AERIAL SERVICES PVT. LTD. - Air Charter Services

POWERPLANTS
Manufacturer	Pratt & Whitney
Model	PT6A42
Shaft- Horsepower per Engine	850 SHP

PROPELLERS
Manufacturer	Hartzel
No.Of Blades	4

EXTERNAL DIMENSIONS
Overall Length	43 ft 10 in
Overall Height	14 ft 10 in
Wing Span	54 ft 6 in
Wing Area	303 sq ft

INTERNAL DIMENSIONS
Cabin Length	16 ft 8 in
Cabin Height	4 ft 9 in
Cabin Width Maximum	4 ft 6 in
Floor Width	4 ft 0 in
Cabin Volume	85 cu ft

ACCOMMODATIONS
Crew Seats (One Pilot Required)	02
Passenger Seats (Typical) 07 Baggage Volume (Accessible In Flight)	55.3 cu ft

DESIGN WEIGHTS
Maximum ramp Weight	2590 lb
Maximum Take-Off Weight	12500 lb
Maximum Landing weight	12500 lb
Maximum Zero Fuel Weight	11000 lb
Basic Operating weight (Std BEW Plus One Crew @ 200	8483 lb
Maximum Fuel Capacity	544 U.S. Gal
Maximum Fuel Capacity weight	3645 lb
Useful Load (Standard Airplane)	4107 lb

RANGE (Maximum Range Power, FL 350, NBAA IFR Reserve 100 mm Alt)
4 Passengers / 800 Lb Payload	1530 nm
8 Passengers / 1600 Lb Payload	1255 nm

TAKE-OFF
distance over 50 ft obstacle flaps approach Sea Level, ISA, 12500 Lb (MTOW)	2579 ft
300 Nm 8 Passengers Mission, Sea Level, ISA
Maximum Cruise Power, Fl250, NBAA IFR Reserve 100 nm Alt	2277 ft

Accelerate Stop distance flaps approach
Sea Level, ISA, 12500 lb (MTOW)	3413 ft
300 nm 4 Passengers Mission, Sea Level, ISA Msximum Cruise Power, Fl250, NBAA IFR Reserve 100 nm Alt	3174 ft

Landing distance over 50 ft. Obstacle (with out propeller Reversing)
Sea Level, ISA, 12500 lb (MLW)	2845 ft
300 nm 4 passengers Mission, Sea Level, ISA Maximum Cruise Power, Fl250, NBAA IFR Reserve 100 nm Alt	2230 ft

MAXIMUM DESIGN SPEEDS
Maxium Cruise Speed	292 KTAS

RATE OF CLIMB
Initial All-Engine	2460 ft / min
Intital Engine- Out	740 ft / min

CEILINGS
Maximum Certified Altitude	35000 ft
All-Engine Service Ceiling	35000 ft
Engine-Out Service Ceiling	21900 ft