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
Summary of Contents for 35A
Page 26: ...1 8 Center of Gravity Envelope Figure 1 3 FAA APPROVED 4 30 76 REISSUED 2 25 81 ...
Page 47: ...1 24 111 111 INTENTIONAlLY LEFf BlANK FAA APPROVED 4 30 76 REISSUED 2 25 81 CHANGE 12 ...
Page 115: ...2 58 INTENTIONALLY LEFT BLANK FAA APPROVED 4 30 76 REISSUED 2 25 81 CHANGE 12 ...
Page 117: ...2 60 INTENTIONALLY LEFT BlANK FAA APPROVED 4 30 76 REISSUED 2 25 81 CHANGE 12 ...
Page 158: ...INTENIlONAlLY LEFT BlANK FAA APPROVED 4 30 76 REISSUED 2 25 81 CHANGE 12 3 13 ...