Learjet 35A - Airspeed;Mach Limits

FAA APPROVED 4-30-76 1-9
REISSUED 2-25-81, CHANGE 13
AIRSPEED/MACH LIMITS
All Airspeed/Mach Limits are expressed in terms of in-
dicated values unless otherwise stated. Instrument error
is assumed to be zero.
MAXIMUM OPERATING SPEED V
MO
/M
MO
Do not extend spoilers, or operate with spoilers
deployed, at speeds above V
MO
/M
MO
due to signifi-
cant nose-down pitching moment associated with spoil-
er deployment.
V
MO
/M
MO
shall not be deliberately exceeded in any regime of flight
(climb, cruise or descent) unless a higher speed is authorized for flight test.
V
MO
Sea Level to 14,000 feet .............................................. 307 KIAS
V
MO
above 14,000 feet ....................................................... 359 KIAS
M
MO
...................................................................................... 0.83 M
I
M
MO
with any missing Boundary Layer Energizers (Aircraft 35-279 and
subsequent, 36-045 and subsequent and prior aircraft incorporat-
ing AAK 79-10 or AMK 83-5) .......................................... 0.78 M
I
M
MO
Mach Trim and Autopilot disengaged or inoperative .......... 0.74 M
I
M
MO
Stick Puller inoperative ................................................... 0.74 M
I
Refer to figure 1-4, entitled AIRSPEED/MACH LIMITS.
MANEUVERING SPEED V
A
Avoid rapid and large alternating control inputs, espe-
cially in combinations with large changes in pitch, roll
or yaw, as they may cause structural failure at any
speed, including below V
A
.
Refer to figure 1-4 entitled AIRSPEED/MACH LIMITS, this section for V
A
.
Maneuvers involving full application of rudder and aileron controls, as
well as maneuvers that involve pusher angles of attack should be confined
to speeds below V
A
.
MAXIMUM LANDING GEAR OPERATING SPEED V
LO
V
LO
is the maximum speed at which the landing gear can be safely extend-
ed or retracted.
V
LO
.................................................................................. 202 KIAS
NOTE
WARNING
CAUTION
, CHANGE
13
FAA APPROVED 4-30-76 1-9
REISSUED 2-25-81, CHANGE 13
AIRSPEED/MACH LIMITS
All Airspeed/Mach Limits are expressed in terms of in-
dicated values unless otherwise stated. Instrument error
is assumed to be zero.
MAXIMUM OPERATING SPEED V
MO
/M
MO
Do not extend spoilers, or operate with spoilers
deployed, at speeds above V
MO
/M
MO
due to signifi-
cant nose-down pitching moment associated with spoil-
er deployment.
V
MO
/M
MO
shall not be deliberately exceeded in any regime of flight
(climb, cruise or descent) unless a higher speed is authorized for flight test.
V
MO
Sea Level to 14,000 feet .............................................. 307 KIAS
V
MO
above 14,000 feet ....................................................... 359 KIAS
M
MO
...................................................................................... 0.83 M
I
M
MO
with any missing Boundary Layer Energizers (Aircraft 35-279 and
subsequent, 36-045 and subsequent and prior aircraft incorporat-
ing AAK 79-10 or AMK 83-5) .......................................... 0.78 M
I
M
MO
Mach Trim and Autopilot disengaged or inoperative .......... 0.74 M
I
M
MO
Stick Puller inoperative ................................................... 0.74 M
I
Refer to figure 1-4, entitled AIRSPEED/MACH LIMITS.
MANEUVERING SPEED V
A
Avoid rapid and large alternating control inputs, espe-
cially in combinations with large changes in pitch, roll
or yaw, as they may cause structural failure at any
speed, including below V
A
.
Refer to figure 1-4 entitled AIRSPEED/MACH LIMITS, this section for V
A
.
Maneuvers involving full application of rudder and aileron controls, as
well as maneuvers that involve pusher angles of attack should be confined
to speeds below V
A
.
MAXIMUM LANDING GEAR OPERATING SPEED V
LO
V
LO
is the maximum speed at which the landing gear can be safely extend-
ed or retracted.
V
LO
.................................................................................. 202 KIAS
NOTE
WARNING
CAUTION
, CHANGE
13