PC-7 MkII Fact Sheet

Transcription

PC-7 MkII Fact Sheet
PC-7 mkII
the basic trainer
PC-7 MkII
THE BASIC TRAINER
Since its introduction in 1994, the PC-7 MkII has come with an
exceptional standard of equipment, performance and cost-effectiveness in this class of training aircraft.
Offering a reliable and economic training platform, the docile behaviour of the PC-7 MkII in the hands of a beginner provides a confidencebuilding environment for inexperienced cadets. With its highly costefficient PT6A-25C engine, it provides the lowest engine operating
costs of all turboprop trainer aircraft. The use of airframe and avionics
systems common with the PC-9 M enables owners and operators to
profit from the benefits of a combined infrastructure established at
Pilatus to support both these aircraft types.
TRAINING ROLES
- Ab Initio Training
- Basic Flying Training
FEATURES
Hartzell four-blade
aluminium propeller
Birdstrike
resistant canopy
Ejection seats
PERFORMANCE
The PC-7 MkII, in the aerobatic configuration, at MTOW, 5,180 lbs
(2,350 kg) has the following performance under international standard atmospheric (ISA) conditions:
Take-off distance over 50 ft
(15 m) obstacle at sea level
1,500 ft
457 m
Landing distance over 50 ft
(15 m) obstacle at sea level
2,255 ft
687 m
Max. rate of climb, sea level
2,675 ft/min
13.59 m/sec
Max. operating speed (Vmo)
300 KEAS
556 km/h
Max. cruise speed (VH)
- at sea level
- at 10,000 ft
242 KTAS
250 KTAS
448 km/h
463 km/h
Stall speed
- flaps and gear up (Vs)
- flaps and gear down (Vso)
77 KCAS
69 KCAS
143 km/h
128 km/h
g loads
- max. positive
- max. negative
Aerobatic
+ 7.0 g
– 3.5 g
Utility
+ 4.5 g
– 2.25 g
800 nm
1,482 km
Basic empty weight
(depending on configuration)
3,792 lb
1,720 kg
Max. take-off weight
- aerobatic
- utility
5,180 lb
6,283 lb
2,350 kg
2,850 kg
Max. range
Anti-g system
700 shp Pratt & Whitney
PT6A-25C engine (850 shp
thermodynamic rating)
On-board oxygen
generating system
(OBOGS)
Stepped, tandem
seating with full
dual-glass cockpit
Six underwing
hardpoints
10 ft 8 in (3.26 m) typical
WEIGHTS
8 ft (2.44 m) dia.
PC-7 MkII
7 ft 7 in
(2.31 m)
8 ft 4 in (2.54 m)
33 ft 4 in (10.18 m)
Wing area
175.27 ft 2 (16.28 m2 )
STA0214E
12 ft 3 in (3.66 m)
33 ft 5 in (10.19 m)
3 ft 2 in
(0.97 m)
www.pilatus-aircraft.com

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