Page 37 - (KU)01-75GAJ-1.5 - Change 1

INTRO

EP'S (KU)01-75GAJ-1.5 A FIGURES

1.2.2 CAUTIONS B
ACAWS
Alert/Condition Crew Action
AIRSPEED MISCOMPARE C GROUND
The airspeed difference Compare the two airspeeds with the
between ADC 1 and ADC 2 VWDQGE\ LQGLFDWRU DQG NQRZQ ÀLJKW D
is greater than 10 knots. FRQ¿JXUDWLRQ FKDQJHV WR GHWHUPLQH
which is more accurate. TAKEOFF
E
If the standby airspeed indicator is not
functional: FIRE/SMK
NORM Do not use ADC2 data. F

If unable to determine the faulty PRES/OXY
NOT FOR FLIGHT
indicator: G
Use the most conservative airspeed.
H ENG/PROP
NOTE

:KHQ À\LQJ DW WKH SHUFHQW I
ÀDSV DSSURDFK UHIHUHQFH FUEL
speed (with no crosswind
or gusts) the HUD waterline L
should be about 5 to 6 degrees AAR
above the CDM.
ALL BLD AIR LEAK DET FAIL M
SPEC Primary and secondary sensor At pilot discretion, shut down all bleed ELEC
monitor failed or primary and air and descend to an altitude not N
secondary ground test failure. requiring oxygen.
All zone automatic overheat HYD
protection is lost. Icing conditions........................... Avoid O
ALTITUDE MISCOMPARE

The altitude difference between Compare the two altitudes with P FLT CTRL
ADC 1 and ADC 2 is greater the standby altitude indicator and
than the allowable difference NQRZQ ÀLJKW FRQ¿JXUDWLRQ FKDQJHV WR
(60 feet at 0 feet altitude to 350 determine which is more accurate. R GEAR
feet at 40,000 feet altitude).
If unable to determine the faulty
altimeter:
S DOR/RMP
PERF Use the most conservative altitude.

T JETTISON

U
LANDING

V
DITCHING
W
BAILOUT
X

OPER FAULT LG

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