LIMITATIONS
AIRPLANE
FLIGHT
MANUAL
2-10 ANAC APPROVED
Page 6 code 02 REVISION 2
AFM-1912
MANEUVERING FLIGHT LOAD FACTORS
These corresponding accelerations limit the bank angle during turns
and limit the pull-up maneuvers.
LOAD FACTOR LIMIT FLAPS UP
FLAPS DOWN
(1, 2, 3, 4, 5 AND
FULL)
Positive 2.5 g 2.00 g
Negative - 1.00 g 0 g
RUNWAY
Runway Slope............................................................... -2% TO +2%
Runway Surface Type................................................... PAVED
TOWING
Towbarless towing is prohibited, unless the towbarless towing
operations are performed in compliance with the appropriate
operational requirements using towbarless towing vehicles that are
designed and operated to preclude damage to the airplane nose
landing gear, steering system and associated fuselage structure. For
steering system, if damage cannot be precluded a reliable and
unmistakable warning must be provided when damage to the steering
system may have occurred.
Towbarless towing vehicles that are specifically accepted for this type
of airplane are listed in the AMM Chapter 9.
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