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33 Cards in this Set
- Front
- Back
Forced landing final approach airspeed (flaps LDG)
|
55
|
|
Min. engine-out airspeed to sustain windmilling prop
|
60
|
|
Forced landing final approach airspeed (flaps T/O)
|
60
|
|
Forced landing final approach airspeed (flaps CRUISE)
|
64
|
|
Best glide airspeed (1764 lbs) (L/D Max)
|
73
|
|
V_FE (flaps LDG)
(Max Airspeed with flaps extended) |
78
|
|
V_FE (flaps T/O)
(Max Airspeed with flaps extended) |
100
|
|
V_A (1764 lbs)
(No full or abrupt control inputs above V_A or overstress conditions will occur) |
106
|
|
V_NO
(Max. structural cruising speed) |
118
|
|
Force propeller to windmill if stopped and starter is inop
|
137
|
|
V_NE
(Never exceed airspeed) |
164
|
|
Maximum permissible bank angle for steep turns
|
60^o
(^o is the degrees symbol) |
|
Voltmeter green arc (volts)
|
12.5-16
|
|
Usable fuel (US gal.)
|
24.0
|
|
Max. takeoff weight (lbs)
|
1764
|
|
Min. rpm for in-flight (area) idle beyond gliding range of a runway
|
1400
|
|
Min. rpm operations with fuel pump off
|
1400
|
|
Max. permissible continuous rpm
|
2800
|
|
Oil pressure normal operating range (psi)
|
30-60
|
|
Max. time for oil pressure to reach 10 psi after start
|
30 sec.
|
|
Max. oil pressure (psi)
|
100
|
|
Max. rpm after start until oil temp indication registers
|
1000
|
|
Oil temperature normal operating range (^o F)
|
170-220
|
|
Min oil temp. to begin an area SFL at Area Idle (^o F)
|
170
|
|
Min. oil quantity (US qts)
|
4
|
|
Max. oil quantity (US quarts)
|
6
|
|
Max. continuous starter operation
|
10 sec.
|
|
Max cumulative starter op. before cooling 3-5 min.
|
30 sec.
|
|
Max. total wind student dual (kts)
|
25
|
|
Max. total wind student solo (kts)
|
20
|
|
DA20 max. demonstrated crosswind component (kts)
|
20
|
|
Max. crosswind component student solo (kts)
|
10
|
|
Max. tailwind component (kts)
|
5
|