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Part 2: Step by step calculations for train sets or single vehicles; EN 14535: Railway applications — Brake discs for railway rolling stock Part 1: Brake discs pressed or shrunk onto the axle or drive shaft, dimensions and quality requirements; Part 2: Brake discs mounted onto the wheel, dimensions and quality requirements
Its 28.5 ft (8.7 m) span wing has an area of 112.1 sq ft (10.41 m 2). The standard engine available is the 100 hp (75 kW) Continental O-200 four-stroke powerplant. The 125 to 140 hp (93 to 104 kW) Lycoming O-290 has also been used.
The resulting aircraft, designated 2-T-1, was a single bay biplane of mixed, fabric-covered construction and with a tailskid undercarriage. Power was by a single 85 hp (63 kW) Cirrus III inline engine (as the Detroit Aircraft Corporation , the holding company for Great Lakes, also held the American rights to the Cirrus, so all Sports Trainers ...
SC-360 Super Chub. A modified Wag-Aero Sportsman 2+2 with a Lycoming O-360 engine. The Wag-Aero CHUBy CUBy is a high-wing four-seat homebuilt cabin monoplane of tube-and-fabric construction, it is a modern representation of the Piper PA-14 taildragger with elements from other Piper family members.
Its 28.00 ft (8.5 m) span wing lacks flaps and has a wing area of 126.0 sq ft (11.71 m 2). The acceptable power range is 85 to 160 hp (63 to 119 kW) and the standard engines used are the 125 hp (93 kW) Continental O-240 or the 125 hp (93 kW) Lycoming O-290 powerplants.
A Citation II seen shortly after landing. The Citation II (Model 550) was developed to provide the same docile low-speed handling and good short-field performance as the preceding Citation I while addressing a primary criticism of that aircraft — its relatively slow cruise speed of around 350 kn (650 km/h) at altitude. [2]
Data from Terpstra General characteristics Crew: one Capacity: one passenger Length: 18 ft 10.25 in (5.75 m) Wingspan: 21 ft 8 in (6.60 m) Height: 6 ft 7.75 in (2.03 m) Wing area: 152 sq ft (14.12 m 2) Empty weight: 875 lb (397 kg) Gross weight: 1,520 lb (690 kg) Powerplant: 1 × Lycoming O-360 4-cylinder, air-cooled, horizontally-opposed piston aircraft engine, 180 hp (134 kW) Performance ...
A higher-performance design revision was granted FAA approval as the 14-19 Cruisemaster on September 26, 1949. [2] The new model had structural upgrades, a 190 hp (142 kW) Lycoming O435-A engine, an increased gross weight of 2,600 lb (1,179 kg), hydraulically operated landing gear and flaps, and an improved interior. 99 of these airplanes were produced between 1949 and 1951.