Estimate from the variant's published specs, 0-5; scores are only comparable within one criteria year. DC-10-10 (CF6-6D, MTOW 430,000 lb). Range 3,500 nmi with 270 passengers (Wikipedia table) = 2. Capacity 270 typical (222Y+48J) = 3.5. Speed Mach 0.82 typical = 3. Runway 9,000 ft at MTOW, sea level, ISA (Wikipedia table citing the DC-10 airport-planning manual) = 2.5. Comfort null: both Airways pieces are about the -30/-40 (Biman, Northwest), not the -10. Efficiency null: no published fuel-burn figure for this variant was found (airport-planning manual has none; operator pages checked give only fleet-level savings). Only 2 reviews found (key.aero BA captain interview blocked).[2]
Captain Ishrat Ahmed, a 27-year veteran of Biman, talked about the DC10 being a “pilot’s aircraft, very stable.
Sitting up high, with electric seats, huge windows, and a spacious cockpit, watching icebergs pass beneath those magnificent wings gave the impression of lounging on a cruise ship.
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This Day in Aviation: "29 August 1970: The McDonnell Douglas prototype widebody airliner, DC-10-10, N10DC, made its first flight from Long Beach Airport to Edwards Air Force Base"; AirlineReporter[4]: "the type's first flight on August 29th, 1970 from Long Beach".
Specifications table (CF6-6D, MTOW, range, takeoff field) and the 1968 American announcement.[1]
Rollout of N10DC on 23 July 1970 and its test record.[1]
Confirms the 29 August 1970 first flight, the 929-flight test program and the July 1971 certificate.[1]
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256 mixed-class seats in the L-1011-1 (exit limit 400) - range about 2,680-5,345 nmi across variants - in service since April 1972 (Eastern)
SumberRange about 2,900-4,050 nmi across variants - GE CF6 or Pratt and Whitney engines - first flight October 1972, in service since May 1974 (Air France)
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