ELECTRICAL POWER FAILURE
(HELICOPTERS EQUIPPED WITH EMERGENCY BUS) 3–45
RAD-MSTR (RADIO MASTER) SWITCH FAILURE 3–48V
HELIPILOT MALFUNCTION 3–48V
AUTOTRIM MALFUNCTION 3–50
INTERCOMMUNICATION SYSTEM FAILURE 3–50
INTEGRATED DISPLAY SYSTEM FAILURE 3–51
FIRE 3–56
ENGINE FIRE 3–56
ENGINE FIRE DURING START 3–56
ENGINE FIRE IN FLIGHT 3–57
SMOKE IN CABIN, TOXIC FUMES, ETC. 3–58
STATIC PORT OBSTRUCTION 3–59
FLIGHT IN THUNDERSTORM - LIGHTNING 3–59
EMERGENCY PROCEDURE FOR LIMIT OVERRIDE PUSH-
BUTTON OPERATION 3–60
LIST OF ILLUSTRATIONS
Page
Figure 3-1 - Cockpit Layout of the Warning and Caution System. 3–4
RFM A109E
Table of Contents (Cont.)
3-ii E.A.S.A. Approved
Rev. 35
To Next Page
Loading...