B77L

BOEING 777-200LR and 777-F

Aircraft
Name
777-200LR and 777-F
Manufacturer
Body
Wide
Wing
Fixed Wing
Position
Low wing
Tail
Regular tail (Dihedral)
WTC
H
APC
C
Type Code
L2J
RFF Category
9
Engine
Jet
Engine Count
Multi
Position
Underwing mounted
Landing gear
Tricycle retractable
Manufacturered as
BOEING 777-200LR
BOEING 777-F

B77L

The 777-200LR became the world's longest-range commercial airliner when it entered service in 2006. It has a maximum range of 9,395 nm and was intended for ultra-long-haul routes such as New York to Singapore, or Chicago to Sydney - up to about 19 hours flying time. The -200LR features an increased MTOW and the same wing as the 777-300ER. The 777F is a cargo version of this variant. Three optional auxiliary fuel tanks take the baseline fuel tank capacity from 181,289 l to 203,570 l. Other new features include raked wingtips, redesigned main landing gear, and additional structural strengthening. As with the -300ER, the -200LR is equipped with wingtip extensions of 3.90 m. B77L is member of the B777 family of aircraft.

Technical Data
Wing span (metric)
64.80 m
Length (metric)
63.70 m
Height (metric)
18.60 m
Powerplant

2 x GE 90-110B1 (489 kN) or
2 x GE 90-115BL (512 kN).

Engine Model(s)
General Electric GE90
Indicative Performance Data
Take-Off
V2
123 kts
Distance
2970 m
MTOW
347450 kg
Initial Climb (to 5000 ft)
IAS
175 kts
ROC
2500 ft/min
Initial Climb (to FL150)
IAS
280 kts
ROC
2000
Initial Climb (to FL240)
IAS
280 kts
ROC
1500 ft/min
MACH Climb
MACH
0.83
ROC
2000 ft/min
Cruise
TAS
490 kts
MACH
0.84
Ceiling
431
Range
9380 NM
Initial Descent (to FL240)
MACH
0.84
ROD
1000 ft/min
Descent (to FL100)
IAS
240 kts
ROD
3000 ft/min
Descent (FL100 & below)
IAS
210 kts
MCS
240 kts
ROD
2000 ft/min
Approach
Vapp (IAS)
140 kts
Distance
1700 m

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