Utility Aircraft Corporation

SPECIFICATIONS

FUEL CAPACITY:

Total Capacity: 861 litres (227.4 U.S. gallons, 1512 lbs)
Total Useable: 841 litres (221 U.S. gallons, 1476 lbs)

TANK	TOTAL CAPACITY	UNUSABLE FUEL	USABLE
FRONT LEFT TANK *	284 * litres, 499 lbs 75 * U.S. Gallons	10 litres, 18 lbs 3 U.S. Gallons	274 litres, 481 lbs 72 U.S. Gallons
FRONT RIGHT TANK	293 Litres, 515 lbs 77 U.S. Gallons	10 litres, 18 lbs 3 U.S. Gallons	283 litres, 497 lbs 74 U.S. Gallons
REAR LEFT TANK	142 litres, 249 lbs 37.5 U.S. Gallons	0	142 litres, 249 lbs 37.5 U.S. Gallons
REAR RIGHT TANK	142 litres, 249 lbs 37.5 U.S. Gallons	0	142 litres, 249 lbs 37.5 U.S. Gallons
TOTAL	861 litres, 1512 lbs 227 U.S. Gallons	20 litres, 36 lbs 6 U.S. Gallons	841 litres, 1476 lbs 221 U.S. Gallons
* Includes 26 litres (6.8 U.S. gallons, 45 lbs) of fuel in sump tank

MAXIMUM CERTIFIED WEIGHTS:

MAXIMUM CERTIFIED TAKEOFF WEIGHT:	7500 lbs (3410 kgs)
MAXIMUM CERTIFIED LANDING WEIGHT:	7125 lbs (3231 kgs)

TYPICAL AIRPLANE WEIGHTS:

BASIC EMPTY WEIGHT:	3100 lbs (1405 kgs)
MAXIMUM USEFUL LOAD: (will vary with basic empty weights)	4400 lbs (1995 kgs)

CABIN AND ENTRY DIMENSIONS:

CABIN WIDTH: (maximum width)	54" (137.16 cm)
CABIN LENGTH: (measured from behind pilot's seat to rear cabin bulkhead)	158" (401.32 cm)
CABIN HEIGHT: (maximum Height)	56" (142.24 cm)
ENTRY WIDTH: (varies depending on door type)	50"-48" (127 cm - 121.92 cm)
ENTRY HEIGHT: (measured from behind pilot's seat to rear cabin bulkhead)	47" - 45" (front of door frame) (119.38 cm - 114.3 cm) 41.3" - 39.3" (rear of door frame) (104.90 cm - 99.82 cm)
SILL HEIGHT: (oleos fully extended)	44" (111.76 cm)
CABIN VOLUME:	220 cubic ft
With Additional Rear Baggage Compartment:	247 cubic ft
Anticipated Cargo Pod Volume:	113 CU FT
Total with Additional Rear Baggage and Pod:	360 CU FT
DISTANCE CARGO DOOR TO HORIZONTAL STABILISER:	121.75" (309.24cm)
CARGO POD STRUCTURAL LIMITATIONS:
Maximum Combined Load is:	1000 lb (454 kg)
Maximum Distributed Load is:	50 lb/ft² (244 kg/m²)
Maximum Load FWD & MID bays:	500 lb (227 kg)
Maximum Load AFT bay:	100 lb (45 kg)
THE CARGO POD DOOR OPENINGS ARE AS FOLLOWS:
Front door:	33.5”w x 12.25”h (With corner cut off at front).
Middle door:	31.5”w x 12.25”h
Rear side door:	31.5”w x 12”h (front) / 5”h (rear)
Back door:	31.5”w x 47”h.

OUTSIDE DIMENSIONS:

SPECIFIC LOADINGS:

WING LOADING:	24.59 lb/ft²
POWER LOADING:	10 lbs/shp

PERFORMANCE:

MAXIMUM OPERATING ALTITUDE (6095 m)	20,000 ft.
STALL SPEEDS, IAS AT 7500 LBS
Flaps up, power idle	69 kts.
Flaps landing, power idle	58 kts.
TAKEOFF Sea level, 7500 lbs (3405 kgs) MTOW, carrying useful load of 4400 lbs (1997 kgs)
Ground roll	886 feet
Take off distance to 50 ft. obstacle	1482 ft.
CLIMB PEFORMANCE Sea level, 7500 lbs (3405 kgs) MTOW, carrying useful load of 4400 lbs (1997 kgs) using maximum continuous power
Climb to 12,000 ft. (3657 m) from brakes release	12 minutes
LANDING PERFORMANCE Maximum landing weight, carrying useful load of 4025 lbs (1827 kgs) 3 degree glidepath, over 50 ft (15 m) obstacle, no reverse (FAR 23.75 (a))	2016 ft (614 m)
CRUISE
10,000 ft, ISA + 20	169 kts
10,000 ft, ISA	169 kts
RANGE 7500 lbs (3405 kgs) MTOW, carrying useful load of 4400 lbs (1997 kgs), includes fuel for start, taxi, takeoff, climb, descent and 45 minutes reserve remaining after landing	582 nautical miles
ENDURANCE 7500 lbs (3405 kgs) MTOW, carrying useful load of 4400 lbs (1997 kgs), includes fuel for start, taxi, takeoff, climb, descent and 45 minutes reserve remaining after landing	5 hours
BEST RATE OF CLIMB	95 KIAS
BEST ANGLE OF CLIMB	85 KIAS
MAXIMUM DEMONSTRATED CROSSWIND	14 kts

DESIGN:

The P-750 XSTOL is certified to FAR Part 23 in the Normal Category.
MAXIMUM OPERATING SPEED		170 KIAS
MANEUVRING SPEED		131 KIAS
FLAP SPEEDS
0-20 degrees		120 KIAS
21-40 degrees		110 KIAS
FLIGHT LOAD FACTOR LIMITS
	g	g
FLAPS UP:	+3.47	-1.39
FLAPS TAKE OFF:	+3.0	-0
FLAPS LANDING:	+3.0	-0