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Technical characteristics


Geometric parameters
Dimensions of passenger cabin (cargo compartment) and hatches
Basic specifications
Options
Flight deck
 

GEOMETRIC PARAMETERS

Length, ft 36,42
Wing length, ft 46
Ramp height, ft 11,15
Maximum width of fuselage, ft 6,56
Track of landing gear, ft 6
Wheelbase of landing gear, ft 11,23
Wing area, ft2 217,4

DIMENSIONS OF PASSENGER CABIN (CARGO COMPARTMENT) AND HATCHES

length, ft 11,32
width, ft 5,381
height, ft 4,068
Cabin capacity, ft3 130,7
Maximum length of cargo, ft 14,53
Front upper access door, ft 1,47 х 1,90
Rear upper access door, ft 5,545 x 4,232
Emergency doors (left, right), ft 2,23 х 2,23

BASIC SPECIFICATIONS

Maximum takeoff weight, lb 5997
Maximum useful comercial load, lb 1764
Maximum fuel capacity (ferrying), gal 396,3
Maximum altitude, ft 14760
Maximum allowable speed, ktas 189,5
Maximum speed of horizontal flight, ktas 170,9
Cruise speed (economy) ktas 146
Range of flight (payload 1764 lb), nm (max) 648/2160
 
Duration of flight (max t.o.w.), pay load) 5,6
Rate of climb, ft/min. At full load ft/min 787-1181
Runway length land/water level (max t.o.w.), ft 1148/1476
Landing speed (at maximum weight), ktas 53
Maximum overload +3,8—1,9

FLIGHT DECK

Basic 0 (standard) avionics set provide the VFR operation. Weight of basic equipment is included in standard empty weight.
The aircraft may be equipped with additional (optional) IFR avionics. This configuration means special architecture of power supply system and air pressure system, in consideration with FAR-23 requirement.
Weight of additional equipment and supply system will be added to standard empty weight.
Configuration of additional avionics will be specified with Customer

2.2.2 Standard avionic and equipment set (Fig.6)

(a) Controls and system’s monitoring, standard

1 – control wheel
2 – power levers / reverse control
3 – RPM control
4 – supercharge control (for M-337C)
4(a) – mixture control (for O-540)
5 – trimmer tab control
6 – pitch trim position indication’
7 – yaw trim position indication
8 – flaps control
9 – flaps position indicator
10 – landing gear control
11 – landing gear position indication’
12 – engine electric control
13 – electric power distribution panel
14 – circuit beakers panel

15 – engine diagnostic monitor:
- RPM
- Manifold pressure
- Oil pressure
- Oil temperature
- Fuel pressure
- Cylinder head temperature
- Fuel flow
- Fuel quantity
- Estimated flight duration
-OAT
- voltmeter
- ammeter
- engine log recorder
16 – main hydraulic system pressure gauge
17 – emergency pneumatic system pressure gauge
18 – warning and annunciate lights panel
19 – static source selector
20 – reverse check switches
21 – air speed indicator
22 – altimeter
23 – chronometer
24 –magnetic compass
25 - stall warning system
26 – VHF transceiver

Basic 1

Basic 2


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