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foot per minute: fpm ≡ 1 ft/min = 5.08 × 10 −3 m/s: foot per second: fps ≡ 1 ft/s = 3.048 × 10 −1 m/s: furlong per fortnight: ≡ furlong/fortnight ≈ 1.663 095 × 10 −4 m/s: inch per hour: iph ≡ 1 in/h = 7.0 5 × 10 −6 m/s inch per minute: ipm ≡ 1 in/min = 4.2 3 × 10 −4 m/s inch per second: ips ≡ 1 in/s = 2.54 × 10 − ...
Data from World Directory of Leisure Aviation 2011–12 and Alisport General characteristics Crew: one Length: 6.35 m (20 ft 10 in) Wingspan: 13.3 m (43 ft 8 in) Height: 1.25 m (4 ft 1 in) Wing area: 8.9 m 2 (96 sq ft) Aspect ratio: 20:1 Airfoil: 16% IMD 050 Empty weight: 205 kg (452 lb) Gross weight: 315 kg (694 lb) Propellers: 2-bladed composite, 1.0 m (3 ft 3 in) diameter Performance Stall ...
Speed limit sign in the Republic of Ireland, using "km/h.". The SI representations, classified as symbols, are "km/h", "km h −1" and "km·h −1".Several other abbreviations of "kilometres per hour" have been used since the term was introduced and many are still in use today; for example, dictionaries list "kph", [3] [4] [5] "kmph" and "km/hr" [6] as English abbreviations.
A very strong typhoon has wind speeds between 85–104 kn (44–54 m/s; 98–120 mph; 157–193 km/h), while a violent typhoon has wind speeds of 105 kn (54 m/s; 121 mph; 194 km/h) or greater. [8] The HKO, SMG and the CMA also divide the typhoon category into three categories, with both assigning a maximum wind speed of 80 kn (41 m/s; 92 mph ...
Cruise speed: 220 km/h (140 mph, 120 kn) at 3,660 m (12,010 ft) (65% power) Stall speed: 78 km/h (48 mph, 42 kn) (flaps down) Never exceed speed: 281 km/h (175 mph, 152 kn) Range: 1,250 km (780 mi, 670 nmi) at 3,660 m (12,010 ft) (65% power) Endurance: 6 hr 30 min (55% power) Rate of climb: 5.80 m/s (1,142 ft/min) Takeoff run to 15 m (50 ft ...
Data from Jane's All the World's Aircraft 2010-11 General characteristics Crew: 1 Capacity: 3 pax Length: 6.61 m (21 ft 8 in) Wingspan: 8.6 m (28 ft 3 in) Height: 2.6 m (8 ft 6 in) Wing area: 11 m 2 (120 sq ft) Empty weight: 336 kg (741 lb) Max takeoff weight: 600 kg (1,323 lb) Max useful weight: 269 kg (593 lb) Powerplant: 1 × Rotax 912 ULS 4-cylinder air-cooled horizontally-opposed piston ...
AMF Microflight began production of the Chevvron in 1987, with 19 completed at their Membury factory by 1990. [3] A single example was built of the Sea Chevvron, a floatplane version fitted with a more powerful (48 horsepower (36 kW)) König engine, [4] while examples were also fitted with a 45 horsepower (34 kW) Limbach engine.
Maximum speed: 259 km/h (161 mph, 140 kn) at 10,000 feet MSL; Cruise speed: 230 km/h (140 mph, 120 kn) Range: 1,759 km (1,093 mi, 950 nmi) Endurance: 9.2 hr @ 55% power; Maximum glide ratio: 53:1; Rate of climb: 4.21 m/s (829 ft/min) Wing loading: 45.11 kg/m 2 (9.24 lb/sq ft) at MTOW