# N987DN: 2000 Boeing 717-200, registration cancelled 2025-03-01 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 1, 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: 55064 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 3, 2016 - Certificate issued: January 4, 2016 - Last registry action: July 7, 2023 - Mode S code: ADC57D - 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/N987DN - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=987DN - Page: https://openairdocs.org/deregistered/N987DN-2025-03-01 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 (61, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA2020030601668](https://openairdocs.org/sdr/DALA2020030601668), Mar 6, 2020: SKIN. CRACKED. VERTICAL STABILIZER RAM AIR INLET LEADING EDGE IS CRACKED ON THE LEFT SIDE. REPAIRED PER B717 SRM 55-30-01-2R PROCEDURE 1. REQUIRES REPETITIVE VISUAL INSPECTION - [SDR DALA2019050102763](https://openairdocs.org/sdr/DALA2019050102763), Apr 29, 2019: BATTERY PACK. INOPERATIVE. MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS OUT IN THE CABIN DURING THE TURN AROUND CHECK. TROUBLE SHOOTING PER MD88 SSM 33-51 FOUND THE BATTERIES B5-123, B5-259 - [SDR DALA2018041602479](https://openairdocs.org/sdr/DALA2018041602479), Apr 16, 2018: WIRE. LOOSE. THE AFT EMERGENCY EXIT LIGHT CAME ON AND WOULD NOT EXTINGUISH. MAINTENANCE FOUND A LOOSE WIRING AND SECURED IT. THE EMERGENCY EXIT LIGHT WORKS PROPERLY. - [SDR DALA2018040602228](https://openairdocs.org/sdr/DALA2018040602228), Apr 5, 2018: DOOR FRAME. CORRODED. CORROSION ON THE SPLICE OF THE DOOR FRAME AT THE AFT CARGO BAY, BS 954 AND 994. THE SPLICES WERE REPLACED IAW SRM 53-20-15-2R FIG 201. - [SDR DALA201801240085](https://openairdocs.org/sdr/DALA201801240085), Jan 24, 2018: TAB. DELAMINATED. DURING NON ROUTINE UNSCHEDULED CHECK, FOUND THE AILERON TAB TO BE DELAMINATED. - [SDR DALA201812210058](https://openairdocs.org/sdr/DALA201812210058), Dec 21, 2017: TAB. DELAMINATED. CUSTOMER FOUND DURING INSPECTION CHECK DELAMINATION ON LOWER AND UPPER SURFACE- FULL SKIN REPLACEMENT REQUIRED - [SDR DALA2016040602655](https://openairdocs.org/sdr/DALA2016040602655), Apr 5, 2016: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY FLOOD LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO - [SDR DALA2016033102566](https://openairdocs.org/sdr/DALA2016033102566), Mar 30, 2016: SKIN. DENTED. DENT ON RUDDER TAB L/H SIDE, 33" FROM LOWER EDGE AND 5" FROM AFT EDGE. CUT OUT DAMAGED AREA IN RUDDER TAB LT SIDE AND ACCOMPLISHED A HOT BOND DOUBLER REPAIR IAW - [SDR DALA2016033102565](https://openairdocs.org/sdr/DALA2016033102565), Mar 30, 2016: SKIN. DENTED. DENT ON RUDDER TAB RT SIDE, 35" FROM LOWER EDGE AND 6.5" FROM AFT EDGE. CUTOUT DAMAGED AREA ON RUDDER TAB RT SIDE 35" FROM LOWER EDGE AND ACCOMPLISHED A HOT BON - [SDR DALA2016032202625](https://openairdocs.org/sdr/DALA2016032202625), Mar 22, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 222YF IS DELAMINATED WITH 2 EA DAMAGED STIFFENERS AND 1 EACH COVER DAMAGED. MAIN CABIN FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND O - [SDR DALA2016032202624](https://openairdocs.org/sdr/DALA2016032202624), Mar 22, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 222ATF IS DELAMINATED. MAIN CABIN FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FAB - [SDR DALA2016032202623](https://openairdocs.org/sdr/DALA2016032202623), Mar 21, 2016: KEELBEAM. CRACKED. RT KEELBEAM BARREL FORMER CRACKED AT BS 696 OTBD END. RELACED RT KEELBEAM FORMER AT BS 696 OTBD END. CRACK DIM. 4.0" IAW SRM 51-41-02, 51-41-05, DWG 9923418, RE - [SDR DALA2016031802622](https://openairdocs.org/sdr/DALA2016031802622), Mar 18, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 222ADF IS DELAMINATED WITH DAMAGE TO LT COVER AND RT STIFFENER. MAIN CABIN FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS - [SDR DALA2016031702621](https://openairdocs.org/sdr/DALA2016031702621), Mar 16, 2016: KEELBEAM. CORRODED. UNDER WING BARREL KEELBEAM AT BS 679 OTBD END OF FORMER CRACKED RT SIDE. REMOVED FORMER AND SHEAR CLIP FROM RT OF UNDER WING BARREL KEELBEAM AT BS 679, AND LOCA - [SDR DALA2016031702620](https://openairdocs.org/sdr/DALA2016031702620), Mar 16, 2016: KEELBEAM. CORRODED. UNDER WING BARREL KEELBEAM BS 695, LONG 29R CORRODED. UNDER WING BARREL KEELBEAM LONGERON 29RT, FITTING FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-00. RE - [SDR DALA2016031702619](https://openairdocs.org/sdr/DALA2016031702619), Mar 16, 2016: KEELBEAM. CORRODED. UNDER WING BARREL KEELBEAM BS 662 LONG 29LT CORRODED. CORROSION DAMAGE ON UNDER WING KEELBEAM LONGERON 29LT, FITTING, FOUND OUT OF LIMITS. REPAIRED IAW SRM 51-4 - [SDR DALA2016031702617](https://openairdocs.org/sdr/DALA2016031702617), Mar 16, 2016: SKIN. CORRODED. AFT CARGO COMPARTMENT DOOR CUTOUT INTERIOR FWD LOWER CORNER BS 946-954 SKIN HAS CORROSION LOWER SURFACE HAS CORROSION AT 4 EA SEAT TRACK N/P'S. CORROSION DAMAGE - [SDR DALA2016031702618](https://openairdocs.org/sdr/DALA2016031702618), Mar 15, 2016: STOP FITTING. CRACKED. FWD CARGO COMPARTMENT DOOR UPPER FWD INT DOOR STOP FITTING IS CRACKED. REPLACED STOP FITTING FROM FWD CARGO DOOR UPPER FWD INT. ARA IAW SRM 51-41-01, IAW DWG 99 - [SDR DALA2016031602616](https://openairdocs.org/sdr/DALA2016031602616), Mar 15, 2016: KEELBEAM. CRACKED. UNDERWING BARREL KEELBEAM-BS 679 OTBD END OF FORMER CRACKED LT. INSTALLED FOR FORMER AT BS 679 IAW SRM 51-41-02, 51-41-05, AND DWG 9923453, REV A. PLEASE DISREG - [SDR DALA2016031602615](https://openairdocs.org/sdr/DALA2016031602615), Mar 15, 2016: KEELBEAM. CRACKED. UNDERWING BARREL KEELBEAM BS 679 OTBD END OF FORMER CRACKED LT. INSTALLED FOR FORMER AT BS 679 IAW SRM 51-41-02, 51-41-05, AND DWG 9923453, REV A. ASSOCIATED ER - [SDR DALA2016031602614](https://openairdocs.org/sdr/DALA2016031602614), Mar 15, 2016: FLOOR PANEL. DAMAGED. FLIGHT COMPARTMENT FLOOR PANEL 211AJF IS DAMAGED. CUTOUT DAMAGED AREA ON FLOOR PANEL NR 211AJF DIM. 2.1250" X 3" IAW SRM 53-10-50 REPAIR 1. FABRICATED REPAIR DO - [SDR DALA2016031602607](https://openairdocs.org/sdr/DALA2016031602607), Mar 15, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD NR 222LF IS DELAMINATED. FLOORBOARD FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED, FAB - [SDR DALA2016031602606](https://openairdocs.org/sdr/DALA2016031602606), Mar 15, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD NR 222DF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED, FAB - [SDR DALA2016031602605](https://openairdocs.org/sdr/DALA2016031602605), Mar 15, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD NR 222GF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED, FAB - [SDR DALA2016031602608](https://openairdocs.org/sdr/DALA2016031602608), Mar 14, 2016: STOP FITTING. CRACKED. FWD CARGO DOOR MID FWD STOP BRACKET IS CRACKED. REMOVED , LOCATED, DRILLED, AND INSTALLED A NEW BRACKET ALL IAW SRM 51-41-05, 51-40-08 AND DWG 5910141, REV FE, - [SDR DALA2016031502604](https://openairdocs.org/sdr/DALA2016031502604), Mar 14, 2016: SEAT TRACK. DAMAGED. SCRATCHES AND GOUGES THROUGHOUT SEAT TRACK CROWN AND INNER FLAT SURFACES AT AFT CABIN FLOOR, FROM BS 798 - 898 AND RBL 56.0. REMOVED SCRATCHES AND GOUGES THROUG - [SDR DALA2016031502603](https://openairdocs.org/sdr/DALA2016031502603), Mar 14, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 222JF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED, FABRIC - [SDR DALA2016031502602](https://openairdocs.org/sdr/DALA2016031502602), Mar 14, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 222BF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED, FABRIC - [SDR DALA2016031502601](https://openairdocs.org/sdr/DALA2016031502601), Mar 14, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 222AVF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED AND FA - [SDR DALA2016031502600](https://openairdocs.org/sdr/DALA2016031502600), Mar 14, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD NR 221LF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A - [SDR DALA2016031502599](https://openairdocs.org/sdr/DALA2016031502599), Mar 14, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 211ALF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A N - [SDR DALA2016031502598](https://openairdocs.org/sdr/DALA2016031502598), Mar 14, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 221AF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NE - [SDR DALA2016031502597](https://openairdocs.org/sdr/DALA2016031502597), Mar 14, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD NR 221KF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A - [SDR DALA2016031502596](https://openairdocs.org/sdr/DALA2016031502596), Mar 14, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 221DF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NE - [SDR DALA2016031502595](https://openairdocs.org/sdr/DALA2016031502595), Mar 14, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 221HF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NE - [SDR DALA2016031502594](https://openairdocs.org/sdr/DALA2016031502594), Mar 14, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 221CF IS DELAMINATED. FLOORBOARD FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NE - [SDR DALA2016031502593](https://openairdocs.org/sdr/DALA2016031502593), Mar 14, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 221EF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FL - [SDR DALA2016031502592](https://openairdocs.org/sdr/DALA2016031502592), Mar 14, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 221FF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NE - [SDR DALA2016031502591](https://openairdocs.org/sdr/DALA2016031502591), Mar 14, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 221JF IS DELAMINATED. FLOORBOARD FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NE - [SDR DALA2016031302590](https://openairdocs.org/sdr/DALA2016031302590), Mar 12, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 222APF IS DELAMINATED. FLOORBOARD FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FABRICATED A - [SDR DALA2016031302589](https://openairdocs.org/sdr/DALA2016031302589), Mar 12, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 222AMF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A N - [SDR DALA2016031302588](https://openairdocs.org/sdr/DALA2016031302588), Mar 12, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 222AHF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A N - [SDR DALA2016031302587](https://openairdocs.org/sdr/DALA2016031302587), Mar 12, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 222AGF IS DELAMINATED. FLOORBOARD FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A N - [SDR DALA2016031302586](https://openairdocs.org/sdr/DALA2016031302586), Mar 12, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 222AAF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINTED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NE - [SDR DALA2016031302585](https://openairdocs.org/sdr/DALA2016031302585), Mar 12, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 222ABF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCNET DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A N - [SDR DALA2016031302584](https://openairdocs.org/sdr/DALA2016031302584), Mar 12, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 221BF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NE - [SDR DALA2016031302583](https://openairdocs.org/sdr/DALA2016031302583), Mar 12, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 221UF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NE - [SDR DALA2016031302582](https://openairdocs.org/sdr/DALA2016031302582), Mar 12, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 211ANF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A N - [SDR DALA2016031302581](https://openairdocs.org/sdr/DALA2016031302581), Mar 12, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 222PF IS DELAMINATED. MAIN CABIN FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FAB - [SDR DALA2016031302580](https://openairdocs.org/sdr/DALA2016031302580), Mar 12, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 223DF IS DELAMINATED. MAIN CABIN FLOORBOARD FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABR All 61: https://openairdocs.org/deregistered/N987DN-2025-03-01/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.