Learjet 36A - Pressurization Limit; Windshield and Radome Anti-Ice Fluid; Thrust Reversers (if Installed)

FAA APPROVED 4-30-76 1-18.A
REISSUED 2-25-81, CHANGE 10
SYSTEM LIMITS (CONT)
PRESSURIZATION LIMIT
Maximum Differential Pressure................................................. 10.0 PSI
WINDSHIELD AND RADOME ANTI-ICE FLUID
Methyl Alcohol (Methanol) per Federal Specification O-M-232, Grade A, is
required.
THRUST REVERSERS (IF INSTALLED)
When thrust reversers are installed, refer to the applicable Thrust Reverser
Supplement for limitations, normal procedures, emergency procedures, ab-
normal procedures, and performance data.
1-18A
FAA APPROVED 4-30-76 1-18.A
REISSUED 2-25-81, CHANGE 10
SYSTEM LIMITS (CONT)
PRESSURIZATION LIMIT
Maximum Differential Pressure................................................. 10.0 PSI
WINDSHIELD AND RADOME ANTI-ICE FLUID
Methyl Alcohol (Methanol) per Federal Specification O-M-232, Grade A, is
required.
THRUST REVERSERS (IF INSTALLED)
When thrust reversers are installed, refer to the applicable Thrust Reverser
Supplement for limitations, normal procedures, emergency procedures, ab-
normal procedures, and performance data.
1-18A