Specifications
Table Of Contents
- 560 ENCORE OPERATING MANUAL

SECTION VI
MODEL 560 EMERGENCY PROCEDURES
ELECTRICAL FIRE OR SMOKE (Continued)
KNOWN SOURCE
5. Faulty Circuit(s) - PULL CIRCUIT BREAKER(s) to isolate.
6. Land as soon as practical.
UNKNOWN SOURCE
5. INTERIOR MASTER Switch - OFF.
6. Overhead FLOOD LTS - FULL BRIGHT.
7. BATT Switch - EMER.
8. L/R GEN Switches - OFF - With the battery switch in EMER and the generators OFF, a properly
charged battery will supply power for approximately 30 minutes to the following equipment:
COMM 1 LH and RH N
1
Indicators Overhead Flood Lights
NAV 1 Standby Pitot and Static Heaters Pilot’s and Copilot’s Audio Panels
DG 1 Landing Gear Control & Indication Standby HSI and Standby
RMU 1 Flap Control Flight Display
Standby Radio Control Head Interior Entry Lights
DME 1 (560-0552 only)
CAUTION
WHEN LANDING WITH EMERGENCY POWER (BATTERY SWITCH-EMER AND
BOTH GENERATORS OFF), THE FOLLOWING ARE NOT AVAILABLE:
f
THE ANTISKID/POWER BRAKE SYSTEM IS INOPERATIVE; ONLY THE
EMERGENCY BRAKE SYSTEM IS AVAILABLE.
f
THE WING AND ENGINE ANTI-ICE VALVES WILL BE OPEN. REFER TO
ANTI-ICE ON THRUST CHARTS.
f
THE RAM AIR TEMPERATURE GAUGE IS INOPERATIVE. SET GO-AROUND
THRUST BASED ON REPORTED GROUND TEMPERATURE.
f
ALL ENGINE INSTRUMENTS EXCEPT THE N
1
INDICATORS WILL BE
INOPERATIVE.
f
THE CABIN MUST BE DEPRESSURIZED WITH THE MANUAL TOGGLE
SWITCH. THE EMERGENCY DUMP SWITCH IS INOPERATIVE.
NOTE
The standby flight display will continue to operate on its own emergency battery pack.
This battery pack also provides 5-volt emergency instrument lighting for the standby
flight display, standby HSI, N
1
indicator, and standby radio control head.
(Continued Next Page)
I
56OMB-01 Configuration AB 6-15










