DA20-100 ‘Katana’ 4X Manual
Neither the software nor the documentation may
be used for real aviation and training purposes.
03<12
page
3.3.8 GLIDING
EMERGENCY PROCEDURES
1.
Wing Flaps
2.
Airspeed at 1653 lbs (750 kg)
(V
IAS
)
73 kts / 84 mph / 135 km/h
T/O
3.
Glide Ratio 14, which means at
1000 ft/305m above ground, and with no
wind the distance of glide is
2.3 NM (4.25 km)
NOTE:
!
The glide distance from 1000 ft altitude increases for each 10 kts tail
wind by 1968 ft (0.6 km).
The glide distance from 1000 ft altitude decreases for each 10 kts
head wind by 2296 ft (0.7 km).
3.3.9 ELECTRICAL POWER FAILURE
a) Total Electrical Power Failure
1.
Battery Circuit Breaker
2.
Master Switch (Gen/Battery)
check ON
3.
If unsuccessful
Land at nearest suitable
airport
If tripped, reset
(GEN. Annunciator Illuminated)
b) Generator Failure
1.
2.
3.
4.
Master Switch (Generator)
Gen. Circuit Breaker
Gen. Control Circuit Breaker
If Gen. can't be brought on-line
Cycle OFF - ON
If tripped, reset
If tripped, reset
Switch OFF all non-flight
essential electrical consumers.
Monitor Ammeter and Voltmeter.
Land at nearest suitable airport.
Summary of Contents for DA20-100
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