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The F406 Caravan II is a twin turboprop engined, fourteen-seat low-wing monoplane of conventional aluminium (airframe) and steel (engine internal parts, exhaust, landing gear) construction. It is a development of the Cessna 404 Titan with two Pratt & Whitney PT6A turboprop engines.
The Cessna 208 Caravan is a utility aircraft produced by Cessna. The project was commenced on November 20, 1981, and the prototype first flew on December 9, 1982. The production model was certified by the FAA in October 1984 and its Cargomaster freighter variant was developed for FedEx. The 4 ft (1.2 m) longer 208B Super Cargomaster first flew ...
The airspeed indicator (ASI) or airspeed gauge is a flight instrument indicating the airspeed of an aircraft in kilometres per hour (km/h), knots (kn or kt), miles per hour (MPH) and/or metres per second (m/s).
The Soloy Pathfinder 21 was a twin-engined, single-propeller, turboprop aircraft. It is a modification by Soloy Aviation Solutions of a Cessna 208 Caravan airframe. First flown in 1995, the aircraft was essentially a stock Cessna 208 airframe that has been stretched by 72 inches (1.83 m) with structural reinforcement, powered by twin Pratt & Whitney Canada PT6D-114A engines in a side-by-side ...
The instrument is of little interest during launching and landing, with the exception of aerotow, where the pilot will usually want to avoid releasing in sink. The vertical speed indicator from a Robinson R22. This is the most common type used in aircraft, showing vertical speed in feet per minute (ft/min). Diaphragm Variometer operation
An annunciator panel, also known in some aircraft as the Centralized Warning Panel (CWP) or Caution Advisory Panel (CAP), is a group of lights used as a central indicator of status of equipment or systems in an aircraft, industrial process, building or other installation. Usually, the annunciator panel includes a main warning lamp or audible ...
Data from The Complete Guide to the Single-Engine Cessnas, AOPA Pilot, and Aircraft Specification No. A-768. General characteristics Crew: one Capacity: one passenger Length: 21 ft 6 in (6.55 m) Wingspan: 33 ft 4 in (10.16 m) Height: 6 ft 3 in (1.91 m) Wing area: 159.3 sq ft (14.80 m 2) Empty weight: 890 lb (404 kg) Gross weight: 1,450 lb (658 kg) Fuel capacity: 25 US gallons (95 liters), of ...
The horizontal situation indicator (commonly called the HSI) is an aircraft flight instrument normally mounted below the artificial horizon in place of a conventional heading indicator. It combines a heading indicator with a VHF omnidirectional range - instrument landing system (VOR-ILS) display.