-200 SRM 51-41-01-0G, 51-41-02
- [SDR DALA2023021401122](https://openairdocs.org/sdr/DALA2023021401122.md): Unknown · unknown · Feb 9, 2023 · N893AT · Boeing 717200 · Fuselage Floor Panel
  > IN REF NRC 00294: CRACK ON FWD PAN OF FWD CARGO DOOR ON BEAM 5. SUMMARY OF NRC 00628: FWD PAN OF FWD CARGO DOOR ON BEAM 5 WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #2621821)
- [SDR DALA2023021401133](https://openairdocs.org/sdr/DALA2023021401133.md): Unknown · unknown · Feb 7, 2023 · N893AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > WORN ON PREVIOUS REPAIR (2EA) OF FWD CARGO DOOR BARRIER LATCHES. SUMMARY OF NRC 00547: REPAIR DOUBLERS WERE REPLACED PER ER/A 559579-14MA REV ORIGINAL, SECTION I. PERMANENT REPAIR ASSOCIATED ER/A 14-559579 ADDED FOR AC 9553. (LP #2618071)
- [SDR DALA2023020700926](https://openairdocs.org/sdr/DALA2023020700926.md): Not Reported · not reported · Feb 7, 2023 · N893AT · Boeing 717200 · Fuselage Main, Frame
  > IN REF TO NRC 00497: FABRICATE CUSP WEB. SUMMARY OF NRC 00497: CUSP WEB WAS FABRICATED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #2618064)
- [SDR DALA2023020600882](https://openairdocs.org/sdr/DALA2023020600882.md): Not Reported · not reported · Feb 5, 2023 · N893AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK WAS FOUND AT AFT BRACKET OF LOWER LINNER SUPPORT BRACKETS. SUMMARY OF NRC 00619: AFT BRACKET (ANGLE) OF PASSENGER DOOR L1 IN LOWER INTERNAL STRUCTURE WAS FABRICATED AND REPLACED PER B717-200 SRM 51-41-02-0G AND DWG 5914121 REV. AV. (LP #2616255)

Next page: https://openairdocs.org/aircraft/N893AT/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N893AT/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.