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NAV Canada Aviation Basics Course
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Piston efficient altitude
Ground to 12,000 ft
Piston max speed
250 KT
Piston most likely speed
100 KT
Piston rate of climb
500 to 1500 FPM
Piston rate of descent
500 to 1500 FPM
Piston rate of turn
Rate One: 3º/sec
Piston acceleration delay
No delay
Piston run up time
Long run up time
Piston disadvantages
Many complex parts
Engine has a high weight ratio compared to the rest of the AC
Horizontally opposed piston advantages
• Reduced drag
• Better visibility
• Ease of maintenance
• Lightweight
Horizontally opposed piston disadvantages
• Cooling problems
• Increased drag from air scoops
Radial piston advantages
• Compact
• Accessible for maintenance
• Lightweight
• Supplies good power for its size and weight
Radial piston disadvantages
• Interference to forward visibility
• Imposes considerable drag
Jet speed
300 to 500 KT
Jet efficient altitude
25,000 to 36,000 ft
Jet rate of descent
2000 to 6000 FPM
Jet max rate of climb
1500 to 6000 FPM
Turboprop speed
200 to 300 KT
Turboprop altitude
13,000 to 25,000 ft
Turboprop rate of climb
1500 to 3,000 FPM
Jet most likely rate of climb
1500 to 3,000 FPM
Turboprop rate of descent
1500 to 4,000 FPM
Turboprop turning radius
Rate One: 3º/sec
Jet turning radius
Rate 0.5: 1.5º/sec
Turboprop run up time
Short run up time
Jet run up time
No run up time