Maximum operating altitude
9000 feet to allow landing within five minutes in case of fire
Main rotor diameter
33 feet
Tail rotor diameter
4’10”
Maximum operating density altitude
14,000 feet
Air speed limits (never exceed airspeeds)
130 knots: below 2201Ibs
120 knots: above 2200 Ibs
100 knots: autorotation
Rotor speed limits
90% to 108%
Engine tachometer limits
101% to 102%
Where the pressure limits
Lower Redline: 25 psi
Normal range: 55 to 95 psi
Upper redline: 115 psi
Oil temperature limits
75 to 245°F
Cylinder head temperature limits
200 to 500°F
Maximum and minimum gross weight
Maximum gross weight: 2500 lbs
Minimum gross weight: 1600 Ibs