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Max Range
1,172 nm
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Takeoff Distance
721 ft
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Occupants
10
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Max Speed
170 kts
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Useful Load
3,900 lbs
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Max Range
1,172 nm
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Takeoff Distance
721 ft
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Max Occupants
10 - 17
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Max Speed
170 kts
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Useful Load
3,900 lbs


Versatility

One Plane, So Many Applications

Dependability, along with the longest flight range and shortest takeoff length makes the PAC750 perfectly suited for a wide variety of flight applications. The PAC’s ability to provide an extensive number of operational house before performing routine maintenance along with its best in class fuel efficiency makes the PAC the perfect choice for your business.

 

Configuration Options


The PAC750’s is specifically designed to provide the widest array of configuration choices of any aircraft in its market segment.
PAC750 Passenger + Freight Configuration
PAC750 Photographic Survey Configuration
PAC750 Geophysical Survey Configuration
PAC750 Agriculture Solid Configuration
PAC750 Agriculture Liquid Configuration
PAC750 Skydiving Configuration
PAC750 Medevac Configuration
PAC750 Firebombing Configuration
PAC750 Freight Configuration
PAC750 Search and Rescue Configuration

Configuration Options


The PAC750’s is specifically designed to provide the widest array of configuration choices of any aircraft in its market segment.
PAC750 Passenger + Freight Configuration
PAC750 Photographic Survey Configuration
PAC750 Geophysical Survey Configuration
PAC750 Agriculture Solid Configuration
PAC750 Agriculture Liquid Configuration
PAC750 Skydiving Configuration
PAC750 Medevac Configuration
PAC750 Firebombing Configuration
PAC750 Freight Configuration
PAC750 Search and Rescue Configuration

Configuration Options


The PAC750’s is specifically designed to provide the widest array of configuration choices of any aircraft in its market segment.
PAC750 Passenger + Freight Configuration
PAC750 Photographic Survey Configuration
PAC750 Geophysical Survey Configuration
PAC750 Agriculture Solid Configuration
PAC750 Agriculture Liquid Configuration
PAC750 Skydiving Configuration
PAC750 Medevac Configuration
PAC750 Firebombing Configuration
PAC750 Freight Configuration
PAC750 Search and Rescue Configuration

The Toughest Aircraft


Short field takeoff and landing capability along with landing gear perfectly suited for the roughest of runways. The PAC750 is made for the toughest of conditions.
Range & Fuel Consumption
The PAC-750 XSTOL III Provides
Maximum Efficiency & Range
Max Range at Optimum Speed @ 15,000 Ft
1,172 nm
2,183 km
Endurance at optimum speed (no reserves)
8 Hours
10 Hours w/ Aux Fuel
Avg Fuel Consumption at optimum cruise
49 Gal/hr
184 Litres/hr
Useable Fuel Capacity (Standard Tank)
330 US Gal
1,256 Litres
Max Range with Aux Fuel Tank
1,400 nm
2,593 km
Range & Fuel Consumption
The PAC-750 XSTOL III Provides
Maximum Efficiency & Range
Max Range at Optimum Speed @ 15,000 Ft
1,172 nm
2,183 km

Endurance at optimum speed (no reserves)
8 Hours
10 Hours w/ Aux Fuel

Average Fuel Consumption at optimum cruise settings
49 US Gal/hr
184 Litres/hr

Useable Fuel Capacity
330 US Gal
1,256 Litres

Max Range with Aux Fuel Tank
1,400 nm
2,593 km
Out range the competition

PAC-750 XSTOL III (1,172 NM)
Cessna Caravan (1,070 nm)
Quest Kodiak (845 nm)

Xstol

TakeOff and Land Virtually Anywhere


The shortest ground roll required by any aircraft in its class

 

Passenger Flights

Utility Needs & Personnel Transport

The unparalleled quick change versatility of the P-750 XSTOL allows for the cabin to be rearranged for passenger flights within minutes. Additional cargo may be stowed during maximum occupancy flights within a large 1,000lb cargo compartment pod that has no influence on cruise speed.


Interior

Deluxe Cabin Seating


The P-750 XSTOL III offers durable deluxe cabin seating to insure that all passengers are comfortable and well accommodated.

Powerplant

Proven Reliability

The ultra efficient and cost effective 750hp Pratt and Whitney PT6-34 engine

 

Cargo

Unmatched Cargo Capacity


The PAC750 offers the highest useful load of any aircraft in its class.

Key Features

01Easy access 'gull-wing' crew doors

02High visibility cockpit for superior awareness in any situation.

03Well proven and globally supported Pratt & Whitney Canada PT6A-34 Turbine Engine producing 750shp.

04Outer wing dihedral for lateral stability.

05Thick chord wing for high lift.

06Constant speed, full feathering and reversible propeller for short-field performance. (3-Blade Standard, 4-Blade Optional)

07Large air intake is optimized for rapid climb, and provides RAM air and thrust recovery even at low forward speeds. An effective inertia separation system for FOD protection is incorporated in the inlet.

08Large 240ft3 cabin with the ability for it to be rapidly reconfigured between roles.

09Easily removed engine cowling allowing for complete access to the engine and systems.

10High volume (70ft3, 1,000lb) single compartment (removable divider nets) cargo pod with a hinged rear loading ramp able to take full lengths of plywood, roofing iron and other over sized items.

11All metal construction for durability, ruggedness and ease of repair in the field.

12Large double doors for rapid loading and unloading of passengers and freight.

13Large powerful single slotted flaps, spanning the center wing and providing 58kts stall speed.

14Large passenger windows for excellent visibility.

15Low wing for superior low speed stability, final approach visibility and ease of access for pre-flight checks, refueling and  maintenance.

16High strength fixed landing gear with oleo pneumatic shock strut allowing for customization of the cylinder pressure to the conditions. High Floating Wheel (optional) significantly improves soft ground performance and gives at least a 46% increase in the footprint tyre.

17A quick change, multi-role floor allows operators to move easily between different role configurations to maximize aircraft utilization.

 
Key Features

01Easy access 'gull-wing' crew doors

02High visibility cockpit for superior situation awareness for the pilot.

03Well proven and globally supported Pratt & Whitney Canada PT6A-34 Turbine Engine producing 750shp.

04Outer wing dihedral for lateral stability.

05Thick chord wing for high lift.

06Constant speed, full feathering and reversible propeller for short-field performance. (3-Blade Standard, 4-Blade Optional)

07Large air intake is optimized for rapid climb, and provides RAM air and thrust recovery even at low forward speeds. An effective inertia separation system for FOD protection is incorporated in the inlet.

08Large 240ft3 cabin with the ability for it to be rapidly reconfigured between roles.

09Easily removed engine cowling allowing for complete access to the engine and systems.

10High volume (70ft3, 1,000lb) single compartment (removable divider nets) cargo pod with a hinged rear loading ramp able to take full lengths of plywood, roofing iron and other over sized items.

11All metal construction for durability, ruggedness and ease of repair in the field.

12Large double doors for rapid loading and unloading of passengers and freight.

13Large powerful single slotted flaps spanning the center wing providing 58kts stall speed.

14Large passenger windows for excellent visibility.

15Low wing for superior low speed stability, final approach visibility and ease of access for pre-flight checks, refueling and  maintenance.

16High strength fixed landing gear with oleo pneumatic shock strut allowing for customization of the cylinder pressure to the conditions. High Floating Wheel (optional) significantly improves soft ground performance and gives at least a 46% increase in the footprint tyre.

17A quick change, multi-role floor allows operators to move easily between different role configurations to maximize aircraft utilization.

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Available Avionics

The Right Technology for Your Needs

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The Standard
Avionics Package
  • Easy-to-use with multiple functions and useful features that make navigation simple and provide an extra margin of safety
  • At a glance, see your aircraft's position relative to terrain, obstructions, weather, airways, navaids, restricted airspace and more
  • Select between several charting options and easily add or remove details with the simple press of a soft key
  • New rotary knob allows for quicker map scale changes and entry of data
  • Front loading SD card-slot allows for expanded memory and makes loading updated charts uncomplicated
  • Fits in same panel space as the MX20 and includes more serial ports for added sensor capacity Detailed Data
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The Deluxe
Garmin G600
  • Dual 6.5-inch diagonal color LCDdisplays; portrait orientation
  • Large and clear display fonts
  • 4.8-inch diagonal attitude indicator
  • SVT synthetic vision renders terrain-alerting data into realistic virtuallandscape
  • Proven solid-state Attitude and Heading Reference System (AHRS) and Air DataComputer (ADC)
  • XM WX Satellite Weather and XM Radio (optional)
  • Built-in terrain elevation and towers/obstacles databases
  • Standard FliteCharts® and SafeTaxi® databases
  • Optional ChartView™ shows the aircraft position on the Jeppesen approachcharts and airport surface diagrams
  • Offers control/display for available GWX 68 airborne weather radar
  • Displays GPS mapping, as well as optional traffic, terrain and datalinksystems
  • Flight director for selected autopilots
  • Real-time winds aloft data on PFD
  • GAD 43 adapter provides AHRS reference for autopilot interface on selectmodels (allows replacement of gyro attitude, yaw, and baro correction; radarstabilization; and bootstrap heading).
Specifications & Performance

Performance Enhanced Profit

Weights

Basic Empty Weight3,600 lbs* (1,633 kg)
Maximum Ramp Weight7,540 lbs (3,420 kg)
Maximum Take-Off Weight7,500 lbs (3,402 kg)
Maximum Landing Weight7,125 lbs (3,232 kg)
Maximum Useful Load3,900 lbs (1,769 kg)
Center of Gravity Range102.8 to 124.60 inces aft of datum

2.3% to 28.5& MAC (Mean Aerodynamic Chord)
*Basic Empty Weight is complete aircraft, empty of usable fuel and without optional equipment, but including engine oil, unusable fuel. BEW will vary between aircraft serial numbers depending upon final configuration and equipment specification selected.

External Dimensions

Length38 ft 10 in (11.84 m)
Height13 ft 3 in (4.04 m)
Wingspan42 ft (12.8 m)
Wing Area305 ft2 (28.32 m2)
Wheelbase12 ft 1 in (3.68 m)

Cabin Interior

Length16 ft 5 in (5 m)
Height4 ft 8 in (1.42 m)
Wingspan42 ft (12.8 m)
Width4 ft 4 in (1.32 m)
Max Passengers10 - 17

Speeds

TAS (True Air Speed) 10,000 FT167 kts (309 km/h)
Never Exceed Speed (VNE)170 kts (315 km/h)
Design Cruise Speed (Vc)140 kts (259 km/h)
Maximum Maneuvering Speed (VA)131 kts (243 km/h)
Maximum Flap Extended Speed (VFE)120 kts (222 km/h)
Stall Speed (Idle Power) With Flaps Up (VS)58 kts (107 km/h)

Range

Max. Range at Optimum Speed (nil wind, no reserves), 15,000ft.1,172 nm (2,183 km)
Endurance at Optimum Speed (no reserves8 hrs Standard (10 hrs w/ Aux.Fuel.)
Average Fuel Consumption (optimum cruise settings)49 US Gal/hr (184 Litres/hr)
Fuel Capacity (useable)330 US Gal (1,256 Litres)
Max. Range with Aux. Fuel Tank fitted (102US.Gal/387L usable)**1,400 nm (2,593 km)
**Estimate based on optimum cruise settings, nil wind and nil reserves

Powerplant

ManufacturerPratt & Whitney Canada
ModelPT6A-34
Power Rating750 shp

Takeoff & Landing Performance

Take-Off Ground Roll at Sea Level, ISA721 ft (220 m)
Take-Off Distance To 15 m (50 ft), ISA1,503 ft (458 m)
Landing Ground Roll at Sea Level**543 ft (166 m)
Landing Distance From 15 m (50 ft)**950 ft (289 m)
Nil wind, 7,500 MTOW, Aircraft optimised for STOL performance (flight test data not yet published in POH)
**Reverse thrust selected on touchdown

Climb (at MTOW)

Maximum Rate of Climb at Sea Level1,067 ft/min (325 m/min)
Maximum Rate of Climb at 8,000 FT951 ft/min (290 m/min)
Climb to 12,000 FT From Brakes Release14 min
Maximum Positive G+3.5 G
Maximum Negative G-1.4 G
Wing Loading120.07 KG/M2 (24.59 LB/FT2)
Power Loading10.0 LB/SHP (4.5 KG/SHP)

Altitude Limits

Maximum Operating Altitude20,000 ft*** (6,096 m)
Service Ceiling (at Max. Weight)25,000 ft**** (7,620 m)
***Demonstrated to 32,000ft. Approval pending for certification to 25,000ft.
****Estimate based on previous flight testing.