Lockheed L1011-1 FDE v1
Copyright 2000 by Sam Chin
All Rights Reserved

MTOW: 430,000 lbs
MLW: 358,000 lbs
ZFW: 291,500 lbs
STALL: 108/148 
VMO/MMO: 350kias/M0.90
CRUISE: M.80 (econ) to 520ktas
Vref: 145 at MLW (48% total fuel)
V1/Vr/V2: 160/165/172 at MTOW
RANGE: 2,870 with full capacity/cargo (this air file is full capacity)

FAA Specifications

I - Model L-1011-385-1 (Transport Category Aircraft), Approved April 14, 1972

Engines: 	3 Rolls-Royce RB 211-22C-02 engines
	3 Rolls-Royce RB 211-22B engines

	-22C Engine
		Static thrust at sea level
		Takeoff (5 min.) 41,030 lbs. (flat rated to ISA 1 + 3.8 C)
		Maximum continuous 36,900 lbs. (flat rated to ISA + 10 C)
	-22B Engine
		Static thrust at sea level
		Takeoff (5 min.) 41,030 lbs. (flat rated to ISA + 13.9 C)
		42,670 lbs. (flat rated to ISA + 8.4 C)2
		Maximum continuous 40,140 lbs. (flat rated to ISA + 9.0 C to 25,000 ft. and
		ISA + 13 C above 25,000 ft.)
		40,140 lbs. (flat rated to ISA + 8.4 C to 5600 ft.
		Thereafter, thrust reduces linearly to be
		same as the -22B at ISA + 13.9 C and 10,000 ft.)

		N 1 (%)	 N 2 (%)	 N 3 (%)	 N 1 (%)	 N 2 (%)	 N 3 (%)
Takeoff(5min) 	99.0 	99.5	 99.5 	99.5 	101.5 	95.0
Max continuous 	97.5 	98.8 	94.3 	101.0 	101.5 	93.7
Ground idle 	24			25

Maximum turbine temperature (measured at low pressure NGV 6 :
		-22C Engine Only 		-22B Engine Only
Takeoff (5 min.) 	1328 F (720 C) 		1342 F (728 C)
Maximum continuous 1292 F (700 C) 	1292 F (700 C)
Starting 		1022 F (550 C) 		1022 F (550 C)
Reverse thrust (30 sec.) 1265 F (685 C) 	1265 F (685 C)5
Max for acceleration (2 min.) 1337 F (725 C) 	1360 F (738 C)

V fe Load Relieving System Operative
Flap Angle Selected, in Degrees Knots IAS/mach No.
4 	250K M = 0.6
10 	230K M = 0.5
14 	215K M = 0.5
18 	210K M = 0.5
22 	205K M = 0.5
27 	200K M = 0.5
33 	170K M = 0.4
42 	164K M = 0.4

V LO (landing gear)
Retraction 230k not to exceed (M = 0.85)
Extension 300k not to exceed (M = 0.85)
V L3 (landing gear extended) 300k not to exceed (M = 0.85)

VMO/MMO   	IAS
At Sea Level 	350K
At 10,000 feet 	375K
At 26,200 feet 	375K (M = 0.9)
At 42,000 feet 	264K (M = 0.9)
At 43,000 feet 	256K (M = 0.9)