# Service difficulty reports: N975AT, cancelled Nov 19, 2025

A list on [N975AT, cancelled Nov 19, 2025](https://openairdocs.org/deregistered/N975AT-2025-11-19.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 · 122 reports

- [SDR DALA2019040800000](https://openairdocs.org/sdr/DALA2019040800000.md): Skin · delaminated · Apr 8, 2019 · N975AT · Boeing 717200 · Spoilers
  > SPOILER SKIN, UNSCHEDULED REMOVAL. FOUND DELAMINATED.
- [SDR DALA2018070204300](https://openairdocs.org/sdr/DALA2018070204300.md): Relay · faulty · Jul 2, 2018 · N975AT · Boeing 717200 · Emergency Lighting
  > OVERWING EMERGENCY LIGHTS WON'T EXTINGUISH AFTER SETTING EMERGENCY LIGHT SWITCH TO OFF AS REPORTED BY 2ND SHIFT (WILL ONLY SWITCH OFF ON 'ARM' POSITION). T/S PER FIM 33-51-00-802. REMOVED AND REPLACED OVERWING EMER EVAC LIGHTS BATTERY PACK RELAY R2-273 IAW A
- [SDR DALA2017090306564](https://openairdocs.org/sdr/DALA2017090306564.md): Cusp Web · corroded · Sep 2, 2017 · N975AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON THE CUSP WEB, RBL 54 AND 60, BS 416 TO 417, OUT OF LIMITS. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 216.
- [SDR DALA2016122310056](https://openairdocs.org/sdr/DALA2016122310056.md): Hinge · damaged · Dec 22, 2016 · N975AT · Boeing 717200 · Leading Edge Devices
  > ELONGATED HOLE ON LT WING OUTBOARD FLAP FWD OUTBOARD HINGE IAW NRTC 00456. THE HINGE WAS REMOVED IAW AMM 20-50-01 AND AMM 27-50-01. THE BEARING WAS REPLACED, AND THE HINGE WAS REPAIRED IAW ER/A 552872-14 REV ORIGINAL
- [SDR DALA2016122109992](https://openairdocs.org/sdr/DALA2016122109992.md): Skin · cracked · Dec 20, 2016 · N975AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKED EXTERNAL FUSELAGE SKIN STA 1021 BTW LONG 13/14 LT. EXTERNAL FUSELAGE SKIN WAS REPAIRED PER ETI-17-16-183 REV. ORIGINAL AND ER/A 552865-14 REV ORIGINAL SECTION I. PERFORM REPETITIVE EXTERNAL GENERAL VISUAL INSPECTION OF THE REPAIR EVERY C-CHECK OR 24 MO
- [SDR DALA2016122009962](https://openairdocs.org/sdr/DALA2016122009962.md): Stiffener · cracked · Dec 19, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AFT ACCESSORY COMPARTMENT HAS A CRACK ON STIFFENER STA Y=1200 CANT LONG PROJECTION 2L. STIFFENER WAS REPAIRED PER SRM 53-00-00 REPAIR 1 FIG 201 IN REF ORNRC 00394.
- [SDR DALA2016122009961](https://openairdocs.org/sdr/DALA2016122009961.md): Support · cracked · Dec 19, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT HAS A CRACK ON VERTICAL SUPPORT STA Y=816 LONG 30 (AMDS 5331-2001). CRACK DIMENSION IS.650". CRACK IN VERTICAL SUPPORT WAS STOP DRILLED PER SRM 53-00-00 FIG 201, HFEC WAS ACCOMPLISHED. NO CRACK WERE FOUND AFTER STOP DRILL PER NDT SPM 06-
- [SDR DALA2016121809948](https://openairdocs.org/sdr/DALA2016121809948.md): Support · cracked · Dec 17, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT HAS A CRACKED SUPPORT ON STA Y=655 BTW LONGS 23R AND 24R. SUPPORT WAS REPAIRED PER SRM 53-00-00 FIG 201 SHEET 1 REF ONNRC 363.
- [SDR DALA2016121809945](https://openairdocs.org/sdr/DALA2016121809945.md): Angle · cracked · Dec 17, 2016 · N975AT · Boeing 717200 · Cargo/Baggage Doors
  > FWD CARGO DOOR: CRACK ON ANGLE UPPER EDGE OF DOOR BETWEEN BS 408-410. DAMAGE AREA WAS REPAIRED IAW SRM 52-00-00 REPAIR 2, AND DWG 9957663 REV W.
- [SDR DALA2016121709943](https://openairdocs.org/sdr/DALA2016121709943.md): Longeron · cracked · Dec 16, 2016 · N975AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > IN THE AFT ACCESORY COMPARTMENT THERE IS A CRACK ON LONGERON 4L, BS 1152. THE LONGERON WAS REPAIRED IAW SRM 53-00-05, REPAIR 2, FIGURE 201, 51-40-08, AND 51-41-05.
- [SDR DALA2016121709942](https://openairdocs.org/sdr/DALA2016121709942.md): Bulkhead Web · cracked · Dec 16, 2016 · N975AT · Boeing 717200 · Fuselage Main, Bulkhead
  > FWD CARGO COMPARTMENT HAS CRACKED WEB OF FWD BULKHEAD BS 218, 15 INCHES ABOVE LONGERON 27. THE BULKHEAD WAS REPAIRED BS SRM 53-00-00 REPAIR 1.
- [SDR DALA2016121609905](https://openairdocs.org/sdr/DALA2016121609905.md): Longeron · cracked · Dec 15, 2016 · N975AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > AFT ACCESORIES COMPARTMENT HAS A CRACK ON LONGERON 3L BS 1152. REPAIRD IAW SRM 53-00-05 REPAIR 2 FIGURE 201 AND 51-41-02.
- [SDR DALA2016121609904](https://openairdocs.org/sdr/DALA2016121609904.md): Frame · cracked · Dec 15, 2016 · N975AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME BS 1037, LONGERON 17R. THE FRAME WAS REPAIRED IAW SRM 53-20-07 REPAIR 4, 51-41-01, AND 51-41-05.
- [SDR DALA2016121409840](https://openairdocs.org/sdr/DALA2016121409840.md): Support · cracked · Dec 13, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT: CRACKED RT SUPPORT ON STA Y=664 LONG PROJECTION 23R AND 24R. FITTING WAS REPLACED PER SRM 51-41-02.
- [SDR DALA2016121409839](https://openairdocs.org/sdr/DALA2016121409839.md): Access Panel · corroded · Dec 13, 2016 · N975AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON FUEL ACCESS PLATE 620DT. CORROSION WAS REMOVED ON COUNTERSINK AREA AND SETTLEMENT SURFACE ON ACCESS PLATE 620DT PER SRM 51-10-04 PAR 26, COUNTERSINK AREA WAS MEASURED MAXIMUM COUNTERSINK DIAMETER ALLOWABLE IS 0.660", MAX DIAMETER MEASURED IS 0.705
- [SDR DALA2016121409832](https://openairdocs.org/sdr/DALA2016121409832.md): Frame · cracked · Dec 13, 2016 · N975AT · Boeing 717200 · Fuselage Main, Frame
  > BARREL KEEL BEAMS; CRACKS ON RT/LT FRAMES KEEL AREA FROM STA Y=655 TO Y=737. FRAMES WERE REPAIRED PER SRM 51-70-11 REPAIR 1, SRM 51-41-02, 51-41-05, AND 51-10-04 PAR 15, 21, AND 37. CRACK FRAME DIMENSIONS, STA 679LH 0.656 IN, 694RH 0.906 IN, AND 715R 0.406 IN
- [SDR DALA2016121409831](https://openairdocs.org/sdr/DALA2016121409831.md): Fitting · cracked · Dec 13, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON FRAME CLIP AT STA Y=1022 BTW LONG 16L AND LONG 17L. FRAME CLIP WAS REPLACED PER DWG 9912243 REV JS, SRM 51-41-02 AND 51-41-05.
- [SDR DALA2016121309810](https://openairdocs.org/sdr/DALA2016121309810.md): Cusp Web · cracked · Dec 12, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON LT CUSP WEB LBL 54 - 60, BS 656 - 674. REPAIRED IAW SRM 53-00-55 FIG 215.
- [SDR DALA2016121309809](https://openairdocs.org/sdr/DALA2016121309809.md): Beam · cracked · Dec 12, 2016 · N975AT · Boeing 717200 · Passenger/Crew Doors
  > L1 DOOR HAS A CRACKED AFT EDGE ON BEAM NR 7. REPAIRED IAW SRM 52-10-02 REPAIR 13 FIGURE 201.
- [SDR DALA2016121309808](https://openairdocs.org/sdr/DALA2016121309808.md): Beam · cracked · Dec 12, 2016 · N975AT · Boeing 717200 · Passenger/Crew Doors
  > L1 DOOR HAS A CRACKED AFT EDGE ON BEAM NR 1. REPAIRED IAW SRM 52-10-02 REPAIR 7 FIGURE 201.
- [SDR DALA2016121309807](https://openairdocs.org/sdr/DALA2016121309807.md): Frame · cracked · Dec 12, 2016 · N975AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED FRAME ANGLE ON BS 1022, LONGERONS 13 - 14L. REPLACED IAW DWG 9912243 REV. JS, SRM 51-41-02 AND 51-41-05.
- [SDR DALA2016121309806](https://openairdocs.org/sdr/DALA2016121309806.md): Door Frame · cracked · Dec 12, 2016 · N975AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKED DOOR FRAME WEB BS 207 LONGERON 11 AND 15L. REPAIRED IAW SRM 53-10-15.
- [SDR DALA2016121209753](https://openairdocs.org/sdr/DALA2016121209753.md): Skin · delaminated · Dec 11, 2016 · N975AT · Boeing 717200 · Rudder, Tab Structure
  > DELAMINATON ON RUDDER TAB SKIN. THE RUDDER TAB SKIN WAS REPAIRED IAW SRM 55-41-01 REPAIR 1, AND 51-70-02 REPAIR 3 PAR 5.
- [SDR DALA2016121209752](https://openairdocs.org/sdr/DALA2016121209752.md): Cusp Web · cracked · Dec 11, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED RT CUSP WEB BS 671 - 674, RBL 45. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 FIG 203.
- [SDR DALA2016121209751](https://openairdocs.org/sdr/DALA2016121209751.md): Cusp Web · cracked · Dec 11, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED CUSP WEB BS 652 - 655, RBL 45. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 FIG 211.
- [SDR DALA2016121009803](https://openairdocs.org/sdr/DALA2016121009803.md): Floor Panel · delaminated · Dec 9, 2016 · N975AT · Boeing 717200 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 211ALF. THE FLOOR PANEL WAS FABRICATED AND REPLACED IAW SRM 53-20-50.
- [SDR DALA2016121009802](https://openairdocs.org/sdr/DALA2016121009802.md): Floor Panel · delaminated · Dec 9, 2016 · N975AT · Boeing 717200 · Fuselage Floor Panel
  > DELAMINATION ON FLOOR PANEL. THE FLOOR PANEL WAS FABRICATED AND REPLACED IAW SRM 53-20-50.
- [SDR DALA2016120909746](https://openairdocs.org/sdr/DALA2016120909746.md): Pan · cracked · Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKED RT RING PAN UPPER AFT CORNER BS 832. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG. 202.
- [SDR DALA2016120909745](https://openairdocs.org/sdr/DALA2016120909745.md): Pan · cracked · Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKED RT RING PAN UPPER FWD CORNER BS 696. REPAIRED THE RING PAN WAS REPAIRED IAW SRM 56-20-02 FIG. 202.
- [SDR DALA2016120909744](https://openairdocs.org/sdr/DALA2016120909744.md): Pan · cracked · Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKED RT RING PAN LOWER FWD CORNER BS 889. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG. 202.
- [SDR DALA2016120909743](https://openairdocs.org/sdr/DALA2016120909743.md): Pan · cracked · Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKED RT RING PAN UPPER & LOWER AFT CORNERS BS 851. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG 202.
- [SDR DALA2016120909742](https://openairdocs.org/sdr/DALA2016120909742.md): Pan · cracked · Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKED RT RING PAN LOWER FWD CORNER BS 794. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG 202.
- [SDR DALA2016120909722](https://openairdocs.org/sdr/DALA2016120909722.md): Pan · cracked · Dec 8, 2016 · N975AT · Boeing 717200 · Passenger Compartment Windows
  > CRACK ON LOWER FWD CORNER AT RING PAN WINDOW LT SIDE BTW STA Y 598-617. CRACKED RING PAN LOWER FWR CORNER BTW STA Y=598-617 LT, WAS REPAIRED PER SRM 56-20-02 FIG 202.
- [SDR DALA2016120909721](https://openairdocs.org/sdr/DALA2016120909721.md): Cusp Web · punctured · Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > PUNCTURES ON RT CUSP WEB BTW STA Y=974 TO Y=975 AND BTW Y=989 TO Y=990, X=49R. PUNCTURE WAS DRILLED, DAMAGE WAS REMOVED PER SRM 53-00-00 PAR 2, AND FASTENERS WERE INSTALLED PER SRM 51-41-02.
- [SDR 2016F00131](https://openairdocs.org/sdr/2016F00131.md): Skin · delaminated · May 31, 2016 · N975AT · Boeing 717200 · Spoilers
  > DURING ROUTINE MAINTANANCE INSPECTION, LT SPOILER FOUND WITH DELAMINATION ALONG THE LOWER AND UPPER SURFACE. SUP: P/N 5940974-1.
- [SDR 2016F00128](https://openairdocs.org/sdr/2016F00128.md): Skin · delaminated · May 31, 2016 · N975AT · Boeing 717200 · Spoilers
  > DURING ROUTINE MAINTANANCE INSPECTION, LT SPOILER FOUND WITH DELAMINATION ALONG THE UPPER AND LOWER SURFACE.
- [SDR DALA2017033003179](https://openairdocs.org/sdr/DALA2017033003179.md): Skin · damaged · Mar 29, 2016 · N975AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DURING ATG4 MODIFICATION, MAINTENANCE NOTED THAT ALL FIVE HOLES COMMON TO THE SKIN OF THE SHEAR TIE WERE DAMAGED AND DID NOT PASS NDT INSPECTION. REPAIRED IAW ER/A 00-545433.
- [SDR DALA2016101007123](https://openairdocs.org/sdr/DALA2016101007123.md): Skin · cracked · Dec 14, 2015 · N975AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > SKIN CRACKED AT BS 1076 LONGERON 14R. REPAIRED THE SKIN IAW PRI 542271-14 REV. 0 AND ER/A 542271-14 REV. ORIGINAL.
- [SDR DALA2015051103188](https://openairdocs.org/sdr/DALA2015051103188.md): Cable · frayed · May 10, 2015 · N975AT · Boeing 717200 · Escape Slide
  > DURING SERVICE CHECK, FOUND TAILCONE SLIDE KEVLAR DEPLOYMENT CABLE FRAYED. REPLACED AFT TAILCONE SLIDE DEPLOYMENT CABLE IAW AMM 25-61. LP 7277097.
- [SDR DALA2014110606004](https://openairdocs.org/sdr/DALA2014110606004.md): Battery Pack · inoperative · Nov 6, 2014 · N975AT · Boeing 717200 · Light System Wiring
  > DURING LINE CHECK, NOTED CEILING EXIT LIGHTS IN FIRST CLASS AND 2 ROWS OF COACH EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED BATTERY PACK, BS-227 IAW AMM 33-51.
- [SDR SWAA2014010223703](https://openairdocs.org/sdr/SWAA2014010223703.md): Lens · cracked · Dec 29, 2013 · N975AT · Boeing 717200 · Emergency Lighting
  > R1 DOOR EXIT LIGHT LENS CRACKED. R & R LENS ASSEMBLY IAW AMM.
- [SDR SWAA2014010823898](https://openairdocs.org/sdr/SWAA2014010823898.md): Wire · loose · Dec 27, 2013 · N975AT · Boeing 717200 · Light System Wiring
  > RT OVERWING EMERGENCY EXIT LIGHT WIRE LOOSE. SECURED WIRE IAW AMM.
- [SDR SWAA2014010823897](https://openairdocs.org/sdr/SWAA2014010823897.md): Wire · loose · Dec 27, 2013 · N975AT · Boeing 717200 · Light System Wiring
  > LT OVERWING EMERGENCY EXIT LIGHT WIRE LOOSE. SECURED WIRE IAW AMM.
- [SDR SWAA2014010223698](https://openairdocs.org/sdr/SWAA2014010223698.md): Wire · disconnected · Dec 27, 2013 · N975AT · Boeing 717200 · Light System Wiring
  > LT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RECONNECTED WIRE IAW WDM.
- [SDR SWAA2013122723652](https://openairdocs.org/sdr/SWAA2013122723652.md): Battery Pack · discharged · Dec 21, 2013 · N975AT · Boeing 717200 · Emergency Lighting
  > OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. R & R OVERWING EMERGENCY LIGHTS BATTERY PACK IAW MM.
- [SDR SWAA2013122623635](https://openairdocs.org/sdr/SWAA2013122623635.md): Light · inoperative · Dec 21, 2013 · N975AT · Boeing 717200 · Emergency Lighting
  > AFT CABIN EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.
- [SDR SWAA2013121823493](https://openairdocs.org/sdr/SWAA2013121823493.md): Intercostal · cracked · Dec 9, 2013 · N975AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED BETWEEN STATION 619 & 636, BL 0. R & R INTERCOSTAL IAW SRM.
- [SDR SWAA2013112522752](https://openairdocs.org/sdr/SWAA2013112522752.md): Stringer Splice · cracked · Nov 13, 2013 · N975AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE 6R DAMAGED & CRACKED AT BS 246. R & R STRINGER SPLICE IAW SRM.
- [SDR SWAA2013120222832](https://openairdocs.org/sdr/SWAA2013120222832.md): Crease Beam · corroded · Nov 8, 2013 · N975AT · Boeing 717200 · Fuselage Main, Structure
  > CREASE BEAM WEB CORRODED BETWEEN STATION 598 TO STATION 617, STRINGER 18L. REPAIRED WEB IAW SRM.
- [SDR SWAA2013121223247](https://openairdocs.org/sdr/SWAA2013121223247.md): Longeron · cracked · Oct 28, 2013 · N975AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > LONGERON CRACKED AT STATION 1133, LONGERON 2R. R & R LONGERON IAW SRM.

Next page: https://openairdocs.org/deregistered/N975AT-2025-11-19/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 = 'N975AT' AND deregistration_id = 'N975AT-2025-11-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N975AT-2025-11-19/reports

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