G222
ALENIA G-222
ALENIA G-222
Aircraft
Name
G-222
Manufacturer
Body
Narrow
Wing
Fixed Wing
WTC
M
APC
B
Type Code
L2T
Engine
Turboprop
Engine Count
Multi
Manufactured as
ALENIA G-222
ALENIA C-27A Spartan
ALENIA Spartan (C-27A)
AERITALIA G-222
G222
The first prototype flew in 1970. After successful testing the first aircraft entered service in 1978.
Technical Data
Wing span (metric)
28.70 m
Length (metric)
22.70 m
Height (metric)
9.80 m
Powerplant
2 x General Electric T64-GE-P4D turboprop (3400 shp).
Engine Model(s)
General Electric T64
Indicative Performance Data
Take-Off
V2
n/a
Distance
123 m
MTOW
28000 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
n/a
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
237 kts
MACH
n/a
Ceiling
250
Range
1600 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
850 m
