# N956AT: 2000 Boeing 717-200, registration cancelled 2025-09-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 30, 2025
- Status when cancelled: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700)
- Engine: [BMW Rolls BR-700 series](https://openairdocs.org/engine/bmw-rolls-br-700-series) (registry code 09500)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 55018
- Year built: 2000
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 7, 2000
- Certificate issued: June 5, 2025
- Last registry action: June 10, 2025
- Mode S code: AD4B03
- 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/N956AT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=956AT
- Page: https://openairdocs.org/deregistered/N956AT-2025-09-30

From the FAA registry file of November 5, 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 (119, newest 50)

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

- [SDR DALA2019060503400](https://openairdocs.org/sdr/DALA2019060503400), Jun 3, 2019: BATTERY PACK. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS IN THE CABIN ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACKS B5-118 AND B5-230 REF B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP 
- [SDR DALA2019040402154](https://openairdocs.org/sdr/DALA2019040402154), Apr 4, 2019: BATTERY PACK. INOPERATIVE. IT WAS FOUND ON SERVICE CHECK THAT THE FORWARD LEFT & RIGHT OVER WING EXIT DOOR EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR TH
- [SDR DALA2018090605514](https://openairdocs.org/sdr/DALA2018090605514), Sep 3, 2018: COVER. MISSING. EMERGENCY EXIT SIGN COVER IS MISSING AT INTERIOR LOCATION 600. INSTALLED LENS. CHECKS GOOD.
- [SDR DALA2018042002652](https://openairdocs.org/sdr/DALA2018042002652), Apr 19, 2018: STRUCTURE. CRACKED. CRACK WAS INDICATED IN 6 LOCATIONS ON THE RIGHT VERTICAL STAB AREAS. REPAIRED PER PRI 567609-14AD. ER/A, 567609-14AD, MATCHES PRI.
- [SDR DALA2017111608164](https://openairdocs.org/sdr/DALA2017111608164), Nov 16, 2017: BATTERY PACK. INOPERATIVE. DURING A SERVICE CHECK, FOUND THE CEILING MID-CABIN DIRECTIONAL EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IAW AMM 33-51 AND THE OPS CH
- [SDR DALA2017051603895](https://openairdocs.org/sdr/DALA2017051603895), May 15, 2017: BATTERY PACK. INOPERATIVE. DURING A SERVICE CHECK, OVERWING EMERGENCY EXIT LIGHTS WOULD NOT STAY ILLUMINATED. R & R THE BATTERY PACK AT 22CDE IAW AMM 33-51. OPS CHECKED GOOD.
- [SDR DALA2016072805624](https://openairdocs.org/sdr/DALA2016072805624), Jul 27, 2016: BRACKET. BROKEN. LOUD VIBERATION UNDER SEAT 20B. FOUND SUPPORT BRACKET FOR OVERWING TO BODY FAIRING BROKEN BELOW AFT OVERWING EXIT DOOR. FABRICATED AND REPLACED THE BRACKET IAW 
- [SDR DALA2016042003045](https://openairdocs.org/sdr/DALA2016042003045), Apr 19, 2016: BEAM. CRACKED. GALLEY DOOR BEAM IS CRACKED AT THE LOWER HINGE MOUNTING FLANGE, MARKED. REPLACED GALLEY DOOR BEAM AT THE LOWER HINGE MOUNTING FLANGE IAW SRM 51-41-00.
- [SDR DALA2016041702960](https://openairdocs.org/sdr/DALA2016041702960), Apr 16, 2016: FRAME. GOUGED. WHEN REMOVING PANEL FOR ACCESS, FOUND FRAME GOUGED AT BS 1146 ALSO 2 FWD BRACKETS CRACKED AT APPROXIMATELY 1106 IN WALKWAY. REPAIR IAW SRM. REPAIRED DAMAGED FRA
- [SDR DALA2016041602959](https://openairdocs.org/sdr/DALA2016041602959), Apr 15, 2016: SKIN. CRACKED. FUSELAGE SKIN CRACKED, BS 1133 OTBD OF STR 2L AT SHEAR TIE FASTENER, HFEC VERIFIED. REPAIRED SKIN CRACK AT BS Y1133 OTBD OF STR SL IAW ER/A 544353-14AD. SEE NON
- [SDR DALA2016041602958](https://openairdocs.org/sdr/DALA2016041602958), Apr 15, 2016: SKIN. CRACKED. FUSELAGE SKIN CRACKED, BS 1133, OTBD OF STR 2R AT SHEAR TIE FASTENER, HFEC VERIFIED. REPAIRED SKIN CRACK AT BS 1133 OTBD OF STR 2R IAW ER/A 544354-14AD, REV A. 
- [SDR DALA2016041602957](https://openairdocs.org/sdr/DALA2016041602957), Apr 15, 2016: STRINGER. CRACKED. THREE STRINGERS ARE CRACKED AT THE OTBD ENDS INTERNAL OF THE CANTED KEEL. RT BS 675, AND LT BS 675 AND 696. MARKED EXTERNALLY. REMOVED AND REINSTALLED WING TO B
- [SDR DALA2016041602956](https://openairdocs.org/sdr/DALA2016041602956), Apr 15, 2016: FRAME. CORRODED. FRAME CORRODED IN ALC BS 927, BL0. REPLACED FORMER SECTION OF FRAME IN AFT CARGO STA 927 BL0 IAW B717 SRM 53-00-06 REPAIR 2. FORMER WAS FABBED IAW B717 PL 99155
- [SDR DALA2016041602955](https://openairdocs.org/sdr/DALA2016041602955), Apr 15, 2016: FRAME. CORRODED. FRAME CORRODED IN ALC BS 908 BL0. REPLACED FORMER FRAME SECTION IN C2 AT BS 908 BL0 IAW SRM 53-00-06, REPAIR 2, FIG 201. FORMER WAS FABRICATED AND HEAT TREATED 
- [SDR DALA2016041502927](https://openairdocs.org/sdr/DALA2016041502927), Apr 14, 2016: SKIN. DAMAGED. VERTICAL STABILIZER L/E ZFS 52.267, NUMEROUS FASTENERS LOOSE, SEVERAL FASTENERS PULLED THROUGH AND PARTIALLY PULLED THROUGH. REPAIRED VERTICAL STABILIZER L/W FA
- [SDR DALA2016041402894](https://openairdocs.org/sdr/DALA2016041402894), Apr 9, 2016: FRAME. CORRODED. BS 974 AT STRINGER 30 HAS APPROXIMATELY 6" OF CORROSION COMMON TO FRAME. BLENDED CORRODED AREA IAW SRM 53-00-00, FIG 103. FOUND OUT OF LIMITS IAW SRM 53-20-07. 
- [SDR DALA2016041502926](https://openairdocs.org/sdr/DALA2016041502926), Apr 7, 2016: LONGERON. CORRODED. LONGERON 29L IN BS 908-960 IS CORRODED IN SEVERAL AREAS. REMOVED RIVETS ON STR 29L IAW SRM 51-41-02, INSTALLED NEW RIVETS ON STR 29L IAW SRM 51-41-02 BLENDED CO
- [SDR DALA2016041502924](https://openairdocs.org/sdr/DALA2016041502924), Apr 5, 2016: SKIN. CRACKED. FUSELAGE SKIN CRACKED, HFEC VERIFIED, BS 1087 ABOVE STR 14R AT SHEAR TIE FASTENER. REPAIRED FUSELAGE CRACKED SKIN IAW BS 1087, STR 14R IAW ER/A 544359-14.
- [SDR DALA2016041502923](https://openairdocs.org/sdr/DALA2016041502923), Apr 5, 2016: SKIN. CRACKED. FUSELAGE SKIN CRACKED, HFEC VERIFIED, BS 1087 ABOVE STR 14L SHEAR TIE FASTENER. REPAIRED FUSELAGE CRACKED SKIN IAW ER/A 544359-14.
- [SDR DALA2016041402893](https://openairdocs.org/sdr/DALA2016041402893), Apr 5, 2016: SUPPORT. CRACKED. RIGHT SIDE OF CENTER TANK, RBL 45, SEAT TRACK SUPPORT IS CRACKED AT BOTTOM OF SUPPORT, MARKED. REPLACED SEAT TRACK SUPPORT IAW SRM 51-40-02 AND 53-20-51, FIG 1,
- [SDR DALA2016040602654](https://openairdocs.org/sdr/DALA2016040602654), Apr 5, 2016: SEAT TRACK. CORRODED. LT CTR SEAT TRACK BS 148-1053, X=44.5 HAS MULTIPLE DISCREPANCIES. BLENDED LBL 44.5 LT CTR SEAT TRACK, BS 140-STA 200, STA 246-STA 1053. SEAT TRACK IS WITHIN ALL
- [SDR DALA2016040602653](https://openairdocs.org/sdr/DALA2016040602653), Apr 5, 2016: CUSP WEB. CORRODED. AREA OF CORROSION ON OUTER CUSP WEB NEAR S18R APPROXIMATELY BS 207. REPLACED CUSP WEB IAW SRM 51-41-02, PG 1-4, 51-41-05, PG 1.
- [SDR DALA2016040602652](https://openairdocs.org/sdr/DALA2016040602652), Apr 4, 2016: LONGERON. CORRODED. LONGERON 30 IN BS 908-960 HAS SEVERAL AREAS OF CORROSION. BLENDED CORROSION FROM BS 908-960, L30 IN AFT CARGO IAW SRM 53-00-05, REPAIR 3. THICKNESS CHECK PERFOR
- [SDR DALA2015062603952](https://openairdocs.org/sdr/DALA2015062603952), Jun 25, 2015: PIN. DETACHED. L1 DOOR SLIDE PINS WERE DETACHED. REPLACED L-1 DOOR SLIDE AND COMPLETED REQUIRED INSPECTION.
- [SDR DALA2015052003377](https://openairdocs.org/sdr/DALA2015052003377), May 20, 2015: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, NOTED EMERGENCY LIGHTS IN AFT EXIT AND WALKWAY WERE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY AND FUNCTION CHECK WAS GOOD.
- [SDR DALA2015021101162](https://openairdocs.org/sdr/DALA2015021101162), Feb 6, 2015: CUSP WEB. CRACKED. MAIN CABIN, CUSP WEB CRACKED AT BS 655, LBL 54. REPAIRED IAW SRM 53-00-55, REP 4, FIG 223 & DWG 9910151.
- [SDR DALA2015020701010](https://openairdocs.org/sdr/DALA2015020701010), Feb 6, 2015: CUSP WEB. CRACKED. MAIN CABIN CUSP MEMBRANE CRACKED AT STA 717, LBL 49. DAMAGED SECTION REPLACED IAW SRM 53-00-55, REP 4, FIG 219 AND DWG 9910151, REV AL & CH.
- [SDR SWAA2014042227296](https://openairdocs.org/sdr/SWAA2014042227296), Apr 13, 2014: ANGLE. CRACKED. FORMER ANGLE CRACKED AT BS 1050, LONGERON 26L. R & R ANGLE IAW SRM & DWG.
- [SDR SWAA2014042827397](https://openairdocs.org/sdr/SWAA2014042827397), Apr 6, 2014: LIGHT. INOPERATIVE. AFT LOWER EMERGENCY EXIT LIGHT BULB INOPERATIVE. RE-LAMPED BULB IAW MM.
- [SDR SWAA2014042827396](https://openairdocs.org/sdr/SWAA2014042827396), Apr 6, 2014: MOUNT BRACKET. BROKEN. CEILING EMERGENCY LIGHT AT ROW 1 MOUNTING BRACKET BROKEN. R & R LIGHT IAW MM.
- [SDR SWAA2014042227295](https://openairdocs.org/sdr/SWAA2014042227295), Apr 6, 2014: PAN. CORRODED. AFT CARGO DOOR LOWER JAMB PAN CORRODED BETWEEN BS 954 TO BS 970. REPAIRED JAMB PAN IAW SRM.
- [SDR SWAA2014040926955](https://openairdocs.org/sdr/SWAA2014040926955), Apr 6, 2014: PAN. CORRODED. AFT CARGO DOOR CUT OUT LOWER PAN CORRODED BETWEEN BS 954 TO BS 970. REPAIRED PAN IAW SRM.
- [SDR SWAA2014040726892](https://openairdocs.org/sdr/SWAA2014040726892), Apr 5, 2014: SUPPORT. CRACKED. LEFT AILERON NR 4 HINGE UPPER PANEL SUPPORT CRACKED. R & R SUPPORT IAW SRM.
- [SDR SWAA2014040726891](https://openairdocs.org/sdr/SWAA2014040726891), Apr 1, 2014: HINGE. CRACKED. EXTERNAL POWER DOOR HINGE CRACKED. R & R HINGE IAW SRM & DWG.
- [SDR SWAA2014040826939](https://openairdocs.org/sdr/SWAA2014040826939), Mar 7, 2014: SKIN. CRACKED. LEFT WING NR 5 SLAT CTR TRACK SKIN CUT OUT FIXED LE CRACKED. REPAIRED SKIN IAW SRM.
- [SDR SWAA2014031826173](https://openairdocs.org/sdr/SWAA2014031826173), Mar 6, 2014: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 223GF DAMAGED. R & R PANEL IAW SRM.
- [SDR SWAA2014031826198](https://openairdocs.org/sdr/SWAA2014031826198), Mar 5, 2014: FLOOR PANEL. DELAMINATED. CENTER FLOOR PANEL 211ALF IN FLIGHT COMPARTMENT DELAMINATED. R & R PANEL IAW SRM & DWG.
- [SDR SWAA2014040726909](https://openairdocs.org/sdr/SWAA2014040726909), Mar 4, 2014: SKIN. CORRODED. AFT PRESS BULKHEAD FWD FACE BULKHEAD SKIN CORRODED AT FS 1053, BETWEEN LONGERON 30R TO LONGERON 29R. REPAIRED SKIN IAW SRM.
- [SDR SWAA2014040326779](https://openairdocs.org/sdr/SWAA2014040326779), Mar 4, 2014: WEB. CRACKED. WEB CRACKED AT BS 200, LBL 7. REPAIRED WEB IAW SRM & EA.
- [SDR SWAA2014030725863](https://openairdocs.org/sdr/SWAA2014030725863), Feb 28, 2014: CUSP WEB. DAMAGED. CUSP WEB DAMAGED AT BS 219, RBL 44.5. REPAIRED WEB IAW SRM.
- [SDR SWAA2014031426051](https://openairdocs.org/sdr/SWAA2014031426051), Feb 27, 2014: FLOOR SUPPORT. CORRODED. CABIN FLOOR SUPPORT BEAM CORRODED AT STATION 160 TO STATION 200, LBL 7. R & R SUPPORT IAW SRM.
- [SDR SWAA2014030725834](https://openairdocs.org/sdr/SWAA2014030725834), Feb 27, 2014: FLOOR SUPPORT. CORRODED. CABIN FLOOR SUPPORT BEAM CORRODED BETWEEN BS 160 TO BS 200, RBL 10. R & R BEAM IAW SRM & DRAWING.
- [SDR SWAA2014030625808](https://openairdocs.org/sdr/SWAA2014030625808), Feb 27, 2014: FLOOR SUPPORT. CORRODED. CABIN FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 10 TO RBL 44. R & R SUPPORT IAW SRM & DRAWING.
- [SDR SWAA2014030625809](https://openairdocs.org/sdr/SWAA2014030625809), Feb 27, 2014: SEAT TRACK. CORRODED. CABIN SEAT TRACK CORRODED AT BS 237, RBL 44. R & R SEAT TRACK IAW SRM.
- [SDR SWAA2014031726126](https://openairdocs.org/sdr/SWAA2014031726126), Feb 22, 2014: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD DELAMINATED 222BF. R & R PANEL IAW SRM.
- [SDR SWAA2014031726125](https://openairdocs.org/sdr/SWAA2014031726125), Feb 22, 2014: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL GF DELAMINATED. R & R PANEL IAW SRM.
- [SDR SWAA2014031726124](https://openairdocs.org/sdr/SWAA2014031726124), Feb 22, 2014: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 222DF DELAMINATED. R & R PANEL IAW SRM.
- [SDR SWAA2014040926958](https://openairdocs.org/sdr/SWAA2014040926958), Feb 18, 2014: BULKHEAD. CORRODED. AFT FUSELAGE PRESS BULKHEAD FWD FACE CORRODED BETWEEN ROW 26L TO ROW 26R. R & R BULKHEAD IAW SRM & DWG.
- [SDR SWAA2014040726908](https://openairdocs.org/sdr/SWAA2014040726908), Feb 15, 2014: PAN. CORRODED. AFT CARGO DOOR LOWER JAMB PAN CORRODED BETWEEN BS 954 TO BS 970. REPAIRED PAN IAW SRM.
- [SDR SWAA2014040726907](https://openairdocs.org/sdr/SWAA2014040726907), Feb 15, 2014: PAN. CORRODED. FORWARD CARGO DOOR LOWER JAMB CORRODED BETWEEN BS 417 TO BS 425. R & R PAN IAW SRM.

All 119: https://openairdocs.org/deregistered/N956AT-2025-09-30/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ATL07LA016](https://openairdocs.org/ntsb/ATL07LA016), Nov 11, 2006: Boeing 717-200 (N956AT), Memphis, TN, substantial damage. Probable cause: The captain's inadequate visual look out during taxi.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20061110031149A](https://openairdocs.org/incident/20061110031149A), Nov 10, 2006: Boeing 717200 (N956AT), Memphis, TN, Substantial damage. (-23) The accident airplane was directed by Memphis tower to land on runway 36 right. After landing the airplane was to turn left at the next intersection and…
- [Incident 20040217008249I](https://openairdocs.org/incident/20040217008249I), Feb 17, 2004: Boeing 717200 (N956AT), Buffalo, NY. (-23) On February 17, 2004, at 1134 am EDT, a Boeing 717, N956AT, flight 558, operated by air tran airlines landed on runway 23 at Buffalo international…

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.