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The "Project Falcon Hear" program involved the optimizing of air-ground communications on the AS-211 by upgrading and installing the AN/ARC-34 UHF radios from the F-5A/B. [9] These aircraft were fitted with a belly-mounted gun pod, which was designed, developed and manufactured by Philippine company Aerotech Industries Philippines, Inc. (AIPI).
Electronic counter measures equipped C-212-200 of the Portuguese Air Force (late 1980s) Lloyd Aviation C-212 at Perth Airport (early 1990s). C-212A Original military production version. Also known as C-212-5, C-212-5 series 100M, and by the Spanish Air Force as the T-12B and D-3A (for medevac aircraft), 129 built. C-212AV VIP transport version ...
An aircraft flight manual (AFM) is a paper book or electronic information set containing information required to operate an aircraft of certain type or particular aircraft of that type (each AFM is tailored for a specific aircraft, though aircraft of the same type naturally have very similar AFMs). The information within an AFM is also referred ...
A Blue Air Boeing 737-300 in 2010 showing an older livery. Founded by Nelu Iordache, [14] Blue Air started operating in December 2004. Blue Air initially operated domestic and international flights, although domestic services were soon discontinued due to low sales and competition from TAROM, as well as Căile Ferate Române, the Romanian rail company.
The 1.8-litre engined cars and all diesels used Rover's PG1 5-speed manual gearbox throughout the car's life. The Rover 25 also saw the introduction, from autumn 2000, of the 16V twin-cam version of the 1.1 L K-Series engine, replacing the 1.1 single-cam 8-valve K-Series engine previously found in the Rover 211i.
Aircraft specific NATOPS manual cover. These manuals are typically about 2 inches thick. These are manuals for specific aircraft models containing standardized ground and flight operating procedures, training requirements, aircraft limitations, and technical data necessary for safe and effective operation of the aircraft.
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Data from Manufacturer General characteristics Crew: one Capacity: one passenger Length: 7.4 m (24 ft 3 in) Wingspan: 10.3 m (33 ft 10 in) Height: 2.4 m (7 ft 10 in) Wing area: 10.5 m 2 (113 sq ft) Empty weight: 520 kg (1,146 lb) Max takeoff weight: 750 kg (1,653 lb) Fuel capacity: 120 litres (26 imp gal; 32 US gal) Powerplant: 1 × Rotax 912S horizontally opposed piston aircraft engine, 73.5 ...