Production History: 1987 to 2003
The original Gulfstream GIV (G-IV) entered service in 1987 with Rolls-Royce Tay 610 engines producing 13,850 lbs of thrust each. The aircraft delivered 4,000 nm range, a cabin 6 feet 1 inch tall and 7 feet 4 inches wide, and Mach 0.80 cruise speed. It was the first business jet capable of nonstop transatlantic crossings in both directions under standard wind conditions. That capability was not merely a performance milestone. It changed how corporations thought about international travel.
The GIV-SP (Special Performance) variant entered production in 1992 with upgraded Tay 611-8 engines producing 13,850 lbs of thrust (same rating but improved fuel efficiency), increased range to 4,220 nm, and reduced takeoff distance. The SP designation became the standard production model, and most surviving GIVs in active service today are SP variants. Of the 560 total GIV/GIV-SP produced, approximately 380 remain on civil registries worldwide.
Gulfstream produced the GIV at its Savannah, Georgia facility alongside the smaller GV, which debuted in 1997 and eventually replaced the GIV in the product line. The GV stretched the GIV fuselage, added Rolls-Royce BR710 engines, and pushed range to 5,800 nm. But the GIV's fundamental airframe design, cabin cross-section, and wing geometry carried forward through the GV, G550, and arguably into the current G500/G600 family.
Specifications and Performance
The GIV's cabin cross-section (7 feet 4 inches wide, 6 feet 1 inch tall) established the benchmark that competitors spent two decades trying to match. Bombardier's Challenger 604, launched in 1995, offered 7 feet 11 inches of width but only 6 feet of height. The Dassault Falcon 900, in production since 1986, offered 7 feet 8 inches of width but only 6 feet 2 inches of height. The GIV's combination of width, height, and 45-foot cabin length created a three-zone interior (forward galley, mid-cabin conference, aft stateroom) that became the standard heavy jet layout.
The Tay Engine: Reliability and Limitations
The Rolls-Royce Tay 610/611-8 engine is a derivative of the Rolls-Royce Spey, originally designed for military applications in the 1960s. The Tay added a new fan stage, improved turbine materials, and digital FADEC control. The engine compiled an excellent safety record across 560 GIV installations and additional use on the Fokker 70/100 regional jet family.
The Tay's limitation is fuel efficiency. Burning approximately 400-430 gallons per hour at cruise, the GIV-SP consumes roughly the same fuel as a modern G550 (which carries it 1,500 nm farther) and significantly more than a modern G500 (which matches the GIV's range on 280 gallons per hour). At $6.50 per gallon, the GIV-SP costs $2,600-$2,800 per hour in fuel alone. A G500 burns $1,820 per hour for equivalent mission capability.
Engine maintenance costs have increased as the Tay fleet ages. Rolls-Royce's CorporateCare program covers the GIV fleet, but hourly rates have risen as the pool of overhauled modules diminishes. Engine maintenance reserves run $450-$600 per flight hour on a power-by-the-hour plan. Hot section inspections occur at approximately 5,000-hour intervals. Full overhauls run $1.2-$1.8 million per engine.

