# Service difficulty reports: N945AT

A list on [N945AT](https://openairdocs.org/aircraft/N945AT.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 · 228 reports

- [SDR DALA2026071704217](https://openairdocs.org/sdr/DALA2026071704217.md): Coalescer Bag · odor · Jul 16, 2026 · N945AT · Boeing 717200 · Humidity Control System
  > PUNGENT ODOR THROUGHOUT THE ENTIRE AIRPLANE, R & R COALESCER BAGS IAW AMM 21-54. (1703467) (AIRCRAFT GROUNDED).
- [SDR DALA2026061603616](https://openairdocs.org/sdr/DALA2026061603616.md): Idg · malfunctioned · Jun 15, 2026 · N945AT · Boeing 717200 · AC Generator-Alternator
  > SHIP 9505-ATO- RIGHT GENERATOR OFF MESSAGE AT THROTTLE UP. REPLACED THE RIGHT IDG. ALL RTS NORMAL. (LP 8906976 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026042102514](https://openairdocs.org/sdr/DALA2026042102514.md): Girt Bar · unsecure · Apr 15, 2026 · N945AT · Boeing 717200 · Emergency Equipment
  > R1 DOOR GIRT BAR CONNECTOR IS DETACHED FROM SLIDE. RESECURED RELEASE LATCH FOR SLIDE AMM 25-61 (8554330) (AIRCRAFT GROUNDED).
- [SDR DALA2026040102118](https://openairdocs.org/sdr/DALA2026040102118.md): Tire · failed · Mar 24, 2026 · N945AT · Boeing 717200 · Tire
  > RETURNED TO ATL DUE TO NR 1 MLG TIRE FAILURE, RT SYS HYDRAULIC LOSS AND SUBSEQUENT LT ENGINE DAMAGE ON TAKEOFF. REPLACED #1 ENGINE AND REPAIRED DAMAGE.(8616524)
- [SDR DALA2026032401969](https://openairdocs.org/sdr/DALA2026032401969.md): Tire · failed · Mar 18, 2026 · N945AT · Boeing 717200 · Tire
  > ATB/TIRE- RETURNED TO ATL DUE TO #1 MLG TIRE FAILURE, RT SYS HYDRAULIC LOSS AND SUBSEQUENT LT ENGINE DAMAGE ON TAKEOFF. CORRECTIVE ACTION: REPLACED #1 ENGINE.
- [SDR DALA2026012200498](https://openairdocs.org/sdr/DALA2026012200498.md): Tee Fitting · detached · Jan 20, 2026 · N945AT · Boeing 717200 · Passenger/Crew Doors
  > DOOR ARMING MECHANISIM ON FOWARD SERVICE DOOR INOP. FOUND TEE CLIP ON THE SLIDE LANYARD OFF. REATTACHED SAME PER B717 AMM 25-61. A/C OK FOR SVC. (7904618)
- [SDR DALA2026010500067](https://openairdocs.org/sdr/DALA2026010500067.md): Cable · misinstalled · Dec 31, 2025 · N945AT · Boeing 717200 · Emergency Equipment
  > GALLEY SERVICE DOOR R1 DOOR GIRT BAR CABLE MAY BE IMPROPERLY INSTALLED. REPOSITIONED CABLE REF AMM 25-61, OK TO CONTINUE (8385642)
- [SDR DALA2025111108260](https://openairdocs.org/sdr/DALA2025111108260.md): Skin · punctured · Nov 8, 2025 · N945AT · Boeing 717200 · Elevator, Plate/Skin
  > PUNCTURE ON LT ELEVATOR LOWER SURFACE BTW STA XHS 108 TO XHS 136. LT ELEVATOR LOWER SURFACE BTW STA XHS 108 TO XHS 136 WAS REPAIRED PER SRM 51-70-13 (1293791)
- [SDR DALA2025103107964](https://openairdocs.org/sdr/DALA2025103107964.md): Longeron · cracked · Oct 29, 2025 · N945AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED LONGERON 2R AT BS 1133. LONGERON 2R REPAIRED IAW SRM 53-00-05. (1277454)
- [SDR DALA2025081105985](https://openairdocs.org/sdr/DALA2025081105985.md): Compressor · stalled · Aug 8, 2025 · N945AT · Boeing 717200 · Turbine Engine Compressor Section
  > SHIP 9505 GOING THRU 10,000 ON CLIMBOUT WE GOT COMPRESSOR STALL TGT HAD AN X OFF AND ON. CORECTIVE ACTION: EPLACED HARNESS PER B717 AMM 77-21. REPLACED ALL 6 TGT PROBES PER B717 AMM 77-21. (7417510)
- [SDR DALA2025070104877](https://openairdocs.org/sdr/DALA2025070104877.md): Bulkhead · no discrepancy · Jun 29, 2025 · N945AT · Boeing 717200 · Standard Practices/Structures
  > SHIP 9505 DUE TO HARD LANDING ON FL1405, PERFORM DETAILED INSP IAW ER/A 565522-14AD. CORRECTIVE ACTION: INSPECTED A/C 9505 CANTED BULKHEAD IAW ER/A 565522-14AD. (1053477)
- [SDR DALA2025040802696](https://openairdocs.org/sdr/DALA2025040802696.md): Lanyard · severed · Mar 27, 2025 · N945AT · Boeing 717200 · Emergency Equipment
  > FOUND R1 DOOR SLIDE RELEASE LANYARD CABLE SEVERED. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE R1 DOOR SLIDE RELEASE LANYARD ASSEMBLY REF B717 AMM 25-61-03. (LP #6874
- [SDR DALA2024111410954](https://openairdocs.org/sdr/DALA2024111410954.md): Doubler · cracked · Nov 5, 2024 · N945AT · Boeing 717200 · Fuselage Main, Bulkhead
  > -AD- STA 1178.225 LONGERON 3L BULKHEAD DOUBLER CRACKED. ACCOMPLISH ER/A 565522-14AD REV A SECTION IV FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-565522 ADDED FOR AC 95
- [SDR DALA2024042404675](https://openairdocs.org/sdr/DALA2024042404675.md): Power Supply · inoperative · Apr 24, 2024 · N945AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN ON ROW 19CDE IS INOPERATIVE. MAINTENANCE THE FOUND POWER SUPPLY INOPERATIVE. THE POWER SUPPLY (B5-121) WAS REPLACED PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #4343895)
- [SDR DALA2023101408451](https://openairdocs.org/sdr/DALA2023101408451.md): Unknown · unknown · Oct 13, 2023 · N945AT · Boeing 717200 · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS ARE INOPERATIVE IN THE TAIL COMPARTMENT CEILING. MAINTENANCE REPLACED THE BATTERY AND THE PSU AT THE RIGHT AFT LAVATORY CEILING. TAIL COMPARTMENT EMERGENCY LIGHTS CHECKED GOOD PER B717 AMM 33-51-10. (LP #4295229)
- [SDR DALA2023092908007](https://openairdocs.org/sdr/DALA2023092908007.md): Unknown · unknown · Sep 28, 2023 · N945AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY CEILING LIGHTS ROW 24-27 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTER PACK AT SEAT 25 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4480888)
- [SDR DALA2023090507189](https://openairdocs.org/sdr/DALA2023090507189.md): Unknown · unknown · Sep 2, 2023 · N945AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK INDICATION AT LEFT OVERWING FRAME STA 696 WHILE PERFORMING AMDS 5310-01436-01B STEP 10. COMPLIED WITH AMDS CARD 5310-01436-03A FOR L/H OVER-WING FRAME REPLACEMENT STA 696. SEE NRC 162. (LP #2949537)
- [SDR DALA2023090507181](https://openairdocs.org/sdr/DALA2023090507181.md): Unknown · unknown · Aug 31, 2023 · N945AT · Boeing 717200 · Escape Slide
  > L1 DOOR SLIDE FOUND LACED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. REPLACED SLIDE PER B 717 AMM 25-61-01. (LP #2946641)
- [SDR DALA2024022102372](https://openairdocs.org/sdr/DALA2024022102372.md): Floor Support · corroded · Aug 20, 2023 · N945AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED JUST I/B OF R-1 DOOR UNDER FLOOR PANEL 221EF- MARKED. SUMMARY SEE NRC 087-0025:5310-2005/009 00399: REPLACED FLOOR SUPPORT REF BOEING DWG 9936534. (LP #2927991)
- [SDR DALA2023070405375](https://openairdocs.org/sdr/DALA2023070405375.md): Unknown · unknown · Jul 3, 2023 · N945AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT LIGHT LENS COVER AT ROW 19 NEEDS TO BE REATTACHED. MAINTENANCE ATTACHED THE EMERGENCY LIGHT LENS COVER AT ROW 19CDE. THE AIRCRAFT IS OK FOR SERVICE. (LP #4642349)
- [SDR DALA2023062705160](https://openairdocs.org/sdr/DALA2023062705160.md): Unknown · unknown · Jun 26, 2023 · N945AT · Boeing 717200 · Hydraulic System, Main
  > SHIP 9505 -HYD/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC DUE TO THE RIGHT HYDRAULIC QUANTITY READING LOW. THE CREW WAS ABLE TO PRESSURIZE THE R HYD SYSTEM BETWEEN 5,000-10,000 PSI PER THE QRH. DURING THIS TIME WHEN THE R HYD LIGHT WENT OUT AND PRESS W
- [SDR DALA2022081005448](https://openairdocs.org/sdr/DALA2022081005448.md): Skin · damaged · Aug 10, 2022 · N945AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > B717-200-FUSELAGE SKIN DAMAGE BETWEEN STA 994 1002 AND STR 24R 26R. NRC 002-0001:0514-2001/001 00001: REPAIRED PER ER/A 601169-14 REV. ORIGINAL (PRI 601169-14 REV. 1-7 MATCH ER/A 601169-14 REV. O.) (LP #2358789)
- [SDR DALA2022081005447](https://openairdocs.org/sdr/DALA2022081005447.md): Frame · damaged · Aug 10, 2022 · N945AT · Boeing 717200 · Fuselage Main, Frame
  > FRAME AT STA 994 SHOWS EVIDENCE OF DAMAGE CAUSED BY BELT LOADER IMPACT. NRC 002-0001:0514-2001/013 00013: REPAIRED FRAME PER B717 SRM 51-70-11-2R-1. (LP #2358780)
- [SDR DALA2022081005446](https://openairdocs.org/sdr/DALA2022081005446.md): Threshold · damaged · Aug 10, 2022 · N945AT · Boeing 717200 · Fuselage Main, Frame
  > THE AFT CARGO DOOR JAMB WEB JUST AFT OF STA 994 WAS DAMAGED FROM BELT LOADER IMPACT. NRC 002-0001:0514-2001/006 00006: REPAIRED WEB PER ERA 601169-14 REV ORIG. (LP #2358778)
- [SDR DALA2022081005445](https://openairdocs.org/sdr/DALA2022081005445.md): Skin · damaged · Aug 7, 2022 · N945AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > COMPLY WITH PRI/ERA 601064-14 REPAIR OF FUSELAGE SKIN DAMAGE AFT OF AFT CARGO DOOR. COMPLIED WITH STEPS 1,2,3, AND 4 OF PRI 601064-14 REV ORIGINAL PRI REV 0. PERFORMED RII INSPECTION OF PRI 601064-14 REV O. ERA REV ORIG STEPS 1,2,3, & 4. NO ADDITIONAL DAMAGE N
- [SDR DALA2022041902666](https://openairdocs.org/sdr/DALA2022041902666.md): None · none · Apr 15, 2022 · N945AT · Boeing 717200 · Fuselage Main, Bulkhead
  > A CRACKED AFT BULKHEAD IN THE NOSE LANDING GEAR WHEEL WELL STA 110 WAS FOUND (IN REF NRC 00167). SUMMARY OF NRC 00169: BULKHEAD WAS REPAIRED PER ERA 598690-14 REV. ORIGINAL SECTION I: TEMPORARY REPAIR. ACCOMPLISH THE SECTION II: REPETITIVE INSPECTIONS EVERY 24
- [SDR DALA2022040802421](https://openairdocs.org/sdr/DALA2022040802421.md): Door Frame · corroded · Apr 7, 2022 · N945AT · Boeing 717200 · Cargo/Baggage Doors
  > CORROSION ON AFT DOOR JAMB OF AFT CARGO DOOR (SM). SUMMARY OF NRC 00007: CORROSION LEVEL 2, PREVIOUS REPAIR AT DOOR JAM OF AFT CARGO WAS REPLACED PER B717 SRM 53-20-15-2R REPAIR 7. PERFORM A DECAL CONDITION INSPECTION EVER C-CHECK PER TOPP 30-10-70 PAGE 14 PAR
- [SDR DALA2022030301343](https://openairdocs.org/sdr/DALA2022030301343.md): None · none · Jan 17, 2022 · N945AT · Boeing 717200 · Aerodynamic Fairings
  > THE FUSELAGE INTERCOSTAL WAS FOUND CRACKED AT BEND STA 1212 STA 1225, WHICH AFFECTED THE TAILCONE DEPLOYMENT CABLE ATTACH POINT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. A TEMPORARY REPAIR WAS
- [SDR DALA2020110403576](https://openairdocs.org/sdr/DALA2020110403576.md): Cam · misinstalled · Oct 29, 2020 · N945AT · Boeing 717200 · Aerodynamic Fairings
  > THE TAIL CONE RELEASE CAM MECHANISM IS NOT INSTALLED CORRECTLY. THE ROLLERS DO NOT ENGAGE CAM WHEN TURNED. MAINTENANCE ADJUSTED THE TAILCONE RELEASE MECHANISM CAM, PER B717 AMM 53-52-03 820-801. OK FOR SERVICE.
- [SDR DALA2019082654961](https://openairdocs.org/sdr/DALA2019082654961.md): Cable · misrouted · Aug 23, 2019 · N945AT · Boeing 717200 · Aerodynamic Fairings
  > TAIL CONE LOCK IS CABLE ROUTED INCORRECTLY TO THE EXTERIOR RELEASE HANDLE. MAINTENANCE REROUTED THE LOCKING CABLE CORRECTLY TO EXTERIOR HANDLE ASSEMBLY IAW B717 AMM 53-52-01 830-802. RII COMPLETED BY QC2045. (LP #1236960)
- [SDR DALA2019081504764](https://openairdocs.org/sdr/DALA2019081504764.md): Doubler · corroded · Aug 14, 2019 · N945AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL PRODUCTION DOUBLER BTW STA 1022 AND LONG 29RH AT AFT CARGO COMPARTMENT. THE DOUBLER WAS REPAIRED PER ER/A 580391-14 REV ORIG AND ETI -17-19-122 REV 2.
- [SDR DALA2019081504763](https://openairdocs.org/sdr/DALA2019081504763.md): Tray · corroded · Aug 14, 2019 · N945AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SPOTS OF CORROSION ON WASTE SRVC TRAY PANEL. CORROSION WAS REMOVED PER B717-200 SRM 51-10-04-0G AND REMAINING THICKNESS IS 0.030"; OUT OF LIMITS IAW SRM 53- 00-00-1A ALLOWABLE DAMAGE PAR. 4 FIG-.103. WASTE SRVC TRAY PANEL WAS REPLACED IAW DWG 5965767-7, SR
- [SDR DALA2019081404755](https://openairdocs.org/sdr/DALA2019081404755.md): Sliding Window · cracked · Aug 13, 2019 · N945AT · Boeing 717200 · Flight Compartment Windows
  > CRACK ON UPPER AFT CORNER SLIDING WINDOW LEFT SIDE (CPIL). NRC 00575: CRACK ON UPPER AFT CORNER SLIDING WINDOW LEFT SIDE WAS REPAIRED PER B717-200 SRM 56-10-02-2R-1.
- [SDR DALA2019081434753](https://openairdocs.org/sdr/DALA2019081434753.md): Frame Angle · cracked · Aug 12, 2019 · N945AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED FRAME CLIP ON STA 1152 AND X=9 CROWN AREA, AFT ACCESORY COMPARTMENT (CAT). NRC 00422: AREA WAS REPAIRED PER ER/A 580410-14 REV ORIG AND ETI-17-19-141 REV 1. ASSOCIATED ER/A 14-580410 ADDED FOR AC 9505. (LP #1219535)
- [SDR DALA2019081204733](https://openairdocs.org/sdr/DALA2019081204733.md): Frame · corroded · Aug 11, 2019 · N945AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME ON BS 890, STRINGER 25L IS OUT OF LIMITS AT AFT CARGO COMPARTMENT, MINIMUM REMAINING THICKNNES IS 0.032" AND OUT OF LIMITS IAW SRM 53-00-00-1A, ALLOWABLE DAMAGE 1, PAR 4, FIG 103. DUE TO FRAME OUT LIMITS, THE FRAME WAS REPAIRED IAW SRM 53
- [SDR DALA2019081204732](https://openairdocs.org/sdr/DALA2019081204732.md): Door · damaged · Aug 10, 2019 · N945AT · Boeing 717200 · Emergency Exits
  > ELONGATED SCREW HOLES ON LH FWD OVERWING EMERGENCY EXIT DOOR FROM PASSENGER INNER SKIN AND PAN AT LH FWD OVERWING EMERGENCY EXIT DOOR REPAIRED IAW ETI-17-19-134 REV 2, AND ER/A 580350-14, REV ORIGINAL, SECTION I, PERMANENT REPAIR.
- [SDR DALA2019081204730](https://openairdocs.org/sdr/DALA2019081204730.md): Skin · delaminated · Aug 10, 2019 · N945AT · Boeing 717200 · Trailing Edge Flaps
  > DELAMINATED AREA WAS FOUND ON LOWER SKIN DENTED. DELAMINATED AREA (0.875 IN X 0.625) ON LOWER SKIN AT RT UPPER MOVABLE VANE WAS REPAIRED IAW ETI-17-19-143 REV. 2 AND ER/A 580374-14 REV. ORIG, SECTION I, PERMANENT REPAIR.
- [SDR DALA2019082005180](https://openairdocs.org/sdr/DALA2019082005180.md): Skin · corroded · Aug 9, 2019 · N945AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / DOUBLER / STA Y=1022.091 AND L29R / ARE CORRODED. ASSOCIATED ER/A 00-580391 ADDED FOR AC 9505. (LP #1214643)
- [SDR DALA2019081204729](https://openairdocs.org/sdr/DALA2019081204729.md): Door · damaged · Aug 9, 2019 · N945AT · Boeing 717200 · Emergency Exits
  > ELONGATED SCREW HOLES ON LH AFT OVERWING EMERGENCY EXIT DOOR FROM PASSENGER CABIN. LT AFT OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER ETI-17-19-135 REV 1 AND ER/A 580351-14 REV ORIGINAL SECTION I PERMANENT REPAIR.
- [SDR DALA2019081204728](https://openairdocs.org/sdr/DALA2019081204728.md): Door · damaged · Aug 9, 2019 · N945AT · Boeing 717200 · Emergency Exits
  > ELONGATED SCREW HOLES ON RH FWD OVERWING EMERGENCY EXIT DOOR FROM PASSENGER CABIN. RH FWD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER ETI-17-19-137 REV ORIGINAL AND ER/A 580352-14 REV ORIGINAL SECTION I PERMANENT REPAIR.
- [SDR DALA2019081204727](https://openairdocs.org/sdr/DALA2019081204727.md): Door · damaged · Aug 9, 2019 · N945AT · Boeing 717200 · Emergency Exits
  > ELONGATED SCREW HOLES ON THE RT AFT OVERWING EMERGENCY EXIT DOOR FROM PASSENGER CABIN. RT AFT OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER ETI-17-19-138 REV ORIGINAL AND ER/A 580353-14 REV ORIGINAL SECTION I, PERMANENT REPAIR.
- [SDR DALA2019081204726](https://openairdocs.org/sdr/DALA2019081204726.md): Cargo Track · corroded · Aug 9, 2019 · N945AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH TIE TRACK BTW STA Y=899 TO Y=1022 AT AFT CARGO COMPARTMENT. CORROSION WAS REMOVED IAW SRM 51-10-04-0G PAR 26. MAXIMUM REMAINING THICKNESS IS 0.038 AND THEREFORE IT IS OUT OF LIMITS IAW SRM 53-20-52-1A-2 FIG 101. LT TIE TRACK WAS REPLACED IAW
- [SDR DALA2019080904673](https://openairdocs.org/sdr/DALA2019080904673.md): Frame · cracked · Aug 8, 2019 · N945AT · Boeing 717200 · Fuselage Main, Frame
  > AWR HIDDEN CRACK: AFTER REMOVAL OF LONGERON IN REFERENCE NRC 00484 CRACK ON FRAME WAS FOUND STA Y 1037 AND LONG 17 LH. AREA WAS REPAIRED PER B717-200 SRM 53-20-07-2R-4 (ET) HFEC INSPECTION WAS PERFORMED ON FRAME STA Y 1037 AND LONG 17LH. NO CRACKS WERE FOUND A
- [SDR DALA2019080804651](https://openairdocs.org/sdr/DALA2019080804651.md): Door Frame · cracked · Aug 8, 2019 · N945AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON LH DOOR JAM STA 46 APROX AT NLG WHEEL WELL (FYT). NRC 00402: CRACK ON LH DOOR JAM STA 46 APROX AT NLG WHEEL WELL WAS REPAIRED PER B717-200 SRM 53-10-14-2R-2 FIG 201. (LP #1211495)
- [SDR DALA2019080804650](https://openairdocs.org/sdr/DALA2019080804650.md): Door Frame · cracked · Aug 8, 2019 · N945AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON RH DOOR JAM STA 46 APROX AT NLG WHEEL WELL (FYT). NRC 00404: CRACK ON RH DOOR JAM STA 46 APROX AT NLG WHEEL WELL WAS REPAIRED PER B717-200 SRM 53-10-14-2R-2 FIG 201. (LP #1211487)
- [SDR DALA2019080804649](https://openairdocs.org/sdr/DALA2019080804649.md): Access Panel · corroded · Aug 7, 2019 · N945AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON FUEL ACCESS PANELS (620CB & 620GB) ON COUNTERSINK AND SETTLEMENT AREA. (FUS). NRC 00619: LEVEL CORROSION 2, FUEL ACCESS PANELS #620CB & 620GB ARE OUT OF LIMITS AND WERE REPLACED. EFFECTIVITY WAS VERIFIED PER B717-200 IPC 57-23-01- 01 AND MUST BE I
- [SDR DALA2019080804647](https://openairdocs.org/sdr/DALA2019080804647.md): Gusset · cracked · Aug 7, 2019 · N945AT · Boeing 717200 · Fuselage Main, Bulkhead
  > CRACK GUSSET BTW STRGR 7R STA 1022 AFT FACE OF BULKHEAD (CPAX). NRC 00530: CRACK GUSSET BTW STRGR 7R STA 1022 AFT FACE OF BULKHEAD WAS REPAIRED PER ETI-17-19-126 REV 1 AND ER /A 580279-14 REV ORIG. SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-580279 ADDED
- [SDR DALA2019080544573](https://openairdocs.org/sdr/DALA2019080544573.md): Longeron · cracked · Aug 3, 2019 · N945AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 6R, BS 1022, AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.
- [SDR DALA2019080544572](https://openairdocs.org/sdr/DALA2019080544572.md): Longeron · cracked · Aug 3, 2019 · N945AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 4R, BS 1022 AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.
- [SDR DALA2019080544571](https://openairdocs.org/sdr/DALA2019080544571.md): Longeron · cracked · Aug 3, 2019 · N945AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 7L, BS 1022 AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.

Next page: https://openairdocs.org/aircraft/N945AT/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 = 'N945AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N945AT/reports

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