BELL-BOEING V-22

Aircraft
Name: 
V-22
Manufacturer: 
Body: 
Narrow
Wing: 
Rotary
Position: 
Three-blade tandem rotors
Tail: 
Double fin, low set
WTC
M
Type Code: 
T2T
Engine: 
Turboshaft
Engine Count: 
Multi
Position: 
(Front) Wing leading mounted
Landing gear: 
Tricycle retractable
Manufacturered as
BELL-BOEING 901 Osprey
BELL-BOEING CV-22 Osprey
BELL-BOEING MV-22 Osprey
BELL-BOEING Osprey
BELL-BOEING V-22 Osprey

V22

The Bell-Boeing V-22 Osprey is an American multi-mission, military, tiltrotor aircraft with both a vertical takeoff and landing (Vertical Take-Off and Landing (VTOL)), and short takeoff and landing (Short Take-Off and Landing (STOL)) capability. It is designed to combine the functionality of a conventional helicopter with the long-range, high-speed cruise performance of a turboprop aircraft.

Technical Data
Wing span: 
25.80 m
Length: 
17.50 m
Height: 
6.73 m
Powerplant: 

2 x Rolls-Royce Allison T406/AE 1107C-Liberty turboshafts, 6,150 hp (4,590 kW) each.

Engine Model: 
Rolls-Royce AE 1107C-Liberty
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
n/a
MTOW: 
27400 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
600 ft/min
Initial Climb (to FL150)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL240)
IAS: 
n/a
ROC: 
n/a
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
275 kts
MACH: 
n/a
Ceiling: 
260
Range: 
1730 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
n/a
ROD: 
n/a
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
n/a
Distance: 
n/a

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