# Service difficulty reports: N895AT

A list on [N895AT](https://openairdocs.org/aircraft/N895AT.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 3 · 104 reports

- [SDR DALA2026100205473](https://openairdocs.org/sdr/DALA2026100205473.md): Anti-Skid Sys · warning message · Oct 1, 2026 · N895AT · Boeing 717200 · Brake Anti-Skid Section
  > ATO- DISCONTINUED TAKEOFF ROLL AT 25KTS AFTER RECEIVING AN ANTI-SKID FAIL MESSAGE. MAINTENANCE TROUBLESHOOT PER B717 FIM 32-45, NO MESSAGES AND ALL RETURN TO SERVICE TEST PASSED. (9516202) (AIRCRAFT GROUNDED).
- [SDR DALA2025120508916](https://openairdocs.org/sdr/DALA2025120508916.md): Pitot Tube · faulted · Dec 3, 2025 · N895AT · Boeing 717200 · Pitot/Static Anti-Ice System
  > ATB/DE- RETURNED ATL DUE TO RUDDER PITOT HEAT FAIL MESSAGE. REPLACED RUDDER LIMITER PITOT PROBE. MESSAGE CLEARED. OPS CHECK GOOD.(7974434)
- [SDR DALA2025052203940](https://openairdocs.org/sdr/DALA2025052203940.md): Wire · broken · May 16, 2025 · N895AT · Boeing 717200 · Equipment/Furnishings Wiring
  > SHIP 9555-SMKE/FUME- CREW REPORTED ON FINAL THE FWD F/A SMELLED SMOKE FROM FWD LAV AND REPORTED SPARKS. CORRECTIVE ACTION: MAINTENANCE REPAIRED A BROKEN WIRE AT THE TERMINAL BLOCK.
- [SDR DALA2025042103071](https://openairdocs.org/sdr/DALA2025042103071.md): Skin · cracked · Apr 16, 2025 · N895AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DAMAGE T: CRACK ON FUSELAGE LOWER SKIN BTW STA 1048 - 1053 AND LONG 30. SUMMARY OF NRC 00136: FUSELAGE LOWER SKIN BTW STA 1048 - 1053 AND LONG 30 WAS REPAIRED PER PRI 625673-14 REV 2 AND ERA 625673 -14 REV ORIGINAL. SECTION I: PERMANENT REPAIR. MAINTENANCE REQ
- [SDR DALA2025040902759](https://openairdocs.org/sdr/DALA2025040902759.md): Skin · cracked · Apr 8, 2025 · N895AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS ON SKIN AT STA Y=1087 AND LONG 14R ON AFT FUSELAGE. SUMMARY OF NRC 00013: SKIN AT STA Y=1087 AND LONG 14R ON AFT FUSELAGE WAS REPAIRED PER PRI 625399-14 REV 4 AND ERA 625399-14 REV ORIGINAL SECTION I: PERMANENT REPAIR SEC II. ACCOMPLISH SECTION II: REPE
- [SDR DALA2025050603513](https://openairdocs.org/sdr/DALA2025050603513.md): Pin · misinstalled · Apr 6, 2025 · N895AT · Boeing 717200 · Aerodynamic Fairings
  > INSPECTION FOUND THAT THE RELEASE CAM PIN WAS INSTALLED INCORRECTLY AND THAT AN ADJUSTMENT WAS NEEDED ON THE TAIL CONE DEPLOYMENT SYSTEM. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY O
- [SDR DALA2024112611228](https://openairdocs.org/sdr/DALA2024112611228.md): Slide · out of position · Nov 25, 2024 · N895AT · Boeing 717200 · Escape Slide
  > ON WAKE-UP CHECK FOUND THE AFT TAIL CONE SLIDE PACK HAD ROTATED OUT OF SECURED POSITION. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REMOVED THE TAIL SLIDE PACK REF W/C 2561-9006
- [SDR DALA2024092509408](https://openairdocs.org/sdr/DALA2024092509408.md): Battery Pack · inoperative · Sep 24, 2024 · N895AT · Boeing 717200 · Emergency Lighting
  > FOUND THE LEFT FORWARD ENTRY EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD OVERHEAD EMERGENCY LIGHT BATTERY PACK IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6464450)
- [SDR DALA2023122810696](https://openairdocs.org/sdr/DALA2023122810696.md): Unknown · unknown · Dec 26, 2023 · N895AT · Boeing 717200 · Escape Slide
  > DURING SERVICE CHECK FOUND R1 EMERGENCY SLIDE BOTTLE PRESSURE UNSERVICEABLE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED R1 SLIDE PER AMDS CARD 2561-9005. RII COMPLETE BY
- [SDR DALA2023052304103](https://openairdocs.org/sdr/DALA2023052304103.md): Unknown · unknown · May 23, 2023 · N895AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN STA Y=214 BTW STR 28R AND STR 29R AT (E/E). SUMMARY OF NRC 00458: CORROSION LEVEL 2. SKIN STA Y=214 BTW STR 28R AND STR 29R WAS REPAIRED PER ER/A 608703-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR TIME CONTROLLED ITEMS, ACCOMPLISH SECTION II
- [SDR DALA2023052504149](https://openairdocs.org/sdr/DALA2023052504149.md): Unknown · unknown · May 22, 2023 · N895AT · Boeing 717200 · Passenger/Crew Doors
  > BENT AND CRACK TWO SECTIONS ON L1 DOOR SKIN LOWER EDGE. PTAS. FWD PASSENGER ENTRANCE SERVICEABLE DOOR REMOVED. SUMMARY OF NRC 00682: PASSENGER FORWARD ENTRANCE DOOR WAS REPLACED PER B717-200 AMM 52-11-01. THIS LOG PAGE SHOULD HAVE BEEN A YES FOR RII AND WORK T
- [SDR DALA2023052304102](https://openairdocs.org/sdr/DALA2023052304102.md): Unknown · unknown · May 20, 2023 · N895AT · Boeing 717200 · Passenger/Crew Doors
  > BENT AND CRACK TWO SECTIONS ON L1 DOOR SKIN LOWER EDGE. PTAS. SUMMARY OF NRC 00090: PASSENGER ENTRANCE DOOR WAS REPLACED FOR SERVICIABLE PASSENGER ENTRANCE DOOR PER B717-200 AMM 52-11-01. (LP #2775388)
- [SDR DALA2023052204052](https://openairdocs.org/sdr/DALA2023052204052.md): Unknown · unknown · May 20, 2023 · N895AT · Boeing 717200 · Elevator, Plate/Skin
  > SHEARED OUT AND ELONGATED HOLE ON SKIN, CLOSE TO HINGE #1 OH CONTROL TAB AT RH ELEVATOR STA XE=17 HVS. SUMMARY OF NRC 00339: SKIN, CLOSE TO HINGE #1 OH CONTROL TAB AT RH ELEVATOR STA XE=17 HVS WAS REPAIRED PER ER/A 607692-14 REV. ORIGINAL SECTION I: PERMANENT
- [SDR DALA2023052004042](https://openairdocs.org/sdr/DALA2023052004042.md): Unknown · unknown · May 19, 2023 · N895AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON FWD STOP FITTING AT AFT CARGO COMPARTMENT DOOR, (PTAS). SUMMARY OF NRC 00205: AFT CARGO DOOR WAS REPLACED FOR SERVICEABLE AFT CARGO DOOR. (LP #2773786)
- [SDR DALA2024112511161](https://openairdocs.org/sdr/DALA2024112511161.md): Skin · no discrepancy · May 16, 2023 · N895AT · Boeing 717200 · Standard Practices/Structures
  > REPAIR TO FUSELAGE SKIN & DOUBLER AT STA Y=1037 B/W L-13L & L-14L IS PENDING DTE STAGE II & III APPROVAL WITHIN 24 MONTHS OF 12MAY23. DISCONTINUE REVENUE SERVICE ON OR BEFORE 12MAY25 PENDING STAGE II & III APPROVAL. ASSOCIATED ER/A 00-607682 ADDED FOR AC 9555.
- [SDR DALA2023051703947](https://openairdocs.org/sdr/DALA2023051703947.md): Unknown · unknown · May 16, 2023 · N895AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL FUSELAGE SKIN STA Y=1037 BTW LONG 13LH & 14LH (FUS). SUMMARY OF NRC 00512: EXTERNAL FUSELAGE SKIN STA Y=1037 BTW LONG 13LH & 14LH WAS REPAIRED PER ER/A 607682-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTH
- [SDR DALA2023051603855](https://openairdocs.org/sdr/DALA2023051603855.md): Unknown · unknown · May 14, 2023 · N895AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > WEAR ON FWD SEAL RETAINER AREA AFT CARGO DOOR (PTAS). SUMMARY OF NRC 00081: REPAIR ANGLE AT SEAL RETAINER AREA WAS REPLACED PER B717-200 SRM 52-30-02-2R PROCEDURE 4, REPAIR 4. (LP #2766108)
- [SDR DALA2023051203748](https://openairdocs.org/sdr/DALA2023051203748.md): Unknown · unknown · May 11, 2023 · N895AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > DURING ATENTION OF NRC 00192, AFTER REMOVE CORROSION, LONGERON 30 FROM STA Y=908 TO Y=927 WAS FOUND OUT OF LIMITS. SUMMARY OF NRC 00550: CORROSION LEVEL 2. LONGERON 30 STA Y=900 TO Y=936 WAS REPAIRED PER B717-200 SRM 53-20-05-2R REPAIR 1. (LP #2762922)
- [SDR DALA2023051003664](https://openairdocs.org/sdr/DALA2023051003664.md): Unknown · unknown · May 9, 2023 · N895AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON LOWER SURFACE BTW STA Y=370-427 AT FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00202: CORROSION LEVEL 2. DOOR LOWER JAMB PAN WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 6 REPAIR 6. (LP #2759022)
- [SDR DALA2023050803569](https://openairdocs.org/sdr/DALA2023050803569.md): Unknown · unknown · May 7, 2023 · N895AT · Boeing 717200 · Fuselage Main, Frame
  > WEAR ON ANGLES (2 EA) OF FLIGHT ATTENDANT SEAT STOWAGE AREA AT AFT CABIN BULKHEAD DOOR (PTAS). SUMMARY OF NRC 00184: ANGLES (2 EA) OF FLIGHT ATTENDANT SEAT AT AFT CABIN BULKHEAD DOOR WERE EVALUATED AND REPAIRED AS FOLLOWS: LH HAND SIDE ANGLE WAS BLENDED OUT AN
- [SDR DALA2023050803567](https://openairdocs.org/sdr/DALA2023050803567.md): Unknown · unknown · May 6, 2023 · N895AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR PANEL STRAP AND FITTINGS AT R1 ENTRY CPAX. SUMMARY OF NRC 00445: CORROSION LEVEL 2. FLOOR PANEL STRAP AND FITTINGS WERE REPLACED PER DGW 995782 REV AB & DWG 3936190 REV. (LP #2753530)
- [SDR DALA2023050803566](https://openairdocs.org/sdr/DALA2023050803566.md): Unknown · unknown · May 6, 2023 · N895AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA 1021 LONG 7 LH PAX CABIN (CPAX). SUMMARY OF NRC 00312: FRAME STA 1021 LONG 7 LH WAS REPAIRED PER ER/A 607808-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. (LP #2753465)
- [SDR DALA2023050803565](https://openairdocs.org/sdr/DALA2023050803565.md): Unknown · unknown · May 5, 2023 · N895AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAMES STA Y=674 & Y=696 AT LH KEEL BEAM AREA (SM). SUMMARY OF NRC 00295: FRAMES STA Y=674 & Y=696 AT LH KEEL BEAM AREA WERE REPAIRED PER B717-200 SRM 51-70-11-2R, REPAIR 1. (LP #2753140)
- [SDR DALA2023050803564](https://openairdocs.org/sdr/DALA2023050803564.md): Unknown · unknown · May 5, 2023 · N895AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAMES STA Y=674 & Y=696 AT RH KEEL BEAM AREA (SM). SUMMARY OF NRC 00296: FRAMES STA Y=674 & Y=696 AT RH KEEL BEAM AREA WERE REPAIRED PER B717-200 SRM 51-70-11-2R, REPAIR 1. (LP #2753031)
- [SDR DALA2023050803563](https://openairdocs.org/sdr/DALA2023050803563.md): Unknown · unknown · May 5, 2023 · N895AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 2 RH/LH ON STA Y=1133 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00417: LONGERON 2 RH/LH ON STA Y=1133 WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE, REPAIR 2. (LP #2752081)
- [SDR DALA2023050803562](https://openairdocs.org/sdr/DALA2023050803562.md): Unknown · unknown · May 4, 2023 · N895AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON CUSP WEB AT STA Y=674 LH/RH ALSO STA Y=715 (X=56) RH SIDE AT PASSENGER CABIN. SUMMARY OF NRC 00415: CUSP WEB AT STA Y=674 LH/RH ALSO STA Y=715 (X=56) RH WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2751970)
- [SDR DALA2023050403460](https://openairdocs.org/sdr/DALA2023050403460.md): Unknown · unknown · May 4, 2023 · N895AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON RH CUSP WEB STA Y=474, Y=488, FROM Y=446 TO Y=465, Y=545 AND Y=575 AT PAX CABIN. SUMMARY OF NRC 00623: CORROSION LEVEL 2. RH CUSP WEB STA Y=474, Y=488, FROM Y=446 TO Y=465, Y=545 AND Y=575 WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REP
- [SDR DALA2023050303432](https://openairdocs.org/sdr/DALA2023050303432.md): Unknown · unknown · May 2, 2023 · N895AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON CUSP WEB STA Y=529-530, Y=905-908, Y=923.5-924.5 AND Y=952-953 AND CUSP WEB STA Y=952-953 AND 975-976 RH SIDE AT PAX CABIN IN REF NRC S/N 403. SUMMARY OF NRC 00619: CORROSION LEVEL 2. CUSP WEB STA Y=529-530, Y=905-908, Y=923.5-924.5 AND CUSP WEB S
- [SDR DALA2023050303431](https://openairdocs.org/sdr/DALA2023050303431.md): Unknown · unknown · May 2, 2023 · N895AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON LH CUSP WEB ON LIGHTENING HOLE UPPER SIDE ALSO LOWER SIDE STA Y=633, STA Y=670, AND STA Y=810 AT CABIN PAX FLOOR SRTUCTURE. FUS. IN REF NRC 0402. SUMMARY OF NRC 00616: CORROSION LEVEL 2. LH CUSP WEB ON LIGHTENING HOLE UPPER SIDE ALSO LOWER SIDE ST
- [SDR DALA2023050203396](https://openairdocs.org/sdr/DALA2023050203396.md): Unknown · unknown · May 2, 2023 · N895AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON RH CUSP WEB SPLICE LOWER SURFACE BELOW ANGLE CUSP SPLICE AT STA Y=900 X -59. SUMMARY OF NRC 00408: CORROSION LEVEL 2. RH CUSP WEB SPLICE UPPER AND LOWER SURFACE BELOW ANGLE CUSP SPLICE AT STA Y=900 X -59 WAS REPLACED PER B717-200 SRM 51-41-05-0G &
- [SDR DALA2023050203392](https://openairdocs.org/sdr/DALA2023050203392.md): Unknown · unknown · Apr 29, 2023 · N895AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON INTERCOSTAL BTW STA Y=1002 TO Y=1022 AND X=0 AT CABIN PAX (CPAX). SUMMARY OF NRC 00592: INTERCOSTAL BTW STA Y=1002 TO Y=1022 AND X=0 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. (LP #2742787)
- [SDR DALA2023042803323](https://openairdocs.org/sdr/DALA2023042803323.md): Unknown · unknown · Apr 28, 2023 · N895AT · Boeing 717200 · Entrance Stairs
  > CORROSION ON FORWARD STAIRWELL DOOR INTERNAL SKIN AND RUSTED HARDWARE WERE FOUND IN REFERENCE TO NRC 00256. SUMMARY OF NRC 00577: CORROSION LEVEL 2. FORWARD STAIRWELL DOOR WAS REPLACED PER B717-200 AMM 52-63-01 420-801. (LP #2741310)
- [SDR DALA2023042803321](https://openairdocs.org/sdr/DALA2023042803321.md): Unknown · unknown · Apr 27, 2023 · N895AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON LH CUSP WEB UPPER SIDE STA Y=421 ALSO STA Y=468 TO Y=471 IN REF NRC 00401. SUMMARY OF NRC 00614: CORROSION LEVEL 2. LH CUSP WEB STA Y=421 ALSO STA Y=468 TO Y=471 WERE REPAIRED PER B717-200 SRM 53-00-55- 2R FIG 215 AND 216. (LP #2740723)
- [SDR DALA2023042803320](https://openairdocs.org/sdr/DALA2023042803320.md): Unknown · unknown · Apr 27, 2023 · N895AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SETLEMENT ON INBD SEAT TRACK STA 196 TO 200 RBL 20 AT PAX CABIN. W1. SUMMARY OF NRC 00503: CORROSION LEVEL 2. SECTION SEAT TRACK STA 196 TO 265 RBL 20 WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR. 5 (LP #2740710)
- [SDR DALA2023042603249](https://openairdocs.org/sdr/DALA2023042603249.md): Unknown · unknown · Apr 26, 2023 · N895AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORTS FROM STA Y=157 TO Y=200 LBL 44 & 54 AT PAX CABIN. (W1). SUMMARY OF NRC 00526: CORROSION LEVEL 2. FLOOR SUPPORTS FROM STA Y=157 TO Y=200 LBL 44 & 54 WERE REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2737864)
- [SDR DALA2023042603247](https://openairdocs.org/sdr/DALA2023042603247.md): Unknown · unknown · Apr 25, 2023 · N895AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED FRAME STA Y=1037 LONG 17 RH AT PAX CABIN (W2). SUMMARY OF NRC 00554: FRAME STA Y=1037 LONG 17 RH WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PER TOPP 30-10-70 PAGE 14 PAR I. (LP #27
- [SDR DALA2023042603246](https://openairdocs.org/sdr/DALA2023042603246.md): Unknown · unknown · Apr 25, 2023 · N895AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED FRAME STA Y=1037 LONG 17 RH AT PAX CABIN (W2). SUMMARY OF NRC 00554: FRAME STA Y=1037 LONG 17 RH WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PER TOPP 30-10-70 PAGE 14 PAR. LOG PAGE
- [SDR DALA2023042703289](https://openairdocs.org/sdr/DALA2023042703289.md): Unknown · unknown · Apr 24, 2023 · N895AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON GALLEY SUPPORT STA 218 RBL 11 AT PAX CABIN FLOOR STRUCTURE. W1. SUMMARY OF NRC 597: CORROSION LEVEL 2. GALLEY SUPPORT STA 218 RBL 11 AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2735690)
- [SDR DALA2023042703288](https://openairdocs.org/sdr/DALA2023042703288.md): Unknown · unknown · Apr 24, 2023 · N895AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORTS STA Y=198 LBL 57 AT PAX CABIN FLOOR SUPPORT. CPAX. SUMMARY OF NRC 00596: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=198 LBL 57 AT PAX CABIN FLOOR SUPPORT WAS REPLACED PER B717-200 SRM 51-41-01-0G AND SRM 51-41-05-0G. (LP #2735528)
- [SDR DALA2023042503241](https://openairdocs.org/sdr/DALA2023042503241.md): Unknown · unknown · Apr 24, 2023 · N895AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED FRAME STA Y=1037 LONG 17 LH AT PAX CABIN (W2). SUMMARY OF NRC 00553: FRAME STA Y=1037 LONG 17 LH WAS REPAIRED PER B717-200 SRM. 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #2735918)
- [SDR DALA2023042503239](https://openairdocs.org/sdr/DALA2023042503239.md): Unknown · unknown · Apr 23, 2023 · N895AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS FROM STA Y=157 TO Y=200, LBL 7, RBL 7, RBL 44, & RBL 53 AT PAX CABIN (W1). SUMMARY OF NRC 00521: CORROSION LEVEL 2. FLOOR SUPPORTS (4EA) FROM STA Y=157 TO Y=200, LBL 7, RBL 7, RBL 44, & RBL 53 AT PAX CABIN WERE REPLACED PER B717-200
- [SDR DALA2023042103142](https://openairdocs.org/sdr/DALA2023042103142.md): Unknown · unknown · Apr 20, 2023 · N895AT · Boeing 717200 · Fuselage Main, Frame
  > DURING REMOVED FLOOR SUPPORT FROM STA Y=157 TO STA Y=200 & LBL 54 AT PAX CABIN (2EAS) CORROSION ON WEB WAS FOUND IN REFERENCE TO NRC 00526. SUMMARY OF NRC 00580: CORROSION LEVEL 2. WEB BTW STA 160 TO 200 AND X=54 TO X=60 WAS REPAIRED PER B717-200 SRM 51-70-10-
- [SDR DALA2023042103140](https://openairdocs.org/sdr/DALA2023042103140.md): Unknown · unknown · Apr 20, 2023 · N895AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON SPLICES 29L AND 29RH, INTERNAL STRUCTURE AFT FUSELAGE STA 1110 TO 1120 APROX. SUMMARY OF NRC 00327: CORROSION LEVEL 2. LONGERON SPLICES 29LH AND 29RH, INTERNAL STRUCTURE AFT FUSELAGE STA 1110 TO 1120 WERE REPLACED PER B717-200 SRM 51-41-0
- [SDR DALA2023042003111](https://openairdocs.org/sdr/DALA2023042003111.md): Unknown · unknown · Apr 20, 2023 · N895AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORTS AT STA Y=177 FROM RBL 10 TO RBL 43 AND STA Y=200 FROM RBL 10 TO RBL 43 IN REF NRC 0522. SUMMARY OF NRC 00595: CORROSION LEVEL 2. FLOOR SUPPORTS AT STA Y=177 FROM RBL 10 TO RBL 43 AND STA Y=200 FROM RBL 10 TO RBL 43 WERE REPLACED PER
- [SDR DALA2023041803051](https://openairdocs.org/sdr/DALA2023041803051.md): Unknown · unknown · Apr 18, 2023 · N895AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT STA Y=1026 AND Y=1056 LBL 46 AT PAX CABIN. SUMMARY OF NRC 00507: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=1026 AND Y=1056 LBL 46 WAS REPLACED PER B717-200 SRM 51-41- 01-0G. (LP #2724884)
- [SDR DALA2020062202492](https://openairdocs.org/sdr/DALA2020062202492.md): Power Supply · inoperative · Jun 20, 2020 · N895AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS AT WING EXIT DOORS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY IN REFERENCE TO B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7080575)
- [SDR DALA2019111866741](https://openairdocs.org/sdr/DALA2019111866741.md): Pressure Blkhd · damaged · Nov 15, 2019 · N895AT · Boeing 717200 · Fuselage Main, Bulkhead
  > HOLE IN PRESSURE DOME BELOW THE NOSE LANDING GEAR ACTUATOR. NRC 001-0270:5300-2001/001 00014: COMPLIED WITH ER/A 582891-14 REV O. (LP #1361132)
- [SDR DALA2023050903612](https://openairdocs.org/sdr/DALA2023050903612.md): Unknown · unknown · Nov 14, 2019 · N895AT · Boeing 717200 · Fuselage Main, Bulkhead
  > FUSELAGE BULKHEAD STA 110 LBL 14 WEB DAMAGE. REPAIR APPROVAL IS LIMITED TO THE NEXT C-CHECK (NOT TO EXCEED 24 MONTHS) SERVICE FROM DATE OF APPROVAL ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT.
- [SDR DALA2019111106536](https://openairdocs.org/sdr/DALA2019111106536.md): Threshold · corroded · Nov 8, 2019 · N895AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FOUND CORROSION IN C-2 THRESHOLD AREA. NRC 001-0262:5300-2016/001 00011: CORROSION LEVEL 1, MAINTENANCE REPLACED THE DOOR JAMB PAN REF B717 SRM 53-20-15-2R PROC 7. (LP #1351022)
- [SDR DALA2019092305440](https://openairdocs.org/sdr/DALA2019092305440.md): Battery Pack · discharged · Sep 22, 2019 · N895AT · Boeing 717200 · Emergency Lighting
  > THE OVERWING EMERGENCY ESCAPE LIGHTS WILL TURN ON WHEN THE SWITCH IS TURNED OFF. MAINTENANCE REPLACED THE OVERWING EMERGENCY ESCAPE LIGHTING BATTERY PACK IAW AMM 33-51. LIGHTS NOW OPERATE NORMALLY. (LP #6025180)

Next page: https://openairdocs.org/aircraft/N895AT/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 = 'N895AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N895AT/reports

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