Pitts S2-B

 

The S-2B, a world class aerobatic aircraft used by top airshow performers and competition pilots is a certified two seat, dual control aircraft rated for -3 G to +6 G.  It is powered by a Lycoming AEIO540 (260HP) and the new Hartzell constant speed composite propeller. It also has an inverted fuel and oil system, symmetrical airfoil wings, elevator servo tabs and aileron spades making it an excellent platform for basic to advanced aerobatics.

Other equipment in our Pitts include: smoke system, aerobatic sight gauge & it is IFR certified.

Engine

 

Lycoming AEIO-540, 260 hp

Recommended TBO

 

1,200 hr

Propeller

 

Hartzell, constant speed, composite two-blade, 78 in dia

Length

 

18' 9"

Height

 

6' 7"

Wing Span

 

20'

Wing Area

 

125sq ft

Wing Loading

 

13.0 lb/sq ft (normal category)
12.7 lb/sq ft (aerobatic)

Power Loading

 

6.59 lb/hp (normal category)
6.25 lb/hp (aerobatic)

Seats

 

2 tandem

Cabin Length

 

6' 11"

Cabin Width

 

28"

Cabin Height

 

47"

Empty Weight

 

1,155 lb

Maximum Gross Weight - normal

Maximum Gross Weight - aerobatic

 

1700 lb

1,625 lb

Useful Load

 

545 lb (normal category)
470 lb (aerobatic)

Payload w/Full Fuel

 

371 lb

Fuel Capacity (w/5-gal wing tank)

 

29 gal (28 gal usable)
aerobatic flight, 24 gal (23 gal usable)

Aerobatic flight load limits

 

+6 G/-3 G

Takeoff distance ground roll

 

554 ft

Takeoff distance over 50-ft obstacle

 

860 ft

Max demonstrated crosswind component

 

17 kt

Rate of climb, sea level (minimum weight)

 

2,700 fpm

Maximum level speed, sea level

 

169 kt

Cruise speed w/30 min rsv. @ 75% power

 

150 KTAS/ 1.6 hrs

Range w/30 min rsv. @ 75% power

 

277 nm

Fuel consumption @ 75% power

 

(84 pph/14gph)

Best economy

 

6,000 ft

Landing distance over 50-ft obstacle

 

1,200 ft

Landing distance, ground roll

 

750 ft

VX (best angle of climb)

 

KIAS N/A at this time

VY (best rate of climb)

 

KIAS 82

VA (design maneuvering)

 

KIAS 134

VNO (max structural cruising)

 

KIAS 134

VNE (never exceed)

 

KIAS 185

VSI (stall, clean)

 

KIAS 55

Harmon Rocket F1

 

Engine

Lycoming AEIO-540, 300 HP

Propeller

2 blade Hartzell Constant Speed

Top Speed

250 m.p.h.

Cruise Speed

230 m.p.h

( TAS @ 10,000MSL @ 60% power)

Stall Speed

54 m.p.h.

Range @55%pwr

1000 sm

Rate of climb sea level

3500 fpm

Take off Distance

300ft

Landing Distance

700ft

Fuel Capacity

52 gal

Empty Weight

1200lbs

Gross Weight

2000 lbs

Length

21 ft.

Wing Span

21' 10"

Wing Area

104 sq. ft.

No. of Seats

2

Landing Gear

tail wheel

Building Material

Metal

G. Limit

+6 -3 g

Pitts S1-S

Engine

 

Lycoming AEIO-360 200 h.p.

Propeller

   

Top speed

 

185 mph

G limit

 

+6/-3

Max. Range

 

309 miles

Empty Weight

 

830 lbs

Length

 

15 feet, 6 inches

Wing Span

 

17 feet, 4 inches

Height

 

6 feet, 6 inches

 

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