title: Lockheed Air Express
text: # Lockheed Air Express
  
  The Lockheed Air Express was the second aircraft design created by the Lockheed Aircraft Company after its founding in 1927; the type first flew in April 1928.
  
  ## Description
  
  The Air Express design incorporated the original fuselage of the Vega, but in order to meet the requirements of Western Air Express, the wing was raised to a parasol configuration above the fuselage and the cockpit was moved behind the wing, while a more powerful Pratt & Whitney Wasp engine was fitted to ease operations over the Sierra Nevada mountains. The design was a commercial success for the company although only seven were built, plus one Air Express Special.
  
  No Air Expresses have survived to the present day. One, registered NR3057, was flown by Roscoe Turner.
  
  ## Variants
  
  ### Lockheed 3 Air Express
  
      Single-engined passenger and mail transport aircraft, seating between four and six passengers in an enclosed cabin, able to carry up to 1,000-lb (454-kg) of mail, powered by a 410-hp (306-kW) Pratt & Whitney Wasp radial piston engine; seven built.
  
  ### Air Express Special
  
      One-off version built for Laura Ingalls, for a non-stop trans-Atlantic flight in 1931; one built.
  
  ## Operators
  
  ### Brazil
  
  * Panair do Brasil
  
  ### United States
  
  * American Airways
  * New York, Rio, and Buenos Aires Line
  * Pan American Airways
  * Texas Air Transport
  * Western Air Express
  
  ## Specifications
  
  Data from Lockheed Aircraft since 1913
  
  General characteristics
  
  * Crew: 1
  * Capacity: 4 passengers or 100 cu ft (2.8m³) mail
  * Length: 27 ft 6 in (8.38 m)
  * Wingspan: 42 ft 6 in (12.95 m)
  * Height: 8 ft 4.5 in (2.553 m)
  * Wing area: 288 sq ft (26.8 $m^2)$
  * Empty weight: 2,533 lb (1,149 kg)
  * Gross weight: 4,375 lb (1,984 kg)
  * Powerplant: 1 × Pratt & Whitney Wasp C , 420 hp (310 kW)
  
  Performance
  
  * Maximum speed: 176 mph (283 km/h, 153 kn) (with NACA cowling)
  * Cruise speed: 151 mph (243 km/h, 131 kn)
  * Range: 750 mi (1,210 km, 650 nmi)
  * Service ceiling: 17,250 ft (5,260 m)
  * Rate of climb: 1,460 ft/min (7.4 m/s)
  