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Lockheed Tristar - EuroHolidays




Class 7


Lockheed Tristar
Climb Chart
Climb Chart
Descent Chart
Descent Chart
Rolls-Royce engines
5000 nm range
330 pax, 11 t cargo capacity

Lockheed developed the shortened fuselage L-1011 TriStar 500 as a long range, smaller capacity derivative of the TriStar 200. Launched in August 1976, the key changes incorporated in the 500 over the standard L-1011s are the 4.11m (13ft 6in) shorter fuselage, greater takeoff weights, increased fuel capacity and more powerful RB211-524 engines. The shortened fuselage reduces seating capacity to a maximum of 330, 70 less than the standard length TriStars, while the below deck galleys that had been a feature of the L-1011 family were replaced with conventional main deck units. Other improvements include enhanced wing-to-fuselage and fuselage-to-rear engine intake fairings, automatic braking and automatic thrust control.

EuroHarmony used the L1011 as a Class 7 high capacity holiday charter aircraft when we entered into this highly competitive market in the 1980s. The aircraft was made by Mike Stone in Gmax.

General Information
Length50.05 m
Wingspan50.09 m
Height16.87 m
EngineRR RB211-524B
Cruise Speed483 kts
Service Ceiling43,000 ft
Gross Weight231.3 t
Capacity330 pax | 11 t
Crew3 pilots 12 hosts
Price50M EUR
ManufacturerLOCKHEED
PicturesAirliners.net
Operating Information
OEW232,749 lbs
MTOW510,000 lbs
Fuel Capacity31,600 gal
Fuel Weight221,200 lbs
Long Range AltitudeFL410
Long Range Speed504 kts
Max Speed570 kts
Range (MLoad...MFuel) 5,000... 6,100
Engine Thrust3 x 222.4 kN
Takeoff RWY Length (Min)7,000 ft
Takeoff RWY Length (Max)8,100 ft
Landing RWY Length6,000 ft
V Rotate / Flaps160kts / 18 deg
V Approach / Flaps145kts / 33 deg
Max climb rate3200 ft/min
Max descent rate-2700 ft/min
 
You will be able to fly this aircraft in 6 promotions



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Lockheed TristarMSFS 2004