Learjet 35 - Takeoff and Landing Operational Limits

3-20 Developed for Training Purposes Leerjet 35/36
February 1998
CAE SimuFlite
Takeoff and Landing Operational Limits
Demonstrated Crosswind Component . . . . . . . . 24.7 KTS
Nosewheel Steering Speed:
Maximum Speed. . . . . . . . . . . . . . 45 KTS GROUNDSPEED
With any 2 of the right 3
anti-skid lights illuminated . . . . . 10 KTS GROUNDSPEED
Maximum (Pressure) Altitude . . . . . . . . . . . . . . . . . .10,000 FT
Maximum Tailwind Component . . . . . . . . . . . . . . . . . . . 10 KTS
Temperature Limits
(at Sea Level). . . . . . . . . . . . -54°TO +50°C (-65.2° TO +122°F)
Main Tires Limiting Speeds . . . . 182 KTS GROUNDSPEED
Do not operate if water and/or slush accumulation on the run-
way exceeds 3/4 inch (19 mm).
Do not take off or land with the cabin pressurized.
Maximum tip tank fuel for landing is 925 lbs (420 kg) each tip
tank.
Minimum 600 lbs (272 kg) fuel in each wing are required for
takeoff and intentional go-around.
Seat belts and shoulder harnesses must be worn during takeoff
and landing.
When OAT is below -25°C (-13°F), engines should be operated
for three minutes prior to takeoff to bring the hydraulic system
up to normal operating temperature.
No more than three vortex generators can be missing from
each wing.
Information shown in italics is not included in the AFM Limitations chapter.