Page 338 - (KU)01-75GAJ-1.5 - Change 1
P. 338
INTRO
EP'S (KU)01-75GAJ-1.5 FIGURES
B. Icing conditions......................................................... Exit, if practical
ACAWS
Wing/empennage A/I valve failure may not be detected. If icing
conditions cannot be avoided, monitor wing/empennage ice
protected surfaces for lack of ice shedding. GROUND
C. Landing gear............................................................... Visually verify
TAKEOFF
The left main landing gear indication failed. Visually verify landing
gear position before landing or before exceeding limiting speeds
after gear retraction.
FIRE/SMK
NORM D. Aircraft hydraulic systems..................................................... Monitor
Utility system pressure indication and HYD PMP 1 and 2 PRESS PRES/OXY
LO (C) ACAWS failed. Periodically scan aircraft and utility hydraulic
UHVHUYRLU IRU VLJQV RI ÀXLG ORVV RU OHDNDJH 0RQLWRU XWLOLW\ UXGGHU
boost pressure for indication of utility system pressure (rudder ENG/PROP
SUHVVXUH ZLOO EH LQ ORZ ERRVW ZLWK ÀDSV UHWUDFWHG
E. Potential Mission Impacts..................................................... Review FUEL
Hydraulic pumps No. 1 and No. 2 fail-safe on. Hydraulic pumps
No. 1 and No. 2 cannot be isolated using the HYDRAULIC AAR
ENGINE PUMPS, UTIL (No. 1 and No. 2) switches in the event
of a hydraulic leak. Engine shutdown may be required.
SPEC NOT FOR FLIGHT ELEC
NOTE
This item may remain in its last state if BAU lost 1553 HYD
bus communications but is still powered.
APU EGT indicator failed. APU will continue to run (if already FLT CTRL
running) but cannot be started.
APU bleed air valve failed closed. GEAR
NOTE
DOR/RMP
PERF These values may remain in their last state if BAU lost
1553 bus communications but is still powered.
JETTISON
BLEED AIR PRESSURE indication latched on last known value;
consider inoperative.
LANDING
/HIW ODQGLQJ OLJKW FRYHUW UHIXHOLQJ SUREH ÀRRGOLJKW DQG FRYHUW
formation lights inoperative.
DITCHING
NOTE
These values may remain in their last state if BAU lost BAILOUT
1553 bus communications but is still powered.
OPER FAULT LG
1 -298 Use, copying and/or disclosure is
governed by the statement on the
BACK title page of this document. CHARTS