# Service difficulty reports: N943AT

A list on [N943AT](https://openairdocs.org/aircraft/N943AT.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 5 · 213 reports

- [SDR DALA2026051703032](https://openairdocs.org/sdr/DALA2026051703032.md): Cover · broken · May 13, 2026 · N943AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY LIGHT COVER IN FRONT OF FIRST CLASS LAV HAS BROKEN OFF. INSTALLED NEW LIGHT COVER FWD EMG LIGHT PER AMM 33-51 (8903400) (AIRCRAFT GROUNDED)
- [SDR DALA2026041302319](https://openairdocs.org/sdr/DALA2026041302319.md): Acm · contaminated · Apr 8, 2026 · N943AT · Boeing 717200 · Cabin Cooling System
  > FUME/SMKE - ON TAXI IN WITH RT PACK ON, WET SOCK SMELL WITH VISIBLE FOG/SMOKE. CORRECTIVE ACTION: FOUND APU WITH NO OIL IN OIL TANK AND EXTENSIVE OIL CONTAMINATION IN BLEED DUCT. APU CHANGE COMPLETED AND BLEED DUCTS CLEANED. STILL HAVE ODOR AND HAZE ON APU BLE
- [SDR DALA2025121509137](https://openairdocs.org/sdr/DALA2025121509137.md): Windshield · arced · Dec 9, 2025 · N943AT · Boeing 717200 · Windshield/Door Rain/Ice Removal
  > WHEN TURNING ON THE WINDSHIELD ANTI ICE SWITCH SENSOR ON F/O'S FWD WINDOW STARTED ARCHING. REMOVED AND REPLACED CENTER WINDSHIELD REF B717 AMM 56-11. (7791708)
- [SDR DALA2025121009012](https://openairdocs.org/sdr/DALA2025121009012.md): Switch · faulted · Dec 8, 2025 · N943AT · Boeing 717200 · Central Warning
  > ATB, CREW REPORTED SMOKE IN THE COCKPIT WITH ASSOCIATED ELECTRICAL SMELL. FOUND ELECTRICAL ODOR TO BE EMITTING FROM THE FIRST OFFICERS MASTER CAUTION PUSH BUTTON SWITCH AND WARM TO TOUCH. REPLACED SWITCH.(7791702)
- [SDR DALA2025081806157](https://openairdocs.org/sdr/DALA2025081806157.md): Tire · failed · Aug 1, 2025 · N943AT · Boeing 717200 · Tire
  > TIRE- #1 MLG TIRE FAILURE AFTER LANDING WITH LEFT ANTISKID FAIL MESSAGE. REPLACED #1 ANTISKID TRANSDUCER, ANTISKID CONTROLLER AND #1-#2 MLG WHEEL ASSEMBLIES. OPS CHECKS GOOD.(7436618)
- [SDR DALA2025060704351](https://openairdocs.org/sdr/DALA2025060704351.md): Seat Track · corroded · Jun 2, 2025 · N943AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 9503, FWD GALLEY AREA CORROSION: RH O/B SEAT TRACK CORRODED AT FWD END. CORRECTIVE ACTION: REPAIRED SEAT TRACK PER B717 SRM 53-20-52-2R-5. (LP 1001907)
- [SDR DALA2025060604347](https://openairdocs.org/sdr/DALA2025060604347.md): Web · cracked · Jun 1, 2025 · N943AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9503 CUSP MEMBRANE DAMAGE (CRACKED) RIGHT SIDE STA STA 200. CORRECTIVE ACTION: REPAIRED PER B717-200SRM 53-00-55-2R PROCEDURE 4. (0999891)
- [SDR DALA2025020400815](https://openairdocs.org/sdr/DALA2025020400815.md): Battery Pack · inoperative · Feb 4, 2025 · N943AT · Boeing 717200 · Emergency Lighting
  > THE FWD EXIT SIGN IS NOT ILLUMINATING. MAINTENANCE REPLACED THE BATTERY PACK AT THE FWD OVERHEAD EQUIPMENT F5-259 COMPARTMENT PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6858025)
- [SDR DALA2025010300044](https://openairdocs.org/sdr/DALA2025010300044.md): Skin · damaged · Dec 31, 2024 · N943AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > SKIN AT FWD LOWER CORNER OF LAV WASTE DUMP CUT OUT PUSHED OUT APPROX.75" FWD LAV WASTE BOX. CREASE IN SKIN APPROX 4" LONG. MAX DEEP IN GAP BETWEEN SKIN AND WASTE BOX APPROX 1". PERFORMED EXTERNAL DOUBLER AND TRIPLER REPAIR IAW ER/A 622994-14 REV O. FOLLOW ON
- [SDR DALA2024121611739](https://openairdocs.org/sdr/DALA2024121611739.md): Wire · shorted · Dec 14, 2024 · N943AT · Boeing 717200 · Light System Wiring
  > THE FWD EXIT SIGN OVER FWD F/A SEAT IS INOPERATIVE. ALSO, 4 EXIT LIGHTS ON AFT CATWALK ARE INOPERATIVE. MAINTENANCE REPLACED THE FWD EMERGENCY EXIT SIGN (L2-790). ALL LIGHTS ASSOCIATED WITH BATTERY PACK B5-260 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY
- [SDR DALA2024091809133](https://openairdocs.org/sdr/DALA2024091809133.md): Angle · cracked · Sep 14, 2024 · N943AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > ANGLE BRACKET AT STATION 1178.255 ABOVE L-9L CRACKED. REPLACED ANGLE BRACKET AT STATION 1178.255 ABOVE L-9L IAW B717 SRM 51-40-02 AND B DRAWING 5420838. INSTALLED LT & RT LOUVER PANELS. COMPLIED WITH INSP PER B717 W/C 5312-01194-01.
- [SDR DALA2024042504694](https://openairdocs.org/sdr/DALA2024042504694.md): Power Supply · no test · Apr 25, 2024 · N943AT · Boeing 717200 · Emergency Lighting
  > DURING THE SERVICE CHECK, THE EMERGENCY LIGHTS AT THE CATWALK WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY B5-237 PER B717 AMM 33-51-03. (LP #5853294)
- [SDR DALA2023091508000](https://openairdocs.org/sdr/DALA2023091508000.md): Rudder · damaged · Aug 8, 2023 · N943AT · Boeing 717200 · Rudder Structure
  > RUDDER RH SKIN PANEL DAMAGED ON UPPER SIDE NEAR STA ZR165.3.
- [SDR DALA2023072505985](https://openairdocs.org/sdr/DALA2023072505985.md): Unknown · unknown · Jul 25, 2023 · N943AT · Boeing 717200 · Emergency Lighting
  > THE TAILCONE COMPARTMENT EMERGENCY LIGHTING IS INOPERATIVE. MAINTENANCE TROUBLE SHOT PER B717 FIM 33-50-00-810-801, WDM 33-51-13, AND 33-51-14. FOUND B5-116 BATTERY ASSEMBLY DISCONNECTED FROM CRADLE SOCKET. ALSO FOUND THE BATTERY BASE FOR B5-260 WAS BAD. THE B
- [SDR DALA2023071305675](https://openairdocs.org/sdr/DALA2023071305675.md): Unknown · unknown · Jul 10, 2023 · N943AT · Boeing 717200 · Aerodynamic Fairings
  > THE TAIL CONE RELEASE CAM IS CLOCKED INCORRECTLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE ADJUSTED THE RELEASE CAM REF AMDS WORKCARD 5352-2001. (LP #2859456)
- [SDR DALA2024022002330](https://openairdocs.org/sdr/DALA2024022002330.md): Panel · corroded · Jul 2, 2023 · N943AT · Boeing 717200 · Fuselage Main, Structure
  > AREA OF CORROSION NOTED DIRECTLY FWD OF LEFT SLANT PANEL (MARKED). COMPLIED WITH ERA 610004-14 REV ORIG. PRI 610004-14 REV 0 MATCHES ERA 610004-14 REV ORIG. ASSOCIATED ERA 14-610004 ADDED FOR AC 9503. (LP #2846122)
- [SDR DALA2023080406298](https://openairdocs.org/sdr/DALA2023080406298.md): Unknown · unknown · Jul 2, 2023 · N943AT · Boeing 717200 · Fuselage Main, Structure
  > AFT CARGO DOOR JAMB CORROSION ON SKIN TO LONGERON ADJACENT TO REAR CARGO DOOR FRAME AT STA 1000. REPAIRED PER ER/A 610079-14 REV. ORIGINAL. (LP #2846315)
- [SDR DALA2023070305303](https://openairdocs.org/sdr/DALA2023070305303.md): Unknown · unknown · Jul 1, 2023 · N943AT · Boeing 717200 · Fuselage Floor Panel
  > AFT CARGO DOOR LOWER PAN HAS CORROSION IN SEVERAL LOCATIONS. MARKED. SUMMARY SEE NRC 001-0270:5300-2016/003 00024: EDGED SEALED AFT CARGO DOOR LOWER PAN REF REPAIRED CARGO DOOR FRAME LOWER PAN REF B717-200 SRM 53-20-15-2R REPAIR 7 AFT CARGO LOWER JAMB PAN CORR
- [SDR DALA2023063005258](https://openairdocs.org/sdr/DALA2023063005258.md): Unknown · unknown · Jun 26, 2023 · N943AT · Boeing 717200 · Fuselage Main, Frame
  > FWD CARGO DOOR FRAME LOWER PAN HAS CORROSION IN AT LEAST 2 LOCATIONS NEAR STOP FITTINGS. MARKED. SUMMARY SEE NRC 001-0270:5300-2016/001 00018: REPAIRED CARGO DOOR FRAME LOWER PAN REF B717-200 SRM 53-20-15-2R REPAIR 6. FORWARD CARGO LOWER JAMB PAN CORROSION SPL
- [SDR DALA2023060604564](https://openairdocs.org/sdr/DALA2023060604564.md): Unknown · unknown · Jun 6, 2023 · N943AT · Boeing 717200 · Emergency Lighting
  > FOUND THAT THE EMERGENCY LIGHT IN ROW 20 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-230. OPERATIONAL CHECK WAS GOOD PER B717 AMM 33-51. (LP #9964533)
- [SDR DALA2023013100774](https://openairdocs.org/sdr/DALA2023013100774.md): Charger · inoperative · Jan 28, 2023 · N943AT · Boeing 717200 · Emergency Lighting
  > THE AFT WALKWAY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE AFT BATTERY CHARGER ASSEMBLY PER B717 AMM 33-51-01. (LP #4048883)
- [SDR DALA2023010300006](https://openairdocs.org/sdr/DALA2023010300006.md): Battery Pack · no test · Jan 3, 2023 · N943AT · Boeing 717200 · Emergency Lighting
  > DURING THE SERVICE CHECK, MAINTENANCE FOUND THE SIDE EXIT LIGHTS INOPERATIVE ON L1, R1 DOORS & FWD OVERWING L&R DOORS. THE EMERGENCY LIGHT BATTERY B5-118 WAS REPLACED IAW B717 AMM 33-51-03 000-082. OPERATIONAL CHECK WAS GOOD.
- [SDR DALA2022112107449](https://openairdocs.org/sdr/DALA2022112107449.md): Light · inoperative · Nov 18, 2022 · N943AT · Boeing 717200 · Emergency Lighting
  > THE OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE AT ROW 10. MAINTENANCE FOUND SPLICE FOR EMERGENCY LIGHT TO BE BROKEN. AFTER RESPLICE, THE LIGHT OPERATIONAL CHECK FAILED. RELAMPING BOTH EMERGENCY LIGHTS DID NOT CORRECT THE PROBLEM. THE EEP LIGHTS WERE DEFERRED PE
- [SDR DALA2022110807207](https://openairdocs.org/sdr/DALA2022110807207.md): None · none · Nov 5, 2022 · N943AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT LIGHT OVER THE AFT CABIN BULKHEAD DOOR AND THE TAIL COMPARTMENT EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY B5-116 PER B717 AMM 33-51. (LP #9639470)
- [SDR DALA2022071504932](https://openairdocs.org/sdr/DALA2022071504932.md): None · none · Jul 14, 2022 · N943AT · Boeing 717200 · Emergency Lighting
  > THE FLIGHT ATTENDANT REPORTS THAT THE EMERGENCY SEAT MOUNTED LIGHTING IS INOPERATIVE AT SEAT 20B. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT AT 20B PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #2320352)
- [SDR DALA2022071504931](https://openairdocs.org/sdr/DALA2022071504931.md): None · none · Jul 14, 2022 · N943AT · Boeing 717200 · Emergency Lighting
  > THE FLIGHT ATTENDANT REPORTS THAT THE EMERGENCY SEAT MOUNTED LIGHTING IS INOPERATIVE AT SEAT 20A. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT AT 20A PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #2320351)
- [SDR DALA2022031401649](https://openairdocs.org/sdr/DALA2022031401649.md): None · none · Mar 11, 2022 · N943AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT LOCATOR (SIGN) AT L2-791 BY SEAT ROW IA, ON THE CEILING IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN THE POWER SUPPLY B5-259. THE EMERGENCY EXIT LOCATOR L2-791 NOW CHECKS GOOD REF B717 AMM 33-51. (LP #8550478)
- [SDR DALA2022091406089](https://openairdocs.org/sdr/DALA2022091406089.md): None · none · Oct 2, 2021 · N943AT · Boeing 717200 · Rudder, Plate/Skin
  > REPEAT INSPECTION PER ER/A 594509-14 REQUIRED EVERY 3000FC AFTER REPAIR INSTALLATION. REPAIR IS APPLIED TO RUDDER SN 55010 INSTALLED. ASSOCIATED ER/A 00-594509 ADDED FOR AC 9503. REDEFERRED LOG TO QC, ESTABLISHED MONITOR INSP. ERA 594509-14 REV A IS NOW CURREN
- [SDR DALA2022091406088](https://openairdocs.org/sdr/DALA2022091406088.md): None · none · Oct 2, 2021 · N943AT · Boeing 717200 · Rudder, Plate/Skin
  > ESTABLISHING DTE RESTRICTION FOR ER/A 594509-14. REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE FROM THE APPROVAL DATE. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONT SERVICE BEYOND THIS LIMIT. REPAIR IS APPLIED TO RUDDER SN 55010 I
- [SDR DALA2021051002629](https://openairdocs.org/sdr/DALA2021051002629.md): Power Supply · inoperative · May 9, 2021 · N943AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN ABOVE THE AFT CABIN DOOR IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7569558)
- [SDR DALA2021040501963](https://openairdocs.org/sdr/DALA2021040501963.md): Battery Pack · inoperative · Apr 4, 2021 · N943AT · Boeing 717200 · Emergency Lighting
  > THE FLIGHT ATTENDANT NOTED THAT THE EMERGENCY EXIT SIGN LIGHTS AT THE GALLEY SERVICE DOOR AND CABIN ENTRANCE DOOR, THE LOWER EXIT SIGN LIGHTS AT RT & LT FWD OVER WING EXIT DOORS, AND THE TAIL COMPT ESCAPE PATH LIGHTING WERE ALL INOPERATIVE. MAINTENANCE REPLACE
- [SDR DALA2021011100137](https://openairdocs.org/sdr/DALA2021011100137.md): Battery Pack · inoperative · Jan 9, 2021 · N943AT · Boeing 717200 · Emergency Lighting
  > THE TAIL CONE SECTION EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE B5-260 AND B5 -116 BATTERY PACKS AND THE OPERATIONAL CHECKS WERE GOOD, PER B717 AMM 33-51.
- [SDR DALA2020091403054](https://openairdocs.org/sdr/DALA2020091403054.md): Drive Assy · damaged · Sep 13, 2020 · N943AT · Boeing 717200 · Leading Edge Slat Control System
  > THE CREW DIVERTED THE AIRCRAFT INTO IAH FOLLOWING A "SLAT DISAGREE" UPON SLAT EXTENSION. IAH HAS A LONGER RUNWAY THAN HOU. CORRECTIVE ACTION: MAINTENANCE FOUND THE NR 1 RIGHT HAND SLAT DRIVE MECHANISM DAMAGED. REPLACED THE RIGHT WING SLAT DRIVE AND ACTUATOR
- [SDR DALA2020090802971](https://openairdocs.org/sdr/DALA2020090802971.md): Lens · missing · Sep 6, 2020 · N943AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY LIGHT LENS AT 29L IS MISSING. MAINTENANCE REPLACED THE LENS IAW B717 AMM 33-51.
- [SDR DALA2020050502351](https://openairdocs.org/sdr/DALA2020050502351.md): Lanyard · out of position · May 3, 2020 · N943AT · Boeing 717200 · Escape Slide
  > THE R1 DOOR SLIDE LANYARD WAS FOUND TO BE INSTALLED IMPROPERLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REINSTALLED THE R1 DOOR SLIDE LANYARD CORRECTLY PER B717 AMM 25-61. (LP #65355
- [SDR DALA2019120307003](https://openairdocs.org/sdr/DALA2019120307003.md): Battery Pack · inoperative · Dec 3, 2019 · N943AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT LIGHTS ABOVE THE AFT DOOR AND IN THE AFT ACCESSORY COMPARTMENT ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK REF AMM 33-51. OPERATIONAL CHECK IS GOOD AND THE AIRCRAFT HAS RETURNED TO SERVICE.
- [SDR DALA2019070704061](https://openairdocs.org/sdr/DALA2019070704061.md): Access Panel · corroded · Jul 6, 2019 · N943AT · Boeing 717200 · Wing, Plate/Skin
  > OUT OF LIMITS - CORROSION IN ACCESS 520FT, 520GB, 520DT, 520CT, 520CB AND CENTER FUEL TANK UPPER ACCES PANNEL, SETTLEMENT AREA AND COUNTERSINK HOLES. AT FUEL TANK (AI). ALL PANELS WERE REPLACED. (LP1157907)
- [SDR DALA2019070704060](https://openairdocs.org/sdr/DALA2019070704060.md): Access Panel · corroded · Jul 6, 2019 · N943AT · Boeing 717200 · Wing, Plate/Skin
  > OUT OF LIMITS- CORROSION IN ACCESS 620 CB, 620AT AND 620 DT SETTLEMENT AREA AND COUNTERSINK HOLES. AT FUEL TANK (AD). ACCES PANEL 620CB WAS REPLACED AND PART NUMBER WAS VERIFIED PER IPC 57-23-01-01 (SHEET 6) (ITEM 465J) AND ACCES PANNEL 620AT AND 620DT WERE RE
- [SDR DALA2019070604055](https://openairdocs.org/sdr/DALA2019070604055.md): Hinge Bracket · corroded · Jul 6, 2019 · N943AT · Boeing 717200 · Elevator Structure
  > AWR, HIDDEN CORROSION (IN REF NRC S/N 00283): CORROSION WAS FOUND ON ELEVATOR HINGE BRACKET HOLES AT RT HORIZONTAL STABILIZER STA XHS=104, 158, 204 AND 2. CORROSION ON ELEVATOR HINGE BRACKET HOLES AT RT HORIZONTAL STABILIZER STA XHS=104, 158, 204 AND 225 (EHV)
- [SDR DALA2019070604054](https://openairdocs.org/sdr/DALA2019070604054.md): Longeron · corroded · Jul 5, 2019 · N943AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: SEVERAL CORROSION ON LONGERON L30 FROM STA 889 TO STA 1053 AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2 CORROSION ON LONGERON 30 BTW STA Y=894-1076 WAS REMOVED PER SRM 51-10-04-0G PAR 26 (UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR.5 FIG 3
- [SDR DALA2019070504040](https://openairdocs.org/sdr/DALA2019070504040.md): Fastener · damaged · Jul 4, 2019 · N943AT · Boeing 717200 · Aerodynamic Fairings
  > INITIAL INSPECTION: DAMAGED INTERNAL HARDWARE ON LEVER OF THE TAIL CONE JETTISON MECHANISM AT RT LOWER CORNER OF THE TAILCONE CUTOUT. NEW HARDWARE ON LEVER OF THE TAIL CONE JETTISON MECHANISM AT RT LOWER CORNER OF THE TAILCONE WERE INSTALLED PER AMM TAILCONE A
- [SDR DALA2019070504038](https://openairdocs.org/sdr/DALA2019070504038.md): Skin · dented · Jul 4, 2019 · N943AT · Boeing 717200 · Aileron Tabs
  > SEVERAL DENTS ( 7 EAS) ON RH WING AILERON CONTROL TAP UPPER SKIN BTW STATION XAC=3.5 TO XAC=48.2. RT AILERON CONTROL TAB UPPER SKIN DENT 7 WAS REPAIRED PER SRM 51-70-02-2R PROCEDURE 6 REPAIR 6. TAP TEST INSPECTION WAS PERFORMED AFTER REPAIR AND NO DISBONDS WE
- [SDR DALA2019070404035](https://openairdocs.org/sdr/DALA2019070404035.md): Handle · out of adjust · Jul 3, 2019 · N943AT · Boeing 717200 · Aerodynamic Fairings
  > AWR: DURING CHECK OF THE TAILCONE RELEASE SYSTEM, TAILCONE WAS NO RELEASED WITH "EMERGENCY OPERATING HANDLE" OF THE PASSENGER AFT ENTRANCE DOOR PER 5352-2001, STEP 2. NRC 00534 EMERGENCY OPERATING HANDLE OF THE PASSENGER AFT ENTRANCE DOOR WAS ADJUSTED AND TEST
- [SDR DALA2019070404033](https://openairdocs.org/sdr/DALA2019070404033.md): Skin · cracked · Jul 3, 2019 · N943AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > INITIAL INSPECTION: CRACKED FUSELAGE SKIN STA Y=97 ON NLG DOOR CUT OUT LT AFT HINGE DOOR. SUMMARY IN REF OF NRC 00039 AREA WAS REPAIRED PER SRM 53-10-01-2R-11, SRM 51-41-02-0G AND 51-41-05-0G. (LP1153816)
- [SDR DALA2019070404031](https://openairdocs.org/sdr/DALA2019070404031.md): Skin · corroded · Jul 3, 2019 · N943AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > INITIAL INSPECTION: CORROSION ON FUSELAGE SKIN BTW STA Y= 1022 - 1035 AND LONG 23L - 26L. CORROSION LEVEL 2 IN REF OF NRC 00063 AREA WAS REPAIRED PER ER/A 578990-14 REV ORIGINAL AND ETI-17-19-085 REV 3. TIME CONTROLLED ITEMS: ACCOMPLISH SECTION II: REPETITIVE
- [SDR DALA2019070203974](https://openairdocs.org/sdr/DALA2019070203974.md): Frame · corroded · Jul 1, 2019 · N943AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME OF STA 974 FROM L29R TO L28L AT AFT CARGO COMPARMENT (C2). NRC 00152: CORROSION LEVEL 2, CORROSION WAS REMOVED PER SRM 51-10-04-0G PAR 26. (LP #1150270)
- [SDR DALA2019070203973](https://openairdocs.org/sdr/DALA2019070203973.md): Frame · corroded · Jul 1, 2019 · N943AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME AFT AND FWD SURFACE AT STA 1022 BTW L28R TO L28L AT AFT CARGO COMPARMENT (C2). NRC 00156: CORROSION LEVEL 2, CORROSION ON FRAME AFT AND FWD SURFACE AT STA 1022 BTW L29R TO L29L WAS REMOVED PER SRM 51-10-04-0G PAR. 26. (LP #1150161)
- [SDR DALA2019070103956](https://openairdocs.org/sdr/DALA2019070103956.md): Intercostal · corroded · Jun 30, 2019 · N943AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AT LONG 30 STA=1022-1040 AT AFT CARGO COMPARMENT (REF NRC SN 146) (C2). NRC 00210: CORROSION LEVEL 2, INTERCOSTAL AT LONG 30 STA=1022-1040 WAS REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G. (LP #1149302)
- [SDR DALA2019070103955](https://openairdocs.org/sdr/DALA2019070103955.md): Frame · corroded · Jun 30, 2019 · N943AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON AFT AND FWD FRAME SURFACE AT STA 1037 AFT CARGO COMPARMENT (C2). NRC 160: CORROSION LEVEL 2, CORROSION ON AFT AND FWD FRAME SURFACE AT STA 1037 WAS REMOVED PER SRM 51-10-04-0G PAR 26. (LP #1149264)
- [SDR DALA2019070103954](https://openairdocs.org/sdr/DALA2019070103954.md): Hinge · corroded · Jun 30, 2019 · N943AT · Boeing 717200 · Fuselage, Door Hinge
  > CORROSION ON LT APU DOOR UPPER SECTION HINGE (FUS). NRC 0064: CORROSION LEVEL 2, CORROSION IN UPPER HINGE ON LT APU DOOR WAS REMOVED PER SRM 51-10-04-0G PAR. 26. HINGE ON LT APU DOOR WAS REPLACED PER AMM 52-45-01-400-801. (LP #1149074)

Next page: https://openairdocs.org/aircraft/N943AT/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 = 'N943AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N943AT/reports

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