# N690TP: 1982 Gulfstream AM Corp Comm Div 690D, registration cancelled 2019-07-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 23, 2019
- Exported to: Canada
- Status when cancelled: Valid registration
- Airframe: [Gulfstream AM Corp Comm Div 690D](https://openairdocs.org/model/gulfstream-am-corp-comm-div-690d) (registry code 3970405)
- Engine: [AiResearch TPE331 series](https://openairdocs.org/engine/airesearch-tpe331-series) (registry code 01514)
- Data sheets: [TCDS 2A4](https://openairdocs.org/tcds/2A4) (OpenAirDocs)
- Serial number: 15001
- Year built: 1982
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: June 15, 1999
- Certificate issued: April 3, 2018
- Last registry action: April 3, 2018
- Mode S code: A92C6D
- Owner when cancelled: [Isr Platforms LLC](https://openairdocs.org/faa-owner/ISR%20PLATFORMS%20LLC)
- Location: [Mclean, VA](https://openairdocs.org/faa-place/VA/Mclean)
- Owner type: LLC
- Owner's area on the map: 38.9511° N, 77.2292° W: Placed by OpenAirDocs at the center of ZIP code 22102, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N690TP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=690TP
- Page: https://openairdocs.org/deregistered/N690TP-2019-07-23

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 Gulfstream AM Corp Comm Div 690D: https://openairdocs.org/model/gulfstream-am-corp-comm-div-690d.md

## Service difficulty reports (1)

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

- [SDR MV5R055N](https://openairdocs.org/sdr/MV5R055N), Mar 13, 2001: ANGLE. CRACKED. RIGHT MAIN LANDING GEAR INBOARD GEAR MOUNT SIDE BRACE TO WING ATTACHMENT ANGLE CRACKED. CRACK LOCATED AT THE AFT PORTION OF THE ANGLE EXTENDING ONE INCH FORWARD

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