Learjet 35A - Takeoff and Landing Operational Limits

111.11, •••• al
TAKEOFF AND lANDING OPERATIONAL UMlTS
TEMPERA11JRE LIMITS I
Refer to AMBIENT TEMPERATURE UMITS, Figure 1-4A.
E[~ Refer to FUEL TEMPERATURE UMrrS, this section.
MAXIMUM AL1TnJDE
Pressure Altitude ................................................................ 10,000 Feet
WIND COMPONENTS
MAXIMUM TAILWIND COMPONENT ................................... 10 Knots
DEMONSTRATED CROSSWIND COMPONENT
Refer to METEOROLOGICAL DEFINITIONS in Section V - PERFOR-
MANCE.
RUNWAY CONDmONS
Takeoff and landing is limited to paved runways.
Do not operate if water and/or slush accumulation on the runway exceeds
3/4 inch (19 mm).
MAXIMUM NOSE WHEEL SlEEKING SPEED
Maximum .............................................. 45 KNOTS GROUND SPEED
With any two of the foDowing
three Anti-Skid System lights
iUwninated: Two inboard and right
outboard ................................................
10 KNOTS GROUND SPEED
11RE LIMITING SPEED
Main Tires..... ............. ........ .......... ....... 182 KNOTS GROUND SPEED
11P TANK FUEL
Maximum
tip tank fuel for landing is 925 pounds (420 kg) each tip tank.
MINIMUM FUEL
I
Fuel Load - Minimum 600 pounds (272 kg) in each wing required for take- I
off and intentional go-around.
FAA APPROVED 4-30-76
RBSSUED 2-25-81, CHANGE 10
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