# N987AT: 2001 Boeing 717-200, registration cancelled 2025-06-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 28, 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: 55088 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 24, 2001 - Certificate issued: December 9, 2024 - Last registry action: May 15, 2025 - Mode S code: ADC537 - 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/N987AT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=987AT - Page: https://openairdocs.org/deregistered/N987AT-2025-06-28 From the FAA registry file of October 29, 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 (146, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2019F00222](https://openairdocs.org/sdr/2019F00222), May 31, 2019: SKIN. DELAMINATED. LARGE DISBOND, SKIN CORROSION - [SDR DALA2017112708330](https://openairdocs.org/sdr/DALA2017112708330), Nov 26, 2017: BATTERY PACK. INOPERATIVE. MAINTENANCE FOUND THE EMERGENCY LIGHT BATTERY INOPERATIVE AT LOCATION B5-260. MAINTENANCE REPLACED THE BATTERY IAW AMM 33-55. OPS NORMAL. - [SDR DALA2017051803978](https://openairdocs.org/sdr/DALA2017051803978), May 17, 2017: POWER SUPPLY. INOPERATIVE. ON SERVICE CHECK FOUND FORWARD CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY B5-227 AND BATTERY PACK REF AMM 33-51. OPERATIONAL CHECK IS GOO - [SDR DALA2017032002192](https://openairdocs.org/sdr/DALA2017032002192), Mar 20, 2017: BATTERY PACK. DISCHARGED. DURING SERVICE CHECK, FOUND FWD CEILING EMERGENCY LIGHTS COME ON MOMENTARILY DURING TEST. REPLACED EMERGENCY LIGHT BATTERY PACK AT BIN 4R / SEAT ROW 11R PER AMM - [SDR SWAA2017011600000](https://openairdocs.org/sdr/SWAA2017011600000), Jan 16, 2017: SKIN. DELAMINATED. DURING UNSCHEDULE MAINTENANCE CHECK, THE LT OTBD SPOILER FOUND DELAMINATED. - [SDR 2017F00016](https://openairdocs.org/sdr/2017F00016), Dec 29, 2016: SKIN. DELAMINATED. DURING UNSCHEDULE MAINTENANCE CHECK RT INBD SPOILER FOUND DELAMINATED. - [SDR 2017F00015](https://openairdocs.org/sdr/2017F00015), Dec 29, 2016: SKIN. DELAMINATED. DURING UNSCHEDULED MAINTENANCE CHECK, RT OTBD SPOILER FOUND DELAMINATED. - [SDR DALA2016111808913](https://openairdocs.org/sdr/DALA2016111808913), Nov 17, 2016: CUSP WEB. CRACKED. RT CUSP WEB JUST FORWARD OF FRAME STA 505 IS CRACKED AROUND RIVET AND AREA OF CORROSION. REMOVED DAMAGE PART OF CRACKED CUSP WEB. FABRICATED NEW PARTS. INSTALLE - [SDR DALA2016111408746](https://openairdocs.org/sdr/DALA2016111408746), Nov 11, 2016: BATTERY PACK. DISCHARGED. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGH - [SDR DALA2016102807810](https://openairdocs.org/sdr/DALA2016102807810), Oct 27, 2016: CUSP WEB. CORRODED. RIGHT CUSP WEB HAS CORROSION BETWEEN BS 1002-1022. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-51 FIG 1 ITEM 2. REPAIRED THE CUSP WEB IAW SRM - [SDR DALA2016102807809](https://openairdocs.org/sdr/DALA2016102807809), Oct 27, 2016: SEAT TRACK. CORRODED. SEAT TRACK FOUND TO BE CORRODED BEYOND LIMITS, AT RBL 56 IN MULTIPLE AREAS BS 200-590. REPLACED THE SEAT TRACK IAW SRM 53-20-52 REPAIR 5 AND 51-41-01. - [SDR DALA2016102807806](https://openairdocs.org/sdr/DALA2016102807806), Oct 27, 2016: FRAME. CORRODED. FRAME AT BS 908 HAS CORROSION ON UPPER AND LOWER AREAS ON LOWER FLANGE BETWEEN STRINTERS 29 AND 30L. BLEND CORRODED AREA IAW SRM 53-00-00 FIG 103, AND FOUND TO - [SDR DALA2017010500110](https://openairdocs.org/sdr/DALA2017010500110), Oct 26, 2016: SKIN. CORRODED. CORR SKIN AT STA 1002 STR 28R-25R. BLENDED CORROSION ON INTERNAL DOUBLER "SKIN" AT STA 1002 L25R-L28R FOUND TO BE WITHIN LIMITS IAW SRM 53-20-15 NOMINAL .071 .0 - [SDR DALA2016102607650](https://openairdocs.org/sdr/DALA2016102607650), Oct 25, 2016: STRINGER. CORRODED. STRINGER 30 CORRODED AT BS 908. BLENDED CORROSION IAW SRM 53-00-00 FIG 103. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPAIRED THE STRINGER IAW SRM 53 - [SDR DALA2016102607645](https://openairdocs.org/sdr/DALA2016102607645), Oct 25, 2016: INTERCOSTAL. CRACKED. INTERCOSTAL AT BS 665 UNDER LEFT INBOARD SEAT TRACK CRACKED. REPLACED IAW DWG 9911751 REV Z. - [SDR DALA2016102807808](https://openairdocs.org/sdr/DALA2016102807808), Oct 24, 2016: SEAT TRACK. DAMAGED. RIGHT OTBD SEAT TRACK RBL 56 IS GOUGED AND CORRODED IN SEVERAL AREAS FROM BS 813 - 908. BLENDED, AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TR - [SDR DALA2016102707765](https://openairdocs.org/sdr/DALA2016102707765), Oct 24, 2016: SEAT TRACK. DAMAGED. RIGHT OUTBOARD SEAT TRACK HAS KNICKS AND CORROSION BS 500 - 600. BLENDED AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-01 AND - [SDR DALA2016102607649](https://openairdocs.org/sdr/DALA2016102607649), Oct 24, 2016: INTERCOSTAL. CRACKED. INTERCOSTAL AT BS 665 UNDER THE RIGHT INBOARD SEAT TRACK CRACKED. REPLACED THE INTERCOSTAL IAW DWG 9911751 REV 2. - [SDR DALA2016102707766](https://openairdocs.org/sdr/DALA2016102707766), Oct 23, 2016: CUSP WEB. CRACKED. CUSP WEB AT BS 218 WAS FOUND CRACKED. REMOVED AND REPLACED THE CUSP WEB BS 218-236 IAW SRM 51-41-00 ITEM 1, SRM 51-40-08, SRM 51-41-02, AND 51-41-05. - [SDR DALA2016102607647](https://openairdocs.org/sdr/DALA2016102607647), Oct 23, 2016: FRAME. CORRODED. NR 2 RT AIR GRILL FRAME IS CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 A.D. GENERAL FIG 103. INSTALLED REPAIR DOUBLERS IAW SRM 51 - [SDR DALA2016102607646](https://openairdocs.org/sdr/DALA2016102607646), Oct 23, 2016: CUSP WEB. CORRODED. CORROSION ON CUSP WEB AT BS 218. RBL 56. CUT OUT CORROSION DAMAGE AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 REPAIR 2, AMM 51-10-00 370-803, AND SRM 51-41- - [SDR DALA2016102807807](https://openairdocs.org/sdr/DALA2016102807807), Oct 22, 2016: LONGERON. CORRODED. CORROSION LONGERON 25R BS 1002. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPLACED THE LONGERON IAW SRM 51-41-02 PAGE 1-4. - [SDR DALA2016102607648](https://openairdocs.org/sdr/DALA2016102607648), Oct 22, 2016: CUSP WEB. CRACKED. CUSP WEB AT BS 655 CRACKED. REPLACED THE CUSP WEB IAW SRM 51-41-02 AND 51-41-05. - [SDR DALA2016102307457](https://openairdocs.org/sdr/DALA2016102307457), Oct 22, 2016: SKIN. DAMAGED. VERTICAL STAB LEADING EDGE AT VSS ZFS 52.267 SPLICE HAS NUMEROUS LOOSE SCREWS & SCREWS PULLING INTO SKIN & ELONGATED HOLES. REPAIRED THE VERTICAL STAB LEADING E - [SDR DALA2016102107423](https://openairdocs.org/sdr/DALA2016102107423), Oct 20, 2016: CUSP WEB. CORRODED. CUSP WEB CORRODED ON FWD AND AFT SIDE OF FLOORBEAM AT FS 389 ON UNDERSIDE OF WEB. REPAIRED CORRODED CUSP WEB AT FS 389 BY REMOVING DAMAGED SECTION AND REPAIRING - [SDR DALA2016102107425](https://openairdocs.org/sdr/DALA2016102107425), Oct 19, 2016: SKIN. DENTED. DENT IN FUSELAGE AT C-1 UPPER CORNER CUTOUT. EVALUATED DENT IN FUSELAGE AT C-1 UPPER FWD CORNER CUTOUT IAW SRM 53-01-01 AD3 DENT IS OUT OF LIMITS. REPAIRED DENT - [SDR DALA2016102007384](https://openairdocs.org/sdr/DALA2016102007384), Oct 18, 2016: CUSP WEB. CRACKED. LEFT CUSP WEB FOUND CRACKED BETWEEN BS 579 & 598. REPLACED THE CUSP WEB IAW SRM 51-41-05 PG 17 STEP 8. - [SDR DALA2016101907362](https://openairdocs.org/sdr/DALA2016101907362), Oct 18, 2016: CUSP WEB. CRACKED. RT CUSP WEB AT BS 657 CRACKED. REPAIRED THE CUSP WEB IAW SRM 51-70-10 REP 2 & SRM 53-00-55 REP 4. - [SDR DALA2016101907365](https://openairdocs.org/sdr/DALA2016101907365), Oct 17, 2016: CUSP WEB. CRACKED. CUSP WEB AT BS 674 CRACKED. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 REPAIR 4. - [SDR DALA2016101907367](https://openairdocs.org/sdr/DALA2016101907367), Oct 13, 2016: SEAT TRACK. CORRODED. RIGHT INBD SEAT TRACK BS 200-256, FOUND THREE SPOTS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-05 PG 1. - [SDR DALA2016101907361](https://openairdocs.org/sdr/DALA2016101907361), Oct 13, 2016: FRAME. CRACKED. BS 1022 FRAME ABOVE LONGERON 14R WAS FOUND CRACKED. REPLACED THE FRAME IAW SRM 51-41-02 PG 1-4, & 51-41-05 PG 1. - [SDR DALA2016101907366](https://openairdocs.org/sdr/DALA2016101907366), Oct 12, 2016: STRINGER. CORRODED. STRINGER 29L CORRODED BETWEEN BS 908 - 927. BLENDED THE STRINGER IAW SRM 53-00-00 FIG 103. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPAIRED THE STRI - [SDR DALA2016102107462](https://openairdocs.org/sdr/DALA2016102107462), Oct 10, 2016: SEAT TRACK. DAMAGED. LEFT OTBD SEAT TRACK LBL 56 IS CORRODED AND GOUGED IN SEVERAL AREAS FROM BS 1020 - 1053. BLENDED THE AREAS OF CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53 - [SDR DALA2016101907368](https://openairdocs.org/sdr/DALA2016101907368), Oct 10, 2016: FRAME. CRACKED. CRACK IN BS 1022 MAIN FRAME, AFT SIDE AT STRINGER 7R. REPAIRED THE FRAME IAW SRM 51-70-11 REPAIR 1. - [SDR DALA2016101907364](https://openairdocs.org/sdr/DALA2016101907364), Oct 10, 2016: FRAME. CRACKED. CRACK IN BS 1022 MAIN FRAME AT STRINGER 7L. THE FRAME WAS REPAIRED IAW SRM 51-70-11 REPAIR 1. - [SDR DALA2016101907363](https://openairdocs.org/sdr/DALA2016101907363), Oct 10, 2016: BRACKET. CRACKED. CRACKED BRACKET UNDER UPPER CABIN FLOOR, ABOVE CENTER WING FUEL TANK AT APPROXIMATE BS 735 RBL 48. REMOVED AND REPLACED THE BRACKET IAW SRM 51-41-05. - [SDR DALA2016101007121](https://openairdocs.org/sdr/DALA2016101007121), Oct 10, 2016: ACCESS PANEL. DAMAGED. RT WING UPPER ACCESS PANEL 620FT HAS ELONGATED HOLES. REPLACED THE ACCESS PANEL IAW AMM 28-00-00-410. - [SDR DALA2016101007120](https://openairdocs.org/sdr/DALA2016101007120), Oct 10, 2016: ACCESS PANEL. DAMAGED. RT WING UPPER ACCESS PANEL 620CT HAS ELONGATED HOLES. REPLACED THE ACCESS PANEL IAW AMM 28-00-00-410. - [SDR DALA2016090906508](https://openairdocs.org/sdr/DALA2016090906508), Sep 9, 2016: BATTERY. DISCHARGED. DURING LINE CHECK, MAINTENANCE FOUND THAT A SECTION OF THE EMERGENCY ESCAPE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOO - [SDR DALA2016061304549](https://openairdocs.org/sdr/DALA2016061304549), Jun 11, 2016: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. MAINTENANCE REPLACED THE BATTERY PACK FOR T - [SDR DALA2016022901537](https://openairdocs.org/sdr/DALA2016022901537), Feb 27, 2016: SLIDE. DAMAGED. INSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE WAS NO LONGER IN AN ACCEPTABLE CONFIGURATION. A MISRIGGED, IMPROPERLY MISSING BUSTLE CABLE - [SDR DALA2015090905508](https://openairdocs.org/sdr/DALA2015090905508), Sep 8, 2015: BATTERY PACK. INOPERATIVE. SEVERAL EMERGENCY EXIT SIGNS DO NOT ILLUMINATE; 2 BY RT SERVICE DOOR, 1 OVERHEAD FWD CABIN & 1 AFT CABIN BY AFT PRESSURE BULKHEAD. REPLACED EMERGENCY LIGHT BATT - [SDR DALA2015072104569](https://openairdocs.org/sdr/DALA2015072104569), Jul 20, 2015: BATTERY PACK. INOPERATIVE. DURING SERVICE CHECK, FOUND OVERHEAD CABIN EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACKS B101, 102, 104 & B106. CHECKED GOOD. - [SDR DALA2014121506529](https://openairdocs.org/sdr/DALA2014121506529), Dec 13, 2014: LATCH. WORN. DURING TAILCONE CHECK, FOUND LT UPPER AND LOWER TAILCONE LATCH ASSEMBLIES WORN. REPLACED LT UPPER AND LOWER LATCH ASSYS IAW AMM 53-52. - [SDR SWAA2014101633026](https://openairdocs.org/sdr/SWAA2014101633026), Oct 14, 2014: LIGHT. INOPERATIVE. FORWARD LT OVERWING DOOR EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM. - [SDR SWAA2014101733107](https://openairdocs.org/sdr/SWAA2014101733107), Oct 13, 2014: LIGHT. LOOSE. CAT WALK CEILING EMER LIGHT WIRING LOOSE. SECURED LIGHT IAW SWPM. - [SDR SWAA2014101532952](https://openairdocs.org/sdr/SWAA2014101532952), Oct 8, 2014: CHARGER. INOPERATIVE. RIGHT EXTERIOR OVERWING EMER EVACUATION LIGHTS INOPERATIVE. R & R BATTERY CHARGER ASSEMBLY IAW AMM. - [SDR SWAA2014101532941](https://openairdocs.org/sdr/SWAA2014101532941), Oct 8, 2014: CHARGER. INOPERATIVE. LEFT EXTERIOR OVERWING EMER EVACUATION LIGHTS INOPERATIVE. R & R BATTERY CHARGER ASSEMBLY IAW AMM. - [SDR SWAA2014100732695](https://openairdocs.org/sdr/SWAA2014100732695), Sep 22, 2014: BATTERY PACK. DISCHARGED. RIGHT FWD EMER EXIT OVERWING IDENTIFIER LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM & WDM. - [SDR SWAA2014100732704](https://openairdocs.org/sdr/SWAA2014100732704), Sep 22, 2014: CHARGER. INOPERATIVE. FORWARD OVERHEAD EMER LIGHT BATTERY CHARGER INOPERATIVE. R & R BATTERY CHARGER IAW AMM. All 146: https://openairdocs.org/deregistered/N987AT-2025-06-28/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.