1944 Lockheed Lodestar

Howard 250 executive conversion

Condition: Currently flying & Airworthy

Updated by Howard Aero as the Howard 250, the conversion was to prove popular with about 22 aircraft modified in the early 1960s in San Antonio Texas.

 

  • Some of the upgrades include:
  • Increased fuel capacity to 1100 gallons
  • Gross takeoff weight increased to 22,500 lbs.
  • Extended wing tips
  • Specially developed square tip propellers
  • Engine cowling to nacelle streamlining
  • High flow exhaust system
  • Two speed superchargers
  • Engine fire extinguishers
  • Electric elevator trim
  • In-flight fuel dump system
  • Streamlined flap and wing trailing edges
  • Fully enclosed landing gear doors
  • 12 place oxygen system
  • Stretched cabin picture windows
  • Curved glass windshields
  • Extended cockpit side windows
  • Autopilot
  • Extended nose for Bendix weather radar
  • Freon air conditioning
  • Stinger tail for streamlining
  • Deice boots

 

Lockheed began to develop a larger and updated version of the Model 14 Super Electra in 1939 after the earlier design did not prove a commercial success.

 

The company modified the fourth Super Electra by adding two more rows of seats in a fuselage stretched by 5ft 6in to 49ft 10in. The first of three altered aircraft flew on September 21, 1939, with the first true Model 18 following on February 2, 1940.

 

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