SPECIFICATIONS

Below are the general specifications for the P-750 XSTOL. Greater details can be attained by contacting one of our Sales Representatives or by request to aircraft@aerospace.co.nz.

Technical Specifications

 WEIGHT & BALANCE
BASIC EMPTY WEIGHT (Standard IFR)  3,300 lb*  1,497 kg*
*The basic empty weight is defined as the complete aircraft, empty of usable fuel and without optional equipment, but including engine oil, unusable fuel and items of equipment that are an integral part of the basic aircraft.
** P-750 XSTOL aircraft configured for operation in the Limited and Normal Category in Russia are specified with additional equipment.  The Minimum Operating Empty Weight for Limited and Normal Category P-750 aircraft for Russia is 4,453 LB (2,020KG).
MAXIMUM OPERATING WEIGHTS
Max. Ramp Weight   7,540 lb
3,420 kg
Max. Take-Off Weight  7,500 lb 3,402 kg
Max. Landing Weight 7,125 lb 3,232 kg
Max. Useful Load 4,200 lb
1,905 kg
CENTRE OF GRAVITY RANGE 102.8 to 124.6 inches aft of datum
SPEEDS
Never Exceed Speed (VNE)  170 kn 315 km/h
Design Cruising Speed (VC) 140 kn
259 km/h
Max. Manoeuvring Speed (VA)   131 kn
243 km/h
Max. Flap Extended Speed (VFE) 120 kn 222 km/h
Stall Speed (Idle Power) With Flaps Down (VS) 58 kn
107 km/h
RANGE
Max. Range At Optimum Speed, 45 mins Reserves At 16,000 FT 1,179 NM 2,183 km
Endurance At Optimum Speed, 45 mins Reserves 8 H  
Average Fuel Consumption 50 US gal/H 192 Litres/H
Fuel Capacity, Useable 331.8 US gal
1,256 Litres
PERFORMANCE
TAKE-OFF & LANDING PERFORMANCE
Normal Conditions, 7,500 LB    
Take-Off Ground Roll At Seal Level, ISA  721 ft
220 m
Take-Off Distance To 15 M (50 FT) ISA  1,196 ft
364 m
Landing Ground Roll At Sea Level*  543 ft
166 m
Landing Distance From 15 M (50 FT)* 950 ft
289 m
*Reverse thrust selected on touchdown
CLIMB (AT MTOW)
Max. Rate Of Climb At Sea Level  1,067 ft/min 325 m/min
Max. Rate Of Climb at 8,000 FT 951 ft/min 290 m/min
Climb To 12,000 FT From Brakes Release 12 min  
ALTITUDE LIMITS
Max. Operating Altitude 20,000 ft 6,096 m
Service Ceiling (At Max. Weight) 20,000 ft 6,096 m
NORMAL LOAD FACTORS
Max. Positive G +3.5 G  
Max. Negative G -1.4 G  
Wing Loading 120.07 /m2 24.59 lb/ft2
Power Loading 10.0 lb/shp 4.5 kg/shp
SINGLE PILOT IFR CERTIFIED (FAA)  Yes  

 

External Dimensions
Wing Gross
305.00 Sq. ft
28.34 Sq. m XLSTOL 750 Dimensions Top
Nett 267.80 Sq. ft 24.88 Sq. m
Flaps 31.74 Sq. ft 2.95 Sq. m
Ailerons 21.94 Sq. ft 2.04 Sq. m
Tailplane 33.64 Sq. ft 3.13 Sq. m
Elevator 27.92 Sq. ft 2.59 Sq. m
Fin 19.40 Sq. ft 1.80 Sq. m
Rudder 11.70 Sq. ft 1.09 Sq. m

 XLSTOL 750 Dimensions Front & Side

Internal Dimensions

XLSTOL 750 Dimensions Interior

© 2014 Pacific Aerospace.