# N968AT: 2001 Boeing 717-200, registration cancelled 2026-05-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 3, 2026
- Status when cancelled: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700)
- Engine: [Rolls-Royce BR-700 series](https://openairdocs.org/engine/rolls-royce-br-700-series) (registry code 54565)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 55029
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 19, 2001
- Certificate issued: November 24, 2023
- Last registry action: November 24, 2023
- Mode S code: AD79F0
- Owner when cancelled: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC)
- Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)
- Owner type: Corporation
- Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N968AT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=968AT
- Page: https://openairdocs.org/deregistered/N968AT-2026-05-03

From the FAA registry file of October 31, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 717-200: https://openairdocs.org/model/boeing-717-200.md

## Service difficulty reports (171, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DALA2019103006278](https://openairdocs.org/sdr/DALA2019103006278), Oct 30, 2019: PIN. SPLIT. 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 
- [SDR DALA2019030501444](https://openairdocs.org/sdr/DALA2019030501444), Mar 4, 2019: ADIRU. FAULTY. 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
- [SDR DALA2019030601509](https://openairdocs.org/sdr/DALA2019030601509), Feb 28, 2019: SLIDE. UNSERVICEABLE. 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), Aug 26, 2018: FRAME. CRACKED. FRAME CRACKED AT BS 696. REPAIRED IAW AMDS CARD 5310-01436-03A.
- [SDR DALA2018082875293](https://openairdocs.org/sdr/DALA2018082875293), Aug 26, 2018: FRAME. CRACKED. 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), Aug 23, 2018: DOOR FRAME. CORRODED. 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), Jun 19, 2018: APU. FAILED. 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 SEEME
- [SDR DALA2017111508135](https://openairdocs.org/sdr/DALA2017111508135), Nov 15, 2017: BATTERY PACK. INOPERATIVE. FOUND THE OVERWING EMERGENCY LIGHTS INOPERATIVE, ALSO LIGHTS IN MID-CABIN INOPERATIVE. REPLACED THE BATTERY AND CHARGER ASSEMBLY IN AFT CARGO BAY. EMERGENCY LIG
- [SDR DALA2017032202286](https://openairdocs.org/sdr/DALA2017032202286), Mar 22, 2017: POWER SUPPLY. INOPERATIVE. 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), Mar 6, 2017: BATTERY PACK. INOPERATIVE. OVERWING EMERGENCY LIGHT BATTERY PACK INOPERATIVE.
- [SDR DALA2017030701861](https://openairdocs.org/sdr/DALA2017030701861), Mar 6, 2017: CIRCUIT BOARD. BURNED. 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
- [SDR DALA2016092406808](https://openairdocs.org/sdr/DALA2016092406808), Sep 22, 2016: SKIN. CRACKED. 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-
- [SDR DALA2016092406809](https://openairdocs.org/sdr/DALA2016092406809), Sep 21, 2016: SKIN. CRACKED. 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 RE
- [SDR DALA2016092206771](https://openairdocs.org/sdr/DALA2016092206771), Sep 20, 2016: PANEL. DAMAGED. 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 ENLA
- [SDR DALA2016110208152](https://openairdocs.org/sdr/DALA2016110208152), Sep 19, 2016: SKIN. CORRODED. 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), Sep 19, 2016: CUSP WEB. CRACKED. 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 
- [SDR DALA2016092006725](https://openairdocs.org/sdr/DALA2016092006725), Sep 19, 2016: FRAME. CRACKED. 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, DOUBLE
- [SDR DALA2016092606810](https://openairdocs.org/sdr/DALA2016092606810), Sep 18, 2016: FRAME. CORRODED. 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, 
- [SDR DALA2016092306784](https://openairdocs.org/sdr/DALA2016092306784), Sep 18, 2016: FLOOR SUPPORT. CRACKED. 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. MATERI
- [SDR DALA2016092406807](https://openairdocs.org/sdr/DALA2016092406807), Sep 16, 2016: SEAT TRACK. CORRODED. 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 
- [SDR DALA2016092606811](https://openairdocs.org/sdr/DALA2016092606811), Sep 15, 2016: STRUCTURE. WORN. 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
- [SDR DALA2016092306781](https://openairdocs.org/sdr/DALA2016092306781), Sep 15, 2016: CUSP WEB. CRACKED. 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 RE
- [SDR DALA2016091606668](https://openairdocs.org/sdr/DALA2016091606668), Sep 15, 2016: PAN. CORRODED. 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). REPLA
- [SDR DALA2016091606718](https://openairdocs.org/sdr/DALA2016091606718), Sep 14, 2016: FLOOR PANEL. DAMAGED. 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), Sep 14, 2016: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 222GF DELAMINATING. FABRICATED FLOOR PANEL IAW SRM 53-20-50 3 AND INSTALLED.
- [SDR DALA2016091606716](https://openairdocs.org/sdr/DALA2016091606716), Sep 14, 2016: FLOOR PANEL. DELAMINATED. 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), Sep 14, 2016: FLOOR PANEL. DELAMINATED. 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), Sep 14, 2016: SHEAR TIE. CRACKED. 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), Sep 13, 2016: PANEL. CRACKED. 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. 
- [SDR DALA2016091506638](https://openairdocs.org/sdr/DALA2016091506638), Sep 13, 2016: SEAT TRACK. DAMAGED. 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 SEC
- [SDR DALA2016091506631](https://openairdocs.org/sdr/DALA2016091506631), Sep 13, 2016: BULKHEAD. CRACKED. 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), Sep 13, 2016: ACCESS PANEL. CRACKED. LEFT WING ACCESS PANEL 520GB CRACKED. REPLACED THE ACCESS PANEL IAW AMM 28-00-00-410.
- [SDR DALA2016091406629](https://openairdocs.org/sdr/DALA2016091406629), Sep 13, 2016: FLOORBEAM. CORRODED. 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), Sep 13, 2016: SEAT TRACK. CORRODED. 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), Sep 8, 2016: ACCESS PANEL. CRACKED. LEFT WING ACCESS PANEL 520DB CRACKED. REPLACED THE ACCESS PANEL IAW AMM 28-00-00 410.
- [SDR DALA2016090806455](https://openairdocs.org/sdr/DALA2016090806455), Sep 7, 2016: PAN. GOUGED. 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,
- [SDR DALA2015012300553](https://openairdocs.org/sdr/DALA2015012300553), Jan 22, 2015: WIRE. BURNED. 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 AN
- [SDR DALA2015010100018](https://openairdocs.org/sdr/DALA2015010100018), Dec 31, 2014: CUSP WEB. CRACKED. 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), Sep 13, 2014: COVER. CRACKED. R1 DOOR EXIT SIGN COVER CRACKED. REMOVED COVER IAW AMM.
- [SDR SWAA2014091531996](https://openairdocs.org/sdr/SWAA2014091531996), Sep 13, 2014: LIGHT. CRACKED. R1 DOOR EXIT SIGN MOUNTING LIGHT ASSEMBLY CRACKED. R & R LIGHT ASSEMBLY IAW AMM.
- [SDR SWAA2014091632013](https://openairdocs.org/sdr/SWAA2014091632013), Sep 11, 2014: PANEL. CRACKED. 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), Sep 11, 2014: FLASHLIGHT. MISSING. FORWARD EMER FLASHLIGHT MISSING. INSTALLED FLASHLIGHT IAW AMM.
- [SDR SWAA2014090831685](https://openairdocs.org/sdr/SWAA2014090831685), Sep 7, 2014: BATTERY PACK. DISCHARGED. LEFT MAIN ENTRANCE EMER LIGHT FAILED AT BS 180. REMOVED & INSTALLED BATTERY PACK IAW AMM.
- [SDR SWAA2014090831643](https://openairdocs.org/sdr/SWAA2014090831643), Sep 2, 2014: BATTERY. DISCHARGED. FORWARD OVERWING EXIT DOOR SIGN BATTERY INOPERATIVE. R & R BATTERY IAW AMM.
- [SDR SWAA2014090831642](https://openairdocs.org/sdr/SWAA2014090831642), Aug 30, 2014: WEB. CRACKED. LEFT WING OTBD TE WEB JUST FWD OF AILERON CRACKED. R & R WEB IAW AMM & DWG.
- [SDR SWAA2014090831684](https://openairdocs.org/sdr/SWAA2014090831684), Aug 30, 2014: STRAP. CRACKED. 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), Aug 20, 2014: SKIN. CORRODED. AFT CARGO DOOR CUT OUT LOWER SKIN EDGE CORRODED BETWEEN SKIN LAYERS. REPAIRED SKIN IAW SRM.
- [SDR SWAA2014081930953](https://openairdocs.org/sdr/SWAA2014081930953), Aug 13, 2014: ATTACH FITTING. CRACKED. LEFT WING OTBD AILERON ATTACH FITTING CRACKED. R & R FITTING IAW SRM.
- [SDR SWAA2014090831652](https://openairdocs.org/sdr/SWAA2014090831652), Jul 20, 2014: SKIN. CRACKED. RIGHT ELEVATOR GEARED TAB LOWER SURFACE SKIN CRACKED AT INBD EDGE. REPAIRED TAB IAW AT EA.
- [SDR SWAA2014081830924](https://openairdocs.org/sdr/SWAA2014081830924), Jul 17, 2014: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AT BS 1116, LONGERON 15L. R & R SHEAR TIE IAW DWG.

All 171: https://openairdocs.org/deregistered/N968AT-2026-05-03/reports.md

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