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Armstrong Whitworth Atlas ✕ Aermacchi AL-60 ✕
Manufacturer Armstrong Whitworth Aermacchi
Description The Armstrong Whitworth Atlas was a British single-engine biplane designed and built by Armstrong Whitworth Aircraft. The Aermacchi AL-60 is a light civil utility aircraft of the late 1950s and early 1960s, originally designed by Al Mooney of Lockheed in the United States.
ICAO Code LA60
First Flight 1925-05-10 1959-09-15
Entry Into service 1927-01-01
Production End 1933-01-01 1979-01-01
Service End 1935-01-01
Designer Armstrong Whitworth Al Mooney
Type Army cooperation aircraft Utility aircraft
Length (m) 8.5344 8.79
Height (m) 3.048 3.25
Cockpit Crew 2
Max Seating 8
Max Speed (km/h) 228.5268 238
Cruise Speed (km/h) 220
Min Speed (km/h) 87
Max Ceiling (m) 5120.64 6700
Rate of Climb (m/s) 4.267
Armament 1 × forward firing .303 in (7.7 mm) Vickers machine gun and 1 × .303 in (7.7 mm) Lewis Gun on Scarff ring in rear cockpit; Up to 4 × 112 lb (51 kg) bombs under wings
Capacity Description 6-8 passengers / 602 kg max. payload
Endurance (h) 3
Number Built 478 180
Powerplant Description 1 × Armstrong Siddeley Jaguar IVC 14-cylinder two-row air-cooled radial engine, 336 kW (450 hp) each 1 × Continental TSIO-470-B-A1A 6-cylinder air-cooled horizontally-opposed piston engine, 194 kW (260 hp) each
Primary Users Royal Air Force, Royal Canadian Air Force Mexican Air Force, South African Air Force
Status Retired
Wikipedia Article (URL) en.wikipedia.org/wiki/Armstrong_Whitworth_Atlas en.wikipedia.org/wiki/Aermacchi_AL-60
Flat Wing Span (m) 11.8872 11.84
Flat Wing Area (m²) 36.3251 19.54
Flat Wing Aspect Ratio 7.2
Wake Category L
Aircraft Engine Armstrong Siddeley Jaguar
Number of Engines 1 1