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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 <br />
Length 22.7 m74.475 ft <br />
Height 9.8 m32.152 ft <br />
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 <br />28 tonnes <br /> kg Ceiling FL250 ROD ft/min APC B
WTC M Range 16001,600 nm <br />2,963,200 m <br />2,963.2 km <br />9,721,784.784 ft <br /> NM

Accidents & Serious Incidents involving G222

None on SKYbrary