# N989DN: 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: 55067
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 8, 2016
- Certificate issued: November 24, 2015
- Last registry action: June 23, 2023
- Mode S code: ADCCEB
- 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/N989DN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=989DN
- Page: https://openairdocs.org/deregistered/N989DN-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 (79, newest 50)

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

- [SDR DALA2019120407052](https://openairdocs.org/sdr/DALA2019120407052), Nov 26, 2019: RELEASE MECH. OUT OF POSITION. TAILCONE RELEASE CAM MECHANISM IS CLOCKED INCORRECTLY. NRC 001-0310:5300-2004/015 00218: RECLOCKED CAM REF AMDS CARD 5352-4002 TAILCONE INSTALL. (LP #1377133)
- [SDR DALA2019112836950](https://openairdocs.org/sdr/DALA2019112836950), Nov 22, 2019: SKIN. CORRODED. CORROSION AFT CARGO THRESHOLD DOOR PAN AND LOWER SKIN DOOR CUT OUT. NRC 001-0371:5231-2002/002 00002: COMPLIED WITH ER/A 582992-14 REV O. (LP #1371567)
- [SDR DALA2019111906760](https://openairdocs.org/sdr/DALA2019111906760), Nov 18, 2019: PAN. CORRODED. CORROSION WAS FOUND ON THE AFT CARGO DOOR JAMB PAN. MAINTENANCE REPLACED THE LOWER DOOR JAMB PAN SECTION REF B717 SRM 53-20-15-2R PROCEDURE 7. CORROSION LEVEL 1
- [SDR DALA2019101005821](https://openairdocs.org/sdr/DALA2019101005821), Oct 10, 2019: LENS. MISSING. THE AFT DOOR EMERGENCY EXIT LIGHT DIFFUSER COVER IS MISSING. MAINTENANCE LOCATED THE LENS AND RESECURED IT. SYSTEM IS NOW OK FOR SERVICE. (LP #6567004)
- [SDR DALA2019100105611](https://openairdocs.org/sdr/DALA2019100105611), Oct 1, 2019: BATTERY PACK. INOPERATIVE. THE RH OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE RH OVERWING EMERGENCY EXIT LIGHT BATTERY IAW B717 AMM 33-51-03. OPERATIONAL CHECK 
- [SDR DALA2019031901824](https://openairdocs.org/sdr/DALA2019031901824), Mar 19, 2019: BATTERY. DISCHARGED. THE EMERGENCY LIGHTS AT ROWS 15-19 ARE INOPERATIVE. MAINTENANCE INSTALLED A SERVICEABLE EMERGENCY LIGHT BATTERY POWER SUPPLY AND BATTERY PER AMM 33-51-03. (LP #
- [SDR DALA2018022001002](https://openairdocs.org/sdr/DALA2018022001002), Feb 19, 2018: SPAR CAP. DAMAGED. VERTICAL STABILIZER LEFT FRONT SPAR CAP DAMAGED, BELOW ZFS 52.267. REPAIRED THE SPAR CAP IAW ERA 565658-14AD, REV ORIGINAL.
- [SDR DALA2017060504514](https://openairdocs.org/sdr/DALA2017060504514), Jun 4, 2017: FRAME. CRACKED. FRAME 1225 CRACKED AT TAIL CONE ALIGNMENT PIN 7 O'CLOCK POSITION. REMOVED DAMAGED AREA REF 497316-14MA. MANUFACTURED DOUBLER AND DRILLED REF 497316-14MA. INSTAL
- [SDR DALA2017052304108](https://openairdocs.org/sdr/DALA2017052304108), May 23, 2017: LIGHT. CONTAMINATED. OVERWING AISLE OVERHEAD EMERGENCY EXIT SIGN PARTIALLY OBSCURED. REMOVED DEBRIS FROM INSIDE BOTH LENS, OPS CHECKED GOOD.
- [SDR DALA2016073105683](https://openairdocs.org/sdr/DALA2016073105683), Jul 29, 2016: CONNECTOR. FAILED. THE PILOT REPORTED THAT THE EEPL EXIT SIGN AT THE AFT DOOR AND AT THE OVERWING EXITS IN THE CABIN WERE FLASHING ON & OFF AND WOULD NOT RESPOND TO COMMANDS DURIN
- [SDR DALA2016073105681](https://openairdocs.org/sdr/DALA2016073105681), Jul 29, 2016: POWER SUPPLY. UNKNOWN. THE PILOT REPORTED THAT THE EEPL EXIT SIGN AT THE AFT DOOR AND AT THE OVERWING EXITS IN THE CABIN WERE FLASHING ON & OFF AND WOULD NOT RESPOND TO COMMANDS DURIN
- [SDR DALA2016072705623](https://openairdocs.org/sdr/DALA2016072705623), Jul 27, 2016: SWITCH. INTERMITTENT. THE PILOT REPORTED THAT SOME OF THE EMERGENCY LIGHTS IN THE AIRCRAFT HAD ILLUMINATED UNCOMMANDED. MAINTENANCE REPLACED AN INTERMITTENT EMERGENCY LIGHT SWITCH S1
- [SDR DALA2016072705588](https://openairdocs.org/sdr/DALA2016072705588), Jul 26, 2016: LIGHT. MALFUNCTIONED. THE F/A REPORTED THAT THE EEPL AT THE LOWER SIDEWALL OVERWING AND THE TAIL EXIT LIGHTS HAD ILLUMINATED UNCOMMANDED DURING FLIGHT. MAINTENANCE CYCLED THE EEPL SW
- [SDR DALA2016041103477](https://openairdocs.org/sdr/DALA2016041103477), Apr 5, 2016: LIGHT. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE LT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSY AND PERFORMED A
- [SDR DALA2016030401627](https://openairdocs.org/sdr/DALA2016030401627), Mar 3, 2016: FRAME. CRACKED. UPPER RADIUS BS 696 OF OVERWING FRAME TAB RT CRACKED. REPLACED FRAME AT RT BS 696 IAW SRM 51-41-02, 51-41-05, DWG SR95530013, REV: A, PN SA95530034-9.
- [SDR DALA2016022201273](https://openairdocs.org/sdr/DALA2016022201273), Feb 21, 2016: VANE. PUNCTURED. RIGHT WING, INBD FLAP VANE, INBD END HAS A PUNCTURE HOLE. REMOVED DAMAGE ON RT WING INBD FLAP VANE INBD END IAW SRM 57-53-01 REPAIR NR 1. MATERIAL REMOVED .75" 
- [SDR DALA2016102807812](https://openairdocs.org/sdr/DALA2016102807812), Feb 20, 2016: CARGO TRACK. CORRODED. FWD CARGO BAY. CARGO TRACK CORRODED AT BS 427 - 655. REMOVED CORROSION IAW SRM 51-10-04. FOUND TO BE BEYOND LIMITS IAW SRM 53-20- 52. REPLACED THE CARGO TRACK I
- [SDR DALA2016021901246](https://openairdocs.org/sdr/DALA2016021901246), Feb 18, 2016: LONGERON. DAMAGED. AFT CARGO COMPARTMENT CENTER LONGERON 30 HAS CHIPPED PAINT, POSSIBLE LIGHT CORROSION FRAME BS 908. REMOVED CORRODED IAW SRM 51-10-04 AT AFT CARGO BS 908, L30. E
- [SDR DALA2016102707774](https://openairdocs.org/sdr/DALA2016102707774), Feb 17, 2016: CARGO TRACK. CORRODED. AFT CARGO BAY, CARGO TRACK CORRODED BS 813 TO 1028 S26L. REMOVED CORROSION IAW SRM 51-10-04. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52 AND 51-30-07 AND DWG 595
- [SDR DALA2016021802609](https://openairdocs.org/sdr/DALA2016021802609), Feb 17, 2016: DUCT. DENTED. AFT ACCESSORY COMPARTMENT, GROUND AC DUCT LOWER SIDE HAS DENT.
- [SDR DALA2016021801685](https://openairdocs.org/sdr/DALA2016021801685), Feb 17, 2016: SLAT TRACK. GOUGED. RIGHT WING FIXED L/E INBD SIDE OF SLAT TRACK NR 2 HAS GOUGE ON DOUBLER. ASSOCIATED ER/A 14-542808 ADDED FOR AC 9589. REPLACED EXISTING REPAIR AT RT WING FIXED L
- [SDR DALA2016021501050](https://openairdocs.org/sdr/DALA2016021501050), Feb 1, 2016: CARGO TRACK. CORRODED. AFT CARGO BAY CARGO TRACK AT BS 813 - 1028, CORRODED, REMOVED CORROSION IAW SRM 51-10-04 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52, FIG 101 & 51-30-07, FIG
- [SDR DALA2016031501960](https://openairdocs.org/sdr/DALA2016031501960), Jan 29, 2016: SEAT TRACK. DAMAGED. MAIN CABIN SEAT TRACK HAS CORROSION, SCRATCHES AND GOUGES BETWEEN BS 237-589, RBL 22. REPLACED MAIN CABIN SEAT TRACK AT RBL 22, FS 237-589 IAW SRM 51-41-01. DAM
- [SDR DALA2016013001039](https://openairdocs.org/sdr/DALA2016013001039), Jan 29, 2016: CUSP WEB. CRACKED. MAIN CABIN CUSP WEB CRACKED AT LT BS 674 AND 696 BETWEEN LBL 44 -54. CUT OUT DAMAGE, FABRICATE AND INSTALLED CUSP WEB 7075-T6 .020, 2 EA SPLICES 7075-T6 .032 IA
- [SDR DALA2016013000746](https://openairdocs.org/sdr/DALA2016013000746), Jan 25, 2016: ANGLE. CRACKED. AFT ACCESSORY COMPARTMENT BS 1152 HAS CRACKED ANGLE L2R. REPLACED ANGLE IAW SRM 51-41-05 AND DWG 9911860, REV L.
- [SDR DALA2016102707768](https://openairdocs.org/sdr/DALA2016102707768), Jan 24, 2016: FLOORBEAM. CORRODED. BS 200 FLOORBEAM IS CORRODED BETWEEN RBL 44 & 52. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53- 00-00. THE FLOORBEAM WAS REPLACED IAW DWG 9936534 REV BW
- [SDR DALA2016012400589](https://openairdocs.org/sdr/DALA2016012400589), Jan 23, 2016: FORMER. CORRODED. LEFT KEEL BEAM BARREL, BS 715, OTBD END CORRODED FORMER. REPLACED LT KEELBEAM FORMER BS 715 IAW SRM 51-41-05, DWG 9923454, REV: F. REMOVED CORROSION & EVALUAED 
- [SDR DALA2016012500592](https://openairdocs.org/sdr/DALA2016012500592), Jan 22, 2016: FORMER. CRACKED. LEFT KEELBEAM BARREL BS 696, OTBD END OF FORMER CRACKED. REPLACED LT KEELBEAM FORMER BS 696 IAW SRM 51-41-02 AND 51-41-05 AND DWG 9923453, REV C, REV A.
- [SDR DALA2016012400591](https://openairdocs.org/sdr/DALA2016012400591), Jan 22, 2016: LONGERON. CRACKED. AFT ACCESSORY COMPARTMENT, BS 1133, LONG 2R CRACKED. REMOVED EWIS PROTECTION FROM WORK AREA IAW SWPM 20-10-10. CUTOUT DAMAGED AREA AT AFT ACCESSORY COMPARTMENT 
- [SDR DALA2016012400590](https://openairdocs.org/sdr/DALA2016012400590), Jan 22, 2016: FORMER. NOT REPORTED. REPLACED LT KEELBEAM FORMER BS 696 IAW SRM 51-41-02 AND 51-41-05 AND DWG 9923453, REV C, REV A.
- [SDR DALA2016012400587](https://openairdocs.org/sdr/DALA2016012400587), Jan 22, 2016: DOOR FRAME. CRACKED. CRACKED DOOR LANDING AT FWD OTBD CORNER OF GROUND CONDITIONED AIR SUPPLY DOOR CUTOUT. REMOVED DOOR ASSY FOR CONDITIONED AIR GROUND CONNECTION IAW SRM 51-41-01. 
- [SDR DALA2016012400586](https://openairdocs.org/sdr/DALA2016012400586), Jan 21, 2016: ANGLE. CORRODED. FWD GALLEY SERVICE DOOR LOWER JAMB AREA, Z-ANGLE IS CORRODED FWD OF RBL 54 SEAT TRACK AT FS 202. REMOVED CORROSION FWD GALLEY GALLEY SERVICE DOOR LOWER JAMB ARE
- [SDR DALA2016012400585](https://openairdocs.org/sdr/DALA2016012400585), Jan 21, 2016: FORMER. CRACKED. AFT ACCESSORY COMP BS 1116 BELOW LONGERON 15R FORMER CRACKED. REPLACED FORMER BS 1116 BELOW LONGERON 15R IAW SRM 51-41-02.
- [SDR DALA2016102607662](https://openairdocs.org/sdr/DALA2016102607662), Jan 19, 2016: DOUBLER. CORRODED. LOWER FUSELAGE ANTENNA INTERNAL DOUBLER IS CORRODED AT FS 212 BETWEEN L229L & LONGERON 30 IN E&E COMPARTMENT. APPLIED TOP COAT ON AREA IAW AMM 51-10-00 701. REM
- [SDR DALA2016012100482](https://openairdocs.org/sdr/DALA2016012100482), Jan 19, 2016: SHEAR TIE. CRACKED. AFT FUSELAGE BS 1022 BULKHEAD FWD FACE SHEAR TIE IS CRACKED BETWEEN LONGERON 6L AND L7L, MARKED. REMOVED SHEAR TIE AT AFT FUSELAGE FS 1022 BETWEEN LONG 6L TO L7
- [SDR DALA2016012000473](https://openairdocs.org/sdr/DALA2016012000473), Jan 19, 2016: FORMER. CRACKED. AFT ACCESSORY COMPARTMENT BS 1116 BELOW LONG 15L FORMER CRACKED. REMOVED FORMER BS 1116, BELOW LONGERON 15L IAW SRM 51-41-02 LOCATED, DRILLED, AND DEBARRED NEW 
- [SDR DALA2016012000472](https://openairdocs.org/sdr/DALA2016012000472), Jan 19, 2016: SUPPORT. CHAFED. RUDDER L/E PANEL 370GL CENTER MOUNTING SUPPORT IS CHAFED, MARKED. REMOVED DAMAGED SUPPORT AT RUDDER L/E IAW SRM 51-41-02 LOCATED AND DRILLED NEW SUPPORT IAW SRM
- [SDR DALA2016012300584](https://openairdocs.org/sdr/DALA2016012300584), Jan 16, 2016: FORMER. CRACKED. LEFT KEEL BEAM FORMER BS 674 CRACKED ON OTBD END. INSTALLED NEW FORMER IAW SRM 51-41-02, 51-41-05 AND DWG 9923453, REV C, REV A. REPLACED KEEL BEAM FORMER BS 67
- [SDR DALA2016102607661](https://openairdocs.org/sdr/DALA2016102607661), Jan 15, 2016: PANEL. CORRODED. LT KEEL BEAM PANEL BETWEEN STA 715-747 LONG 30 TO OB SIDE OF CONT KEEL EDGE CORRODED. INSTALLED FASTENERS LT KEEL BEAM STA 715-747 IAW SRM 51-41-02. REMOVED COR
- [SDR DALA2016102607660](https://openairdocs.org/sdr/DALA2016102607660), Jan 14, 2016: KEELBEAM. CORRODED. LT KEEL BEAM BARREL, BETWEEN STA 715-696 LONG 30 TO OB SIDE OF CANT KEEL EDGE CORRODED. TOPCOATED LT KEEL BEAM BARREL IAW SRM 51-10-04. REMOVED CORROSION LT KEE
- [SDR DALA2016012200580](https://openairdocs.org/sdr/DALA2016012200580), Jan 13, 2016: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 221 AF IS DAMAGED. MAIN CABIN FLOOR PANEL 221AF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50. ALLOWABLE DAMAGE 1
- [SDR DALA2016011600430](https://openairdocs.org/sdr/DALA2016011600430), Jan 13, 2016: FLOOR SUPPORT. CORRODED. AFT CARGO - SIDE PLATE FLOOR SUPPORT CORRODED AT BS 994, S 28L MARKED. REMOVED CORROSION AFT CARGO SIDE PLATE FLOOR SUPPORT BS 994 S28L, EVALUATED AREA FOUND OR
- [SDR DALA2016011600429](https://openairdocs.org/sdr/DALA2016011600429), Jan 13, 2016: SHEAR TIE. CORRODED. UPON REMOVAL OF RT KEEL BEAM BARREL FORMER BS 674 FOUND SEVERAL AREAS OF CORROSION ON THE FORMER SHEAR CLIP. REMOVED SHEAR CLIP FROM RT KEELBEAM FORMER BS 674 I
- [SDR DALA2016011600427](https://openairdocs.org/sdr/DALA2016011600427), Jan 13, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD NR 211ATF IS DELAMINATED. FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOOR
- [SDR DALA2016011500360](https://openairdocs.org/sdr/DALA2016011500360), Jan 13, 2016: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 221BF IS DAMAGED. MAIN CABIN FLOOR PANEL 221BF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. 
- [SDR DALA2016011500359](https://openairdocs.org/sdr/DALA2016011500359), Jan 13, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 221LF IS DELAMINATED. MAIN CABIN FLOOR PANEL 221LF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 
- [SDR DALA2016011500358](https://openairdocs.org/sdr/DALA2016011500358), Jan 13, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 211ANF IS DELAMINATED. MAIN CABIN FLOOR PANEL 211 AND FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMA
- [SDR DALA2016011500357](https://openairdocs.org/sdr/DALA2016011500357), Jan 13, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 222AEF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222 AEF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMA
- [SDR DALA2016011500356](https://openairdocs.org/sdr/DALA2016011500356), Jan 13, 2016: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 221EF IS DAMAGED. MAIN CABIN FLOOR PANEL NR 221EF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 
- [SDR DALA2016011500355](https://openairdocs.org/sdr/DALA2016011500355), Jan 13, 2016: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD, 211ALF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 211ALF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE 

All 79: https://openairdocs.org/deregistered/N989DN-2025-03-01/reports.md

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