This question about regulations regarding hydraulic flight controls got me thinking about the history of hydraulic or pilot-assisted controls. As aircraft get larger the control surfaces must grow proportionally but it seems that the forces required to move those surfaces may grow at a non-proportional rate. That means at some point they had to switch from a pure cable/pulley system to an assisted system.

What is the first aircraft to use an electrical/mechanical/hydraulic system to assist the pilot with the control surfaces? I'm mostly interested in an answer from a commercial aircraft standpoint.


1 Answer 1


It was the Lockheed Constellation and the P-80, both introduced in 1943. The DC-3 had hydraulic flaps, but the Connie was the first to have hydraulic flight controls.

The DC‐3 had wings flaps powered by hydraulics (1934). But it wasn’t until the early 1940s that hydraulics were used to power the primary flight control surfaces on the Lockheed Constellation and P‐80 (first US Jet Aircraft).

Source: A History of Aviation Actuation, Control and Fluid Power (PDF)

Also in 1943, the Lockheed P-38J-25-LO version of the WWII fighter aircraft was fitted with hydraulic boosted ailerons.

Source: Lockheed P-38J Lightning, Joe Baugher

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    $\begingroup$ The Bell P-59 predated the P-80 as the first US jet. However, if you describe the P-80 as the first operational US jet that would, I think, be correct since though a number of P-59s were built, they never saw combat. $\endgroup$
    – Terry
    Commented Feb 3, 2017 at 20:16
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    $\begingroup$ @Terry Thanks. I'd qualify the statement, but it's part of the source quotation. $\endgroup$
    – TomMcW
    Commented Feb 3, 2017 at 20:28
  • $\begingroup$ Which was the first fly-by-wire aircraft? $\endgroup$
    – Firee
    Commented Mar 15, 2017 at 14:30
  • $\begingroup$ @Firee AFAIK it was the Airbus A320 $\endgroup$
    – TomMcW
    Commented Mar 15, 2017 at 16:08

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