Specifications

SECTION VI
MODEL 560 EMERGENCY PROCEDURES
LOSS OF BOTH GENERATORS (GEN OFF L AND R CAUTION LIGHTS ON AND MASTER
WARNING) (Continued)
NOTE
When flaps are at approach (15°) and the landing gear is down for the approach to
landing, maintain V
APP
+10 KIAS minimum.
WHEN LANDING ASSURED
6. Pressurization - ZERO DIFFERENTIAL PRIOR TO LANDING (use manual toggle switch to
depressurize cabin).
7. Landing Gear - DOWN.
8. Flaps - LAND (35°).
9. Airspeed - V
REF
+5 KIAS.
10. Landing - Use emergency brake system. Refer to Abnormal Procedures, WHEEL BRAKE
FAILURE.
NOTE
For emergency braking, multiply landing distance by 2.3.
IF ONLY ONE GENERATOR COMES ON
2. Electrical Load - REDUCE as required.
3. Air Conditioner Compressor - OFF or FAN.
NOTE
The Interior Master Switch, located on the LH Oxygen Panel, will shed all
non-essential passenger cabin electrical loads.
AC POWER FAILURE (AC FAIL AND MASTER WARNING LIGHTS ON) AND DUAL INVERTER
FAILURE (MASTER CAUTION AND INVTR FAIL 1 AND 2 CAUTION LIGHTS ON)
1. BATT Switch - EMER.
2. Refer to standby flight display and standby HSI.
NOTE
Placing the battery switch to EMER will provide AC power from the static inverter in
DG1 to power the standby HSI compass display. Both compass and NAV1
information will be displayed on the standby HSI. The PFD's and MFD will be
inoperative with an AC power system failure.
3. INV 1/INV 2 Switch - NORM.
4. AC INVERTER NO. 1 (LH panel) and NO. 2 (RH panel) Circuit Breakers - CHECK and RESET.
IF BOTH INVERTERS WILL NOT RESET
5. AC INVERTER NO. 1 Circuit Breaker (LH panel) - PULL.
6. INVTR FAIL 2 Annunciator - CHECK (No annunciation indicates recovery of Inverter 2). Refer to
IF INVERTER 1 OR 2 RECOVERS.
NOTE
If Inverter NO. 2 recovers, do not reset AC INVERTER NO. 1 breaker.
(Continued Next Page)
I
56OMB-01 Configuration AN 6-19