Leerjet 35/36 Developed for Training Purposes 3-53
February 1998
Limitations – U.K.
Operational Limits
General
Temperature Limits:
Maximum . . . . . . . . . . . . . . . . . . . . . . . . +50°C (ISA + 35°C)
Minimum . . . . . . . . . . . . . . . . . . . . . . . . . . -54°C (ISA - 69°C)
Maximum Altitude Limit
(Pressure Altitude) . . . . . . . . . . . . . . . . . . . . . . . . .45,000 FT
Do not operate above:
Q
43,000 ft at weights in excess of 15,000 lbs
Q
40,000 ft at weights in excess of 16,500 lbs.
With one fuel computer inoperative, the aircraft shall not be
flown for public transport or for any purpose except positioning.
Do not take off or land with the cabin pressurized.
Takeoff
When OAT is below -35°C, engine should be operated for three
minutes prior to takeoff to bring hydraulic system up to normal
operating temperature. If OAT is below the lowest temperature
shown on the performance charts, use performance at the low
est temperature shown.
Maximum Altitude Limit (Pressure Altitude) . . . . . . 10,000 FT
Maximum Tailwind Component . . . . . . . . . . . . . . . . . . 10 KTS
Do not operate if water and/or slush accumulation on runway
exceeds
1/2 inch.
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