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C10T

From SKYbrary Wiki
Aircraft
Name P210 (turbine)
Manufacturer CESSNA
Body Narrow
Wing Fixed Wing
WTC Light
Type code L1T
Engine Turboprop
Engine count Single
Mass group 1


Manufacturered as:

ADVANCED AIRCRAFT Spirit 750
ADVANCED AIRCRAFT Turbine P210
CESSNA P210 (turbine)


CESSNA P210 (turbine)

CESSNA P210 (turbine)

Description

P210 The Cessna 210 Centurion is a six-seat, high-performance, retractable-gear single-engined general aviation aircraft which was first flown in January 1957 and produced by Cessna until 1985.

Technical Data

Wing span 11.20 m36.745 ft
Length 8.59 m28.182 ft
Height 2.95 m9.678 ft
Powerplant 1 x Rolls-Royce (Allison) 250-B17F/2 (450 shp).
Engine model Allison 250

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 193 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance m ROC 930 ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance m
MTOW 18141,814 kg
1.814 tonnes
kg
Ceiling FL270 ROD ft/min APC
WTC L Range 900900 nm
1,666,800 m
1,666.8 km
5,468,503.941 ft
NM

Accidents & Serious Incidents involving C10T

None on SKYbrary