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Learjet 35 - Century III Wing;Fc-200 Autopilot;Ras-AAK 76-4

Learjet 35
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Leerjet 35/36 Developed for Training Purposes 3-9
February 1998
Limitations
Century III Wing/FC-200 Autopilot/RAS-AAK 76-4
MMO, Maximum Operating – Mach:
MMO . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.83 MI
S/N 35-279 and subsequent; 36-045 and subsequent;
prior aircraft with AAK 79-10 or AMK 83-5:
With Missing BLEs . . . . . . . . . . . . . . . . . . 0.78 MI
Mach Trim/Autopilot
Disengaged or Inoperative . . . . . . . . . . . . . . 0.74 MI
Stick Puller Inoperative . . . . . . . . . . . . . . . . 0.74 MI
VMO, Maximum Operating – Airspeed:
Sea Level to 14,000 Ft . . . . . . . . . . . . . . . 307 KIAS
Above 14,000 Ft . . . . . . . . . . . . . . . . . . 359 KIAS
VA, Maximum Maneuvering (See Figure 3-2)
VLE, Maximum Landing Gear Extended . . . . . . . . . . 265 KIAS
VLO, Maximum Landing Gear Operating . . . . . . . . . . 202 KIAS
VFE, Maximum Flap Extended:
Flaps 1° to 8° . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 198 KIAS
Flaps 9° to 20° . . . . . . . . . . . . . . . . . . . . . . . . . . . . 183 KIAS
Flaps 21° to 40° . . . . . . . . . . . . . . . . . . . . . . . . . . . 153 KIAS
VMCA, Minimum Control – Air:
0°F (-18°C) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 112 KIAS
VMCG, Minimum Control – Ground:
0°F (-18°C) at Sea Level. . . . . . . . . . . . . . . . . . . . . 103 KIAS
Turbulent Air Penetration:*
Airspeed* . . . . . . . . . . . . . . . . . . . . . . 250 KIAS OR 0.73 MI,
. . . . . . . . . . . . . . . .WHICHEVER IS LESS
*Avoid flight through severe turbulence.

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