R-22 POH Flashcards
Main rotor diameter
25’ 2”
main rotor chord
7.2” (constant)
Main rotor blade twist
-8 degrees
Main rotor tip speed
672 FPS
Tail rotor diameter
3’ 6”
Tail rotor blade chord
4” (constant)
Tail rotor precone angle
1 degree 11 minutes
Tail rotor tip speed
599 FPS
usable fuel capacity with bladder
combine 26.3
Main 16.9
Aux 9.4
Flight and maneuver limitations
Governor off prohibited except EP training or inflight malfunction Low G pushover prohibited Areobatics Doors off permitted I Flight into known icing conditions Minimum 1 crew Solo right seat Max DA 14,000 A Goal Left seat belt buckled
approved fuel
91/96 AV fuel, 100LL Av Fuel, 100/130 av Fuel
VFR night
Navigation lights
Anti-collision lights
Instrument lights
Landing lights
ground orientation by ground objects illuminated solely by lights on ground or adequate celestial illumination
Mandatory operating components
Governor
OAT gauge
Alternator
Low warning RPM system
Engine max speed
2652 RPM (104%)
Rotor Speed Limits
110% 561
104% 530
101% 515
90% 459