Limitations Model G58
Section 2
2-14
MANEUVER LIMITS
This is a normal category airplane. Acrobatic maneuvers,
including spins, are prohibited.
FLIGHT LOAD FACTORS (5500 Pounds)
Positive Maneuvering Load Factors:
Flaps Up (0°) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3.8 G
Flaps Down (30°) . . . . . . . . . . . . . . . . . . . . . . . . . . . .2.0 G
MINIMUM FLIGHT CREW
One (1) Pilot
MAXIMUM PASSENGER SEATING CONFIGU-
RATION
Five (5) passengers and one (1) pilot
SEATING
Do not take off or land with the seat back of an occupied pilot’s
or copilot’s seat in the full back position. The seat back of an
occupied optional copilot’s full reclining seat and the seat
backs of all other occupied seats must be in the most upright
position for takeoffs and landings. Occupied aft-facing seats
must have headrests fully extended.
ICING LIMITATIONS
Minimum Airspeed During
Icing Conditions . . . . . . . . . . . . . . . . . . . . . . . . . . . . 130 knots
Minimum Ambient Temperature for
Operation of Deicing Boots . . . . . . . . . . . . . . . . . . . . . . . -40°C
Pneumatic pumps are time limited for engine operation to 400
hours.
Do not operate the propeller deice system when propellers are
static.
May, 2015
58-590000-67A12_sec02.fm Page 14 Wednesday, May 27, 2015 8:56 AM
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