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The enhanced 500 Citation I was introduced later in 1976 with the higher gross weight, improved JT15D-1A engines and the increased span wing. Speed and range were enhanced, the aircraft's service ceiling increased from 35,000 to 41,000 feet (11,000 to 12,000 m), and the cabin pressure at altitude was increased from 7.6 to 8.6 psi (52 to 59 kPa).
[1] The Citation XLS was the first "makeover" that the Excel received, with deliveries beginning in 2004. Besides a glass cockpit based on the Honeywell Primus 1000 EFIS avionics suite, the XLS featured the upgraded PW545B engines with increased performance. [4] It was produced in 330 units. [1] By 2018, ten year old XLS models were trading ...
The T-47A was a modified version of the Citation S/II (Model 552) for the U.S. Navy, featuring a 5 ft (1.5 m) wingspan reduction and hydraulically boosted ailerons for enhanced maneuverability, 2,900 lbf (13 kN) thrust JT15D-5 engines, a cockpit roof window for better pilot visibility during hard maneuvering, strengthened windshields for ...
Certified versions of the Pitts are now produced by Aviat Aircraft in Afton, Wyoming.It is available as the S-1 single-seater with an up to 200 hp (150 kW) flat-4 Lycoming engine and a 17 ft 4 in (5.28 m) wingspan, or as the S-2 two-seater variant featuring a 260 hp (194 kW) flat-6 Lycoming and a 20 ft (6.1 m) wingspan.
The Model 15 was designed in 1943–44, perhaps with the input of Taylorcraft founder C. G. Taylor. [7] The prototype, registered NX36320, first flew on November 1, 1944. [1] During testing, the Lycoming engine proved insufficiently powerful, [7] and it was replaced with a Franklin 6A4-150-B3 of 150 hp (120 kW). [1] [6] [7]
Instrument panel 1973 model Cessna 340 1973 model Cessna 340 front view Airstair door. The Cessna 340 is a twin piston engine pressurized business aircraft that was manufactured by Cessna. [1] [2] The Cessna 335 is an unpressurized version, which appears the same externally as the 340. [2] It sold in smaller numbers than the 340. [3]
Certified on 7 May 1971 and introduced in late 1971 as a 1972 model, the PA-34-200 Seneca is powered by a pair of Lycoming IO-360-C1E6 engines. The righthand engine is a Lycoming LIO-360-C1E6 engine variant, the "L" in its designation indicating that the crankshaft turns in the opposite direction, giving the Seneca counter-rotating engines.
Compared to the G-1159 Gulfstream II, the wing has 6 ft (1.8 m) more span and 5 ft (1.5 m) winglets added, the leading edge is longer and its contour is modified. The fuselage is 2 ft (0.6 m) longer aft of the main door, the radome is extended and there is a new curved windshield.