N895AT

Service difficulty reports · 104

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 = 'N895AT' 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 DALA2026100205473Anti-Skid Sys · warning messageATO- 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).Oct 1, 2026 · N895AT · Boeing 717200 · Brake Anti-Skid SectionSDR DALA2025120508916Pitot Tube · faultedATB/DE- RETURNED ATL DUE TO RUDDER PITOT HEAT FAIL MESSAGE. REPLACED RUDDER LIMITER PITOT PROBE. MESSAGE CLEARED. OPS CHECK GOOD.(7974434)Dec 3, 2025 · N895AT · Boeing 717200 · Pitot/Static Anti-Ice SystemSDR DALA2025052203940Wire · brokenSHIP 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.May 16, 2025 · N895AT · Boeing 717200 · Equipment/Furnishings WiringSDR DALA2025042103071Skin · crackedDAMAGE 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 REQApr 16, 2025 · N895AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025040902759Skin · crackedCRACKS 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: REPEApr 8, 2025 · N895AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025050603513Pin · misinstalledINSPECTION 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 OApr 6, 2025 · N895AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2024112611228Slide · out of positionON 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 Nov 25, 2024 · N895AT · Boeing 717200 · Escape SlideSDR DALA2024092509408Battery Pack · inoperativeFOUND 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)Sep 24, 2024 · N895AT · Boeing 717200 · Emergency LightingSDR DALA2023122810696Unknown · unknownDURING 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 BYDec 26, 2023 · N895AT · Boeing 717200 · Escape SlideSDR DALA2023052304103Unknown · unknownCORROSION 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 IIMay 23, 2023 · N895AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023052504149Unknown · unknownBENT 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 TMay 22, 2023 · N895AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2023052304102Unknown · unknownBENT 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)May 20, 2023 · N895AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2023052204052Unknown · unknownSHEARED 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 May 20, 2023 · N895AT · Boeing 717200 · Elevator, Plate/SkinSDR DALA2023052004042Unknown · unknownCRACK 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)May 19, 2023 · N895AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2024112511161Skin · no discrepancyREPAIR 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.May 16, 2023 · N895AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2023051703947Unknown · unknownCRACK 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 MONTHMay 16, 2023 · N895AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023051603855Unknown · unknownWEAR 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)May 14, 2023 · N895AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023051203748Unknown · unknownDURING 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)May 11, 2023 · N895AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023051003664Unknown · unknownCORROSION 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)May 9, 2023 · N895AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023050803569Unknown · unknownWEAR 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 ANMay 7, 2023 · N895AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023050803567Unknown · unknownCORROSION 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)May 6, 2023 · N895AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023050803566Unknown · unknownCRACK 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)May 6, 2023 · N895AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023050803565Unknown · unknownCRACK 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)May 5, 2023 · N895AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023050803564Unknown · unknownCRACK 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)May 5, 2023 · N895AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023050803563Unknown · unknownCRACKED 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)May 5, 2023 · N895AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023050803562Unknown · unknownCRACK 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)May 4, 2023 · N895AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023050403460Unknown · unknownCORROSION 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 REPMay 4, 2023 · N895AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023050303432Unknown · unknownCORROSION 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 SMay 2, 2023 · N895AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023050303431Unknown · unknownCORROSION 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 STMay 2, 2023 · N895AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023050203396Unknown · unknownCORROSION 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 &May 2, 2023 · N895AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023050203392Unknown · unknownCRACK 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)Apr 29, 2023 · N895AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023042803323Unknown · unknownCORROSION 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)Apr 28, 2023 · N895AT · Boeing 717200 · Entrance StairsSDR DALA2023042803321Unknown · unknownCORROSION 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)Apr 27, 2023 · N895AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023042803320Unknown · unknownCORROSION 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)Apr 27, 2023 · N895AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2023042603249Unknown · unknownCORROSION 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)Apr 26, 2023 · N895AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023042603247Unknown · unknownCRACKED 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 #27Apr 25, 2023 · N895AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023042603246Unknown · unknownCRACKED 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 Apr 25, 2023 · N895AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023042703289Unknown · unknownCORROSION 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)Apr 24, 2023 · N895AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023042703288Unknown · unknownCORROSION 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)Apr 24, 2023 · N895AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023042503241Unknown · unknownCRACKED 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)Apr 24, 2023 · N895AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023042503239Unknown · unknownCORROSION 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 B717-200Apr 23, 2023 · N895AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023042103142Unknown · unknownDURING 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-Apr 20, 2023 · N895AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023042103140Unknown · unknownCORROSION 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 51-41-0Apr 20, 2023 · N895AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023042003111Unknown · unknownCORROSION 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 PERApr 20, 2023 · N895AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023041803051Unknown · unknownCORROSION 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)Apr 18, 2023 · N895AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2020062202492Power Supply · inoperativeTHE 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)Jun 20, 2020 · N895AT · Boeing 717200 · Emergency LightingSDR DALA2019111866741Pressure Blkhd · damagedHOLE 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)Nov 15, 2019 · N895AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2023050903612Unknown · unknownFUSELAGE 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. Nov 14, 2019 · N895AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2019111106536Threshold · corrodedFOUND 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)Nov 8, 2019 · N895AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019092305440Battery Pack · dischargedTHE 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)Sep 22, 2019 · N895AT · Boeing 717200 · Emergency Lighting
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