the BASIC tRAINeR

PC-7 MkII

10 ft

8 in

(3.2

6 m

) ty

pica

l

33 ft 4 in (10.18 m)

7 ft 7 in

(2.31 m)

8 ft (2.44 m) dia.

8 ft 4 in (2.54 m)

Wing area(16.28 m )2 175.27 ft 2

3 ft 2 in(0.97 m)

12 ft

3 in

(3.6

6 m

)

33 ft

5 in

(10.

19 m

)

PC-7 MkII

PC-7 MkIIthe BASIC tRAINeR

www.pilatus-aircraft.comSTA0214E

Hartzell four-bladealuminium propeller

700 shp Pratt & WhitneyPT6A-25C engine (850 shp thermodynamic rating)

Ejection seats

Stepped, tandem seating with full dual-glass cockpit

Six underwinghardpoints

Anti-g system

On-board oxygengenerating system (OBOGS)

Birdstrike resistant canopy

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 confidence-building environment for inexperienced cadets. With its highly cost-efficient 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

PeRFORMANCe

the PC-7 MkII, in the aerobatic configuration, at MtOW, 5,180 lbs (2,350 kg) has the following performance under international stand-ard 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 242 KtAS 448 km/h - at 10,000 ft 250 KtAS 463 km/h

Stall speed - flaps and gear up (Vs) 77 KCAS 143 km/h - flaps and gear down (Vso) 69 KCAS 128 km/h

g loads Aerobatic Utility - max. positive + 7.0 g + 4.5 g - max. negative – 3.5 g – 2.25 g

Max. range 800 nm 1,482 km

WeIGhtS

Basic empty weight (depending on configuration) 3,792 lb 1,720 kg

Max. take-off weight - aerobatic 5,180 lb 2,350 kg - utility 6,283 lb 2,850 kg