Gulfstream 200

Overview
The Gulfstream G200 mid size corporate jet is built by Israel Aircraft Industries and was originally marketed and supported by subsidiary Galaxy Aerospace Inc, which was acquired by Gulfstream in May 2001.

The PW-306A engines boast increased fan diameter, improved hot end material and a forced mixer in the exhaust.

The G200 can be configured for eight to 18 passengers. The aircraft has a ten-passenger configuration that includes a conference / dining table for four, with a three-seat divan opposite. The G200 has a cabin height of 6ft 3in (1.91m) and a width of 7ft 2in (2.18m), allowing cabin configurations typically found in large business aircraft.

In February 2005, the Federal Aviation Administration (FAA) issued approved installation of the satellite-based High-Speed Data System (HSDS) in G200 jets, allowing passengers fast access to internet-based communications.

Specifications

Dimensions	Wing span 17.71m (58ft 1in) Length 18.97m (62ft 3in) Height 6.53m (21ft 5in) Wing area 34.3m2 (369.0sq ft).
Powerplants	Two 26.9kN (6040lb) Pratt & Whitney Canada PW-306A turbofans.
Weights	Basic operating 8709kg (19,200lb) Max takeoff 15,808kg (34,850lb).
Capacity	Flightcrew: 2 Seating: 8 or more in executive style arrangements, or up to 18 in a three abreast corporate shuttle configuration.
Performance	Typical cruising speed 871km/h (470kt). Max operating altitude 45,000ft. Max range with four passengers and reserves 6708km (3620nm) Max range with eight passengers and reserves 6226km (3360nm). Range with 18 passengers in corporate shuttle configuration with reserves 5022km (2710nm)