2-12 FAA APPROVED 4-30-76
REISSUED 2-25-81, CHANGE 13
BEFORE STARTING ENGINES (CONT)
(a) As the needle passes the green-yellow margin, the
shaker will actuate and the L STALL warning light shall
flash.
(b) As the needle advances to the red segment, the pusher
will actuate briefly, then stop. L STALL warning light
will illuminate steady just prior to or at pusher actua-
tion. After pusher stops, the needle shall sweep back
and remain in the yellow or green segment.
(4) TEST Button — Release.
(5) Rotate TEST Selector Switch to R STALL. Depress and
hold TEST button. The test operation will be identical to
Step (3) above except needle will sweep the copilot’s
angle-of-attack indicator, and the red R STALL warning
light will flash.
(6) TEST Button — Release.
With STALL WARNING switches On, steady illumina-
tion of the L or R STALL warning light indicates a mal-
function, except during pusher actuation or system test.
(7) Flaps — DN. Check that both angle-of-attack indicators
shift position three times as flaps are lowered to the full
travel.
(8) STALL WARNING Switches — OFF.
19. Third Attitude Gyro — Uncage.
20. Pressurization and Temperature Controls — Check and set as
follows:
a. Pressurization Controls:
• For manual mode pressurization, refer to PRESSUR-
IZATION SYSTEM OPERATION, this section.
• Aircraft with Emergency Pressurization Override
switches installed. For takeoff at field elevations
above 8500 feet pressure altitude, refer to PRES-
SURIZATION SYSTEM OPERATION, this section.
• Aircraft 35-067 thru 35-112 except 35-107. Aircraft 36-
018 thru 36-031.
(1) L and R BLEED AIR Switches — Check, On.
(2) CABIN AIR Switch — OFF.
(3) PRESSURIZATION AUTO-MAN Switch — AUTO.
(4) AIRCRAFT ALT Selector Knob — Rotate to cruise
altitude.
NOTE
◆
NOTE
◆
2-12 FAA APPROVED 4-30-76
REISSUED 2-25-81, CHANGE 13
BEFORE STARTING ENGINES (CONT)
(a) As the needle passes the green-yellow margin, the
shaker will actuate and the L STALL warning light shall
flash.
(b) As the needle advances to the red segment, the pusher
will actuate briefly, then stop. L STALL warning light
will illuminate steady just prior to or at pusher actua-
tion. After pusher stops, the needle shall sweep back
and remain in the yellow or green segment.
(4) TEST Button — Release.
(5) Rotate TEST Selector Switch to R STALL. Depress and
hold TEST button. The test operation will be identical to
Step (3) above except needle will sweep the copilot’s
angle-of-attack indicator, and the red R STALL warning
light will flash.
(6) TEST Button — Release.
With STALL WARNING switches On, steady illumina-
tion of the L or R STALL warning light indicates a mal-
function, except during pusher actuation or system test.
(7) Flaps — DN. Check that both angle-of-attack indicators
shift position three times as flaps are lowered to the full
travel.
(8) STALL WARNING Switches — OFF.
19. Third Attitude Gyro — Uncage.
20. Pressurization and Temperature Controls — Check and set as
follows:
a. Pressurization Controls:
• For manual mode pressurization, refer to PRESSUR-
IZATION SYSTEM OPERATION, this section.
• Aircraft with Emergency Pressurization Override
switches installed. For takeoff at field elevations
above 8500 feet pressure altitude, refer to PRES-
SURIZATION SYSTEM OPERATION, this section.
• Aircraft 35-067 thru 35-112 except 35-107. Aircraft 36-
018 thru 36-031.
(1) L and R BLEED AIR Switches — Check, On.
(2) CABIN AIR Switch — OFF.
(3) PRESSURIZATION AUTO-MAN Switch — AUTO.
(4) AIRCRAFT ALT Selector Knob — Rotate to cruise
altitude.
NOTE
◆
NOTE
◆
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