Page 340 - (KU)01-75GAJ-1.5 - Change 1
P. 340
INTRO
EP'S (KU)01-75GAJ-1.5 FIGURES
NOTE
ACAWS
LANDING GEAR and TOO LOW GEAR Special Alerts
will annunciate during approach.
GROUND
C. Autopilot PITCH......................................................................... OFF
Autopilot pitch axis will not engage.
TAKEOFF
D. Icing conditions...................................................... Avoid, if practical
A failure of the primary vertical tail boot de-icing timer may not be FIRE/SMK
NORM reported.
E. Landing gear............................................................... Visually verify PRES/OXY
NOT FOR FLIGHT
Right main landing gear indication failed. Visually verify landing
gear position before landing or before exceeding limiting speeds ENG/PROP
after gear retraction.
F. Aircraft hydraulic systems..................................................... Monitor FUEL
Booster system pressure indication and HYD PMP 3 and 4 PRESS
LO (C) ACAWS failed. Periodically scan aircraft and booster AAR
K\GUDXOLF UHVHUYRLU IRU VLJQV RI ÀXLG ORVV RU OHDNDJH 0RQLWRU
booster rudder boost pressure for indication of booster system
SPEC SUHVVXUH UXGGHU SUHVVXUH ZLOO EH LQ ORZ ERRVW ZLWK ÀDSV UHWUDFWHG ELEC
G. UNDERFLOOR switch.......................... OFF (below 15,000 ft MSL)
8QGHUÀRRU GXFW RYHUKHDW GHWHFWLRQ IDLOHG %OHHG DLU OHDN GHWHFWLRQ HYD
operative.
H. Potential Mission Impacts..................................................... Review FLT CTRL
Hydraulic pumps No. 3 and No. 4 fail-safe on. Hydraulic pumps
No. 3 and No. 4 cannot be isolated using the HYDRAULIC GEAR
ENGINE PUMPS, BOOST (No. 3 and No. 4) switches in the
event of a hydraulic leak. Engine shutdown may be required.
DOR/RMP
PERF NOTE
JETTISON
These values may remain in their last state if BAU lost
1553 bus communications but is still powered.
LANDING
Right landing light inoperative.
NOTE DITCHING
This item may remain in its last state if BAU lost 1553
bus communications but is still powered. BAILOUT
IFF 1 degraded: ZEROIZE not functional. ZEROIZE the IFF via
OPER pushbutton switch on front of IFF RT. FAULT LG
1 -300 Use, copying and/or disclosure is
governed by the statement on the
BACK title page of this document. CHARTS