Lockheed L-1011 TriStar

Lockheed

ICAOL101
Lockheed L-1011 TriStar aircraft
LockheedLockheed L-1011 TriStar
Photo: Mussi Katz · CC0 · Modified

Details

The Lockheed L-1011 TriStar was the last airliner Lockheed built, and the technically boldest of the three widebodies of its generation — the first with an autoland system certified for Category IIIb, and the only one whose centre engine is fed through an S-duct buried in the tail rather than hung in the fin. Rolls-Royce went into receivership developing its RB211 engine, and the delay let the DC-10 reach the market first. It never recovered the lost orders, and Lockheed left the airliner business for good when the line closed in 1984. The type certificate approves four models, from the 466,000 lb -1-14 to the 510,000 lb long-range -385-3. The cruise speed, cruise Mach, range, ceiling, climb rate, wingspan, length, height and take-off distance are EUROCONTROL's figures for the L101 type code rather than a certificate's: a type certificate states limits and weights, not cruise performance, and the source does not distinguish sub-variants.

4

Variants

Weightscompared to Airbus A380-800

MRW (Maximum Ramp Weight)

232,239kg
0
200k
400k
577k

MTOW (Maximum Takeoff Weight)

231,332kg
0
200k
400k
575k

MLW (Maximum Landing Weight)

172,365kg
0
150k
300k
395k

MZFW (Maximum Zero Fuel Weight)

153,314kg
0
150k
300k
369k

Capacitycompared to Airbus A380-800

Passenger Capacity

400passengers
0
300
600
853

47% of A380 maximum capacity

Crew

Total
3
Cockpit
3

Dimensions

Length

54.3m

Wingspan

47.4m

Height

16.9m

Engine Specifications

Engine Count

3×

Engine Model

Rolls-Royce RB211-22B-02, RB211-22C-02, RB211-524B-02 or RB211-524B3-02 turbofan

Fuel & Cargo

Fuel Capacity

120,704 L

Production & History

Production Status

Out of production

Manufacturing Period

1968–1984

First Flight

November 16, 1970

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