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The ACME Anser was an amphibious twin-jet utility aircraft that was developed in the United States by Air Craft Marine Engineering in 1958. The project was cancelled before the prototype was complete.

Design and development

The ACME Company (Air Craft Marine Engineering Company), was formed in September 1954 by Robert M. Berns, a former Lockheed Missile Systems design engineer, to design and develop the prototype of an eight-seat amphibian executive aircraft. The ACME Anser, (Anser from 'Analytical Services', a contributor to the design), was to have been a 6-passenger jet-powered amphibian incorporating advance features; an advanced hull design from NACA test tank data, boundary layer control system and a retractable outboard motor, for taxiing on water. Aviation Week 9 September 1957

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General characteristics

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|crew=2

|capacity=6 pax /

|length ft=38

|length in=

|length note=

|span ft=46

|span in=

|span note=

|height ft=11

|height in=6

|height note=<br>

  • Cabin width:
  • Cabin length:
  • Cabin headroom:
  • Cabin volume:
  • Baggage hold volume:

|wing area sqft=264.5

|wing area note=

|aspect ratio=7.83

|airfoil=NACA 7 series

|empty weight lb=

|empty weight note=

|gross weight lb=8900

|gross weight note=

|max takeoff weight lb=

|max takeoff weight note=

|fuel capacity=total capacity / ; 2x wing leading edge tanks, 2x wing-tip tanks and a hull mounted bag tank

|more general=

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Powerplant

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|eng1 number=2

|eng1 name=Continental 420

|eng1 type=turbofan engines

|eng1 kn=<!-- jet/rocket engines -->

|eng1 lbf=790

|eng1 note=

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Performance

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|max speed mph=370

|max speed note=

|cruise speed mph=340

|cruise speed note=<br>

  • Landing speed:

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|stall speed note=

|never exceed speed mph=

|never exceed speed note=

|minimum control speed mph=

|minimum control speed note=

|range mi=1160

|range note=

|ferry range mi=

|ferry range note=

|endurance=<!-- if range unknown -->

|ceiling ft=

|ceiling note=

|climb rate ftmin=1200

|climb rate note=

|time to altitude=

|lift to drag=

|wing loading lb/sqft=

|wing loading note=

|fuel consumption lb/mi=

|thrust/weight=

|more performance=

|avionics=

References

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