No aerobatic maneuvers are approved except those listed below:
MANEUVER
Chandelles
Lazy Eights
Steep Turns
Spins
.
.
.
.
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•
Stalls (Except Whip Stalls).
MAXIMUM ENTRY SPEED
. . 109 MPH (95 knots)
. . 109 MPH (95 knots)
. . 109 MPH {95 knots)
Use Slow Deceleration
Use Slow 'Deceleration
During prolonged spins, the aircraft engine may stop; however, spin
recovery is not adversely affected by engine stoppage. Intentional spins
with wing flaps extended are prohibited.
Aerobatics that may impose high inverted loads should not be attempt
ed. The important thing to bear in mind in flight maneuvers is that the
airplane is clean in aerodynamic design and will build up speed quickly
with the nose doWQ. Proper speed control is an essentia:l requirement
for execution of any maneuver, and care should always be exercised to
avoid excessive speed which in turn can impose excessive loads. In the
execution of all maneuvers, avoid abrupt use of controls.
AIRSPEED LIMITATIONS.
The following are the certificated calibrated airspeed limits for
the Cessna 150:
Maximum (Glide or dive, smooth air) .
Caution Range .
.
•
Normal Range .
.
.
.
Flap Operating Range .
Maneuvering Speed*
.
.
.
•
162 MPH (red line)
. 120-162 MPH (yellow arc)
56-120 MPH (green arc)
49-100 MPH {white arc)
.
.
.
•
.
109 MPH
*The maximum speed at which you can use abrupt
control travel without exceeding the design load factor.
ENGINE OPERATION LIMITATIONS.
Power and Speed
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•
.
. . . .
•
.
•
.
.
•
•
100 BHP at 2750 RPM
3-2
t