# Service difficulty reports: N968AT, cancelled May 3, 2026

A list on [N968AT, cancelled May 3, 2026](https://openairdocs.org/deregistered/N968AT-2026-05-03.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 · 171 reports

- [SDR DALA2019103006278](https://openairdocs.org/sdr/DALA2019103006278.md): Pin · split · Oct 30, 2019 · N968AT · Boeing 717200 · Escape Slide
  > THE FWD CATERING DOOR (R1) SPILT PIN OUT OF SLIDE PACK. MAINTENANCE ATTEMPT TO RE-INSTALL SPILT PIN IN SLIDE PACK BUT WHEN THE SLIDE PACK COVER WAS REMOVED THE INFLATION CABLE WAS FOUND TO BE OUT OF THE GROMET TABS. THE R1 DOOR SLIDE WAS REPLACED PER AMDS 2561
- [SDR DALA2019030501444](https://openairdocs.org/sdr/DALA2019030501444.md): Adiru · faulty · Mar 4, 2019 · N968AT · Boeing 717200 · Inertial Guidance System
  > SHIP 9530 - THE CREW SAFELY ABORTED THE TAKEOFF ROLL AT 115 KNOTS DUE TO THE AIRSPEED RAPIDLY ADVANCING UP THE SPEED TAPE. DUE TO THE SPEED NUMBER TURNING AMBER AND THE POSSIBILITY OF WIND SHEAR, THE ABORT WAS INITIATED. CORRECTIVE ACTION: BOTH FCC FAULTED "W/
- [SDR DALA2019030601509](https://openairdocs.org/sdr/DALA2019030601509.md): Slide · unserviceable · Feb 28, 2019 · N968AT · Boeing 717200 · Escape Slide
  > THE TAILCONE SLIDE IS COMING OUT OF PACK COVER. MAINTENANCE REPLACED THE TAILCONE SLIDE PER AMDS WORKCARD 2561-9006. RII COMPLETE. (LP #0963323)
- [SDR DALA2018082875294](https://openairdocs.org/sdr/DALA2018082875294.md): Frame · cracked · Aug 26, 2018 · N968AT · Boeing 717200 · Fuselage Main, Frame
  > FRAME CRACKED AT BS 696. REPAIRED IAW AMDS CARD 5310-01436-03A.
- [SDR DALA2018082875293](https://openairdocs.org/sdr/DALA2018082875293.md): Frame · cracked · Aug 26, 2018 · N968AT · Boeing 717200 · Fuselage Main, Frame
  > FRAME CRACKED AT BS 715. CONDITION 3, GREATER THAN.125 INCH. REPAIRED IAW AMDS CARD 5310-01436-03A.
- [SDR DALA2018082745262](https://openairdocs.org/sdr/DALA2018082745262.md): Door Frame · corroded · Aug 23, 2018 · N968AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION FOUND ON THE AFT CARGO BAY THRESHOLD. SEVERAL PLACES. REPLACED THE DOOR FRAME IAW SRM 53-20-15-2R, PROC 7.
- [SDR DALA2018062004119](https://openairdocs.org/sdr/DALA2018062004119.md): Apu · failed · Jun 19, 2018 · N968AT · Boeing 717200 · APU Core Engine
  > UPON ARRIVAL AT GATE, AS PASSENGERS WERE DEPLANING, F/A NOTIFIED COCKPIT OF SMOKE AND FUMES IN THE CABIN. THE PASSENGERS CONTINUED TO EXIT NORMALLY. MIST SEEMED TO ORIGINATE FROM AFT CABIN AND WORK FORWARD. MAINTENANCE INSPECTED AND FOUND THE APU CAVITY OIL S
- [SDR DALA2017111508135](https://openairdocs.org/sdr/DALA2017111508135.md): Battery Pack · inoperative · Nov 15, 2017 · N968AT · Boeing 717200 · Emergency Lighting
  > FOUND THE OVERWING EMERGENCY LIGHTS INOPERATIVE, ALSO LIGHTS IN MID-CABIN INOPERATIVE. REPLACED THE BATTERY AND CHARGER ASSEMBLY IN AFT CARGO BAY. EMERGENCY LIGHTS CHECKED GOOD. REPLACED THE BATTERY PACK AT BS 1045 AND CABIN LIGHTS NOW CHECKED GOOD IAW AMM
- [SDR DALA2017032202286](https://openairdocs.org/sdr/DALA2017032202286.md): Power Supply · inoperative · Mar 22, 2017 · N968AT · Boeing 717200 · Emergency Lighting
  > CABIN CEILING EMERGENCY LIGHTS ARE OUT. REPLACED THE POWER SUPPLY AND OPS CHECKED NORMAL IAW AMM 33-51.
- [SDR DALA2017030701919](https://openairdocs.org/sdr/DALA2017030701919.md): Battery Pack · inoperative · Mar 6, 2017 · N968AT · Boeing 717200 · Emergency Lighting
  > OVERWING EMERGENCY LIGHT BATTERY PACK INOPERATIVE.
- [SDR DALA2017030701861](https://openairdocs.org/sdr/DALA2017030701861.md): Circuit Board · burned · Mar 6, 2017 · N968AT · Boeing 717200 · Emergency Lighting
  > OVERWING EMERGENCY LIGHT BATTERY POWER SUPPLY CIRCUIT BOARD BURNT. REPLACED OVERWING EMERGENCY LIGHT BATTERY POWER SUPPLY PER AMM 33-51-03 OPS CHECK GOOD. AC OK FOR SERVICE.
- [SDR DALA2016092406808](https://openairdocs.org/sdr/DALA2016092406808.md): Skin · cracked · Sep 22, 2016 · N968AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT UPPER FASTENER IN FORMER 1152 BETWEEN L2-L3 LT LOCATION MARKED. REMOVED DAMAGE FROM FUSELAGE SKIN CRACKED AND REPAIRED IAW ER/A 549614-14. REPAIR REQUIRES REPETITIVE INSPECTIONS EVERY 3000 FLIGHT CYCLES.
- [SDR DALA2016092406809](https://openairdocs.org/sdr/DALA2016092406809.md): Skin · cracked · Sep 21, 2016 · N968AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS IN FUSELAGE SKIN AROUND RIVET HEAD ABOVE RT PYLON STA 1095.868, JUST ABOVE L14 RT LOCATION MARKED. SKIN CRACKS REMOVED AND REPAIRED IAW ER/A 549613-14 REQUIRES REPETITIVE INSPECTIONS EVERY 3000 FLIGHT CYCLES AFTER REPAIR.
- [SDR DALA2016092206771](https://openairdocs.org/sdr/DALA2016092206771.md): Panel · damaged · Sep 20, 2016 · N968AT · Boeing 717200 · Wing, Plate/Skin
  > RIGHT WING L/E PANEL 610RB HAS 2 EA ENLARGED SCREW HOLES WITH SURROUNDING CHAFED SURFACES AND 1 EA HOLES HAS TOOLING MARKS. FABRICATED REPAIR DOUBLER FOR 2 ENLARGE HOLES AND TOOLING MARK REPAIR IAW SRM 57-40-01, REPAIR 2.
- [SDR DALA2016110208152](https://openairdocs.org/sdr/DALA2016110208152.md): Skin · corroded · Sep 19, 2016 · N968AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > SKIN CORRODED AT BS 737-745 RBL 58. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM ALLOWABLE DAMAGE 1. REPAIRED IAW SRA 549615-14.
- [SDR DALA2016092006726](https://openairdocs.org/sdr/DALA2016092006726.md): Cusp Web · cracked · Sep 19, 2016 · N968AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > UPPER CABIN RT CUSP WEB, STA 670 IS CRACKED OTBD OF BL 56R TRACK, MARKED. REMOVED DAMAGED CUSP WEB FROM STA 655-756, OTBD OF RBL 44 IAW SRM 51-41-02. INSTALLED REPLACEMENT CUSP WEB FROM STA 655-756, OTBD OF RBL 44 IAW SRM 51-41-02.
- [SDR DALA2016092006725](https://openairdocs.org/sdr/DALA2016092006725.md): Frame · cracked · Sep 19, 2016 · N968AT · Boeing 717200 · Fuselage Main, Frame
  > UPPER FUSELAGE, AFT CABIN, STA 1037 FRAME 17R, CRACK, MARKED. REPAIRED CRACKED FRAME AT FS 1037 AT 17R BY REMOVED DAMAGE ON FRAME AND INSTALLING FILLERS, DOUBLERS IAW SRM 53-20-07. REPAIR 1, FIG 201, USING DOUBLERS MADE FROM 7075 T6.063 AND FILLERS MADE FROM
- [SDR DALA2016092606810](https://openairdocs.org/sdr/DALA2016092606810.md): Frame · corroded · Sep 18, 2016 · N968AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ALC STA 927 FRAME FORMER, BETWEEN STA 30 AND 29L FWD AND AFT. BLEND, CHECK LIMITS, REPAIR AS REQUIRED. BLENDED CORROSION AT STA 927, LONGERON 30-29L, LOWEST MEASURED THICKNESS WAS.038", FOUND TO BE OUT OF LIMITS. REPAIRED CORRODED FRAME FORMER IA
- [SDR DALA2016092306784](https://openairdocs.org/sdr/DALA2016092306784.md): Floor Support · cracked · Sep 18, 2016 · N968AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CENTER FLOOR PANEL SUPPORT AT STA 636 IS CRACKED. MARKED, PULLEY CLUSTER AT STA 636 REMOVED IAW SRM 51-41-01, PG 1. INTERCOSTAL REMOVED IAW SRM 51-41-02. MATERIAL VERIFICATION IS 7075-T6.050 IAW MFG PROPRIETARY DWG 9936580, REV B. ALODINED AND PRIMED IAW
- [SDR DALA2016092406807](https://openairdocs.org/sdr/DALA2016092406807.md): Seat Track · corroded · Sep 16, 2016 · N968AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT IB SEAT TRACK HAS NUMEROUS AREAS CORRODED OUT OF LIMITS STA 200-588, RBL22. REPAIRED SEAT TRACKS SECTION RBL 22 BETWEEN STA 200-STA 588 FOR OUT OF LIMITS DUE TO CORROSION BLENDING WORK ACCOMPLISHED IAW SRM 53-20-52, REPAIR 5.
- [SDR DALA2016092606811](https://openairdocs.org/sdr/DALA2016092606811.md): Structure · worn · Sep 15, 2016 · N968AT · Boeing 717200 · Nacelle/Pylon Miscellaneous Structure
  > THE NR 2 ENGINE UPPER COWLING PRECOOLER OUTLET INTERNAL CONTACT SURFACE IS WORN. BLEND, CHECK LIMITS. BLENDED WORN AREA IAW SRM 54-20-00 FIG 101,.038 REMAINING FROM ORIGINAL.050, FOUND TO BE OUT OF LIMITS IAW SRM 54-20-00, FIG 101, GAUGE 6784. REPAIRED AR
- [SDR DALA2016092306781](https://openairdocs.org/sdr/DALA2016092306781.md): Cusp Web · cracked · Sep 15, 2016 · N968AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > LEFT CUSP WEB OTBD LIGHTNING HOLE IS CRACKED AT STA 360. REMOVED LT OTBD SEAT TRACK FROM STA 200 TO STA 445. REPAIRED CUSP WEB IAW SRM 53-00-55, REPAIR 4 AND REINSTALLED SEAT TRACK IAW SRM 51-41-01, PAR 6.
- [SDR DALA2016091606668](https://openairdocs.org/sdr/DALA2016091606668.md): Pan · corroded · Sep 15, 2016 · N968AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS OF CORROSION ON FORWARD CARGO DOOR PAN. CLEANED UP CORROSION IAW SRM 53-00-00 FIG 103. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103). REPLACED THE PAN IAW SRM 51-41-02 SEC 4 AND 51-41-09.
- [SDR DALA2016091606718](https://openairdocs.org/sdr/DALA2016091606718.md): Floor Panel · damaged · Sep 14, 2016 · N968AT · Boeing 717200 · Fuselage Floor Panel
  > UPPER CABIN FLOOR PANEL 221CF AT BS 465, LBL 22 HAS DAMAGE ON UPPER SURFACE. FABRICATED A NEW FLOOR PANEL IAW SRM 53-20-50 REPAIR 3 AND INSTALLED.
- [SDR DALA2016091606717](https://openairdocs.org/sdr/DALA2016091606717.md): Floor Panel · delaminated · Sep 14, 2016 · N968AT · Boeing 717200 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 222GF DELAMINATING. FABRICATED FLOOR PANEL IAW SRM 53-20-50 3 AND INSTALLED.
- [SDR DALA2016091606716](https://openairdocs.org/sdr/DALA2016091606716.md): Floor Panel · delaminated · Sep 14, 2016 · N968AT · Boeing 717200 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 222DF DELAMINATING. FABRICATED A NEW FLOOR PANEL IAW SRM 53-20-50 REPAIR 3 AND INSTALLED.
- [SDR DALA2016091606715](https://openairdocs.org/sdr/DALA2016091606715.md): Floor Panel · delaminated · Sep 14, 2016 · N968AT · Boeing 717200 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 223FF IS DELAMINATING. FABRICATED A NEW FLOOR PANEL IAW SRM 53-20-50, AND INSTALLED.
- [SDR DALA2016091506633](https://openairdocs.org/sdr/DALA2016091506633.md): Shear Tie · cracked · Sep 14, 2016 · N968AT · Boeing 717200 · Fuselage Internal Mounting Structure
  > SHEAR TIE CRACKED AT BS 1022 LONGERON 6R. REPLACED THE SHEAR TIE IAW SRM 53-20-07 AND DWG 9912243 AND SRM 51-41-05 PG 1.
- [SDR DALA2016092306785](https://openairdocs.org/sdr/DALA2016092306785.md): Panel · cracked · Sep 13, 2016 · N968AT · Boeing 717200 · Elevator, Plate/Skin
  > ELEVATOR LOWER SURFACE RT PANEL 340 KB IS CRACKED. THE PANEL IS ON THE UPPER TAIL DOCK. FABRICATED NEW PANEL 340KB IAW SRM 51-20-09 AND DWG NR 5910412, REV 05. PANEL 340KB TO BE INSTALLED ON JC 2040-0030.
- [SDR DALA2016091506638](https://openairdocs.org/sdr/DALA2016091506638.md): Seat Track · damaged · Sep 13, 2016 · N968AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CABIN SEAT TRACK LBL 22, BS 520 - 598 HAS TWO AREAS OF EXPOSED METAL. REPLACED THE SECTION OF SEAT TRACK IAW SRM 53-20-52 REPAIR 5. FABRICATED THE NEW SECTION IAW SRM 53-20-05 REPAIR 5.
- [SDR DALA2016091506631](https://openairdocs.org/sdr/DALA2016091506631.md): Bulkhead · cracked · Sep 13, 2016 · N968AT · Boeing 717200 · Fuselage Main, Bulkhead
  > ENGINE PYLON SUPPORT BULKHEAD ON THE RIGHT SIDE AT LONGERON 7R IS CRACKED. REPAIRED BULKHEAD IAW SRM 53-20-07 REPAIR 1.
- [SDR DALA2016091406630](https://openairdocs.org/sdr/DALA2016091406630.md): Access Panel · cracked · Sep 13, 2016 · N968AT · Boeing 717200 · Wing, Plate/Skin
  > LEFT WING ACCESS PANEL 520GB CRACKED. REPLACED THE ACCESS PANEL IAW AMM 28-00-00-410.
- [SDR DALA2016091406629](https://openairdocs.org/sdr/DALA2016091406629.md): Floorbeam · corroded · Sep 13, 2016 · N968AT · Boeing 717200 · Fuselage Main, Floor Beam
  > FLOORBEAM BS 135 R RBL 40 - 50 CORRODED. REPLACED THE FLOORBEAM IAW DWN S00074 AND SRM 51-41-02.
- [SDR DALA2016091406628](https://openairdocs.org/sdr/DALA2016091406628.md): Seat Track · corroded · Sep 13, 2016 · N968AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED. FOUND BEYOND LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-01 PAR 6.
- [SDR DALA2016091506636](https://openairdocs.org/sdr/DALA2016091506636.md): Access Panel · cracked · Sep 8, 2016 · N968AT · Boeing 717200 · Wing, Plate/Skin
  > LEFT WING ACCESS PANEL 520DB CRACKED. REPLACED THE ACCESS PANEL IAW AMM 28-00-00 410.
- [SDR DALA2016090806455](https://openairdocs.org/sdr/DALA2016090806455.md): Pan · gouged · Sep 7, 2016 · N968AT · Boeing 717200 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR PAN GOUGED ABOVE FORWARD DOOR HOLD OPEN HOOK. CLEANED UP GOUGES ON FORWARD CARGO DOOR PAN ABOVE FORWARD DOOR HOLD OPEN HOOK IAW SRM 52-00-00, FIG 103, 52-30-02, PG 1. REMOVED.014 OF.050 BEYOND ALLOWABLE LIMITS, TAG 2721. REPAIRED DOOR P
- [SDR DALA2015012300553](https://openairdocs.org/sdr/DALA2015012300553.md): Wire · burned · Jan 22, 2015 · N968AT · Boeing 717200 · Engine Control System Wiring
  > DURING TAXI, RT ENGINE WOULD NOT SHUTDOWN. CIRCUIT BREAKER FOR RT ENGINE FUEL SWITCH TRIPPED. MAINTENANCE FOUND WIRES SHORTED RT SIDE OF ATC TRANSPONDER NR 1 AND FOUND BURNED WIRES ON TOP OF ATC NR 1. INSPECTED WIRES IAW SWPM 20-10-01, WIRES THAT ARE OUT OF
- [SDR DALA2015010100018](https://openairdocs.org/sdr/DALA2015010100018.md): Cusp Web · cracked · Dec 31, 2014 · N968AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY BS 655, RBL 54 AFT SIDE OF FRAME, CUSP WEB CRACKED. REPAIRED IAW SRM 53-00-55, REPAIR 4.
- [SDR SWAA2014091732054](https://openairdocs.org/sdr/SWAA2014091732054.md): Cover · cracked · Sep 13, 2014 · N968AT · Boeing 717200 · Emergency Lighting
  > R1 DOOR EXIT SIGN COVER CRACKED. REMOVED COVER IAW AMM.
- [SDR SWAA2014091531996](https://openairdocs.org/sdr/SWAA2014091531996.md): Light · cracked · Sep 13, 2014 · N968AT · Boeing 717200 · Emergency Lighting
  > R1 DOOR EXIT SIGN MOUNTING LIGHT ASSEMBLY CRACKED. R & R LIGHT ASSEMBLY IAW AMM.
- [SDR SWAA2014091632013](https://openairdocs.org/sdr/SWAA2014091632013.md): Panel · cracked · Sep 11, 2014 · N968AT · Boeing 717200 · Cargo Compartments
  > SIDEWALL PANEL FWD PIT LT SIDE ACROSS FROM DOOR CRACKED IN LINER OVER FRAME. REPAIRED PANEL IAW SRM.
- [SDR SWAA2014091531995](https://openairdocs.org/sdr/SWAA2014091531995.md): Flashlight · missing · Sep 11, 2014 · N968AT · Boeing 717200 · Emergency Equipment
  > FORWARD EMER FLASHLIGHT MISSING. INSTALLED FLASHLIGHT IAW AMM.
- [SDR SWAA2014090831685](https://openairdocs.org/sdr/SWAA2014090831685.md): Battery Pack · discharged · Sep 7, 2014 · N968AT · Boeing 717200 · Emergency Lighting
  > LEFT MAIN ENTRANCE EMER LIGHT FAILED AT BS 180. REMOVED & INSTALLED BATTERY PACK IAW AMM.
- [SDR SWAA2014090831643](https://openairdocs.org/sdr/SWAA2014090831643.md): Battery · discharged · Sep 2, 2014 · N968AT · Boeing 717200 · Emergency Lighting
  > FORWARD OVERWING EXIT DOOR SIGN BATTERY INOPERATIVE. R & R BATTERY IAW AMM.
- [SDR SWAA2014090831642](https://openairdocs.org/sdr/SWAA2014090831642.md): Web · cracked · Aug 30, 2014 · N968AT · Boeing 717200 · Wing Miscellaneous Structure
  > LEFT WING OTBD TE WEB JUST FWD OF AILERON CRACKED. R & R WEB IAW AMM & DWG.
- [SDR SWAA2014090831684](https://openairdocs.org/sdr/SWAA2014090831684.md): Strap · cracked · Aug 30, 2014 · N968AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT SIDE WALL SUPPORT STRAP CRACKED AT BS 237, LBL 35. R & R STRAP IAW SRM & DWG.
- [SDR SWAA2014090231458](https://openairdocs.org/sdr/SWAA2014090231458.md): Skin · corroded · Aug 20, 2014 · N968AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AFT CARGO DOOR CUT OUT LOWER SKIN EDGE CORRODED BETWEEN SKIN LAYERS. REPAIRED SKIN IAW SRM.
- [SDR SWAA2014081930953](https://openairdocs.org/sdr/SWAA2014081930953.md): Attach Fitting · cracked · Aug 13, 2014 · N968AT · Boeing 717200 · Wing, Control Surface Attach Fittings
  > LEFT WING OTBD AILERON ATTACH FITTING CRACKED. R & R FITTING IAW SRM.
- [SDR SWAA2014090831652](https://openairdocs.org/sdr/SWAA2014090831652.md): Skin · cracked · Jul 20, 2014 · N968AT · Boeing 717200 · Elevator, Tab Structure
  > RIGHT ELEVATOR GEARED TAB LOWER SURFACE SKIN CRACKED AT INBD EDGE. REPAIRED TAB IAW AT EA.
- [SDR SWAA2014081830924](https://openairdocs.org/sdr/SWAA2014081830924.md): Shear Tie · cracked · Jul 17, 2014 · N968AT · Boeing 717200 · Fuselage Internal Mounting Structure
  > SHEAR TIE CRACKED AT BS 1116, LONGERON 15L. R & R SHEAR TIE IAW DWG.

Next page: https://openairdocs.org/deregistered/N968AT-2026-05-03/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 = 'N968AT' AND deregistration_id = 'N968AT-2026-05-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N968AT-2026-05-03/reports

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