# N988DN: 2001 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: 55065
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 2, 2016
- Certificate issued: November 12, 2015
- Last registry action: June 23, 2023
- Mode S code: ADC934
- 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/N988DN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=988DN
- Page: https://openairdocs.org/deregistered/N988DN-2025-03-01

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 (63, newest 50)

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

- [SDR DALA2019112806952](https://openairdocs.org/sdr/DALA2019112806952), Nov 27, 2019: DOOR FRAME. CRACKED. RH OVERWING EXIT FRAME HAS A CONDITION 3 CRACK AT STA 674 FRAME TAB UPPER RADIUS REF 5310-01436-01D STEP 7. NRC 138-0004:5310-01436-01D/001 00087: REPLACED FRAM
- [SDR DALA2018030501385](https://openairdocs.org/sdr/DALA2018030501385), Mar 2, 2018: LIGHT. BROKEN. EMERGENCY LIGHT STRIP BROKEN AT SEAT 21B. REINSTALLED THE LIGHT STRIP. CHECKED OK.
- [SDR DALA20180301295](https://openairdocs.org/sdr/DALA20180301295), Feb 27, 2018: UNKNOWN. MALFUNCTIONED. THE FLIGHT CREW DECLARED AN EMERGENCY ON APPROACH INTO CAE AFTER THE FLAPS STOPPED EXTENDING BEYOND 18 DEGREES. MAINTENANCE FUNCTIONALLY CHECKED THE FLAP CONTRO
- [SDR DALA2018022601169](https://openairdocs.org/sdr/DALA2018022601169), Feb 25, 2018: POWER SUPPLY. INOPERATIVE. THE OVERWING EMERGENCY LIGHT DOES NOT TURN ON. TROUBLE SHOT PER 33-50-00 810-801. DURING CHECK POWER SUPPLY B5-119 REPLACEMENT BECAME REQUIRED. POWER SUPPLY WAS
- [SDR DALA2018022201830](https://openairdocs.org/sdr/DALA2018022201830), Feb 22, 2018: SKIN. CRACKED. CRACK WAS FOUND OF 0.250" ON R1 FWD SERVICE DOOR, BOTTOM AREA, OUTER SKIN. PERMANENT REPAIR. CRACK ON R1 FWD SERVICE DOOR BOTTOM AREA WAS REPAIRED PER SRM 51-70
- [SDR DALA2018022301091](https://openairdocs.org/sdr/DALA2018022301091), Feb 22, 2018: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON FUEL ACCESS PANEL 520DT ON THE LT WING. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01-2R-2, PAR 5, CONDITION II.
- [SDR DALA2017123009014](https://openairdocs.org/sdr/DALA2017123009014), Dec 29, 2017: LENS. DAMAGED. EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED. MAINTENANCE REPLACED LIGHT ASSY IAW DRAWING BR9051. OPS CHECKED GOOD.
- [SDR DALA2017032002193](https://openairdocs.org/sdr/DALA2017032002193), Mar 20, 2017: BATTERY. DISCHARGED. FWD EMERGENCY LIGHT FOUND INOP DURING SERVICE CHECK. REPLACED EMERGENCY LIGHT BATTERY IAW AMM 33-51. OPS CHECK GOOD AT THIS TIME. A/C OK FOR SVC.
- [SDR DALA2016012900837](https://openairdocs.org/sdr/DALA2016012900837), Jan 28, 2016: SKIN. DENTED. AA WORK CARD 2330-01340-01A. DURING STEP 3 OF TASK CARD, 7 EA DENT DOTS FOUND AT ANTENNA INSTALLATION AREA. CUT OUT AREAS ON FUSELAGE SKIN BETWEEN BS 332 AND BS
- [SDR DALA2016012400588](https://openairdocs.org/sdr/DALA2016012400588), Jan 23, 2016: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 218-589, RBL 54. CORROSION DAMAGE ON MAIN CABIN SEAT TRACK, RBL 54, STA 218-589. FOUND OUT OF LIMITS, ORIGINAL THICKNE
- [SDR DALA2016012300583](https://openairdocs.org/sdr/DALA2016012300583), Jan 22, 2016: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK CORRODED UNDER TIEDOWN BS 237, RBL 44. CORROSION DAMAGE ON MAIN CABIN SEAT TRACK BS 237, RBL 44 FOUND OUT OF LIMITS, ORIGINAL THICKNESS .1
- [SDR DALA2016012300582](https://openairdocs.org/sdr/DALA2016012300582), Jan 22, 2016: FLOORBEAM. CORRODED. MAIN CABIN FLOOR SUPPORT, BS 195, LBL 22-LBL 44 CORRODED. CORROSION DAMAGE ON MAIN CABIN FLOOR SUPPORT BS 195, LBL 22-LBL 44 FOUND TO BE OUT OF LIMITS, ORIGINAL
- [SDR DALA2016012100480](https://openairdocs.org/sdr/DALA2016012100480), Jan 20, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL NR 222ADF IS DELAMINATED AND 1 EA COVER DAMAGED. MAIN CABIN FLOOR PANEL NR 222ADF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IA
- [SDR DALA2016012100479](https://openairdocs.org/sdr/DALA2016012100479), Jan 20, 2016: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL, NR 222YF HAS 2 EA DAMAGED COVERS AND 2 EA DAMAGED STIFFENERS, LT AND RT SIDES. REPLACED MAIN CABIN FLOOR PANEL 222YF STIFFENERS, 2 EA AN
- [SDR DALA2016011600425](https://openairdocs.org/sdr/DALA2016011600425), Jan 15, 2016: ANGLE. DAMAGED. UPPER ANGLE FOUND TO BE DAMAGED INSIDE OF CENTER TANK, FWD OF ACCESS PANEL 141AL CUTOUT BS 676, LBL 22. REPLACED UPPER ANGLE IAW SRM 51-41-05 AND DWG 9919346, R
- [SDR DALA2016011600424](https://openairdocs.org/sdr/DALA2016011600424), Jan 15, 2016: CUSP WEB. CORRODED. MAIN CABIN CORRODED ON CUSP WEB CORRODED BETWEEN BS 908 TO 946 RT SIDE. CORROSION DAMAGE FOUND TO BE OUT OF LIMITS IN TWO LOCATIONS, BS 908-927 AND BS 927-946. 
- [SDR DALA2016011500333](https://openairdocs.org/sdr/DALA2016011500333), Jan 14, 2016: FLOOR SUPPORT. BROKEN. FLIGHT COMPARTMENT FLOOR SUPPORT ANGLE IS BROKEN AT APPROXIMATELY BS 150, RBL 52. REPLACED FLIGHT COMPARTMENT FLOOR SUPPORT ANGLE APPROXIMATELY RBL 52, STA 150 
- [SDR DALA2016011500326](https://openairdocs.org/sdr/DALA2016011500326), Jan 14, 2016: FLOOR SUPPORT. CRACKED. MAIN CABIN FLOOR PANEL 222AFF LOWER HAT CHANNEL CRACKED. REPLACED FLOOR PANEL 222AFF LOWER HAT CHANNEL IN MAIN CABIN IAW SRM 51-20-05, DWG 9952521, REV BB, AND 
- [SDR DALA2016011500325](https://openairdocs.org/sdr/DALA2016011500325), Jan 14, 2016: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BETWEEN BS 200-265, RBL 24 CORRODED. FOUND TO BE OUT OF LIMITS DUE TO 100 PERCENT MATERIAL LOSS IAW SRM 53-20-52, ALLOWABLE DAMAGE 1 AND D
- [SDR DALA2016011900471](https://openairdocs.org/sdr/DALA2016011900471), Jan 13, 2016: FLOOR PANEL. PUNCTURED. MAIN CABIN FLOOR PANEL NR 222ZF HAS A PUNCTURE APPROXIMATELY BS 730, RBL 46. CUTOUT DAMAGED AREA ON MAIN CABIN FLOOR PANEL NR 222ZF, DIM 1.8" X 1.2", FABRICATED
- [SDR DALA2016011400272](https://openairdocs.org/sdr/DALA2016011400272), Jan 13, 2016: FORMER. CRACKED. LEFT KEELBEAM BARREL BS 696-OTBD END OF FORMER CRACKED. DISPLACED BARREL WEB LT KEELBEAM AT BS 696 IAW SRM 51-41-02 AND SRM 51-41-05 TO FOM. REMOVED FORMER IAW 
- [SDR DALA2016011400271](https://openairdocs.org/sdr/DALA2016011400271), Jan 13, 2016: WEB. CRACKED. RT SIDE KEELBEAM BARREL BS 696 OTBD END OF FORMER CRACKED. DISPLACED BARREL WEB FOR FOM , R & R RT SIDE KEELBEAM BARREL FORMER, BS 696 IAW SRM 51-41-02, 51-40-0
- [SDR DALA2016011200196](https://openairdocs.org/sdr/DALA2016011200196), Jan 11, 2016: SUPPORT ANGLE. CORRODED. WING TO BS 813, LONGERON 30 CLIP SUPPORT CORRODED. CORROSION DAMAGE ON WING TO BODY CLIP BS 813, BL 0 FOUND TO BE OUT OF LIMITS, ORIG THICKNESS .156", MATERIAL 
- [SDR DALA2016011200195](https://openairdocs.org/sdr/DALA2016011200195), Jan 11, 2016: FORMER. CRACKED. RIGHT SIDE KEEL BEAM BARREL BS 679, OTBD END OF FORMER CRACKED. REPLACED RT KEEL BEAM BARREL BS 679 FORMER IAW SRM 51-41-02 AND DWG 9923453, REV A AND REV C. AC
- [SDR DALA2016011200194](https://openairdocs.org/sdr/DALA2016011200194), Jan 11, 2016: FORMER. CRACKED. LEFT KEEL BEAM BARREL BS 679 OTBD END OF FORMER CRACKED. REPLACED FORMER AS LT KEEL BEAM BARREL BS 679 IAW SRM 51-41-02 AND DWG 9923453, REV C AND REV A. ACCOMP
- [SDR DALA2016011200193](https://openairdocs.org/sdr/DALA2016011200193), Jan 11, 2016: SUPPORT FRAME. CORRODED. RT WING TO BODY FAIRING SUPPORT FRAME BS 851 HAS CORROSION UNDER NUT CLIPS. CORROSION DAMAGE ON RT WING TO BODY FAIRING SUPPORT FRAME BS 851 FOUND OUT OF LIMITS
- [SDR DALA2016011100192](https://openairdocs.org/sdr/DALA2016011100192), Jan 10, 2016: FLOOR PANEL. CRACKED. COCKPIT FLOOR PANEL 211AKF CRACKED. CUT OUT DAMAGED AREA OF COCKPIT FLOOR PANEL 211AKF DIM 2.5" X 1.5" AND INSTALLED A REPAIR IAW SRM 53-10-50 AND 53-10-50, REP
- [SDR DALA2016011100191](https://openairdocs.org/sdr/DALA2016011100191), Jan 10, 2016: CAP. CRACKED. LEFT ELEVATOR OTBD END, T/E END CAP CRACKED. REPLACED LT ELEVATOR OTBD END T/E END CAP IAW SRM 51-41-02 AND DWG 5910412, REV DS CRACK DIM .750".
- [SDR DALA2016011100190](https://openairdocs.org/sdr/DALA2016011100190), Jan 10, 2016: SKIN. DELAMINATED. RUDDER UPPER AFT END DELAMINATED. REPAIRED RUDDER UPPER AFT END DIM 4" X 4" IAW SRM 55-00-01, REPAIR 2.
- [SDR DALA2016011100177](https://openairdocs.org/sdr/DALA2016011100177), Jan 10, 2016: SEAT TRACK. DAMAGED. MAIN CABIN SEAT TRACK HAS SCRATCHES AND GOUGES BETWEEN BS 899- BS 1022, RBL 24. SEAT TRACK SECTION BS 899-1022, RBL 24 FOUND TO BE OUT OF LIMITS DUE TO SCALLOP 
- [SDR DALA2016010900189](https://openairdocs.org/sdr/DALA2016010900189), Jan 8, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 222AEF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222AEF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMA
- [SDR DALA2016010900188](https://openairdocs.org/sdr/DALA2016010900188), Jan 8, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 222DF IS DELAMINATED. MAIN CABIN FLOOR PANEL FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FA
- [SDR DALA2016010900187](https://openairdocs.org/sdr/DALA2016010900187), Jan 8, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 211ANF IS DELAMINATED. MAIN CABIN FLOOR PANEL FOUND TO BE 60 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. F
- [SDR DALA2016010900186](https://openairdocs.org/sdr/DALA2016010900186), Jan 8, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 222ACF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222ACF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMA
- [SDR DALA2016010900185](https://openairdocs.org/sdr/DALA2016010900185), Jan 8, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL NR 222ABF IS DELAMINATED. MAIN CABIN FLOOR PANEL FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1
- [SDR DALA2016010900184](https://openairdocs.org/sdr/DALA2016010900184), Jan 8, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 221AF IS DELAMINATED. MAIN CABIN FLOOR PANEL 221AF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE
- [SDR DALA2016010900183](https://openairdocs.org/sdr/DALA2016010900183), Jan 8, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 221EF IS DELAMINATED. MAIN CABIN FLOOR PANEL FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FA
- [SDR DALA2016010900182](https://openairdocs.org/sdr/DALA2016010900182), Jan 8, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 211AQF IS DELAMINATED. MAIN CABIN FLOOR PANEL 211AQF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMA
- [SDR DALA2016010900181](https://openairdocs.org/sdr/DALA2016010900181), Jan 8, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL NR 222FF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222FF FOUND TO BE 60 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAM
- [SDR DALA2016010900180](https://openairdocs.org/sdr/DALA2016010900180), Jan 8, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 222AAF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222AAF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMA
- [SDR DALA2016010900179](https://openairdocs.org/sdr/DALA2016010900179), Jan 8, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 22GF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222GF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 
- [SDR DALA2016010900178](https://openairdocs.org/sdr/DALA2016010900178), Jan 8, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL NR 211ARF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 211ARF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABL
- [SDR DALA2016010800098](https://openairdocs.org/sdr/DALA2016010800098), Jan 7, 2016: FLOOR SUPPORT. CORRODED. MAIN CABIN BETWEEN BS 149-200, LBL 8 FLOOR SUPPORT CORRODED. REMOVED CORROSION FROM MAIN CABIN FLOOR SUPPORT BS 149-200, LBL 8, WITH 100 PERCENT MATERIAL LOSS O
- [SDR DALA2016010700092](https://openairdocs.org/sdr/DALA2016010700092), Jan 6, 2016: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR SUPPORT CORRODED, BS 145, RBL 44. CORROSION DAMAGE ON FLOOR SUPPORT IN THE MAIN CABIN BS 145, RBL 44 FOUND TO BE OUT OF LIMITS DUE TO 100 PERCE
- [SDR DALA2016010600091](https://openairdocs.org/sdr/DALA2016010600091), Jan 5, 2016: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 589-899, RBL 54. THE SEAT TRACK WAS FOUND OUT LIMITS DUE TO SCALLOP DAMAGE. REPLACED THE SEAT TRACK IAW SRM 51-41-01 A
- [SDR DALA2016010500090](https://openairdocs.org/sdr/DALA2016010500090), Jan 4, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL NR 221BF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 221BF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE 
- [SDR DALA2016010500089](https://openairdocs.org/sdr/DALA2016010500089), Jan 4, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL NR 221JF IS DELAMINATED. MAIN CABIN FLOOR PANEL 221JF FOUND TO BE 30PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMA
- [SDR DALA2016010500088](https://openairdocs.org/sdr/DALA2016010500088), Jan 4, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL NR 221DF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 221DF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE 
- [SDR DALA2016010500087](https://openairdocs.org/sdr/DALA2016010500087), Jan 4, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL NR 211 ASF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 211ASF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWAB
- [SDR DALA2016010500086](https://openairdocs.org/sdr/DALA2016010500086), Jan 4, 2016: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 211 ATF IS DELAMINATED. MAIN CABIN FLOOR PANEL 211ATF FOUND TO BE 50 PERCENT DELAMINATED AND TO BE OUT OF LIMITS IAW SRM 53-20-50 ALLOWAB

All 63: https://openairdocs.org/deregistered/N988DN-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.