Learjet 36A - Maximum Landing Gear Extended Speed; Maximum Flap Extended Speed VFE; Critical Engine Failure Speed VI

111.111 •••• al
AlRSPEED/MACH LIMITS (CONT)
MAXIMUM lANDING GEAR EXTENDED SPEED V1E
VLE is the maximum speed at which the aircraft can be safely flown with the
landing gear extended.
VLE ..................................................................................... 265 KIAS
MAXIMUM FLAP EXTENDED SPEED VFE
VFE is the maximum speed permissible with the wing flaps in a prescribed
extended position.
VFE - Haps 1° to 8° ............................................................ 198 KIAS
VFE - Haps 9
0
to 20° .......................................................... 183 KIAS
VFE - Haps 21
0
to 40° ........................................................ 153 KIAS
MINIMUM CONfROL SPEED AIR VMcA
VMCA is the minimum flight speed at which the airplane is controllable with
5° bank when one engine suddenly becomes inoperative and the remaining
engine is operating at takeoff thrust.
VMCA is a function of altitude and temperature. The speed shown is a max-
imum, which occurs
at Sea Level, -lSOC (O°F). Section V Performance
Charts account for the appropriate values.
VMCA -18°C (O°F) at Sea level .............................................. 112 KIAS
MINIMUM CONfROL SPEED GROUND VMcG
VMCG is the minimum speed on the grotmd at which control can be main-
tained, using aerodynamic controls alone, when
one engine suddenly be-
comes inoperative and the remaining engine is operating at takeoff thrust.
VMCG is a function of altitude and temperature. The speed shown is a max-
imum, which occurs
at Sea Level, -lSOC (O°F). Section V Performance
Charts account for the appropriate values.
VMCG -18°C (O°F) at Sea level .............................................. 103 KIAS
CRITICAL ENGINE FAILURE SPEED VI
Refer to applicable figure entitled CRITICAL ENGINE FAILURE SPEED VI I
in Section V.
FAA APPROVED 4-30-76
REISSUED 2-25-81, CHANGE 10
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