N975AT2002 Boeing 717-200
This N-number isn't registered right now. Below is its last known registration, canceled Nov 19, 2025.
Safety record in brief:No NTSB accidents or incidents since 198217 ADs may apply122 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Individual owner
- City, state
- Atlanta, GA
- Certificate issued
- Nov 20, 2023
- Canceled
- Nov 19, 2025
- Airworthiness
- Standard · Transport
- Airworthiness date
- Mar 20, 2002
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Boeing
- Model
- 717-200
- Year
- 2002
- Serial number
- 55035
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 100
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- AD964A
Engine
- Make and model
- Rolls-Royc Br 700 Series
- Type
- Turbo-fan
- Power
- 14,750 lb thrust
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2023 – 2025Individual ownerAtlanta, GA
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (17)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2025-21-05 | Landing Gear | Jan 2, 2026 | Airframe (717-200)Serial numbers per Boeing Alert Requirements Bulletin 717-32A0043 RB, dated February 12, 2025 |
| 2025-02-07 | Navigation | Mar 17, 2025 | Airframe (717-200)Only with: Collins GLU-2100 MMR P/N 822-2532-100 with software version earlier than COL4C-0087-0003 installed; MD-11/MD-11F modified by STC ST01895WI, 717-200 by STC ST04416AT, 747-400/-400F by STC ST01892WI, 757 by STC ST04436AT, 767 by STC ST04436AT or ST01883WI. |
| 2024-21-01 | Wings | Nov 7, 2024 | Airframe (717-200) |
| 2024-20-02 | Fuselage | Oct 21, 2024 | Airframe (717-200) |
| 2023-12-15 | Navigation | Jun 21, 2023 | Airframe (717-200) |
Show all 17 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2021-12-12 | Wings | Jul 29, 2021 | Airframe (717-200) |
| 2021-02-16 | Ice and rain protection | Mar 30, 2021 | Airframe (717-200) |
| 2018-10-08 | Stabilizers | May 31, 2018 | Airframe (717-200)Serial numbers per Boeing Alert Service Bulletin 717-55A0012, Revision 1, dated April 11, 2018 |
| 2017-01-03 | Standard practices/structures | Mar 14, 2017 | Airframe (717-200) |
| 2015-02-05 | Navigation | Mar 5, 2015 | Airframe (717-200) |
| 2014-05-22 | Fuselage | Apr 15, 2014 | Airframe (717-200) |
| 2013-19-22 | Fuselage | Nov 6, 2013 | Airframe (717-200) |
| 2012-12-09 | Horizontal Stabilizer Structure | Jul 23, 2012 | Airframe (717-200) |
| 2006-10-14 | McDonnell Douglas Model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9-50 Series… | Jun 21, 2006 | Airframe (717-200)Serial numbers per Boeing Service Bulletin 717-52-0007, Revision 1 (for Model 717-200 airplanes). Only with: All DC-9, MD-80, MD-88 and MD-90-30 airplanes; Model 717-200 airplanes only as identified in Boeing Service Bulletin 717-52-0007, Revision 1. |
| 2004-08-02 | McDonnell Douglas Model 717-200 Airplanes | May 19, 2004 | Airframe (717-200)Serial numbers per Boeing Service Bulletin 717-55-0003, dated June 18, 2002 |
| 2004-03-21 | McDonnell Douglas Model 717-200 Airplanes | Mar 17, 2004 | Airframe (717-200)Serial numbers per Boeing Service Bulletin 717-55-0005, dated June 27, 2002 |
| 2001-18-11 | McDonnell Douglas Model 717 Series Airplanes | Oct 1, 2001 | Airframe (717-200)Serial numbers per Boeing Alert Service Bulletin 717-27A0016, including Appendix, dated April 9, 2001 |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (122)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Wings · skin · delaminatedApr 8, 2019
SPOILER SKIN, UNSCHEDULED REMOVAL. FOUND DELAMINATED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · relay · faultyJul 2, 2018
OVERWING EMERGENCY LIGHTS WON'T EXTINGUISH AFTER SETTING EMERGENCY LIGHT SWITCH TO OFF AS REPORTED BY 2ND SHIFT (WILL ONLY SWITCH OFF ON 'ARM' POSITION). T/S PER FIM 33-51-00-802. REMOVED AND REPLACED OVERWING EMER EVAC LIGHTS BATTERY PACK RELAY R2-273 IAW AMM 33-51. OPERATIONAL CHECK SATISFACTORY…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · cusp web · corrodedSep 2, 2017
CORROSION ON THE CUSP WEB, RBL 54 AND 60, BS 416 TO 417, OUT OF LIMITS. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 216.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Wings · hinge · damagedDec 22, 2016
ELONGATED HOLE ON LT WING OUTBOARD FLAP FWD OUTBOARD HINGE IAW NRTC 00456. THE HINGE WAS REMOVED IAW AMM 20-50-01 AND AMM 27-50-01. THE BEARING WAS REPLACED, AND THE HINGE WAS REPAIRED IAW ER/A 552872-14 REV ORIGINAL
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedDec 20, 2016
CRACKED EXTERNAL FUSELAGE SKIN STA 1021 BTW LONG 13/14 LT. EXTERNAL FUSELAGE SKIN WAS REPAIRED PER ETI-17-16-183 REV. ORIGINAL AND ER/A 552865-14 REV ORIGINAL SECTION I. PERFORM REPETITIVE EXTERNAL GENERAL VISUAL INSPECTION OF THE REPAIR EVERY C-CHECK OR 24 MONTHS WHICHEVER COMES FIRST AFTER…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · support · crackedDec 19, 2016
AFT CARGO COMPARTMENT HAS A CRACK ON VERTICAL SUPPORT STA Y=816 LONG 30 (AMDS 5331-2001). CRACK DIMENSION IS .650". CRACK IN VERTICAL SUPPORT WAS STOP DRILLED PER SRM 53-00-00 FIG 201, HFEC WAS ACCOMPLISHED. NO CRACK WERE FOUND AFTER STOP DRILL PER NDT SPM 06-10-01.001. REPAIR PARTS WERE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · stiffener · crackedDec 19, 2016
AFT ACCESSORY COMPARTMENT HAS A CRACK ON STIFFENER STA Y=1200 CANT LONG PROJECTION 2L. STIFFENER WAS REPAIRED PER SRM 53-00-00 REPAIR 1 FIG 201 IN REF ORNRC 00394.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · angle · crackedDec 17, 2016
FWD CARGO DOOR: CRACK ON ANGLE UPPER EDGE OF DOOR BETWEEN BS 408-410. DAMAGE AREA WAS REPAIRED IAW SRM 52-00-00 REPAIR 2, AND DWG 9957663 REV W.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · support · crackedDec 17, 2016
FWD CARGO COMPARTMENT HAS A CRACKED SUPPORT ON STA Y=655 BTW LONGS 23R AND 24R. SUPPORT WAS REPAIRED PER SRM 53-00-00 FIG 201 SHEET 1 REF ONNRC 363.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · bulkhead web · crackedDec 16, 2016
FWD CARGO COMPARTMENT HAS CRACKED WEB OF FWD BULKHEAD BS 218, 15 INCHES ABOVE LONGERON 27. THE BULKHEAD WAS REPAIRED BS SRM 53-00-00 REPAIR 1.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 122 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026