2017 Apr 13 By admin 0 comment

Check the data of the P2012 compared to its main competitors.

Model [unit] C402   Navajo  Kodiak  BN2 Tecnam P2012
Service Entry 1966 1967 2005 1965 2019
Wing Span m 13,45 12,4 13,7 14,94 14
Length m 11,09 9,94 10,42 10,86 11,8
Height m 3,49 3,96 4,48 4,18 4,4
Cabin height m 1,27 1,17 1,45 1,3 1,36
Cabin width m 1,42 0,76 1,37 1,1 1,48
Cabin length m 4,98 4,42 4,83 4,6 4,15
Landing gear Fixed Retr. Fixed Fixed Fixed
ENGINE
Engine manuf. Continental Lycoming PW Lycoming Lycoming
Engine Model TSIO520VB TIO-540A PT6A-34 IO-540 TEO540C1A
Engine Power Hp 2×325 2×310 1×750 2×300 2×375
Propeller manuf. McCauley McCauley Hartzell Hartzell MT-Prop
Prop. diameter m 2,25 2,03 2,44 1,98 2,1
WEIGHTS
Max gross weight Kg 3107 2948 3286 2994 3600
Std. empty weight Kg 1845 1990 1708 1667 2250
Useful load Kg 1262 958 1600 1128 1350
Seating capacity (pax) 9 7 9 9 9
Fuel capacity Lt 780 708 1211 492 800
Wing loading Lb/sqft 30,3 28,35 30,1 20,31 29
Power loading Lb/hp 10,54 10,48 9,67 11 10,6
 PERFORMANCE
Speed, VNE kt 230 226 187 183 240
Max Cruise Speed kt 190 (FL 100) 190 (FL100) 151 (FL120) 139 (SL) 190 (FL100)
Min control speed kt 80 74 Na Na 74
Stall sp. landing kt 71 63 60 40 60
Best RoC Ft/min 1450 1395 1371 860 1500
Range – Max (FL100, 75%) nm 960 850 998 503 (FL?) 907
Takeoff distance m 670 695 446 371 600
Landing distance m 757 554 435 299 500

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