Page 16
Section - 3
EMERGENCY PROCEDURES
FAA Approved
Original Issue: Feb 28, 2006
Hawker 850XP Pro Line 21 Airplane Flight Manual
DOUBLE GENERATOR FAILURE (continued)
If Generator Reset Unsuccessful
ENG CMPTERs 1 & 2 ....................................................OFF
ENG ANTICE 1 & 2........................................................ON
Electrical loads...............................................................Reduce to minimum, at pilot’s
discretion.
NOTES:
1. It is essential that electrical loads are kept to a minimum for flight. If this procedure
is followed, there is sufficient battery power to maintain emergency loads for
approximately 30 minutes. This assumes the continuous use of the following:
Left pitot heater; pilot’s audio system; pilot’s PFD; pilot’s MFD; GPS 1
(Latitude/Longitude data on CDU 1 only); CDU 1; COMM 1; VHF NAV 1
(course guidance data on ESIS only); DME 1 (distance data on ESIS only);
Transponder 1 (Mode C inoperative); ADC 1, AHRS 1 and intermittent use of:
Chart lights.........................................................10 minutes total use
Cabin temperature control .................................In MANUAL mode
2. Other PE services must be switched off or isolated by pulling the relevant
circuit breakers.
The following loads may be selected on at the pilot’s discretion.
Service
Duty Cycle
In Minutes
Reduction In Flight Time
In Minutes
Single Fuel Pump
5
2
10
4
Landing Light
5
2
10
4
ENG IGNITION ON
Single Engine
10
0.5
ENG IGNITION ON
Two Engines
10
1
One Engine Computer
5
0.75
10
1.5
Two Engine Computers
5
1.5
10
3
Continued Next Page
For Training Purposes Only
