# N969AT: 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: [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: 55030
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 30, 2001
- Certificate issued: November 24, 2023
- Last registry action: November 24, 2023
- Mode S code: AD7DA7
- 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/N969AT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=969AT
- Page: https://openairdocs.org/deregistered/N969AT-2025-06-28

From the FAA registry file of October 27, 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 (144, newest 50)

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

- [SDR 2019F00226](https://openairdocs.org/sdr/2019F00226), Jun 20, 2019: SPOILER. DELAMINATED. SPOILER HAD DELAMINATION.
- [SDR DALA2018071604493](https://openairdocs.org/sdr/DALA2018071604493), Jul 15, 2018: LIGHT. DAMAGED. THE EMERGENCY SEAT MOUNTED LIGHTING IS DAMAGED AND INOPERATIVE AT SEAT 27C. MAINTENANCE RESECURED THE PANEL. OK FOR SERVICE.
- [SDR DALA2018071604492](https://openairdocs.org/sdr/DALA2018071604492), Jul 15, 2018: SIGN. LOOSE. THE EMERGENCY EXIT SIGN COVER AT DOOR 1L IS LOOSE. MAINTENANCE RESECURED EXIT THE EEPL SIGN AT 1L DOOR. AIRCRAT IS OK FOR SERVICE.
- [SDR DALA2017122108917](https://openairdocs.org/sdr/DALA2017122108917), Dec 20, 2017: ENGINE. ODOR. ODOR PREVALENT AFTER TAKEOFF AND THROUGHOUT FLIGHT. ODOR STRONGEST FROM RT PACK ON THE NR 2 ENGINE BLEED. NO CONTAMINATION WAS FOUND. FOUND TURBINE OIL ODOR ISO
- [SDR DALA2016120509588](https://openairdocs.org/sdr/DALA2016120509588), Dec 3, 2016: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT X=-52 BTW STA Y=132 TO Y=-148. AT COCKPIT FLOOR STRUCTURE. FLOOR SUPPORT WAS REPLACED PER DRAWING 9936533 ITEM 35 REV CM AND SRM 51-4
- [SDR DALA2016111708911](https://openairdocs.org/sdr/DALA2016111708911), Nov 16, 2016: WINDOW FRAME. CRACKED. CRACK ON LWR FWD SECTION OF RT SLIDE WINDOW COUNTER FRAME AT COCKPIT. DAMAGE AREA WAS REPAIRED PER ETI -17-16-170 REV 1 AND ER/A 551770-14 REV ORIG.
- [SDR DALA2016111608812](https://openairdocs.org/sdr/DALA2016111608812), Nov 15, 2016: PAN. CRACKED. CRACK ON INBD AND OUTBD PAN LOWER EDGE BS 388 AT FWD CARGO DOOR. INBD & OUTBD PAN LOWER EDGE WAS REPAIRED IAW ETI-17-16-161 REV 1 AND ER/A 551739-14 REV ORIGINA
- [SDR DALA2016111208742](https://openairdocs.org/sdr/DALA2016111208742), Nov 12, 2016: VANE. DENTED. SEVERAL DENTS ON AFT MOVABLE FLAP VANE ON THE LT WING. THE FLAP VANE WAS REPAIRED IAW SRM 57-53-01 REP.1 PARAGRAPH 4.
- [SDR DALA2016111208741](https://openairdocs.org/sdr/DALA2016111208741), Nov 11, 2016: SKIN. CRACKED. CRACKED FUSELAGE SKIN BS 1133 BETWEEN LONGERONS 2-3L. THE SKIN WAS REPAIRED IAW ETI-17-16-139 REV. 3 AND ER/A 551722-14AD REV. ORIGINAL.
- [SDR DALA2016111108739](https://openairdocs.org/sdr/DALA2016111108739), Nov 10, 2016: CARGO TRACK. CORRODED. CORROSION ON LT CARGO TRACK BETWEEN BS 899 TO 813 AT AFT CARGO BAY. THE DAMAGE SECTION WAS REPLACED IAW SRM 53-20-51 FIG 1.
- [SDR DALA2016111108707](https://openairdocs.org/sdr/DALA2016111108707), Nov 10, 2016: FITTING. CRACKED. CRACKED FRAME CLIP STA Y 1037 BTW LONG 16-17R AT RT AFT LAVATORY AREA. CLIP WAS REPAIRED PER ETI-17-16-145 REV 1 AND ER/A 551734-14 REV ORIG.
- [SDR DALA2016111108706](https://openairdocs.org/sdr/DALA2016111108706), Nov 10, 2016: FITTING. CRACKED. CRACKED FRAME CLIP STA Y=1037 LONG 16L TO 17L AT W2. CLIP WAS REPAIRED PER ETI-17-16-145 REV 1 AND ER/A 551734-14 REV ORIG.
- [SDR DALA2016111008442](https://openairdocs.org/sdr/DALA2016111008442), Nov 9, 2016: CARGO TRACK. CORRODED. CORROSION ON RT CARGO TRACK BS 899 - 1022 IN AFT CARGO BAY . THE CARGO TRACK WAS REPLACED IAW SRM 53-20-51 FIG 1.
- [SDR DALA2016111008441](https://openairdocs.org/sdr/DALA2016111008441), Nov 9, 2016: CARGO TRACK. CORRODED. CORROSION ON THE LEFT CARGO TRACK BS 899 - 1022. THE CARGO TRACK WAS REPLACED IAW SRM 53-20-51 FIG 1.
- [SDR DALA2016111008436](https://openairdocs.org/sdr/DALA2016111008436), Nov 9, 2016: FRAME. CRACKED. CRACKED FRAME ANGLE BS 1022 BETWEEN LONGERON 13 & 14L, REPLACED IAW SRM 51-41-02, 51-41-05 AND DRAWING 9912243 REV JS.
- [SDR DALA2016111008435](https://openairdocs.org/sdr/DALA2016111008435), Nov 9, 2016: FRAME. CRACKED. CRACKED FRAME BS 1037 LONGERON 17L. THE FRAME WAS REPAIRED IAW SRM 53-20-07 FIG 201 REPAIR 4.
- [SDR DALA2016110908365](https://openairdocs.org/sdr/DALA2016110908365), Nov 8, 2016: ACCESS PANEL. CRACKED. RIGHT WING FUEL ACCESS PANEL 620MB FOUND CRACKED. THE ACCESS PANEL WAS REPLACED, NO LEAK WAS FOUND.
- [SDR DALA2016110808337](https://openairdocs.org/sdr/DALA2016110808337), Nov 7, 2016: STRUCTURE. CRACKED. CRACK ON GROUND CONDITIONED AIR ACCESS CUT OUT. REPLACED PER ETI-17-16-147 REV ORIGINAL, ER/A 551737-14 REV ORIGINAL, AND SRM 51-41-02 AND 51-41-08.
- [SDR DALA2016110808336](https://openairdocs.org/sdr/DALA2016110808336), Nov 7, 2016: LONGERON. CORRODED. CORROSION ON LONGERON 30 FROM STA Y=908-Y=993 AT AFT CARGO COMPARTMENT. SECTION LONGERON 30 FROM STA Y=905-993 WAS REPLACED PER SRM 51-41-01, SRM 51-41-02, SRM 
- [SDR DALA2016110808335](https://openairdocs.org/sdr/DALA2016110808335), Nov 7, 2016: LONGERON. CORRODED. CORROSION ON LONGERON 30 FROM STA Y=988 TO Y=1009 AT AFT CARGO COMPARTMENT. SECTION LONGERON 30 FROM STA Y=900 TO Y=1012 WAS REPLACED PER SRM 51-41-01, SRM 51-4
- [SDR DALA2016110808334](https://openairdocs.org/sdr/DALA2016110808334), Nov 7, 2016: PAN. CRACKED. HIDDEN DAMAGE, CRACK ON INNER PAN STA Y=370 BTW BEAMS 1 AND 2 AT FWD CARGO COMPARTMENT DOOR. HFEC WAS ACCOMPLISHED ON CONFIRMED CRACK NDT SPM 06-10-01.001 IS 1.
- [SDR DALA2016110808333](https://openairdocs.org/sdr/DALA2016110808333), Nov 7, 2016: ANGLE. CORRODED. CORROSION ON ANGLES (2EA) STA Y=383 AND Y=415 FRONT OF LOWER DOOR JAMB PAN AT FWD CARGO COMPARTMENT. ANGLES (2EA) STA Y=383 AND Y=415 FRONT OF LOWER DOOR JAMB P
- [SDR DALA2016110708313](https://openairdocs.org/sdr/DALA2016110708313), Nov 6, 2016: PAN. WORN. WEAR ON INNER PAN OF AFT CARGO DOOR AT BS 994 BETWEEN BEAMS 1 AND 2. THE PAN WAS REPAIRED IAW SRM 52-30-02 REP 5 FIG 201.
- [SDR DALA2016110608312](https://openairdocs.org/sdr/DALA2016110608312), Nov 5, 2016: FRAME. CRACKED. CRACKED FRAME BS 715 RBL-LBL 44. THE FRAME WAS REPAIRED IAW SRM 51-70-11 FIG 201 REP 1.
- [SDR DALA2016110608311](https://openairdocs.org/sdr/DALA2016110608311), Nov 5, 2016: FRAME. CRACKED. CRACKED FRAME BS 674 LBL TO RBL 42. THE FRAME WAS REPAIRED IAW SRM 51-70-11 FIG 201 REP 1.
- [SDR DALA2016110608310](https://openairdocs.org/sdr/DALA2016110608310), Nov 5, 2016: FRAME. CORRODED. CRACKED LH/RH FRAMES BS 696 RBL 32 AND LBL-32 AT KEEL BEAM. THE FRAME WAS REPAIRED IAW SRM 51-70-11 FIG 201 REP 1 .
- [SDR DALA2016110608307](https://openairdocs.org/sdr/DALA2016110608307), Nov 5, 2016: ANGLE. WORN. WEAR ON LOWER RT ANGLE AT THE AFT CABIN BULKHEAD DOOR. THE DAMAGED AREA WAS REPAIRED IAW SRM 52-10-02-2R REPAIR 16 PARAGRAPH 4 B (2).
- [SDR DALA2016110608306](https://openairdocs.org/sdr/DALA2016110608306), Nov 5, 2016: ANGLE. CRACKED. CRACKED ANGLE ON FWD & AFT ENDS OF NR 1 BEAM AT RH FWD OVERWING EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-01, 51-41-02, 51-41-05, AND DWG 995773
- [SDR DALA2016110508305](https://openairdocs.org/sdr/DALA2016110508305), Nov 4, 2016: FLOOR PANEL. CRACKED. CRACKED COCKPIT FLOOR PANEL. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00 FIG 201.
- [SDR DALA2016110508304](https://openairdocs.org/sdr/DALA2016110508304), Nov 4, 2016: ACCESS PANEL. CORRODED. CORROSION ON CENTER TANK FUEL ACCESS PANEL 141AL. THE CORROSION WAS REMOVED AND FOUND OUT LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.
- [SDR DALA2016110508303](https://openairdocs.org/sdr/DALA2016110508303), Nov 4, 2016: ACCESS PANEL. CORRODED. CORROSION ON FUEL TANK ACCESS PANEL 620AT RT WING. THE CORROSION WAS REMOVED. FOUND OUT LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-10-01.
- [SDR DALA2016110408242](https://openairdocs.org/sdr/DALA2016110408242), Nov 3, 2016: ANGLE. CRACKED. CRACKED ANGLE ON FWD END OF BEAM NR 1, AT THE LT AFT OVERWING EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-02 AND 51-41-05.
- [SDR DALA2016110408241](https://openairdocs.org/sdr/DALA2016110408241), Nov 3, 2016: FLOORBEAM. CRACKED. CRACKED FLOORBEAM LBL 54.5 AND BS 737. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-01, 51-41-02, AND 51-41-05.
- [SDR DALA2016110408240](https://openairdocs.org/sdr/DALA2016110408240), Nov 3, 2016: PAN. CRACKED. CRACKED PAN BS 427 BETWEE BEAM 1 AND 2 AT FWD CARGO COMPARTMENT DOOR. HFEC INSPECTION WAS ACCOMPLISHED ON PAN BEAM 1 AND 2 AT FWD CARGO COMPARTMENT DOOR, 2 CRAC
- [SDR DALA2016110408239](https://openairdocs.org/sdr/DALA2016110408239), Nov 3, 2016: ANGLE. CRACKED. CRACKED ANGLE ON BEAM NR 1 FWD END, AT RT AFT OVERWING EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW DWG 9957735 REV. G, SRM 51-41-02 AND 51-41-05.
- [SDR DALA2016110308232](https://openairdocs.org/sdr/DALA2016110308232), Nov 2, 2016: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 223CF IN THE PAX CABIN. THE FLOOR PANEL WAS FABRICATED IAW SRM 53-20-50 AND REPLACED IAW SRM 53-20-50.
- [SDR DALA2016110308181](https://openairdocs.org/sdr/DALA2016110308181), Nov 2, 2016: PAN. CRACKED. CRACK ON INNER PAN STA Y=370 IN BEAM 3 (FWD EDGE) AT FWD CARGO COMPARTMENT DOOR. HFEC INSPECTION WAS ACCOMPLISHED IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR ,ONE C
- [SDR DALA2016110308180](https://openairdocs.org/sdr/DALA2016110308180), Nov 2, 2016: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 222KF AT PASSENGER CABIN. FLOOR PANEL 222KF AT PASSENGER CABIN WAS REPLACED PER SRM 53- 20-50.
- [SDR DALA2016110308179](https://openairdocs.org/sdr/DALA2016110308179), Nov 2, 2016: FITTING. CRACKED. CRACK FRAME CLIP 2 EA, STA Y=1152 PROJECTION LONG 2R AND 2L AT AFT ACCESSORY COMPARTMENT. REPLACED CLIPS PER DRAWING 9911860 REV L AND SRM 51-40-02 AND 51-40-05
- [SDR DALA2016110208141](https://openairdocs.org/sdr/DALA2016110208141), Nov 1, 2016: BEAM. CRACKED. CRACKED BEYOND STOP DRILL ON BEAM NR 1 AT PASSENGER ENTRANCE DOOR (L1). BEAM NR 1 AT PASSENGER ENTRANCE DOOR (L1) WAS REPAIRED PER B-717 SRM 52-10-2 REPAIR 7 FI
- [SDR DALA2016103107949](https://openairdocs.org/sdr/DALA2016103107949), Oct 30, 2016: DOUBLER. CORRODED. CORROSION ON PRODUCTION DOUBLER BETWEEN BS 579 - 598 X -60. THE DOUBLER WAS REPLACED IAW SRM 53-20-51 FIG. 1 ITEM 25 AND 51-41-05.
- [SDR DALA2016103107948](https://openairdocs.org/sdr/DALA2016103107948), Oct 30, 2016: SPLICE. CORRODED. CORROSION ON SPLICE FROM BS 579 TO 598 BETWEEN LONGERONS 17 - 18R. REPAIRED IAW SRM 53-20-51 FIG.1 AND 51-41-05.
- [SDR DALA2016103107947](https://openairdocs.org/sdr/DALA2016103107947), Oct 30, 2016: CUSP WEB. CORRODED. CORROSION ON RT CUSP WEB BETWEEN X -54 TO X -60 BS 638. DAMAGED AREA WAS TRIMMED AND REPAIRED IAW SRM 53-00-55 REPAIR 4 FIG 216, HFEC INSPECTION WAS ACCOMPLISHE
- [SDR DALA2016103107946](https://openairdocs.org/sdr/DALA2016103107946), Oct 30, 2016: SEAT TRACK. CORRODED. CORROSION ON RT SEAT TRACK X -22 AND X -44.5 BS 200 - 256. THE SEAT TRACK WAS REPLACED IAW SRM 53-20-52 REPAIR 5 FIGURE 201.
- [SDR DALA2016103107945](https://openairdocs.org/sdr/DALA2016103107945), Oct 30, 2016: CUSP WEB. CRACKED. CORROSION ON RT CUSP WEB X 14 TO X 60 BS 420. CORROSION WAS REMOVED IAW SRM 53-00-00 FIG 201. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER TR
- [SDR DALA2017010500103](https://openairdocs.org/sdr/DALA2017010500103), Oct 29, 2016: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BTW STA Y=200-208 AND X=-56 AT PAX CABIN (CS) (SM). DUE TO EXCESSIVE DAMAGE SUPPORT WAS REPAIRED PER SRM 53-00-00 REPAIR 1 FIG 201.
- [SDR DALA2016103008231](https://openairdocs.org/sdr/DALA2016103008231), Oct 29, 2016: FLOOR PANEL. DELAMINATED. DELAMINATION ON FLOOR PANEL IN COCKPIT. THE FLOOR PANEL WAS REPAIRED IAW AMM 20-60-10 340-801 SUBTASK 390-002.
- [SDR DALA2016103007944](https://openairdocs.org/sdr/DALA2016103007944), Oct 29, 2016: CHANNEL. CRACKED. CRACKED HAT CHANNEL. REPAIRED IAW SRM 53-20-50 REP. 5.
- [SDR DALA2016102907942](https://openairdocs.org/sdr/DALA2016102907942), Oct 28, 2016: CUSP WEB. CRACKED. CRACKED RT CUSP WEB BELOW SEAT TRACK X 44 BS 219. DAMAGE AREA WAS REPAIRED IAW SRM 53-00-55 FIG 219 AND 51-41-02.
- [SDR DALA2016102907941](https://openairdocs.org/sdr/DALA2016102907941), Oct 28, 2016: STOP FITTING. CRACKED. CRACKED STOP FITTINGS ON FWD EDGE OF AFT CARGO DOOR. THE STOP FITTINGS WERE REPLACED IAW SRM 51-41-01 AND 51-41-05.

All 144: https://openairdocs.org/deregistered/N969AT-2025-06-28/reports.md

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