Ad
related to: cessna 140 cruise speed requirements list of parts names
Search results
Results from the WOW.Com Content Network
The Cessna 140 was originally equipped with a Continental C-85-12 or C-85-12F horizontally opposed, air-cooled, four-cylinder piston engine of 85 hp (63 kW). The Continental C-90-12F or C-90-14F of 90 hp (67 kW) was optional, as was the 108 hp (81 kW) Lycoming O-235-C1 engine, an aftermarket installation authorized in the type certificate .
Model name First flight Number built Type Cessna Comet: 1917 1 Single piston engine monoplane sport plane Cessna Model A: 1927 70 Single piston engine monoplane utility airplane Cessna Model BW: 13 Single piston engine monoplane utility airplane Cessna CG-2: Glider Cessna CH-1: 1953 ~50 Single piston engine utility helicopter Cessna CH-4
Cessna C-34, C-37, C-38, C-145 & C-165 Airmaster series of light utility aircraft; Cessna T-50 Bobcat/Crane; Cessna 120 two-seat light aircraft, economy version of the Cessna 140; Cessna 140 two-seat light aircraft. Cessna 150 & 152 two-seat primary and aerobatic trainers; Cessna 162 Skycatcher two-seat light-sport aircraft; Cessna 170 four ...
To meet an Italian Army requirement for a short take-off liaison aircraft, SIAI-Marchetti modified the design of the Cessna 305A/O-1 Bird Dog with a new turboprop engine and a revised tail unit. The prototype first flew on 24 May 1969 powered by a 317 hp (236 kW) Allison 250 -B15C turboprop engine.
This is the speed at which drag is minimised. For jet aircraft, "long-range cruise" speed (LRC) is defined as the speed which gives 99% of the maximum range, for a given weight. This results in a 3–5% increase in speed. [8] It is also a more stable speed than maximum range speed, so gives less autothrottle movement. [9]
The Cessna Citation V (company designation Model 560) is a business jet built by Cessna that was in production from 1989 until 2011. During that time, 774 such craft were made. The first Model 560 prototype, a stretched version of the Citation S/II, flew in August 1987 and was certified on December 9, 1988.
Data from Les Ailes, May 1928 General characteristics Crew: Two pilots Capacity: Two passengers Length: 23 ft 9 in (7.23 m) Wingspan: 40 ft 7 in (12.36 m) Height: 7 ft 4 in (2.24 m) Wing area: 222 sq ft (20.6 m 2) Empty weight: 1,248 lb (566 kg) Gross weight: 2,273 lb (1,031 kg) Fuel capacity: 42 US gal; 35 imp gal (160 L) Powerplant: 1 × Anzani 10 10-cylinder radial, 120 hp (89 kW ...
Typical missions are 2.0–2.7 hours and with 400 kn (740 km/h) block speeds and most operators can fly 5–6 hours at Mach 0.72–0.76 for a 2,000–2,400 nmi range, with short takeoff requirements and good hot and high performance. A first hour fuel burn of 2,000–2,500 lb (910–1,130 kg) followed by 1,600–1,900 lb (730–860 kg) the ...
Ad
related to: cessna 140 cruise speed requirements list of parts names