# N958AT: 2001 Boeing 717-200, registration cancelled 2025-04-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 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: 55020 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 20, 2001 - Certificate issued: November 29, 2023 - Last registry action: November 29, 2023 - Mode S code: AD5271 - 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/N958AT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=958AT - Page: https://openairdocs.org/deregistered/N958AT-2025-04-30 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 (208, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA2019120307004](https://openairdocs.org/sdr/DALA2019120307004), Dec 3, 2019: BATTERY PACK. INOPERATIVE. THE EMERGENCY LIGHTS ARE OUT IN THE FIRST CLASS & COMFORT PLUS SECTIONS OF THE CABIN. MAINTENANCE REPLACED THE BATTERY PACK, B5-227, IAW AMM 33-51-03. OPS CHECK - [SDR DALA2019090905218](https://openairdocs.org/sdr/DALA2019090905218), Sep 8, 2019: POWER SUPPLY. INOPERATIVE. ALL EMERGENCY LIGHT IN CEILING AFT OF ROW 23 DO NOT TEST. MAINTENANCE REPLACED THE CABIN EMERGENCY LIGHT POWER SUPPLY POS B5-231 AND REPLACED THE COMPLETE EMERG - [SDR DALA2019061703592](https://openairdocs.org/sdr/DALA2019061703592), Jun 15, 2019: TIRE. FAILED. THE CREW RETURNED TO THE DEPARTURE AIRPORT FOLLOWING THE #2 TIRE FAILURE ON TAKEOFF ROTATION. CORRECTIVE ACTION: MAINTENANCE REPLACED BOTH THE #1 AND #2 TIRES. - [SDR DALA2019032901985](https://openairdocs.org/sdr/DALA2019032901985), Mar 29, 2019: BATTERY PACK. DISCHARGED. THE FORWARD DOORS AND FIRST ROW OF OVERWING EMERGENCY EXIT SIGNS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR THE EMERGENCY LIGHTS IAW AMM 33-51. - [SDR DALA2019030601503](https://openairdocs.org/sdr/DALA2019030601503), Jan 13, 2019: SKIN. DAMAGED. ABRASION TO THE FUSELAGE SKIN; STATION 427-434, FORWARD CARGO DOOR CUT-OUT (LOWER CORNER, AFT). REMOVED ALL PAINT, PRIMER, AND SEALANT IN AREA. REMOVED NEGLIGIB - [SDR DALA2019030601502](https://openairdocs.org/sdr/DALA2019030601502), Jan 13, 2019: DOOR FRAME. DAMAGED. DAMAGE TO FWD CARGO DOOR CUT-OUT LOWER EDGE AT STATION 408. INSTALLED DOUBLER AND TRIPLER REPAIR PER ER/A 574411-14 REV ORG. SECTION II. INSTALLED NEW SCUFF PLA - [SDR DALA2018112306745](https://openairdocs.org/sdr/DALA2018112306745), Nov 22, 2018: BOTTLE. LOW PRESSURE. TAIL CONE SLIDE BOTTLE IN THE RED. REMOVED SLIDE S/N 1277 & INSTALLED SLIDE S/N 1399 PER AMDS WORK CARD 2561-9006. (LP5175880) - [SDR DALA2017081406170](https://openairdocs.org/sdr/DALA2017081406170), Aug 11, 2017: LENS. DAMAGED. EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED. REPAIRED THE LENS. OK FOR SERVICE. - [SDR DALA2016092606848](https://openairdocs.org/sdr/DALA2016092606848), Sep 24, 2016: LONGERON. DAMAGED. LEFT FUSELAGE LONGERON L26 DAMAGED BETWEEN Y351 AND Y370. REMOVED DAMAGED SECTION, FABRICATED NEW STR FROM FACTORY SPLICE POINT Y380-Y408 TO NEW POINT Y351-Y370 - [SDR DALA2016071805437](https://openairdocs.org/sdr/DALA2016071805437), Jul 18, 2016: SUPPORT. CRACKED. CRACKED BULKHEAD DIVISOR SUPPORT, STA Y=655, X=22Z=-10 AT FORWARD CARGO COMPARTMENT. BULKHEAD DIVISOR SUPPORT STA Y=655, X=22 Z=-10 WAS REPAIRED WITH ER/A 54788 - [SDR DALA2016071805349](https://openairdocs.org/sdr/DALA2016071805349), Jul 17, 2016: PAN. CRACKED. CRACK ON OUTER PAN STA Y=954, BEAM 1 FORWARD EDGE AT AFT CARGO COMPARTMENT DOOR, C2, CARD 11, ZONE 810. PAN WAS REPAIRED IAW ETI-17-16-081 AND ER/A 547860-14, R - [SDR DALA2016071805348](https://openairdocs.org/sdr/DALA2016071805348), Jul 17, 2016: BEAM. CRACKED. CRACKED BEAM 1 ON FORWARD EDGE OF AFT CARGO COMPARTMENT STA Y=954, REF CARD 11, ZONE 810, CARD 45 ZONE 810. BEAM 1 WAS REPAIRED IAW ETI-17-16-081 REV 2 AND ER/A - [SDR DALA2016071805346](https://openairdocs.org/sdr/DALA2016071805346), Jul 17, 2016: BEAM. CRACKED. CRACKED DOOR JAMB BEAM STA Y=47, RT SIDE AT NLG WW. DOOR JAMB BEAM WAS REPAIRED. ER/A 547858-14, REV ORIGINAL. - [SDR DALA2016071705345](https://openairdocs.org/sdr/DALA2016071705345), Jul 17, 2016: FITTING. CRACKED. CRACKED CLIP AT STA Y=1152 BETWEEN LONGERONS 3R/2R. CLIP WAS REPLACED IAW ER/A 547861-14 REV ORIGINAL. - [SDR DALA2016071705344](https://openairdocs.org/sdr/DALA2016071705344), Jul 17, 2016: SKIN. WORN. WORN RT WING LOWER SKIN BETWEEN STA SXR 69 AND XRS 111.500. REPAIR OF WORN AREA AT RT WING LOWER SKIN WAS PERFORMED WITH ER/A 547869-14, REV ORIGINAL. - [SDR DALA2016071705343](https://openairdocs.org/sdr/DALA2016071705343), Jul 16, 2016: DOOR FRAME. CORRODED. CORROSION ON LOWER DOOR JAMB FROM STA Y=954 TO Y=994 AT AFT CARGO COMPARTMENT, SM, C2, CARD 27, ZONE 810. DUE TO EXCESIVE CORROSION WAS REPLACED IAW SRM 53-20-1 - [SDR DALA2016071705342](https://openairdocs.org/sdr/DALA2016071705342), Jul 16, 2016: SKIN. CRACKED. WEAR AND CRACK ON OUTER SKIN STA Y=972 BETWEEN BEAM 1 AND 2 JUST ABOVE OF HANDLE RELEASE AT AFT CARGO COMPARTMENT DOOR. SKIN STA Y=972 BETWEEN BEAM 1 AND 2 JUST - [SDR DALA2016071705341](https://openairdocs.org/sdr/DALA2016071705341), Jul 16, 2016: LONGERON. CORRODED. EXCESSIVE CORROSION ON LONGERON 630 BETWEEN STA 960-1010, IN REF CARD 10, ZONE 180. SECTION OF LONGERON WAS REPLACED IAW SRM 53-20-05, REPAIR 1, 51-41-05, 51-40 - [SDR DALA2016071605340](https://openairdocs.org/sdr/DALA2016071605340), Jul 15, 2016: CHANNEL. CRACKED. CRACKED FORWARD CHANNEL STA Y=757 AT RT MLG DOOR LOWER SECTION SM, MLG, CARD 1, ZONE 720. CHANNEL WAS REPAIRED IAW ETI-17-16-077 REV 1 AND ER/A 547857-14, REV O - [SDR DALA2016071605339](https://openairdocs.org/sdr/DALA2016071605339), Jul 15, 2016: PAN. CRACKED. CRACKED PAN BETWEEN BEAM 7/8, STA 161.3 AT FWD ENTRY DOOR, CARD 18, ZONE 820. PAN WAS REPAIRED IAW 717, ETI-17-16-073, REV 1 AND ER/A 547853-14, REV ORIGINAL. - [SDR DALA2016071605335](https://openairdocs.org/sdr/DALA2016071605335), Jul 15, 2016: STOP FITTING. CRACKED. CRACK ON DOOR STOP FITTING STA, Y=994, BEAM 3 AT AFT CARGO COMPARTMENT DOOR. DOOR STOP FITTING STA Y=994, BEAM 3 AT AFT CARGO COMPARTMENT DOOR WAS REPLACED IAW - [SDR DALA2016071605334](https://openairdocs.org/sdr/DALA2016071605334), Jul 15, 2016: ANGLE. CRACKED. CRACK ON ANGLE STA Y=994, INNER SIDE BEAM 3 AT AFT CARGO COMPARTMENT DOOR. CRACKED ANGLE STA Y994 WAS REMOVED AND NEW ANGLE WAS INSTALLED IAW SRM 51-41-05. PARA - [SDR DALA2016071605333](https://openairdocs.org/sdr/DALA2016071605333), Jul 15, 2016: SKIN. WORN. WEAR ON FUSELAGE SKIN IN LONGERON 20RT BETWEEN STA Y=520-526, SM, CARD 27, ZONE 110. DAMAGE WAS REPAIRED IAW ETI-17-16-084, REV 1 AND ER/A 547867-14, REV ORIGIN - [SDR DALA2016071605332](https://openairdocs.org/sdr/DALA2016071605332), Jul 15, 2016: SKIN. WORN. WEAR ON FUSELAGE SKIN IN LONGERON 21RT BETWEEN STA Y=503-508,SM, CARD 28, ZONE 110. WEAR ON FUSELAGE SKIN IN LONGERON 21RT BETWEEN STA Y=503-508 OUT OF LIMITS. - [SDR DALA2016071505398](https://openairdocs.org/sdr/DALA2016071505398), Jul 14, 2016: PAN. CRACKED. CRACK ON INNER PAN STA Y=427 BEAM 1 AT FWD CARGO COMPARTMENT DOOR, SM, C1, CARD 33, ZONE 810. INNER PAN WAS REPAIRED IAW SRM 52-30-02, REPAIR 1, FIG 1, FIG 201, - [SDR DALA2016071505296](https://openairdocs.org/sdr/DALA2016071505296), Jul 14, 2016: ACCESS PANEL. DAMAGED. ELONGATED HOLE AND TOOL MARKS ON LOWER ACCESS 440 INBD AT RT PYLON SM, E/P, CARD 40, ZONE 000. TOOL MARKS AND ELONGATED HOLE WERE REPAIRED IAW SRM 54-00-00, FIG - [SDR DALA2016071505294](https://openairdocs.org/sdr/DALA2016071505294), Jul 14, 2016: ACCESS PANEL. CORRODED. CORROSION ON FUEL ACCESS PLATE 520JB COUNTERSINK. 2EA IN REF ORNRC 64, ACFT ZONE 000, CARD 110, ZONE 000, CORROSION WAS REMOVED IAW SRM 54-10-01, COUNTERSINK WE - [SDR DALA2016071505293](https://openairdocs.org/sdr/DALA2016071505293), Jul 14, 2016: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BETWEEN Y=617 TO Y=636 X=0 AT CEILING AREA OF FWD CARGO COMPARTMENT. C1, SM, CARD 26, ZONE 120 CRACK ON INTERCOSTAL WAS REPAIRED IAW SRM 53- - [SDR DALA2016071505292](https://openairdocs.org/sdr/DALA2016071505292), Jul 14, 2016: LONGERON. CORRODED. EXCESSIVE CORROSION ON LONGERON 30 BETWEEN STA 218 TO 237 AT FWD CARGO COMPARTMENT IN REF CARD 15, ZONE 120, CARD 45, ZONE 120. DUE TO EXCESSIVE DAMAGED SECTION - [SDR DALA2017010500099](https://openairdocs.org/sdr/DALA2017010500099), Jul 13, 2016: ACCESS PANEL. CORRODED. CORROSION ON FUEL ACCESS PLATE 620PB COUNTERSINK. (2EA) CORROSION ON FUEL ACCESS PLATE 620PB COUNTERSINK WAS REMOVED AND MEASURE AND FOUND TWO HOLES OUT OF LIMI - [SDR DALA2017010500098](https://openairdocs.org/sdr/DALA2017010500098), Jul 13, 2016: ACCESS PANEL. CORRODED. CORROSION ON FUEL ACCESS PLATE 520GB COUNTERSINK. (2EA) CORROSION ON FUEL ACCESS PLATE 520GB COUNTERSINK WAS REMOVED AND MEASURE AND FOUND TWO HOLES OUT OF LIMI - [SDR DALA2017010500097](https://openairdocs.org/sdr/DALA2017010500097), Jul 13, 2016: ACCESS PANEL. CORRODED. CORROSION ON FUEL ACCESS PLATE 620QB COUNTERSINK. (1EA) CORROSION ON FUEL ACCESS PLATE 620QB COUNTERSINK WAS REMOVE AND MEASURED AND FOUND ONE HOLE OUT OF LIMIT - [SDR DALA2017010500096](https://openairdocs.org/sdr/DALA2017010500096), Jul 13, 2016: ACCESS PANEL. CORRODED. CORROSION ON FUEL ACCESS PLATE 620LB COUNTERSINK. (2EA) CORROSION ON FUEL ACCESS PLATE 620LB COUNTERSINK WAS REMOVED AND MEASURED AND FOUND TWO HOLES OUT OF LIM - [SDR DALA2016110108049](https://openairdocs.org/sdr/DALA2016110108049), Jul 13, 2016: ACCESS PANEL. CORRODED. CORROSION ON DORSAL FIN JUST ON SETTLEMENT AREA OF ACCESS PANEL 370 AL. FABRICATED NEW AND REPLACED IAW SRM 51-41-02, 51-20-09, 51-10-04 PAR 15 AND 21, AND DWG - [SDR DALA2017010500095](https://openairdocs.org/sdr/DALA2017010500095), Jul 12, 2016: ACCESS PANEL. CORRODED. CORROSION ON SETTLEMENT AND COUNTERSINK LT FUEL TANK ACCESS PLATE 520FT. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE 520FT WAS REMOVED AND - [SDR DALA2016110108048](https://openairdocs.org/sdr/DALA2016110108048), Jul 12, 2016: ACCESS PANEL. CORRODED. CORROSION ON SETTLEMENT AND COUNTERSINK FUEL ACCESS PLATE 520HB. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE 520HB WERE REMOVED AND MEASUR - [SDR DALA2016110108047](https://openairdocs.org/sdr/DALA2016110108047), Jul 12, 2016: ACCESS PANEL. CORRODED. CORROSION ON SETTLEMENT AND COUNTERSINK FUEL ACCESS PLATE 520LB. CORROSION ON FUEL ACCESS PLATE 520LB WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED AND FOUND OU - [SDR DALA2016110108046](https://openairdocs.org/sdr/DALA2016110108046), Jul 12, 2016: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK FUEL ACCESS PLATE 620GB. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE NR 620GB WERE REMOVED AND MEASURED AND FOUND - [SDR DALA2016110108045](https://openairdocs.org/sdr/DALA2016110108045), Jul 12, 2016: ACCESS PANEL. CORRODED. CORROSION ON SETTLEMENT AND COUNTERSINK FUEL ACCESS PLATE 620HB. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE 620HB WERE REMOVED AND MEASUR - [SDR DALA2016071305263](https://openairdocs.org/sdr/DALA2016071305263), Jul 12, 2016: BEAM. CRACKED. CRACKED FWD EDGE BEAM NR 7 AT L1 DOOR. BEAM WAS REPAIRED IAW SRM 52-10-02 REPAIR 13 FIGURE 202. - [SDR DALA2016071205262](https://openairdocs.org/sdr/DALA2016071205262), Jul 12, 2016: FRAME. CRACKED. CRACKED FRAME BS 693 BETWEE1 LONGERONS 26 & 27R. THE FRAME WAS REPLACED. - [SDR DALA2016110108042](https://openairdocs.org/sdr/DALA2016110108042), Jul 11, 2016: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620JB. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620JB WERE REMOVED AN - [SDR DALA2016110108041](https://openairdocs.org/sdr/DALA2016110108041), Jul 11, 2016: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620MB. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 620MB WAS REMOVED IAW SRM 51-10-04 AND WA - [SDR DALA2016110108040](https://openairdocs.org/sdr/DALA2016110108040), Jul 11, 2016: ACCESS PANEL. CORRODED. CORROSION ON SETTLEMENT AND COUNTERSINK FUEL ACCESS PLATE 520EB. CORROSION ON COUNTERSINK WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED AND FOUND OUT OF LIMITS - [SDR DALA2016110108039](https://openairdocs.org/sdr/DALA2016110108039), Jul 11, 2016: ACCESS PANEL. CORRODED. CORROSION ON SETTLEMENT AND COUNTERSINK FUEL ACCESS PLATE 520MB. CORROSION ON FUEL ACCESS PLATE WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED ON COUNTERSINK AND - [SDR DALA2016110108038](https://openairdocs.org/sdr/DALA2016110108038), Jul 11, 2016: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620EB. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 620 EB WAS REMOVED IAW SRM 51-10-04 AND W - [SDR DALA2016071205261](https://openairdocs.org/sdr/DALA2016071205261), Jul 11, 2016: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN BS 1022 BETWEE1 LONGERONS 3 - 14L. THE SKIN WAS REPAIRED IAW ER/A 547827-14. - [SDR DALA2016071205260](https://openairdocs.org/sdr/DALA2016071205260), Jul 11, 2016: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN BS 1037 BETWEEN LONGERONS 13 & 14L. THE SKIN WAS REPAIRED IAW ER/A 547828-14. - [SDR DALA2016103107968](https://openairdocs.org/sdr/DALA2016103107968), Jul 10, 2016: ACCESS PANEL. CORRODED. CORROSION ON FUEL ACCESS PANEL COUNTERSINK & SETTLEMENT AREA. THE ACCESS PANEL CANNOT BE REPAIRED UNDER CONDITIONS I AND II THEREFORE WAS REPLACED IAW SRM 57-10 - [SDR DALA2016103107967](https://openairdocs.org/sdr/DALA2016103107967), Jul 10, 2016: ACCESS PANEL. CORRODED. CORROSION ON FUEL ACCESS PANEL COUNTERSINK & SETTLEMENT AREA. THE ACCESS PANEL CANNOT BE REPAIRED UNDER CONDITIONS I AND II THEREFORE WAS REPLACED IAW SRM 57-10 All 208: https://openairdocs.org/deregistered/N958AT-2025-04-30/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.