Midsize jet

N175GA

2025 Gulfstream GVIII-G700

Registered No accidents on file
Built
2025
Serial
87075
Class
Midsize jet
Engines
2 × Rolls Deut BR700-730B214
Status
Current as of October 2026
Registered owner
Gulfstream Aerospace Corp (Corporation)
Based
Savannah, GA
Registration record

N175GA on the FAA register

Type
2025 Gulfstream GVIII-G700
Serial
87075
Engines
2 × Rolls Deut BR700-730B214
Registered owner
Gulfstream Aerospace Corp
Savannah, GA
Certificate issued
—
Airworthiness date
2025-05-18
Registration expires
—
Airworthiness class
Standard · transport
Mode S (hex)
A12C57
Mode S (octal)
50226127
Seats (type)
9
Weight class
20,000 lb and over
Range (type)
7,750 nm
Cruise (type)
488 kt
Status
Current as of October 2026
Registry history

Timeline

  • 2025-05-18
    Airworthiness date on the current FAA record (standard category (transport)).
Overview

About N175GA

N175GA is a 2025 Gulfstream GVIII-G700, serial number 87075. The FAA register lists Gulfstream Aerospace Corp as the registrant in Savannah, Georgia.

The FAA aircraft reference file describes the type as a midsize jet, two Rolls Deut BR700-730B214 engines and 9 seats. Published figures for the type give a cruise speed of about 488 knots and a range of about 7,750 nm; actual performance depends on configuration, load and conditions. Its airworthiness certificate is standard category (transport), dated May 18, 2025.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N175GA. 1 earlier record involves a different aircraft that carried the same N-number.

Cruise
488 kt
Range
7,750 nm
Takeoff over 50 ft
6,250 ft
Landing over 50 ft
2,680 ft
Fuel burn
478 gph

Published figures for the Gulfstream GVIII-G700 type. They describe the model, not this airframe's equipment or condition.

Safety record

Accident & incident history

2000-04-04 Incident · Opa Locka, FL Damage: Minor NTSB · MIA00IA128
Reported aircraft: Dassault DA-20 — a different aircraft that carried the N175GA registration before this airframe.
Probable cause: The failure of the PIC to execute the complete procedure for emergency extension of the landing gear and the subsequent landing with the left main landing gear not locked fully down, resulting in an excursion off the runway and collision with a runway stanchion. A factor in the incident was the fatigue failure of the left MLG door hydraulic emergency slide valve bolts due to non-compliance with a 1984 factory service bulletin that recommended replacement with larger bolts.

Sources: NTSB aviation accident database and CAROL case system, FAA preliminary accident & incident notices. Search accident records

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Data: FAA Aircraft Registry (October 2026), including deregistered aircraft; NTSB and FAA accident data; fyiAero listing history. Individual owners' names are shown to signed-in users and street addresses are never shown. Type figures are published specifications, not this aircraft's.