# N972AT: 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: [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: 55033
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 31, 2002
- Certificate issued: November 24, 2023
- Last registry action: November 24, 2023
- Mode S code: AD8B25
- 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/N972AT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=972AT
- Page: https://openairdocs.org/deregistered/N972AT-2026-05-03

From the FAA registry file of November 4, 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 (167, newest 50)

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

- [SDR 2019F00230](https://openairdocs.org/sdr/2019F00230), Jun 29, 2019: SKIN. DELAMINATED. SPOILER SKIN DELAMINATED.
- [SDR DALA2019030901599](https://openairdocs.org/sdr/DALA2019030901599), Mar 8, 2019: RETAINER. CRACKED. PILOTS SIDE FIXED WINDOW RETAINER IS CRACKED AT AFT SIDE OF JAMB LOWER CORNER. NRC 001-0246:0593-2001/010 00193: REPAIR COMPLIED WITH PER ER/A 576131-14 REV O. 
- [SDR DALA2019030901598](https://openairdocs.org/sdr/DALA2019030901598), Mar 8, 2019: RETAINER. CRACKED. CO-PILOTS SIDE FIXED WINDOW RETAINER IS CRACKED AT AFT SIDE OF JAMB LOWER CORNER. NRC 001-0246:0593-2001/011 00194: REPAIR COMPLIED WITH PER ER/A 576171-14 REV 
- [SDR DALA2018090405390](https://openairdocs.org/sdr/DALA2018090405390), Sep 2, 2018: COVER. MISSING. MID CABIN EMERGENCY LIGHT COVER IS MISSING. MAINTENANCE INSTALLED THE MISSING COVER. OK FOR SERVICE.
- [SDR DALA2018062604205](https://openairdocs.org/sdr/DALA2018062604205), Jun 25, 2018: BATTERY PACK. DISCHARGED. OVERWING EXIT DOOR EMERGENCY CEILING LIGHT FAILED TO TEST. MAINTENANCE FOUND B5-120 BATTERY PACK TO BE BAD. BATTERY PACK WAS REPLACED PER AMM 33-51. OPERATIONAL
- [SDR DALA2017092207032](https://openairdocs.org/sdr/DALA2017092207032), Sep 21, 2017: POWER SUPPLY. INOPERATIVE. AFT EMERGENCY DOOR EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY POWER SUPPLY IAW AMM 33-51.
- [SDR DALA2017032102230](https://openairdocs.org/sdr/DALA2017032102230), Mar 20, 2017: PAN. CORRODED. AFT CARGO DOOR CUTOUT, FWD EDGE BS 954 IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 1A. ACCOMPLISHED DOOR PAN SPLICE REPAIR IAW
- [SDR DALA2017032102229](https://openairdocs.org/sdr/DALA2017032102229), Mar 18, 2017: LONGERON. CRACKED. LONGERON 16L CRACKED AT BS 1022. REPLACED THE LONGERON IAW SRM 53-00-05, REPAIR 2.
- [SDR DALA2017032002228](https://openairdocs.org/sdr/DALA2017032002228), Mar 15, 2017: NOT REPORTED. CORRODED. BS 954 CORROSION. FOUND OUT OF LIMITS IAW SRM 53-00-00 FIG 103.0 . REPLACED THE SPLICE IAW SRM 51-41-05 AND DWG 9958214.
- [SDR DALA2017032002227](https://openairdocs.org/sdr/DALA2017032002227), Mar 15, 2017: SEAT TRACK. CORRODED. BS 994 TO 1028 SEAT TRACK CORRODED. . REPLACED THE SEAT TRACK IAW SRM 51-41-01, 51-41-05.
- [SDR DALA2017031302011](https://openairdocs.org/sdr/DALA2017031302011), Mar 10, 2017: FLOORBEAM. CORRODED. CORROSION ON THE LOWER SURFACE OF THE FORWARD CABIN SUBFLOOR (E/E CEILING) ON THE AFT SIDE OF FLOORBEAM AT STA 200, FROM BL5R TO BL9R. REPAIRED SUB FLOOR CORROS
- [SDR DALA2017031101951](https://openairdocs.org/sdr/DALA2017031101951), Mar 10, 2017: SEAT TRACK. DAMAGED. SEAT TRACK, RBL 44.5, BS 465 - 565, HAS AREAS OF GOUGING AND CORROSION. BLENDED CORROSION OUT OF LIMITS. REPAIRED IAW SRM 53-20-52 REPAIR 1, RESTORED TOP COAT I
- [SDR DALA2017031101950](https://openairdocs.org/sdr/DALA2017031101950), Mar 10, 2017: FLOORBEAM. CORRODED. CORROSION ON THE LOWER SURFACE OF THE FORWARD CABIN SUBFLOOR (E/E CEILING) ON THE FORWARD SIDE OF FLOORBEAM AT BS 146 AT RBL 7, AND AT BS 157 AT RBL 5. BLENDED 
- [SDR DALA2017031101949](https://openairdocs.org/sdr/DALA2017031101949), Mar 10, 2017: SEAT TRACK. DAMAGED. SEAT TRACK RBL 44.5 IS CORRODED, AND GOUGED BS 332 - 408. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS AT BS 361. REPAIRED IAW SRM 53-20-52-2R REPAIR.
- [SDR DALA2017031101948](https://openairdocs.org/sdr/DALA2017031101948), Mar 10, 2017: FLOOR SUPPORT. CORRODED. FORWARD CABIN BS 157 - 180, LBL 44 FLOOR SUPPORT CORRODED. REMOVED THE CORROSION IAW SRM 53-00-00 ALLOWABLE DAMAGE 1. FOUND TO BE BEYOND ALLOWABLE LIMITS. REPLA
- [SDR DALA2017031101947](https://openairdocs.org/sdr/DALA2017031101947), Mar 10, 2017: FLOORBEAM. CRACKED. FLOORBEAM BS 737, LBL 44 IS CRACKED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-41-02 AND 51-41-05.
- [SDR DALA2017031101946](https://openairdocs.org/sdr/DALA2017031101946), Mar 10, 2017: INTERCOSTAL. CRACKED. INTERCOSTAL BETWEEN UPPER FLOORBEAMS IN FORWARD CARGO BSW 617 - 636 CRACKED. REPAIRED THE INTERCOSTAL IAW SRM 51-70-10 REPAIR 1.
- [SDR DALA2017031101963](https://openairdocs.org/sdr/DALA2017031101963), Mar 10, 2017: SHEAR TIE. CRACKED. BS 1136, LONGERON 15R SHEAR TIE IS CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-05, SRM 51-40-08, AND DWG 5913596.
- [SDR DALA2017031101962](https://openairdocs.org/sdr/DALA2017031101962), Mar 10, 2017: SEAT TRACK. CORRODED. UPPER CABIN SEAT TRACK CORRODED AT BS 468 RBL 44.5. BLENDED OUT OF LIMITS. REPAIRED IAW 53-20-52, REPAIR .
- [SDR DALA2017031101961](https://openairdocs.org/sdr/DALA2017031101961), Mar 10, 2017: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT BS 148 - 157, BL0 CORRODED. CLEANED THE CORROSION ON FLOOR SUPPORT IAW SRM 53-00-00-1A, FIG 103, 53-10-51-0I-2, AND 51-30-07-06, FIG 9 BEYOND ALLO
- [SDR DALA2017031101960](https://openairdocs.org/sdr/DALA2017031101960), Mar 10, 2017: CUSP WEB. CORRODED. RIGHT CUSP WEB, BS 518, RBL 54.5 CORRODED. REPAIRED THE CUSP WEB IAW SRM 53-08-35-2R-4, AND 53-20-51-01-1.
- [SDR DALA2017031101959](https://openairdocs.org/sdr/DALA2017031101959), Mar 10, 2017: CUSP WEB. CORRODED. RIGHT CUSP WEB, BS 598 TO 617, RBL 54.5 CORRODED. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4.
- [SDR DALA2017031101958](https://openairdocs.org/sdr/DALA2017031101958), Mar 10, 2017: CUSP WEB. CRACKED. RIGHT CUSP WEB IS CRACKED AT BS 216, RBL 45. CUT OUT CRACKED AREA IAW SRM 53-00-00-2R 1 & 2. FABRICATED A REPAIR DOUBLER & FILLER IAW SRM 53-00-00 2 R2, AND INS
- [SDR DALA2017031101957](https://openairdocs.org/sdr/DALA2017031101957), Mar 10, 2017: SEAT TRACK. DAMAGED. RIGHT CENTER SEAT TRACK, RBL 44.5, BS 200 - 256, GOUGED AND CORRODED. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-20-52-2R REPAIR 1.
- [SDR DALA2017031101956](https://openairdocs.org/sdr/DALA2017031101956), Mar 10, 2017: SEAT TRACK. CORRODED. RIGHT INBD SEAT TRACK, RBL 22, BS 200 - 256 IS GOUGED AND HAS AREAS OF CORROSION. THE SEAT TRACK WAS FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-20-52-2R REPAIR 1.
- [SDR DALA2017031101955](https://openairdocs.org/sdr/DALA2017031101955), Mar 10, 2017: CUSP WEB. CORRODED. RIGHT CUSP WEB CORRODED RBL 44 BS 201. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55-1A-1. PERFORMED TYPICAL REPAIR ON THE CUSP WEB IAW SRM 5
- [SDR DALA2017031101954](https://openairdocs.org/sdr/DALA2017031101954), Mar 10, 2017: SEAT TRACK. DAMAGED. LEFT CENTER SEAT TRACK, LBL 44.5, BS 986 - 1053 HAS AREAS SCRATCHED AND LIGHT CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, REPAIRED IAW SRM 53-20
- [SDR DALA2017031101953](https://openairdocs.org/sdr/DALA2017031101953), Mar 10, 2017: SEAT TRACK. DAMAGED. LEFT CENTER SEAT TRACK BS 756 - 856, LBL 44.5, HAS CORRODED, SCRATCHED, AND GOUGED. BLENDED THE SEAT TRACK AND FOUND OUT OF LIMITS IAW SRM 53-20-52-1A. REPLACED
- [SDR DALA2017031101952](https://openairdocs.org/sdr/DALA2017031101952), Mar 10, 2017: CUSP WEB. CORRODED. BS 889 - 908 CUSP WEB AND ANGLE SPLICE LT SIDE CORRODED. REMOVED CORROSION, AND FOUND OUT OF LIMITS IAW SRM 53-00-55. REPLACED THE CUSP WEB IAW SRM 53-00-55, AN
- [SDR DALA2017032002226](https://openairdocs.org/sdr/DALA2017032002226), Mar 8, 2017: FLOOR SUPPORT. CORRODED. FORWARD FUSELAGE FLOOR SUPPORT BS 202-218, 221-239, LBL 14 CORRODED. REPLACED THE FLOOR SUPPORT IAW DWG 9936535.
- [SDR DALA2017030801866](https://openairdocs.org/sdr/DALA2017030801866), Mar 7, 2017: CUSP WEB. CORRODED. FUSELAGE, CABIN, RT CUSP WEB, STA 487 R54.5, UNDERSIDE, CORROSION. REPAIRED CUSP WEB STA 389-503 RT SIDE IAW SRM 53-00-55 2R-4. FABRICATED AND INSTALLED 7075-T6
- [SDR DALA2017030801865](https://openairdocs.org/sdr/DALA2017030801865), Mar 7, 2017: CUSP WEB. CORRODED. FUSELAGE, CABIN, RT CUSP WEB, STA 584 R56.0 AT DOUBLER, UNDERSIDE CORROSION. REPAIRED DAMAGED CUSP 584 RT SIDE, IAW SRM 53-00-55 REPAIR 4.
- [SDR DALA2017031802190](https://openairdocs.org/sdr/DALA2017031802190), Mar 6, 2017: SEAT TRACK. CORRODED. RIGHT INBOARD SEAT TRACK BL22R STATIONS 465-565 HAS AREAS OF GOUGES AND CORROSION. BLENDED AREA AT VL 22R STA 489-491 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2
- [SDR DALA2017030701860](https://openairdocs.org/sdr/DALA2017030701860), Mar 6, 2017: DOUBLER. CORRODED. FUSELAGE, CABIN, RT STA 889 TO 908 R56.0, SPLICE DOUBLER, UNDERSIDE, CORROSION. REPLACED LOWER SKIN SPLICE DOUBLER AT STA 889-908 IAW SRM 51-41-05.
- [SDR DALA2017030701859](https://openairdocs.org/sdr/DALA2017030701859), Mar 6, 2017: STRUCTURE. CORRODED. SUB FLOOR AT STA 157 BL5R CORRODED ON LOWER SURFACE. REPAIRED CORRODED AREA ON SUB FLOOR STA 157 BL5R IAW 51-70-10-2R-2 AND SRM 51-41-02 PG 3 PAR F.
- [SDR DALA2017030801862](https://openairdocs.org/sdr/DALA2017030801862), Mar 3, 2017: DOUBLER. CORRODED. STA 870-889 CORROSION WAS FOUND ON EXISTING CUSP WEB REPAIR DOUBLER AND WAS FOUND TO BE OUT OF LIMITS IAW 51-00-00 .015" MATERIAL REMOVED. REMOVED AND INSTALLED
- [SDR DALA2017030701857](https://openairdocs.org/sdr/DALA2017030701857), Mar 3, 2017: MEMBRANE. CRACKED. FWD FLOOR CUSP MEMBRANE CRACKED IN EXISTING REPAIR DOUBLER AT FS190 RBL8. MARKED. REPLACED FWD FLOOR CUSP MEMBRANE REPAIR DOUBLER AT FS 190RBL 8 IAW SRM 51-40-0
- [SDR DALA2017030801864](https://openairdocs.org/sdr/DALA2017030801864), Mar 2, 2017: CUSP WEB. CORRODED. STA 908-927 CORROSION ON BOTH SIDES OF CUSP LT SIDE. INSTALLED EXTERNAL AND RING DOUBLER REPAIR LT CUSP WEB STA 913 FOR BLENDS OUT OF LIMITS REF SRM 53-00-55-2R
- [SDR DALA2017030801863](https://openairdocs.org/sdr/DALA2017030801863), Mar 2, 2017: FORMER. CRACKED. FORMER IS CRACKED JUST ABOVE LONGERON 15L AND STA 1022. REPLACED SHEAR TIE / FORMER WITH NEW SHEAR TIE / FORMER IAW SRM 51-41-02, 51-41-05, AND DRAWING 99122434
- [SDR DALA2017030201698](https://openairdocs.org/sdr/DALA2017030201698), Feb 28, 2017: PAN. CRACKED. FLC DOOR LOWER FWD CORNER HAS A CRACK ON DOOR PAN.
- [SDR DALA2016121609908](https://openairdocs.org/sdr/DALA2016121609908), Dec 15, 2016: POWER SUPPLY. NO TEST. DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING L2-791 WAS NOT TESTING. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED 
- [SDR DALA2016071505297](https://openairdocs.org/sdr/DALA2016071505297), Jul 15, 2016: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE CABIN SERVICE DOOR EMERGENCY LIGHT IN THE CEILING WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE L
- [SDR DALA2016032402269](https://openairdocs.org/sdr/DALA2016032402269), Mar 24, 2016: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE P
- [SDR DALA2015072004568](https://openairdocs.org/sdr/DALA2015072004568), Jul 19, 2015: CUSP WEB. CRACKED. CUSP MEMBRANE FOUND CRACKED AT BS 674. REPAIRED IAW ER/A 533035-14MA.
- [SDR DALA2015071904567](https://openairdocs.org/sdr/DALA2015071904567), Jul 18, 2015: DOOR FRAME. CRACKED. RT OVERWING FRAME CRACKED IN RADIUS OVER .125 CONDITION 3 FOUND. REPLACED FRAME IAW AMDS WC 5310-01436-03B.
- [SDR SWAA2014111334121](https://openairdocs.org/sdr/SWAA2014111334121), Nov 13, 2014: HOLDER. LOOSE. L2 DOOR EMER EVAC SLIDE GIRT BAR HOLDER LOOSE. R & R HOLDER ASSEMBLY IAW SIP.
- [SDR SWAA2014111033964](https://openairdocs.org/sdr/SWAA2014111033964), Nov 7, 2014: FLASHLIGHT. OUT OF POSITION. FORWARD ENTRY DOOR FLASHLIGHT CHARGE INDICATOR LIGHT INOPERATIVE. REPOSITIONED FLASHLIGHT IN HOLDER IAW AMM.
- [SDR SWAA2014102833391](https://openairdocs.org/sdr/SWAA2014102833391), Oct 28, 2014: LIGHT. BROKEN. EMERGENCY EXIT LIGHT BROKEN AT CEILING PANEL ROW 1. R & R EXIT LIGHT ASSEMBLY IAW MM.
- [SDR SWAA2014072230210](https://openairdocs.org/sdr/SWAA2014072230210), Jul 19, 2014: BATTERY PACK. DISCHARGED. AFT OVERHEAD EMER EXIT SIGN INOPERATIVE AFTER TEST. R & R BATTERY PACK IAW MM.
- [SDR SWAA2014061829140](https://openairdocs.org/sdr/SWAA2014061829140), Jun 17, 2014: FASTENER. LOOSE. R1 DOOR EMER EVAC SLIDE GIRT BAR HOLDER LOOSE. R & R FASTENER IAW AMM.

All 167: https://openairdocs.org/deregistered/N972AT-2026-05-03/reports.md

## FAA accident and incident reports (1)

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.

- [Incident 20100812043589I](https://openairdocs.org/incident/20100812043589I), Aug 12, 2010: Boeing 717-200 (N972AT), Vandalia, OH, Minor damage. Crew stated per aircraft log page #1652769: "climbing through 17,000 ft, observed a lt eng gen off alert and a loud bang followed by a violent shaking of the…

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