8/6/2019 Pilatus Aircraft Ltd - PC-7 Fact Sheet

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PC-7 MkII TURBO TRAINER

8/6/2019 Pilatus Aircraft Ltd - PC-7 Fact Sheet

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PERFORMANCE

  The PC-7 MkII, in the aerobatic configuration, has the following performance

under international standard atmospheric (ISA) conditions:

 Take-off distance over 50 ft 

(15 m) obstacle at sea level 1,360 ft (415 m)

Landing distance over 50 ft 

(15 m) obstacle at sea level 2,180 ft (665 m)

Max. rate of climb, sea level 2,910 ft/min (14.79 m/sec)

Max. operating speed (Vmo) 300 KEAS (556 km/h)

Max. level cruise speed (VH) at sea level 245 KTAS (454 km/h)

Max. level cruise speed (VH) at 10,000 ft 255 KTAS (472 km/h)

Stall speed

- flaps and gear up (Vs) 75 KEAS (139 km/h)

- flaps and gear down (Vso) 68 KEAS (126 km/h)

g loads Aerobatic Utility

- Max. positive + 7.0 g + 4.5 g  

- Max. negative – 3.5 g – 2.25 g  

Max. range 810 NM (1,500 km)

WEIGHTS

Basic empty weight 

(depending on configuration) 3,771 lb (1,710 kg)

Max. take-off weight, aerobatic 4,960 lb (2,250 kg)

Max. take-off weight, utility 6,283 lb (2,850 kg)

   3 .   2

   6   m    (   1

   0   f   t   8   i   n   )

10.18 m (33 ft 4 in)

2.312 m

(7 ft 7 in)

2.440 m (8 ft) dia.

2.540 m (8 ft 4 in)

Wing area16.283 m2 (175.27 ft 2)

0.972 m(3 ft 2 in)

   3 .   6

   6   m    (   1

   2   f   t   3   i   n   )

   1   0 .   1

   9   m    (   3

   3   f   t   5   i   n   )

PC-7 MkII 

PC-7 MkII 

   P   C  -   7   M

   k   I   I

Hartzell four-blade

aluminium

propeller 

700 shp

Pratt & Whitney

PT6A-25C engine(850 shp thermodynamic

rating)

Ejection seats

Stepped, tandem

seating with full

dual-glass cockpit 

Six underwing 

hardpoints

Anti-g system

On-board oxygen generating 

system (OBOGS)

PC-7 MkII

 TURBO TRAINER

FEATURES

Since its introduction in 1994, the PC-7 MkII has come with an

exceptional standard of equipment, performance, and cost-effective-

ness in this class of training aircraft.

Offering a reliable and economic training platform, the docile behav-

iour of the PC-7 MkII in the hands of a beginner provides a confi-

dence-building environment for inexperienced cadets. With its highlycost-efficient PT6A-25C engine, it provides the lowest engine operat-

ing 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.

www.pilatus-aircraft.com

TRAINING ROLES

Ab Initio Training 

Basic Flying Training