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ALENIA G-222

From SKYbrary Wiki

G222
Aircraft
Name G-222
Manufacturer ALENIA
Body Narrow
Wing Fixed Wing
WTC Medium
APC B
Type code L2T
Engine Turboprop
Engine count Multi
Mass group 4


Manufacturered as:

AERITALIA G-222
ALENIA G-222
ALENIA C-27A Spartan
ALENIA Spartan (C-27A)


ALENIA G-222

ALENIA G-222

Description

The first prototype flew in 1970. After successful testing the first aircraft entered service in 1978.

Technical Data

Wing span 28.7 m94.16 ft
Length 22.7 m74.475 ft
Height 9.8 m32.152 ft
Powerplant 2 x General Electric T64-GE-P4D turboprop (3400 shp).
Engine model General Electric T64

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 237 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 123 m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance 850 m
MTOW 2800028,000 kg
28 tonnes
kg
Ceiling FL250 ROD ft/min APC B
WTC M Range 16001,600 nm
2,963,200 m
2,963.2 km
9,721,784.784 ft
NM

Accidents & Serious Incidents involving G222

None on SKYbrary