limit for full DOWN extension (100%) of the wing flaps is
control airspeed (Vmc) at sea level standard conditions is 89
157 KIAS. If wing flaps are extended above these speeds,
K I A S .
the flaps or their operating mechanisms may be damaged.
MAXIMUM DESIGN MANEUVERING SPEED.
5-25. MINIMUM SINGLE-ENGINE CONTROL
The maximum design maneuvering speed is 173 KIAS.
Chapter 7, Section X describes minimum single-
engine control airspeed. The minimum single-engine
Section VI. MANEUVERING LIMITS
G's with wing flaps up or a positive load factor of
2.0 Gs, or a negative 1.227 Gs with wing flaps
a. The following maneuvers are prohibited.
b. Recommended turbulent air penetration airspeed is
2. Aerobatics of any kind.
3. Abrupt maneuvers above 173 KIAS.
5-28. BANK AND PITCH LIMITS.
a. Bank limits are 60° left or right.
4. Any maneuver which results in a positive load fac-
tor of 3.10 Gs or a negative load factor of 1.227
b. Pitch limits are 30° above or below the horizon.
Change 3 5-8.1