# N688DR: 2015 Embraer ERJ 190-200 LR, registration cancelled 2025-12-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 1, 2025
- Exported to: Serbia
- Status when cancelled: Valid registration
- Airframe: [Embraer ERJ 190-200 LR](https://openairdocs.org/model/embraer-erj-190-200-lr) (registry code 3260520)
- Engine: [GE CF34-10E5A1](https://openairdocs.org/engine/ge-cf34-10e5a1) (registry code 30022)
- Data sheets: [TCDS A57NM](https://openairdocs.org/tcds/A57NM), [TCDS E00070EN](https://openairdocs.org/tcds/E00070EN) (OpenAirDocs)
- Serial number: 19000688
- Year built: 2015
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 13, 2025
- Certificate issued: September 12, 2025
- Last registry action: September 12, 2025
- Mode S code: A9214A
- Owner when cancelled: [Wilmington Trust Company Owner Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20OWNER%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N688DR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=688DR
- Page: https://openairdocs.org/deregistered/N688DR-2025-12-01

From the FAA registry file of November 7, 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 Embraer ERJ 190-200 LR: https://openairdocs.org/model/embraer-erj-190-200-lr.md

## Service difficulty reports (12)

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

- [SDR EE4Y2025110523420](https://openairdocs.org/sdr/EE4Y2025110523420), Nov 5, 2025: RIB. CORRODED. DURING THE ACCOMPLISHMENT OF TASK CARD 57-50-033-1295, AZORRA AVIATION IDENTIFIED CORROSION ON THE RH WING IINBOARD FLAP RIB 1 LOWER FLANGE. THIS CONDITION WAS 
- [SDR EE4Y2025110523419](https://openairdocs.org/sdr/EE4Y2025110523419), Nov 5, 2025: RIB. CORRODED. DURING THE ACCOMPLISHMENT OF TASK CARD 57-50-033-1295, AZORRA AVIATION IDENTIFIED CORROSION ON THE RH WING INBOARD FLAP RIB 1 LOWER FLANGE. THIS CONDITION WAS R
- [SDR EE4Y2025100623293](https://openairdocs.org/sdr/EE4Y2025100623293), Oct 6, 2025: INLET. DENTED. DURING THE STRUCTURAL INSPECTION, IT WAS FOUND P/N 341-1010-511A, S/N 1395001, AIR INLET MODULE WITH SEVERAL DENTS ON THE INNER BARREL UPPER AND LOWER ACOUSTIC 
- [SDR EE4Y2025100623292](https://openairdocs.org/sdr/EE4Y2025100623292), Oct 6, 2025: INLET. DENTED. DURING THE STRUCTURAL INSPECTION, IT WAS FOUND P/N 341-1010-509F, S/N 1192001, AIR INLET MODULE WITH SEVERAL DENTS ON THE INNER BARREL UPPER AND LOWER ACOUSTIC 
- [SDR EE4Y2025100623291](https://openairdocs.org/sdr/EE4Y2025100623291), Oct 6, 2025: SKIN. DAMAGED. AZORRA REPORTS THAT DURING THE STRUCTURE INSPECTION, WE FOUND THE CENTER FUSELAGE I – AT FR31+380MM, S-26R+30MM EXTERNAL SKIN WITH LIGHTNING STRIKE. THE DAMAGE 
- [SDR EE4Y2025100623290](https://openairdocs.org/sdr/EE4Y2025100623290), Oct 6, 2025: SKIN. DAMAGED. AZORRA REPORTS THAT DURING THE STRUCTURE INSPECTION, WAS FOUND THE CENTER FUSELAGE I – AT FR27+370MM, S-26R+60MM EXTERNAL SKIN WITH LIGHTNING STRIKE. THE DAMAGE
- [SDR EE4Y2025100623289](https://openairdocs.org/sdr/EE4Y2025100623289), Oct 6, 2025: SKIN. DAMAGED. DURING THE STRUCTURAL INSPECTION, IT WAS FOUND ON FORWARD FUSELAGE, AT FR18+18MM AND STGR-26R+85MM, EXTERNAL SKIN WITH A LIGHTNING STRIKE DAMAGE. EVALUATED THOU
- [SDR EE4Y2025100623287](https://openairdocs.org/sdr/EE4Y2025100623287), Oct 6, 2025: SKIN. SCRATCHED. DURING THE STRUCTURAL INSPECTION IT WAS FOUND ON FORWARD FUSELAGE, RH-LATERAL SEAT TRACK FROM FR19 TO FR20 OTBD CROWN AREA WITH SCRATCH. EVALUATED BLEND OUT ARE
- [SDR EE4Y2025091723170](https://openairdocs.org/sdr/EE4Y2025091723170), Sep 17, 2025: SKIN. DAMAGED. DURING STRUCTURE INSPECTION, FOUND FWD FUSELAGE, FR 18+50MM, & S27L + 155MM (JUST 8.0MM FROM STR 28L FASTENER ROW), EXTERNAL SKIN WITH LIGHTNING STRIKE WITH EXI
- [SDR EE4Y2025091723168](https://openairdocs.org/sdr/EE4Y2025091723168), Sep 17, 2025: SKIN. DAMAGED. CENTER FUSELAGE I SKIN HAS A LIGHTNING STRIKE DAMAGE AT FRAME 30+290MM AND STRINGER 27R. SEE FIGURE 1. THE DAMAGE WAS REMOVED BY BLENDING AND WAS FOUND BEYOND L
- [SDR EE4Y2025091723167](https://openairdocs.org/sdr/EE4Y2025091723167), Sep 17, 2025: HEAT SHIELD. MISREPAIRED. DURING THE STRUCTURE INSPECTION, AN EXISTING REPAIR WAS FOUND INSTALLED WITHOUT RECORDS AT RH ENGINE PYLON HEAT SHIELD BAY #8. DUE TO THIS FACT, THE REPAIR WAS 
- [SDR EE4Y2025091723166](https://openairdocs.org/sdr/EE4Y2025091723166), Sep 17, 2025: SEAT. CORRUPTED. PER CUSTOMER REQUEST, PASSENGER CABIN SEATS DIAPHRAGMS 41191032-35, 41191032-36, 41191032-37, 41191032-38 WERE FOUND WITH CRACKS AND MUST BE REPAIRED.THE CONDIT

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