# Service difficulty reports: N983AT

A list on [N983AT](https://openairdocs.org/aircraft/N983AT.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 · 132 reports

- [SDR DALA2026072004262](https://openairdocs.org/sdr/DALA2026072004262.md): Bustle · unsecure · Jul 17, 2026 · N983AT · Boeing 717200 · Escape Slide
  > SLIDE BUSTLE CAME LOOSE. RESECURED BUSTLE DUE TO SLIDE BEING LEFT IN THE ARM POSITION PER AMM 25-61. A/C OK FOR SVC. (8683063) AIRCRAFT GROUNDED.
- [SDR DALA2026060903440](https://openairdocs.org/sdr/DALA2026060903440.md): Girt Bar · out of adjust · Jun 3, 2026 · N983AT · Boeing 717200 · Emergency Equipment
  > L1 GIRT BAR DIFFICULT TO OPERATE. READJUSTED GIRT BAR RETAINER IAW AMM 25-61. OPS CHK OK. (8656666) (AIRCRAFT GROUNDED)
- [SDR DALA2026052803226](https://openairdocs.org/sdr/DALA2026052803226.md): Skin · cracked · May 23, 2026 · N983AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL FUSELAGE SKIN STA Y=1076 BTW. PERMANENT REPAIR AND PER PRI 634510-14 (1609411) (AIRCRAFT GROUNDED)
- [SDR DALA2026052803219](https://openairdocs.org/sdr/DALA2026052803219.md): Longeron · cracked · May 21, 2026 · N983AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON END 2LH, STA Y=1133 AT AFT ACCESSORIES COMPARMENT. REPAIRED PER B717-200 SRM 53-00- 05 (1605407) (AIRCRAFT GROUNDED)
- [SDR DALA2025112408547](https://openairdocs.org/sdr/DALA2025112408547.md): Anti-Skid Sys · faulted · Nov 24, 2025 · N983AT · Boeing 717200 · Brake Anti-Skid Section
  > PERFORMED GO AROUND AND DECLARED AN EMERGENCY DUE TO LEFT ANTISKID CAUTION MESSAGE ON FINAL APPROACH. RECORDED BCU INTERNAL FAULT CODE 32417A. REPLACED BCU. OPS CHECK GOOD. (LP 7834420)
- [SDR DALA2025090206468](https://openairdocs.org/sdr/DALA2025090206468.md): Door · not seated · Aug 24, 2025 · N983AT · Boeing 717200 · Cargo/Baggage Doors
  > AIRCRAFT RETURNED TO ATL DUE TO A CABIN INFLOW MSG. FOUND AFT CARGO DOOR LATCHED BUT NOT SEATED, MAINTENANCE PERFORMED A DETAILED VISUAL INSPECTION AND REPLACED THE AFT CARGO DOOR. OPS AND LEAK CHECK GOOD.(7595084)
- [SDR DALA2025081105986](https://openairdocs.org/sdr/DALA2025081105986.md): Latch · not seated · Aug 8, 2025 · N983AT · Boeing 717200 · Cargo/Baggage Doors
  > SHIP 9560-ATB- AIRCRAFT RETURNED TO CLT DUE TO A CABIN INFLOW MSG. CORRECTIVE ACTION: FOUND AFT CARGO DOOR LATCHED BUT NOT SEATED, RESECURED DOOR AND PERFORMED A FUSELAGE LEAK TEST, AFT CARGO DOOR PROX SENSORS TESTED NORMAL. A/C RETURNED TO SERVICE.(7731932)
- [SDR DALA2025080205795](https://openairdocs.org/sdr/DALA2025080205795.md): Skin · ground damage · Jul 28, 2025 · N983AT · Boeing 717200 · Wing, Plate/Skin
  > GSE TOW TRUCK CAME IN CONTACT OF LH, OUTBOARD UNDER WING. C/W ER/A 628016-14.
- [SDR DALA2024102910497](https://openairdocs.org/sdr/DALA2024102910497.md): Duct · disconnected · Oct 26, 2024 · N983AT · Boeing 717200 · Air Distribution System
  > SHIP 9560 -FUME/DE- DURING THE DECENT WHEN THE POWER WAS REDUCED TO IDLE, THE F/A REPORTED A "BURNT CARPET/CRAYON" SMELL IN THE CABIN. F/O NOTIFIED THE CAPT THAT HE TOO SMELLED IT IN THE COCKPIT AND BOTH DONNED O2 MASKS. THE CAPT DECLARED AN EMERGENCY WITH ATC
- [SDR DALA2024103010525](https://openairdocs.org/sdr/DALA2024103010525.md): Access Door · detached · Oct 1, 2024 · N983AT · Boeing 717200 · Horizontal Stabilizer, Plate/Skin
  > HORIZONTAL STABILIZER BEARING AND CENTER SECTION ACCESS DOORS WERE DISCOVERED MISSING DURING POSTFLIGHT INSPECTION. MEL NUMBER ADDED FOR DISPATCH RELEASE, LOG REDEFERRAL REQUIRED. DISPATCH APPROVAL VALIDATION IS ACCOMPLISHED PANEL 370SL BEARING COVER PANEL MIS
- [SDR DALA2024052305457](https://openairdocs.org/sdr/DALA2024052305457.md): Connector · damaged · May 22, 2024 · N983AT · Boeing 717200 · Light System Wiring
  > DURING EMERGENCY LIGHTS CHECK, THE EXTERIOR EMERGENCY LIGHTS TURN ON WITH FLIGHT CABIN SWITCH IN ARM POSITION. SUMMARY OF NRC00627: CONTINUITY WAS PERFORMED PER B717-200 WDM 33-51-11 IN CONNECTOR (P1-125) OF EMERGENCY EVACUATION BATTERY POWER SUPPLY. A MELTED
- [SDR DALA2024052105380](https://openairdocs.org/sdr/DALA2024052105380.md): Skin · scratched · May 20, 2024 · N983AT · Boeing 717200 · Leading Edge Devices
  > SCRATCH ON LOWER SKIN, SLAT PANEL #1 LH WS 168.0. SUMMARY OF NRC 00610: SCRATCH ON LOWER SKIN, SLAT PANEL #1 LH WS 168.0 WAS REPAIRED PER ER/A 618009-14 REV ORIG. SECTION I PERMANENT REPAIR AND PER PRI 618009-14 REV 1. ASSOCIATED ER/A 14-618009 ADDED FOR AC 95
- [SDR DALA2024052105377](https://openairdocs.org/sdr/DALA2024052105377.md): Beam · cracked · May 20, 2024 · N983AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON BEAM #1 AT AFT CARGO DOOR. SUMMARY OF NRC 00575: BEAM #1 AT AFT CARGO DOOR WAS REPAIRED PER ER/A 617654-14 REV ORIGINAL. ASSOCIATED ER/A 14-617654 ADDED FOR AC 9560. (LP #0351759)
- [SDR DALA2024052005346](https://openairdocs.org/sdr/DALA2024052005346.md): Structure · corroded · May 18, 2024 · N983AT · Boeing 717200 · Horizontal Stabilizer Structure
  > CORROSION ON HOLE 18 CENTER BOX LH SIDE AT HORIZONTAL STABILIZER. SUMMARY OF NRC 00589: CORROSION LEVEL 2. HOLE 18 CENTER BOX LH SIDE AT HORIZONTAL STABILIZER WAS REPAIRED PER PRI 617688-14 REV 3 AND ER/A 617688-14 REV ORIG SECTION I: TIME LIMITED REPAIR DTE R
- [SDR DALA2024052005339](https://openairdocs.org/sdr/DALA2024052005339.md): Structure · corroded · May 17, 2024 · N983AT · Boeing 717200 · Horizontal Stabilizer Structure
  > CORROSION ON HOLES 27 AND 28, CENTER BOX RH, AT HORIZONTAL STABILIZER. SUMMARY OF NRC 00581: HOLES 27 AND 28 CENTER BOX RH AT HORIZONTAL STABILIZER. WERE REPAIRED PER PRI 617657-14 REV 1 AND ER/A 617657-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A
- [SDR DALA2024051705298](https://openairdocs.org/sdr/DALA2024051705298.md): Doubler · damaged · May 17, 2024 · N983AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > MISSING MATERIAL IN ONE HOLE WAS FOUND AT INNER DOUBLER. SUMMARY OF NRC 00583: AREA WAS REPAIRED PER ER/A 617844-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-617844 ADDED FOR AC 9560. (LP #0346414)
- [SDR DALA2024051505222](https://openairdocs.org/sdr/DALA2024051505222.md): Skin · cracked · May 14, 2024 · N983AT · Boeing 717200 · Trailing Edge Flaps
  > DENT WITH CRACK (1 EA) 19" FROM OTBD EDGE AND 5.500" FROM LEADING EDGE AND DENT WITH DISBOND (1 EA) 34" FROM OUTBD EDGE AND 4" FROM TRALING EDGE ON LOWER SURFACE AT AFT FLAP MOVABLE VANE AT RIGHT WING. SUMMARY OF NRC 00563: LOWER SURFACE AT AFT FLAP MOVABLE VA
- [SDR DALA2024051405176](https://openairdocs.org/sdr/DALA2024051405176.md): Bottle · low pressure · May 13, 2024 · N983AT · Boeing 717200 · Escape Slide
  > PRESSURE WAS FOUND TO BE OUT OF RANGE ON THE TAIL CONE SLIDE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00519: TAIL CONE SLIDE WAS REMOVED UNDER AMDS 5352-4001 AND REPLACED P
- [SDR DALA2024051305134](https://openairdocs.org/sdr/DALA2024051305134.md): Frame · cracked · May 11, 2024 · N983AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1116 LONGERON 21R AT RH AFT ACCESSORIES COMPARTMENT. SUMMARY OF NRC 00238: FRAME STA Y=1116 LONGERON 21R AT RH AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-07-2R REPAIR 1 FIG 201. (LP #0337618)
- [SDR DALA2024051305133](https://openairdocs.org/sdr/DALA2024051305133.md): Doubler · corroded · May 11, 2024 · N983AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON DOUBLER BTW L29R-L28R STA Y=199-119 AT E&E. SUMMARY OF NRC 00186: CORROSION LEVEL 2. DOUBLER BTW L29R-L28R STA Y=199-119 AT E&E WAS REPLACED PER B717-200 DWG 9923686 REV D AND PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. FORWARD WATER DRAIN MAST
- [SDR DALA2024051305132](https://openairdocs.org/sdr/DALA2024051305132.md): Door Frame · damaged · May 10, 2024 · N983AT · Boeing 717200 · Fuselage Main, Structure
  > BENT AND MISSING MATERIAL ON AFT EDGE OF FWD CARGO DOOR CUTOUT AT EXTERNAL FUSELAGE. SUMMARY OF NRC 00008: AFT EDGE OF FWD CARGO DOOR CUTOUT AT EXTERNAL FUSELAGE WAS REPAIRED PER ERA 617722-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-617722
- [SDR DALA2024050905042](https://openairdocs.org/sdr/DALA2024050905042.md): Support Fitting · corroded · May 8, 2024 · N983AT · Boeing 717200 · Emergency Equipment
  > CORROSION ON R1 DOOR SLIDE GIRT BAR SUPPORT FITTINGS. ALSO CORROSION ON PANEL LOCATED BELOW FITTINGS. SUMMARY OF NRC 00426: CORROSION LEVEL 2. R1 DOOR SLIDE GIRT BAR SUPPORT FITTINGS AND PANEL LOCATED BELOW FITTINGS PANEL WERE FABRICATED AND REPLACED PER DRAWI
- [SDR DALA2024050805023](https://openairdocs.org/sdr/DALA2024050805023.md): Intercostal · cracked · May 8, 2024 · N983AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL STA Y=636, X=0 AT C1. SUMMARY OF NRC 00183: INTERCOSTAL STA Y=636, X=0 AT C1 WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1. (LP #0331871)
- [SDR DALA2024050805021](https://openairdocs.org/sdr/DALA2024050805021.md): Seat Track · corroded · May 7, 2024 · N983AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACKS X=-22, X=-44.5 BTW STA Y=200 TO Y=215. SUMMARY OF NRC 00343: SEAT TRACKS X=-22, X=-44.5 BTW STA Y=200 TO Y=215 WERE REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #0331571)
- [SDR DALA2024050604957](https://openairdocs.org/sdr/DALA2024050604957.md): Cusp Web · corroded · May 4, 2024 · N983AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS IN REF NRC 298, CUSP WEB BTW X=-56 TO -60 AND Y=294-313 AND STA 420 TO 437, STA 674, STA 889 ALSO ON RH CUSP WEB BTW STA X=-44 TO -56 WITH ORIGINAL THICKNESS IS 0.020" AND MINIMUM REMAINING THICKNESS IS 0.08". THEREFORE IT IS OUT OF LIM
- [SDR DALA2024050204888](https://openairdocs.org/sdr/DALA2024050204888.md): Pan · cracked · May 1, 2024 · N983AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON AFT PAN ABOVE BEAM 1 OF FWD CARGO DOOR. SUMMARY OF NRC 00247: AFT PAN ABOVE BEAM 1 OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0321706)
- [SDR DALA2024050805018](https://openairdocs.org/sdr/DALA2024050805018.md): Intercostal · cracked · Apr 28, 2024 · N983AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL OF MECHANISM BTW BEAM #4 AND BEAM #5 OF L1 DOOR. SUMMARY OF NRC 00086: INTERCOSTAL OF MECHANISM BTW BEAM #4 AND BEAM #5 OF L1 DOOR WAS FABRICATED PER DOUGLAS AIRCRAFT COMPANY DWG 9955763 REV M AND REPLACE PER B717-200 SRM 51-41-02-0G. (LP
- [SDR DALA2024043004794](https://openairdocs.org/sdr/DALA2024043004794.md): Floor Panel · corroded · Apr 27, 2024 · N983AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR PANEL 121TF, 121CF, AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00411: CORROSION LEVEL 2. CORROSION WAS FOUND ON FLOOR PANEL 121TF, 121CF, AT FWD CARGO COMPARTMENT. IN ACCORDANCE B717-200 SRM 51-10-04-0G PROCEDURE GENERAL FIG 2 THE PANELS WERE
- [SDR DALA2024043004791](https://openairdocs.org/sdr/DALA2024043004791.md): Cusp Web · corroded · Apr 26, 2024 · N983AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER SURFACE OF LH CUSP WEB BTW STA 359-382. ALSO UPPER SURFACE BTW 660-664 PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00315: CORROSION LEVEL 2. CUSP WEB ON STA 660-664 PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4
- [SDR DALA2024043004789](https://openairdocs.org/sdr/DALA2024043004789.md): Cusp Web · corroded · Apr 25, 2024 · N983AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB BTW STA Y 188\X=58, Y257/X=59, Y275/X=59, Y313/X=59 AT LH CABIN PAX. SUMMARY OF NRC 00650: CORROSION LEVEL 2. CUSP WEB BTW STA Y257/X=59, Y275/X=59, Y313/X=59 AT LH CABIN PAX WERE REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2
- [SDR DALA2024042604727](https://openairdocs.org/sdr/DALA2024042604727.md): Pan · cracked · Apr 25, 2024 · N983AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON FWD PAN ABOVE BEAM 3 OF FWD CARGO DOOR. SUMMARY OF NRC 00246: FWD PAN ABOVE BEAM 3 OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0312268)
- [SDR DALA2023112109574](https://openairdocs.org/sdr/DALA2023112109574.md): Unknown · unknown · Nov 16, 2023 · N983AT · Boeing 717200 · Passenger/Crew Doors
  > UPON ARRIVAL IN BDL, GATE AGENT REPORTED DENT IN L1 DOOR, FORWARD LOWER CORNER NEAR THE EDGE. APPRX 5 TO 6 INCH LONG BY 1 INCH DEEP. *** CONTRACT MAINTENANCE EVENT - OCM: 272623 *** INSPECTED DAMAGE AT 1L DOOR, NO CRACKS OR DAMAGE TO FASTENERS. PERFORMED REPAI
- [SDR DALA2022030101273](https://openairdocs.org/sdr/DALA2022030101273.md): None · none · Feb 26, 2022 · N983AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > AFTER CORROSION REMOVAL IN RH SIDE PLATE BTW STA Y=946-Y=956 AT AFT CARGO COMPARTMENT, CARGO SEAT TRACK WAS FOUND TO BE OUT OF LIMITS. ORIGINAL THICKNESS IS: 0.063IN AND MINIMUM REMAINING THICKNESS IS 0.031IN AND THEREFOR IT IS OUT OF LIMITS PER B717 SRM 53-00
- [SDR DALA2022030201325](https://openairdocs.org/sdr/DALA2022030201325.md): None · none · Feb 24, 2022 · N983AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON INTERCOSTAL BTW Y=994 AND Y=1002, BTW L30 AND L29 RH (SM). SUMMARY OF NRC 00081: CORROSION LEVEL 2, INTERCOSTAL CORRECTIVE ACTION LOCATION PENDING. FOLLOW-UP DUE... "SUPPLEMENTAL INFORMATION": UPDATE DISCREPANCY COMMENT TO STATE: CORROSION ON INTE
- [SDR DALA2022022201131](https://openairdocs.org/sdr/DALA2022022201131.md): None · none · Feb 21, 2022 · N983AT · Boeing 717200 · Escape Slide
  > DUE TO THAT THE SAFETY PIN DOES NOT ALIGN WITH THE ESCAPE SLIDE L1, MCC REQUESTED TO REPLACE THE ESCAPE SLIDE. SUMMARY OF NRC 00154: FORWARD ENTRY EVACUATION SLIDE L1 WAS REPLACED. IT WAS VERIFIED PER B-717 IPC 25-61-01-01 FIGURE 01 (SHEET 001) ITEM 140J THEN
- [SDR DALA2022022201130](https://openairdocs.org/sdr/DALA2022022201130.md): None · none · Feb 21, 2022 · N983AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON BOTH LOWER SPLICE RETAINERS AT LOWER DOOR JAMB, AFT CARGO COMPARTMENT DOOR (C2). SUMMARY OF NRC 00029: CORROSION LEVEL 2. BOTH LOWER SPLICE RETAINERS AT LOWER DOOR JAMB, AFT CARGO COMPARTMENT DOOR WERE REPAIRED PER B717 SRM 53-20-15-2R PROCEDURE 7
- [SDR DALA2022022201129](https://openairdocs.org/sdr/DALA2022022201129.md): None · none · Feb 21, 2022 · N983AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR (C2). SUMMARY OF NRC 00028: CORROSION LEVEL 2. LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #2130071)
- [SDR DALA2022021601012](https://openairdocs.org/sdr/DALA2022021601012.md): None · none · Feb 15, 2022 · N983AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON BOTH LOWER SPLICE RETAINERS AT LOWER DOOR JAMB, FWD CARGO COMPARTMENT DOOR (C1). SUMMARY OF NRC 00030, CORROSION LEVEL 2: FWD LOWER SPLICE RETAINER AT LOWER DOOR JAMB, FWD CARGO COMPARTMENT DOOR WAS REPLACED PER B-717 SRM 53-20-15-2R PROCEDURE 6.
- [SDR DALA2019091105261](https://openairdocs.org/sdr/DALA2019091105261.md): Cover · departed · Sep 10, 2019 · N983AT · Boeing 717200 · Trailing Edge Flaps
  > PART DEPARTED AIRCRAFT. ROUND ACCESS PANEL MISSING FROM LEFT WING INBOARD FLAP FAIRING COVER. INSTALLED ACCESS PANEL PER PS 900-7-3 NR 03. (LP #5156790)
- [SDR DALA2018080604879](https://openairdocs.org/sdr/DALA2018080604879.md): Lens · damaged · Jul 29, 2018 · N983AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT LENS WAS DAMAGED.
- [SDR DALA2018070204301](https://openairdocs.org/sdr/DALA2018070204301.md): Door · unsecure · Jun 23, 2018 · N983AT · Boeing 717200 · Air Conditioning Doors
  > GROUND AIR CONDITIONER DOOR FELL OFF. DEFERRED. WILL NEED A SUPPLEMENTAL SDR.
- [SDR DALA2017101107422](https://openairdocs.org/sdr/DALA2017101107422.md): Battery Pack · inoperative · Oct 11, 2017 · N983AT · Boeing 717200 · Emergency Lighting
  > BOTH AFT OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-230. OPS CHECKED NORMAL IAW AMM 33-51.
- [SDR DALA2017041202997](https://openairdocs.org/sdr/DALA2017041202997.md): Skin · cracked · Apr 11, 2017 · N983AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON SKIN BS 1022 BETWEEN LONGERONS 12 - 14R. REPAIRED IAW ETI-17-17-037 REV. 3, AND ER/A 556344-14 REV ORIGINAL.
- [SDR DALA2017041102992](https://openairdocs.org/sdr/DALA2017041102992.md): Skin · cracked · Apr 10, 2017 · N983AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN BS 1022 BETWEEN LONGERONS 13 - 14L. THE DAMAGE WAS REPAIRED IAW ETI-17-17-038 REV 1, AND ER/A 556345-14 REV. ORIG.
- [SDR DALA2017041102991](https://openairdocs.org/sdr/DALA2017041102991.md): Skin · cracked · Apr 10, 2017 · N983AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN BS 1087 BETWEEN LONGERONS 13 - 14L. DAMAGED WAS REPAIRED IAW ETI-17-17-040 REV 1 AND ER/A 556347-14 REV. ORIG.
- [SDR DALA2017041102990](https://openairdocs.org/sdr/DALA2017041102990.md): Skin · cracked · Apr 10, 2017 · N983AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON SKIN BS 1076 BETWEEN LONGERONS 12 - 14R. DAMAGED WAS REPAIRED IAW ETI-17-17-042 REV. 1 AND ER/A 556350-14 REV. ORIG.
- [SDR DALA2017041102989](https://openairdocs.org/sdr/DALA2017041102989.md): Attach Angle · cracked · Apr 10, 2017 · N983AT · Boeing 717200 · Fuselage Main, Attach Fittings
  > CRACKED LONGERON ATTACH ANGLE ON AFT LAVATORY SUPPORT BULKHEAD BS 1022, LONGERON 7L. DAMAGE WAS REPAIRED IAW ETI-17-17-045 REV. 1, AND ER/A 556351-14 REV. ORIG.
- [SDR DALA2017040702810](https://openairdocs.org/sdr/DALA2017040702810.md): Skin · damaged · Apr 6, 2017 · N983AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > SEVERAL ELONGATED HOLES ON VERTICAL STABILIZER LEADING EDGE AT ZFS=52.267. REPAIRED IAW SRM 55-30-01-2R-7, 51-41-01, AND 51-41-05.
- [SDR DALA2017040602763](https://openairdocs.org/sdr/DALA2017040602763.md): Cargo Track · corroded · Apr 5, 2017 · N983AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON THE RIGHT CARGO TRACK BETWEEN BS 994 - 1022 IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACEDIAW SRM 51-41-01, AND 51-40-08.
- [SDR DALA2017040602762](https://openairdocs.org/sdr/DALA2017040602762.md): Beam · cracked · Apr 5, 2017 · N983AT · Boeing 717200 · Service Doors
  > CRACKED BEAM NR 3, BS 160 BETWEEN UPPER & LOWER HINGE YOKE, FORWARD RIGHT GALLEY SERVICE DOOR STRUCTURE. THE BEAM WAS REPAIRED IAW SRM 52-00-00 2R.

Next page: https://openairdocs.org/aircraft/N983AT/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 = 'N983AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N983AT/reports

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