Cessna 421 Golden Eagle

Summary

Description

The Cessna 421 Golden Eagle was developed by Cessna in the 1960s as a pressurized derivative of the earlier Cessna 411. First produced in May 1967 as the 1968 model, it was equipped with "Stabila-Tip" fuel tanks on the wingtips, reminiscent of the Cessna 310, and a similar electro-mechanical landing gear system. The 421 was an immediate success, selling 200 aircraft in its first year. The design was refined in 1969 with a three-inch fuselage stretch, increased fuel capacity, and a higher gross weight, leading to its redesignation as the Cessna 421A. In 1971, further improvements led to the Cessna 421B, featuring increased empty and gross weights, a two-foot wingspan extension, and a two-foot nose stretch to accommodate a larger baggage section. In 1976, the 421C model appeared, incorporating wet wings and the removal of wingtip fuel tanks. Production concluded in 1985, with a total of 1,901 aircraft delivered.

The Cessna 421 is an all-metal, low-wing cabin monoplane distinguished by its retractable tricycle landing gear. It is powered by two wing-mounted, geared Continental GTSIO-520-D engines in a tractor configuration. The aircraft's cabin is accessed via a door located on the left-hand side, behind the wing, and it accommodates six occupants in the basic 421 variant, with later versions providing seating for up to ten individuals. The 421C model introduced a trailing-link design for the landing gear from the 1981 model year onward.

The Cessna 421 Golden Eagle is primarily a civil transport aircraft and is not typically equipped with offensive military armament. However, military operators have utilized the aircraft for various support roles such as communications, liaison, and surveillance, which can involve the carriage of specialized COMINT (communications intelligence) equipment as noted with the Philippine Army's use of the 421B variant. The airframe supports a maximum takeoff weight of 7,450 lb (3,379 kg), allowing for the accommodation of various internal payloads, including passenger seating or mission-specific equipment, depending on the requirements of the operating force.

The Cessna 421 has seen operational use in both military and civilian roles across the globe. Militaries that have employed the 421 include the Royal Bahamas Defence Force, the Bolivian Air Force and Army, the Royal Cambodian Air Force, the Ivory Coast Air Force, the Royal New Zealand Air Force (specifically No. 42 Squadron), the Pakistan Army, the Philippine Army (for COMINT purposes with one 421B unit), the Turkish Army Aviation, and the Air Force of Zimbabwe.

Main Variants:

• 421: The initial model, type approved in 1967, was powered by two 375 hp Continental GTSIO-520-D engines and had a maximum takeoff weight of 6,800 lb.

• 421A: This refined design, type approved in 1968, featured a slightly stretched fuselage, increased fuel capacity, and a higher gross weight.

• 421B Golden Eagle/Executive Commuter: This variant, type approved in 1970, was an eight-seat light passenger transport aircraft powered by two 375 hp Continental GTSIO-520-H engines, with a maximum takeoff weight that later models increased to 7,450 lb.

• 421C Golden Eagle/Executive Commuter: Featuring a new wing and landing gear, this model was type approved in 1975 and utilized either Continental GTSIO-520-L or GTSIO-520-N engines, while maintaining a maximum takeoff weight of 7,450 lb.

• Riley Turbine Rocket 421: This conversion of the Cessna 421 involved replacing the original engines with two Lycoming LTP101 turboprop engines, resulting in the designations R421BL and R421CL for the B and C models, respectively.

Technical specifications

Current operating countries

Country		Units
	Turkey	3
	Sri Lanka	1

Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.

All operators

Bahamas • Bolivia • Ivory Coast • Cambodia • Sri Lanka • New Zealand • Pakistan • Paraguay • Turkey

Photo of 421 Golden Eagle