# N975AT: 2002 Boeing 717-200, registration cancelled 2025-11-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 19, 2025 - 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: 55035 - Year built: 2002 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 20, 2002 - Certificate issued: November 20, 2023 - Last registry action: November 29, 2023 - Mode S code: AD964A - 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: Individual - 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/N975AT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=975AT - Page: https://openairdocs.org/deregistered/N975AT-2025-11-19 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 (122, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA2019040800000](https://openairdocs.org/sdr/DALA2019040800000), Apr 8, 2019: SKIN. DELAMINATED. SPOILER SKIN, UNSCHEDULED REMOVAL. FOUND DELAMINATED. - [SDR DALA2018070204300](https://openairdocs.org/sdr/DALA2018070204300), Jul 2, 2018: RELAY. FAULTY. 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 PE - [SDR DALA2017090306564](https://openairdocs.org/sdr/DALA2017090306564), Sep 2, 2017: CUSP WEB. CORRODED. 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), Dec 22, 2016: HINGE. DAMAGED. 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, AN - [SDR DALA2016122109992](https://openairdocs.org/sdr/DALA2016122109992), Dec 20, 2016: SKIN. CRACKED. 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 S - [SDR DALA2016122009962](https://openairdocs.org/sdr/DALA2016122009962), Dec 19, 2016: STIFFENER. CRACKED. 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 003 - [SDR DALA2016122009961](https://openairdocs.org/sdr/DALA2016122009961), Dec 19, 2016: SUPPORT. CRACKED. 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 P - [SDR DALA2016121809948](https://openairdocs.org/sdr/DALA2016121809948), Dec 17, 2016: SUPPORT. CRACKED. 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), Dec 17, 2016: ANGLE. CRACKED. 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), Dec 16, 2016: LONGERON. CRACKED. 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- - [SDR DALA2016121709942](https://openairdocs.org/sdr/DALA2016121709942), Dec 16, 2016: BULKHEAD WEB. CRACKED. 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), Dec 15, 2016: LONGERON. CRACKED. 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), Dec 15, 2016: FRAME. CRACKED. 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), Dec 13, 2016: SUPPORT. CRACKED. 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), Dec 13, 2016: ACCESS PANEL. CORRODED. 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, COUNTERSIN - [SDR DALA2016121409832](https://openairdocs.org/sdr/DALA2016121409832), Dec 13, 2016: FRAME. CRACKED. 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 51-10-0 - [SDR DALA2016121409831](https://openairdocs.org/sdr/DALA2016121409831), Dec 13, 2016: FITTING. CRACKED. 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), Dec 12, 2016: CUSP WEB. CRACKED. 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), Dec 12, 2016: BEAM. CRACKED. 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), Dec 12, 2016: BEAM. CRACKED. 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), Dec 12, 2016: FRAME. CRACKED. 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), Dec 12, 2016: DOOR FRAME. CRACKED. CRACKED DOOR FRAME WEB BS 207 LONGERON 11 AND 15L. REPAIRED IAW SRM 53-10-15. - [SDR DALA2016121209753](https://openairdocs.org/sdr/DALA2016121209753), Dec 11, 2016: SKIN. DELAMINATED. 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), Dec 11, 2016: CUSP WEB. CRACKED. 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), Dec 11, 2016: CUSP WEB. CRACKED. 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), Dec 9, 2016: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 211ALF. THE FLOOR PANEL WAS FABRICATED AND REPLACED IAW SRM 53-20-50. - [SDR DALA2016121009802](https://openairdocs.org/sdr/DALA2016121009802), Dec 9, 2016: FLOOR PANEL. DELAMINATED. DELAMINATION ON FLOOR PANEL. THE FLOOR PANEL WAS FABRICATED AND REPLACED IAW SRM 53-20-50. - [SDR DALA2016120909746](https://openairdocs.org/sdr/DALA2016120909746), Dec 8, 2016: PAN. CRACKED. 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), Dec 8, 2016: PAN. CRACKED. 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), Dec 8, 2016: PAN. CRACKED. 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), Dec 8, 2016: PAN. CRACKED. 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), Dec 8, 2016: PAN. CRACKED. 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), Dec 8, 2016: PAN. CRACKED. 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 FI - [SDR DALA2016120909721](https://openairdocs.org/sdr/DALA2016120909721), Dec 8, 2016: CUSP WEB. PUNCTURED. 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 WE - [SDR 2016F00131](https://openairdocs.org/sdr/2016F00131), May 31, 2016: SKIN. DELAMINATED. 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), May 31, 2016: SKIN. DELAMINATED. DURING ROUTINE MAINTANANCE INSPECTION, LT SPOILER FOUND WITH DELAMINATION ALONG THE UPPER AND LOWER SURFACE. - [SDR DALA2017033003179](https://openairdocs.org/sdr/DALA2017033003179), Mar 29, 2016: SKIN. DAMAGED. 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 E - [SDR DALA2016101007123](https://openairdocs.org/sdr/DALA2016101007123), Dec 14, 2015: SKIN. CRACKED. 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), May 10, 2015: CABLE. FRAYED. 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), Nov 6, 2014: BATTERY PACK. INOPERATIVE. 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), Dec 29, 2013: LENS. CRACKED. R1 DOOR EXIT LIGHT LENS CRACKED. R & R LENS ASSEMBLY IAW AMM. - [SDR SWAA2014010823898](https://openairdocs.org/sdr/SWAA2014010823898), Dec 27, 2013: WIRE. LOOSE. RT OVERWING EMERGENCY EXIT LIGHT WIRE LOOSE. SECURED WIRE IAW AMM. - [SDR SWAA2014010823897](https://openairdocs.org/sdr/SWAA2014010823897), Dec 27, 2013: WIRE. LOOSE. LT OVERWING EMERGENCY EXIT LIGHT WIRE LOOSE. SECURED WIRE IAW AMM. - [SDR SWAA2014010223698](https://openairdocs.org/sdr/SWAA2014010223698), Dec 27, 2013: WIRE. DISCONNECTED. LT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RECONNECTED WIRE IAW WDM. - [SDR SWAA2013122723652](https://openairdocs.org/sdr/SWAA2013122723652), Dec 21, 2013: BATTERY PACK. DISCHARGED. OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. R & R OVERWING EMERGENCY LIGHTS BATTERY PACK IAW MM. - [SDR SWAA2013122623635](https://openairdocs.org/sdr/SWAA2013122623635), Dec 21, 2013: LIGHT. INOPERATIVE. AFT CABIN EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM. - [SDR SWAA2013121823493](https://openairdocs.org/sdr/SWAA2013121823493), Dec 9, 2013: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED BETWEEN STATION 619 & 636, BL 0. R & R INTERCOSTAL IAW SRM. - [SDR SWAA2013112522752](https://openairdocs.org/sdr/SWAA2013112522752), Nov 13, 2013: STRINGER SPLICE. CRACKED. STRINGER SPLICE 6R DAMAGED & CRACKED AT BS 246. R & R STRINGER SPLICE IAW SRM. - [SDR SWAA2013120222832](https://openairdocs.org/sdr/SWAA2013120222832), Nov 8, 2013: CREASE BEAM. CORRODED. CREASE BEAM WEB CORRODED BETWEEN STATION 598 TO STATION 617, STRINGER 18L. REPAIRED WEB IAW SRM. - [SDR SWAA2013121223247](https://openairdocs.org/sdr/SWAA2013121223247), Oct 28, 2013: LONGERON. CRACKED. LONGERON CRACKED AT STATION 1133, LONGERON 2R. R & R LONGERON IAW SRM. All 122: https://openairdocs.org/deregistered/N975AT-2025-11-19/reports.md --- 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.