# Service difficulty reports: N926AT

A list on [N926AT](https://openairdocs.org/aircraft/N926AT.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 · 179 reports

- [SDR DALA2026100805562](https://openairdocs.org/sdr/DALA2026100805562.md): Light · missing · Oct 8, 2026 · N926AT · Boeing 717200 · Emergency Lighting
  > EXIT LIGHTING STRIP AND TRIM MISSING IN FRONT FWD SIDE, INSTALLED EMERGENCY LIGHTING STRIP IAW AMM 23-50. (8981540) (AIRCRAFT GROUNDED).
- [SDR DALA2026092105263](https://openairdocs.org/sdr/DALA2026092105263.md): Battery Pack · no test · Sep 19, 2026 · N926AT · Boeing 717200 · Emergency Lighting
  > ON SVC CHK FOUND EMER LIGHTS AT ROW 25 TO 28 OUT. R/R EMERGENCY LIGHT BATTERY PACK AT ROW 25 IAW B717 AMM 33-51 OPS CHK GOOD. (9115266) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026041402361](https://openairdocs.org/sdr/DALA2026041402361.md): Fuel Cap · leaking · Apr 10, 2026 · N926AT · Boeing 717200 · Fuel Storage
  > FUEL SMELL IN THE CABIN. FOUND ALL FUEL TANKS AT MAX CAP. AND FUEL LEAK FROM RT OVERWING AUX FUEL FILL PORT. SUSPECT SEAL BAD. R/R AUX FUEL FILL CAP SEAL REF. B717 AMM 28-21. (1536996) (AIRCRAFT GROUNDED)
- [SDR DALA2025091606814](https://openairdocs.org/sdr/DALA2025091606814.md): Door · out of alignment · Sep 14, 2025 · N926AT · Boeing 717200 · Landing Gear Doors
  > DIVERTED TO STL DUE TO INTERMITTENT AIRFRAME VIBRATION ABOVE 270KTS, SLOWED TO 250KTS AND VIBRATION STOPPED. FOUND RIGHT NOSE GEAR DOOR GAP MUCH LARGER THAN LEFT NOSE GEAR DOOR GAP, ADJUSTED GAP ON RIGHT DOOR AND PERFORMED PRELOAD CHECK AND FINAL ADJUSTMENT.
- [SDR DALA2025043003317](https://openairdocs.org/sdr/DALA2025043003317.md): Doubler · cracked · Apr 30, 2025 · N926AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DOUBLER CRACKED. AFT LOWER CORNER OF AFT CARGO DOOR. MARKED NRC 455. REMOVED EXISTING REPAIR & REPLACED DOUBLER REF B717 SRM 53-20-15-2R PROCEDURE 12 REPAIR 12. AFT CARGO DOOR JAMB EDGE SKIN REP- AIR. (LP #0940824)
- [SDR DALA2025042303170](https://openairdocs.org/sdr/DALA2025042303170.md): Wire · damaged · Apr 22, 2025 · N926AT · Boeing 717200 · Light System Wiring
  > SEAT EMERGENCY PATH LIGHTS ARE INOPERATIVE. SUMMARY SEE NRC 087-0001:3351-2001/001 00359: REPAIRED WIRE E9405-7-16N REF B717 SWPM 20-10-03. REPLACED POWER SUPPLY AND BATTERY PACK REF B717 AMM 33-51-03 AND CHECKED OPERATION. (LP #0927540)
- [SDR DALA2025032402192](https://openairdocs.org/sdr/DALA2025032402192.md): Pump · leaking · Mar 23, 2025 · N926AT · Boeing 717200 · Hydraulic Pump (Electric/Engine), Main
  > SHIP 9573 -ATB- ON ROTATION, THE CREW RECEIVED A "HYD R LO PRESS" MESSAGE AND THE INABILITY TO RETRACT THE GEAR. THEY MOVED THE GEAR SELECTION LEVER DOWN AND RECEIVED THREE GREEN "GEAR SAFE" INDICATIONS. AN EMERGENCY WAS DECLARED WITH ATC, THE FLIGHT RETURNED
- [SDR DALA2024122712036](https://openairdocs.org/sdr/DALA2024122712036.md): Reservoir · leaking · Dec 27, 2024 · N926AT · Boeing 717200 · Hydraulic Reservoir, Main
  > SHIP 9573 -MISC- THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO RIGHT HYDRAULIC SYSTEM PRESSURE LOSS AFTER GEAR EXTENSION. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE RIGHT HYDRAULIC RESERVOIR WAS LEAKING. THE RESERVOIR WAS REPLACED PER B717 AMM. OPERATION AND
- [SDR DALA2023112809769](https://openairdocs.org/sdr/DALA2023112809769.md): Unknown · unknown · Nov 28, 2023 · N926AT · Boeing 717200 · Passenger/Crew Doors
  > DOOR 1L WILL NOT OPEN FROM INSIDE OR OUTSIDE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SOMETHING IS CATCHING ON THE UPPER SKIN DOOR SEAL AREA. THE UPPER COSETIC PANEL WAS REMOVED TO INSPEC
- [SDR DALA2023112809767](https://openairdocs.org/sdr/DALA2023112809767.md): Unknown · unknown · Nov 27, 2023 · N926AT · Boeing 717200 · Passenger/Crew Doors
  > THE 1L DOOR WOULD NOT OPEN FROM THE OUTSIDE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE LUBRICATED AND ADJUSTED DOOR 1L IAW B717 FRM/FIM 52-10-00 810-801. OPERATIONAL CHECK WAS N
- [SDR DALA2023061304794](https://openairdocs.org/sdr/DALA2023061304794.md): Unknown · unknown · Jun 12, 2023 · N926AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL REPAIR DOUBLERS BTW STA 966/1000 AND BTW STR 28L/25L APROX AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00158: CORROSION LEVEL 2. REPAIR WAS PERFORMED PER PRI 525610-14 REV 2 AND ERA 525610-14 REV A. SECTION II PERMANENT REPAIR. ACCOMPLI
- [SDR DALA2023060604561](https://openairdocs.org/sdr/DALA2023060604561.md): Unknown · unknown · Jun 5, 2023 · N926AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AFTER P DOME STIFFENER REMOVAL, 4 HOLE LOCATIONS WERE NOTED TO BE MISSDRILED. IN REF TO NRC 00209. SUMMARY OF NRC 00566: HOLES (4 LOCATIONS) WERE REPAIRED PER PRI 608965-14 REV. 1 AND ER/A 608965-14AD REV. ORIGINAL, SECTION I: PERMANENT REPAIR. (LP #2802136)
- [SDR DALA2023060604555](https://openairdocs.org/sdr/DALA2023060604555.md): Unknown · unknown · Jun 2, 2023 · N926AT · Boeing 717200 · Nacelle/Pylon Structure
  > CORROSION ON CHORD ANGLE AT AFT PRESSURE BULKHEAD LOWER AREA (FWD FACE) STA Y=1053 BTW LONG 28LH-28RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00208: CORROSION LEVEL 2. ANGLE AT AFT PRESSURE BULKHEAD LOWER AREA (FWD FACE) STA Y=1053 BTW LONG 28LH-28RH WER
- [SDR DALA2023060104389](https://openairdocs.org/sdr/DALA2023060104389.md): Unknown · unknown · Jun 1, 2023 · N926AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB BTW STA=201 TO STA=220 RH SIDE AT CABIN PAX. SUMMARY OF NRC 00422: CORROSION LEVEL 2. CUSP WEB WAS REPLACED PER B717 SRM 53-10-51-0I FIG 1 SHEET 2 ITEM 32. (LP #2794167)
- [SDR DALA2023060104388](https://openairdocs.org/sdr/DALA2023060104388.md): Unknown · unknown · Jun 1, 2023 · N926AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SEVERE CORROSION ON GALLEY SERVICE DOOR CUSP ANGLE STA 168 TO 201 X=-44 TO X=-60. SUMMARY OF NRC 374: CORROSION LEVEL 2. CUSP ANGLE OF GALLEY SERVICE DOOR STA 168 TO 201 X=-44 TO X=-60 WAS REPAIRED PER PRI 608340-14 REV 1 AND ER/A 608340-14 REV ORIGINAL. (LP #
- [SDR DALA2023060104387](https://openairdocs.org/sdr/DALA2023060104387.md): Unknown · unknown · Jun 1, 2023 · N926AT · Boeing 717200 · Fuselage Structure (General)
  > CRACK ON FRAME CLIP OVER STA Y=1022 AND LONGERON 7LH AT CPAX (CPAX). SUMMARY OF NRC 00215: FRAME CLIP OVER STA Y=1022 AND LONGERON 7LH WAS REPAIRED PER PRI 608496-14 REV 0 AND ER/A 608496-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-608496 A
- [SDR DALA2023060104386](https://openairdocs.org/sdr/DALA2023060104386.md): Unknown · unknown · Jun 1, 2023 · N926AT · Boeing 717200 · Fuselage Structure (General)
  > CRACK ON FRAME CLIP OVER STA Y=1022 AND LONGERON 7 RH AT CPAX (CPAX). SUMMARY OF NRC 00210: FRAME CLIP OVER STA Y=1022 AND LONGERON 7 RH WAS REPAIRED PER PRI 608496-14 REV 0 AND ER/A 608496-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. (LP #2794144)
- [SDR DALA2023053104338](https://openairdocs.org/sdr/DALA2023053104338.md): Unknown · unknown · May 30, 2023 · N926AT · Boeing 717200 · Fuselage Main, Bulkhead
  > CORROSION ON AFT PRESSURE BULKHEAD LOWER AREA (FWD FACE) STA Y=1053 BTW LONG 28LH-28RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00207: CORROSION LEVEL 2. REPAIR ON AFT PRESSURE BULKHEAD LOWER AREA (FWD FACE) STA Y=1053 BTW LONG 28LH-28RH AT AFT CARGO COMP
- [SDR DALA2023053004252](https://openairdocs.org/sdr/DALA2023053004252.md): Skin · cracked · May 27, 2023 · N926AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK AT FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14 RH. (FUS). SUMMARY OF NRC 00300: FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14 RH WAS REPAIRED PER PRI 608247-14 REV 1 AND ER/A 608247-14 REV. ORIGINAL. ACCOMPLISH SECTION II: REPETITIVE INSPECTION WITHIN EVERY 24
- [SDR DALA2023052604191](https://openairdocs.org/sdr/DALA2023052604191.md): Unknown · unknown · May 25, 2023 · N926AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON MEMBRANE STA 148 TO 201, X=- 44 TO X=- 60. SUMMARY OF NRC 00454: CORROSION LEVEL 2. MEMBRANE STA 148 TO 201, X=- 44 TO X=- 60 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2, 51-41-02-0G, AND 51-41-08-0G. (LP #2783928)
- [SDR DALA2023052204053](https://openairdocs.org/sdr/DALA2023052204053.md): Unknown · unknown · May 20, 2023 · N926AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON CUSP WEB BTW STA=201 TO STA=220 RH SIDE AT CABIN PAX. SUMMARY OF NRC 00422: CORROSION LEVEL 2. CUSP WEB WAS REPLACED PER B717 SRM 53-10-51-0I FIG.1 SHEET 2 ITEM 32. (LP #2776332)
- [SDR DALA2023052004044](https://openairdocs.org/sdr/DALA2023052004044.md): Unknown · unknown · May 19, 2023 · N926AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS RH X=- 30 TO X=- 60 STA 148. SUMMARY OF NRC 00455: CORROSION LEVEL 2. FLOOR SUPPORTS RH X=- 30 TO X=- 60 STA 148 WERE REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2774007)
- [SDR DALA2023052004043](https://openairdocs.org/sdr/DALA2023052004043.md): Unknown · unknown · May 19, 2023 · N926AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > REMOVAL CABIN FLOOR SUPORT AT STA Y=148 BTW X=- 44 TO X=- 60, REVEALED CORROSION ON IT, IN REF TO NRC 00454. SUMMARY OF NRC 00565: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=148 BTW X=- 44 TO X=- 60 WAS REPLACED PER B717-200 SRM 53-10-51-01 PROC. 2. (LP #2773853)
- [SDR DALA2023052304104](https://openairdocs.org/sdr/DALA2023052304104.md): Unknown · unknown · May 18, 2023 · N926AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF SUPPORT, CORROSION WAS FOUND ON FLOOR SUPORT STA Y=160 BTW RBL 44 TO RBL 54 CABIN PAX (CPAX). SUMMARY OF NRC 00548: CORROSION LEVEL 2. FLOOR SUPPORTS LH STA 201 X=-8 TO X=8 WAS REPLACED PER B717-200 SRM 53-10-51-0I PROCEDURE 2. (LP #2773618)
- [SDR DALA2023052004041](https://openairdocs.org/sdr/DALA2023052004041.md): Unknown · unknown · May 17, 2023 · N926AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION WAS FOUND ON FLOOR SUPORT STA Y=180 BTW RBL 44 TO RBL 10 CABIN PAX (CPAX) AFTER REMOVAL OF SUPPORT. SUMMARY OF NRC 00547: CORROSION LEVEL 2. FLOOR SUPORT STA Y=180 BTW RBL 44 TO RBL 10 WAS REPLACED PER B717-200 SRM 53-10-51- 01 PROC 2 AND MUST BE INS
- [SDR DALA2023051803949](https://openairdocs.org/sdr/DALA2023051803949.md): Unknown · unknown · May 17, 2023 · N926AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SEVERE CORROSION ON MAIN ENTRANCE DOOR JAMB WEB STA 200. SUMMARY OF NRC 00372: CORROSION LEVEL 2. DOOR JAMB WEB WAS REPLACED PER B717-200 SRM 51-41-02-0G PAR 4. (LP #2771772)
- [SDR DALA2023051603856](https://openairdocs.org/sdr/DALA2023051603856.md): Unknown · unknown · May 15, 2023 · N926AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB STA=389 RH SIDE AT CABIN PAX. SUMMARY OF NRC 00424: CORROSION LEVEL 2. CUSP WEB STA=389 RH WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1. (LP #2768693)
- [SDR DALA2023051203747](https://openairdocs.org/sdr/DALA2023051203747.md): Unknown · unknown · May 12, 2023 · N926AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON CUSP WEB STA=370 RH SIDE AT CABIN PAX. SUMMARY OF NRC 00423: CUSP WEB STA=370 RH SIDE AT CABIN PAX WAS REPAIRED PER B717-200 SRM 51-41-02-0G PAR 4 AND SRM 53-00-55-2R PAR 5 B (23) FIG 225 REPAIR 4. (LP #2762882)
- [SDR DALA2023051203746](https://openairdocs.org/sdr/DALA2023051203746.md): Unknown · unknown · May 11, 2023 · N926AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON CUSP WEB RH STA=650 TO STA=660 PROX. SUMMARY OF NRC 00439: CUSP WEB RH STA=650 TO STA=660 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2762620)
- [SDR DALA2023051003668](https://openairdocs.org/sdr/DALA2023051003668.md): Unknown · unknown · May 10, 2023 · N926AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON BEAM #1, STA Y=195 FWD PASSENGER DOOR (L1). SUMMARY OF NRC-00101: CRACK WAS FOUND PREVIOUSLY REPAIRED PER B717-200 SRM 52-10-02-2R, REPAIR 7, PAR. 6, FIG. 201. AND MEETS REPAIR REQUIREMENTS. MAINTENANCE REQUIREMENTS: PERFORM VISUAL INSPECTION EVERY "C
- [SDR DALA2023051003667](https://openairdocs.org/sdr/DALA2023051003667.md): Unknown · unknown · May 10, 2023 · N926AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON BEAM #1, STA Y=160 FWD PASSENGER DOOR (L1). SUMMARY OF NRC 00100: CRACK WAS FOUND PREVIOUSLY REPAIRED PER B717-200 SRM 52-10-02-2R, REPAIR 7, PAR. 6, FIG. 202. AND MEETS REPAIR REQUIREMENTS. MAINTENANCE REQUIREMENTS: PERFORM VISUAL INSPECTION EVERY "C
- [SDR DALA2023050803572](https://openairdocs.org/sdr/DALA2023050803572.md): Unknown · unknown · May 8, 2023 · N926AT · Boeing 717200 · Wing, Plate/Skin
  > WEAR AND ELONGATED FASTENER HOLE AT FUEL ACCESS PLATE 520MB LH WING. SUMMARY OF NRC 459: FUEL ACCESS PLATE 520MB WAS NOT POSSIBLE REPAIR AS PER B717-200 SRM-57-10-01-2R-2 PROCEDURE 2 REPAIR 2 PAR 5 B. CONDITION II, AND WAS REPLACED PER B717 AIPC 57-23-01- 01-1
- [SDR DALA2023050803571](https://openairdocs.org/sdr/DALA2023050803571.md): Unknown · unknown · May 8, 2023 · N926AT · Boeing 717200 · Wing, Plate/Skin
  > WEAR AND ELONGATED FASTENER HOLE AT FUEL ACCESS PLATE 620PB RH WING. SUMMARY OF NRC 470: FUEL ACCESS PLATE 620PB DUE TO REPAIR OF WAS NOT POSSIBLE AS PER B717-200 SRM-57-10-01-2R-2 PROCEDURE 2 REPAIR 2 PAR. 5 B. CONDITION II AND WAS REPLACED PER B717 AIPC 57-2
- [SDR DALA2023050803570](https://openairdocs.org/sdr/DALA2023050803570.md): Unknown · unknown · May 7, 2023 · N926AT · Boeing 717200 · Fuselage Floor Panel
  > WEAR ON AFT INNER EDGE NEAR OF DOOR LATCH AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00059: INNER PAN AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 8. (LP #2756404)
- [SDR DALA2023050403458](https://openairdocs.org/sdr/DALA2023050403458.md): Unknown · unknown · May 3, 2023 · N926AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK EVIDENCE ON FWD LWR CORNER OF LH WINDOW BELT STA S 851 AND 908 AT PAX CAB. SUMMARY OF NRC 00408: REPAIR WAS PERFORMED PER B717-200 SRM 56-20-02-2R PROCEDURE 1. (LP #2750268)
- [SDR DALA2023050303433](https://openairdocs.org/sdr/DALA2023050303433.md): Unknown · unknown · May 2, 2023 · N926AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORTS X=-8 TO X=8 STA 201. SUMMARY OF NRC 00451: CORROSION LEVEL 2. FLOOR SUPPORT LH STA 201 X=-8 TO X=8 WAS REPLACED PER B717-200 SRM 53-10-51-0I PROCEDURE 2. (LP #2748476)
- [SDR DALA2023031401857](https://openairdocs.org/sdr/DALA2023031401857.md): Unknown · unknown · Mar 11, 2023 · N926AT · Boeing 717200 · Emergency Lighting
  > THE R1 EXIT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE.MAINTENACE REPLACED THE BATTERY B5-259 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4072112)
- [SDR DALA2022100406442](https://openairdocs.org/sdr/DALA2022100406442.md): None · none · Oct 3, 2022 · N926AT · Boeing 717200 · Emergency Lighting
  > THE AFT OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK PER B717 AMM 33-55. (LP #7679774)
- [SDR DALA2022091906176](https://openairdocs.org/sdr/DALA2022091906176.md): None · none · Sep 17, 2022 · N926AT · Boeing 717200 · Emergency Lighting
  > UPON SERVICE CHECK, THE FIRST CLASS EMERENGCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE EMERENGCY LIGHTS BATTERY AT B5-259 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OKAY FOR SERVICE. (LP #7679730)
- [SDR DALA2022081605531](https://openairdocs.org/sdr/DALA2022081605531.md): None · none · Aug 14, 2022 · N926AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT COVER DIFFUSER LENS FELL OFF AT SEAT ROW 20. MAINTENANCE SECURED EXIT ROW SIGN COVER. (LP #2365299)
- [SDR DALA2021050602570](https://openairdocs.org/sdr/DALA2021050602570.md): Battery Pack · inoperative · May 5, 2021 · N926AT · Boeing 717200 · Emergency Lighting
  > THE CEILING EMERGENCY LIGHTS IS OUT AT 16,17,18. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK AT 17CDE, O/H BIN, PER B717 AMM 33-51. THE EMERGENCY LIGHTS NOW OPERATE NORMALLY. CHECK WAS GOOD. (LP #7584468)
- [SDR DALA2021032301674](https://openairdocs.org/sdr/DALA2021032301674.md): Sign · dislodged · Mar 21, 2021 · N926AT · Boeing 717200 · Emergency Lighting
  > THE EXIT SIGN AT RO 19 IS DISLODGED. MAINTENANCE SECURED THE EXIT SIGN. (LP #7446516)
- [SDR DALA2020120703985](https://openairdocs.org/sdr/DALA2020120703985.md): Battery Pack · inoperative · Dec 7, 2020 · N926AT · Boeing 717200 · Emergency Lighting
  > THE LEFT AND RIGHT FORWARD OVER WING EXIT IDENTIFIER LIGHTS WERE NOTED TO BE INOPERATIVE. MAINTENANCE FOUND THE BATTERY FOR POWER SUPPLY B5-118 BAD AND REPLACED IT, IN REF TO B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD.
- [SDR DALA2020102003405](https://openairdocs.org/sdr/DALA2020102003405.md): Charger · inoperative · Oct 20, 2020 · N926AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN AT ROW 1 IS INOPERATIVE. MAINTENANCE REPLACED THE CHARGER AND BATTERY AT B5-259. OPERATIONAL CHECK IS NORMAL, PER B717 AMM 33-54.
- [SDR DALA2020091703103](https://openairdocs.org/sdr/DALA2020091703103.md): Battery Pack · inoperative · Sep 17, 2020 · N926AT · Boeing 717200 · Emergency Lighting
  > DURING SERVICE CHECK, FOUND 5 EACH EMERGENCY CEILING LIGHTS IN THE AFT SECTION INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-231, PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE.
- [SDR DALA2020082402837](https://openairdocs.org/sdr/DALA2020082402837.md): Battery Pack · inoperative · Aug 24, 2020 · N926AT · Boeing 717200 · Emergency Lighting
  > BOTH FORWARD OVERWING EXIT SIGN LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK IS GOOD REF B717 AMM 33-55
- [SDR DALA2020032602045](https://openairdocs.org/sdr/DALA2020032602045.md): Threshold · corroded · Mar 25, 2020 · N926AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT AFT CARGO DOOR THRESHOLD - MARKED. RCN 067-0008:5331-2001/009 00165: REPAIRED REF B717 SRM 53-20-15-2R PROCED 7. CLOSING REQUIREMENTS RII: INSPECTOR 00664880. (LP #1539185)
- [SDR DALA2020032602043](https://openairdocs.org/sdr/DALA2020032602043.md): Floor Support · corroded · Mar 24, 2020 · N926AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT IS CORRODED AT STA 196 LBL 52. NRC 068-0011:2531-4006/001 00280: REPLACED SUPPORT REF BOEING DWG #9936534. (LP #1538491)
- [SDR DALA2017121108490](https://openairdocs.org/sdr/DALA2017121108490.md): Engine · surges · Dec 9, 2017 · N926AT · Boeing 717200 · Engine (Turbine/Turboprop)
  > SHIP 9573 - THE CREW EXPERIENCED AN ENGINE SURGE AND HIGH EXHAUST TEMPERATURES WITH THE #2 ENGINE SO THE FLIGHT DIVERTED TO CAE. THE PILOT DID REDUCE POWER ON THE PROBLEM ENGINE SINCE THAT ENGINE DID NOT RECOVER FROM THE SURGE. THE QRH DIRECTED TO SHUTDOWN THE
- [SDR DALA2017081606258](https://openairdocs.org/sdr/DALA2017081606258.md): Cover · loose · Aug 15, 2017 · N926AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT SIGN COVER LOOSE. SECURED THE SIGN, CHECKED OK.

Next page: https://openairdocs.org/aircraft/N926AT/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 = 'N926AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N926AT/reports

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