The Aviat Pitts S2-C

Specifications of the Pitts S2-C

• Engine: Lycoming AEIO-540, 260 HP
• Propeller: The Claw by Hartzell 76: Composite Constant
• Length: 17 feet 9 inches
• Height: 6 feet 5 inches
• Wing Span: 20 feet
• Wing Area: 127.5 square feet
• Wing Loading: 13.3 lb/sq ft (normal)/ 12.7 lb/sq ft (aerobatic)
• Power Loading: 6.59 lb/hp (normal)/ 6.25 lb/hp (aerobatic)
• Seats: 2 tandem
• abin Length: 6 feet 11 inches
• Cabin Width: 28 inches
• Cabin Height: 47 inches
• Empty Weight: 1,155 pounds
• Maximum Gross Weight: 1,700 pounds
• Useful Load: 545 lb (normal)/ 470 lb (aerobatic)
• Payload w/ Full Fuel: 371 pounds
• Fuel Capacity w/ 5 Gallon Wing Tank: 29 U.S. gallons (28 gallons useable)

Performance

• Aerobatic Flight Load Limits: +6G/-5G
• Takeoff Distance Ground Roll: 554 feet
• Takeoff Distance Over 50 ft. Obstacle: 860 feet
• Max Demonstrated Crosswind Component: 17 kt
• Rate of Climb, Sea Level, Minimum Weight: 2,900 fpm
• Maximum Level Speed, Sea Level: 169 kt
• Cruise Speed w/ 30 min rsv. At 75% Power: 150 KTAS/1.6 hours
• Range w/ 30 min rsv. At 75% Power: 284 st. miles
• Fuel Consumption at 75% Power: 84 pph/14 gph
• Best Economy: 6,000 feet
• Landing Distance over 50 ft. Obstacle: 1,200 feet
• Landing Distance, Ground Roll: 750 feet
• 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 56

USAero/Aviat Related Pages

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