Reading...
Play button
Play button
Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
95 Cards in this Set
- Front
- Back
|
VSO (Stall speed in LDG configuration)
|
34
|
|
|
VS1 (Stall speed in CRUISE configuration)
|
42
|
|
|
VR (Rotate Speed)
|
44
|
|
|
Lift-off airspeed
|
52
|
|
|
Normal landing final approach airspeed
|
60
|
|
|
No-Flap landing final approach airspeed
|
65
|
|
|
Vx (flaps T/O) (Best angle of climb)
|
60
|
|
|
Vx (flaps CRUISE) (Best angle of climb)
|
65
|
|
|
Vy (flaps T/O) (Best rate of climb)
|
66
|
|
|
Vy (flaps CRUISE) (Best rate of climb)
|
70
|
|
|
Positive limit load factor (flaps CRUISE)
|
+4.4
|
|
|
Negative limit load factor (flaps CRUISE)
|
-2.2
|
|
|
Positive limit load factor (flaps T/O or LDG)
|
+2.0
|
|
|
Negative limit load factor (flaps T/O or LDG)
|
-0
|
|
|
Voltmeter lower limit red arc (volts)
|
8-11
|
|
|
Voltmeter caution range yellow arc (volts)
|
11-12.5
|
|
|
Voltmeter upper limit red line (volts)
|
16.1
|
|
|
Approved fuel grade
|
100LL
|
|
|
Fuel tank capacity (US gal.)
|
24.5
|
|
|
Max. ramp weight (lbs)
|
1770
|
|
|
Max. landing weight (lbs)
|
1764
|
|
|
Forward CG limit (at or below 1653 lbs)
|
7.95
|
|
|
Forward CG limit (1764 lbs)
|
8.07
|
|
|
Aft CG limit (1764 lbs)
|
12.16
|
|
|
Aft CG limit (at or below 1653 lbs)
|
12.48
|
|
|
Max. weight in baggage compartment (lbs)
|
44
|
|
|
Min. idle mixture rise leaned to peak (runup/shutdown)
|
50
|
|
|
Min. rpm during engine runup idle check
|
975
|
|
|
Min. permissible static rpm (full throttle runup)
|
2000
|
|
|
Tachometer normal operating range (rpm)
|
700-2800
|
|
|
Min. rpm drop during magneto check
|
25
|
|
|
Max. rpm drop during magneto check
|
150
|
|
|
Max. rpm drop difference between magnetos
|
50
|
|
|
Max. permissible continuous bhp
|
125
|
|
|
Min. oil pressure (psi)
|
10
|
|
|
Max. oil pressure for full power operation if OA < 0 degC
|
70
|
|
|
Min. oil temperature (degF)
|
75
|
|
|
Fuel pressure lower limit red line (psi)
|
3.5
|
|
|
Fuel pressure uper limit red line (psi)
|
32.5
|
|
|
Max time for CHT below 300defF in descent (minutes)
|
5
|
|
|
Min. CHT (degF) takeoff & descent
|
240
|
|
|
CHT normal operating range (degF)
|
300-420
|
|
|
CHT caution range (degF)
|
420-460
|
|
|
Max. CHT (degF)
|
460
|
|
|
Max. OAT (degC) operation w/ full winterization kit
|
0
|
|
|
Max crosswind component student dual (kts)
|
15
|
|
|
Maximum airplane structural temperature (degC)
|
55
|
|
|
Propeller approx. minimum ground clearance (inches)
|
10
|
|
|
Main landing gear tire pressure (psi)
|
33
|
|
|
Max. CHT (degF)
|
460
|
|
|
Max. OAT (degC) operation w/ partial winterization kit
|
12.5
|
|
|
Main landing gear tire pressure (psi)
|
33
|
|
|
Nose gear tire pressure (psi)
|
26
|
|
|
Min. OAT (degC) cabin heat not req for 10 min. before T/O
|
-20
|
|
|
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
|
|
|
VFE (flaps LDG) (Max. Airspeed with flaps extended)
|
78
|
|
|
VFE (flaps T/O) (Max. Airspeed with flaps extended)
|
100
|
|
|
VA (1764 lbs) (No full or abrupts control inputs above VA or overstress conditions will occur.)
|
106
|
|
|
VNO (Max. structural cruising speed)
|
118
|
|
|
Force propeller to windmill if stopped and starter is inop
|
137
|
|
|
VNE (never exceed airspeed)
|
164
|
|
|
Maximum permissible bank angle for steep turns
|
60deg
|
|
|
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 (degF)
|
170-220
|
|
|
Min oil temp. to begin an area SFL at Area Idle (degF)
|
170
|
|
|
Min. oil quantity (US qts)
|
4
|
|
|
Max. oil quantity (US qts)
|
6
|
|
|
Max. continuous starter operation
|
10 sec.
|
|
|
Max. cumulative starter op. before cooling 3-5min.
|
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
|
|
|
ENGINE FIRE ON THE GROUND
|
FUEL SHUTOFF VALVE -- OFF
CABIN HEAT -- OFF |
|
|
ELECTRICAL FIRE ON THE GROUND
|
GEN/BAT MASTER SWITCH -- OFF
|
|
|
ABORT
|
THROTTLE -- IDLE
BRAKES -- AS REQUIRED FLAPS -- CRUISE |
|
|
MALFUNCTION IN FLIGHT (SUFFICIENT RUNWAY REMAINING TO LAND)
|
AIRSPEED -- 60 KIAS
FLAPS -- LDG |
|
|
ENGINE MALFUNCTION IN FLIGHT (FUEL PRESSURE LOSS)
|
FUEL PUMP -- ON
|
|
|
ENGINE FIRE DURING FLIGHT
|
FUEL SHUTOFF VALVE -- OFF
CABIN HEAT -- OFF |
|
|
ELECTRICAL FIRE DURING FLIGHT
|
GEN/BAT MASTER SWITCH -- OFF
AIR VENTS AND WINDOWS -- OPEN |
|
|
CABIN FIRE IN FLIGHT
|
GEN/BAT MASTER SWITCH -- OFF
AIR VENTS AND WINDOWS -- OPEN CABIN HEAT -- OFF |
