DA42 Flashcards
(127 cards)
1
Q
Oil Amount
(min | max)
A
5 L | 7 L
2
Q
Gearbox Temperature
1. Minimum
2. Full Load Minimum
3. Maximum
A
-30 ºC
35 ºC
120 ºC
3
Q
Oil Consumption
A
0.1 L/h per engine
4
Q
Fuel Temperature
(min | max)
A
-30 ºC | 60ºC
5
Q
Fuel Pressure
(min | max)
A
4 bar | 7bar
6
Q
Propeller Diameter
A
1.87 m
7
Q
Propeller Angle Range
(takeoff | feathered)
A
12 | 81º
8
Q
Oil Grade
A
5W-30
9
Q
Fuel Flow at ISA 60%
A
10.4 USG/h
10
Q
Structure type & description
A
Semi-monocoque
Frames and webs of GFRP
Skin of half shells of CFRP
11
Q
The vertical stabilizer is…
A
An integral part of the fuselage
12
Q
How many windows are there?
A
3
13
Q
What are windows made out of?
A
Plexiglass
14
Q
Windows are attached by…
A
High performance elastic adhesive
15
Q
Maximum crosswind flaps UP
Maximum crosswind flaps APP
A
25 kt
20 kt
16
Q
TakeOff/Landing Distance with Wind
A
Headwind -10% for 14kt
Tailwind +10% for 3kt
17
Q
TakeOff Distance with Upslope
Landing Distance with Downslope
A
+12% ground roll for each 1% gradient
+9% ground roll for each 1% gradient
18
Q
Gradient formula
A
0.98*fpm/kt
19
Q
Vyse
A
85 kt
Blue radial
20
Q
Increased temperature leads to a __% performance requirement on _, _ & _
A
+10%
distance, time & fuel
21
Q
Landing Distance with Wet runway
A
+15%
22
Q
MTOM climb gradient
MLM climb gradient
A
6.6%
7.5%
23
Q
Consumption of fuel causes the CG to move ____
A
forward
24
Q
Consumption of de-icing causes the CG to move ____
A
back
25
Total seats
4
26
Garmin model
G1000
27
Airfoil name
FX 63-137/20 Wortmann 4
28
Wing area
16.29 m^2
29
Ailerons area
0.66 m^2
30
Flaps area
2.18 m^2
31
Horizontal empennage
& Elevator area
2.35 m^2
0.66 m^2
32
Vertical empennage
& Rudder area
2.43 m^2
0.78 m^2
33
Landing gear track
Landing gear wheelbase
2.95 m
1.73 m
34
Fuel type
JET-A1
35
What aircraft does NOT have auxiliary tanks?
Romeo
36
Main tank TOTAL
Main tank USABLE
52 USG
50.8 USG
37
Auxiliary TOTAL
Auxiliary USABLE
27.4 USG
26.4 USG
38
Maximum permissible imbalance
5 USG
39
Vfe APP
Vfe LDG
133 kt
113 kt
40
Vle & Vloe
Vlor
188 kt
152 kt
41
Vmca UP
Vmca APP
76 kt red radial
73 kt
42
Vo
112 kt up to 1700kg
119 kt +1700 kg
122 kt +1800 kg
43
White arc
62 kt
113 kt
44
Green arc
69 kt
151 kt
45
Yellow arc
151 kt
188 kt red radial
46
Coolant Temperature
0. Freezing
1. Minimum
2. Full Load Minimum
3. Maximum
-38 ºC
-30 ºC
60 ºC
105 ºC
47
Voltage
(min | max)
24.1 V | 32 V
48
Amperage Maximum
70 A
49
Stationary Prop Restart Speed
100 kt or non-spinning prop speed
50
Windmilling Restart Speed
125 kt - 145 kt
51
Restart time
Below 10,000 ft
Above 10,000 ft
2 min
Immediate
52
Maximum bank
60º
53
Load factor flaps UP
+3.8 G
-1.52 G
54
Load factor flaps APP/LDG
+2 G
-0 G
55
Maximum operating altitude
18,000 ft
56
Approved operations
Day VFR
Night VFR
IFR
Paved & Grass Runways
57
When is the battery legally required to be charged?
Night flights
58
What type of flight is not permitted with emergency switch seal broken?
IFR
59
Should canopy & doors be locked with KEY during flight?
No
60
Autopilot Airspeed
(min | max)
90 kt | 180 kt
61
Autopilot minimum altitude
1. Dep/App
2. Other phases
3. Captures
200 ft
800 ft
1200 ft
62
Autopilot is limited by
Airspeed
Altitude
Single engine operation
63
Engine description
Austro E4-B (4 Line Fuel Drive Turbocharged)
64
RPM Limitations
0. Idle ECU test
1. MCP
2. TakeOff
3. Max Overspeed
0. 740 +-30
1. 2100 RPM
2. 2300 RPM 5 min
3. 2500 RPM 20 s
65
Both Engines Horse Power
(MCP | TakeOff)
305 HP | 331 HP
66
Oil Pressure
1. Min below 1500 RPM
2. Min above 1500 RPM
3. Normal range
4. Max
0.9 bar
2.5 bar
2.5 - 6 bar
6.5 bar
67
To verify an EMPTY auxiliary tank...
1. Master ON
2. Aux Pump ON
3. Check PFD for AUX FUEL CAS
68
To verify a FULL auxiliary tank...
Open the deposit and check level
69
Deice capacity
L & kg
30L
33kg
70
Minimum deice to depart
3/4 deposit
71
Jet A1 density
3.03 kg/USG
72
Rudder movement is facilitated by
Mass & Aerodynamic (both forward of the pivot point)
73
Canopy attachment
and positions
Two hinges forward
Two locking bolts on a semi-open and two more on a safe position
Only pilot side has a "chivato"
74
Fuel drain points
Lowest part of fuel tank (below wings)
Lowest part of fuel filter (below engines)
75
General aircraft description
Low cantilever wings
Twin engine
Retractable landing gear
76
Trim is operated ______ through...
Electrically
Wheel or stick
77
Elevator backstop description
Limits upward from 15.5º to 13º
When both engines are above 20% with flap position
Electrically operated, but physical stop
78
Flap type
Split (inner wing)
Plain (outer wing)
79
Gear is actuated
And pump is actuated
hydraulically
electrically
80
With a fail in hydraulic pressure, gear extends because...
a spring forces it out, weight and air stream add to this
81
Hydraulic fluid capacity
1.5 L
82
Dumper contains
Accumulator contains
Hydraulic fluid
Nitrogen
83
Solenoid valve minimum pressure to extend gear
96.5 bar
84
Landing gear extension time
6 to 10 seconds
85
Solenoid valve pressure for fully retracted gear
113.8 bar
86
How many brake plates are there?
8, for each gear 4
87
Using rudder you can turn nose gear up to _º
Using brakes you can turn nose gear up to _º
9º
42º
88
Sump is of ___ type
wet
89
Reduction gear ratio
1:1.69
90
In case of engine failure, ECU to use is...
Of automatic selection
91
How many low pressure fuel pumps are PER ENGINE?
2
92
Fire warning is triggered above ___ºC
250
93
Blades are made from
Covered whole by
Covered leading edge by
wood
GFRP
Stainless-steel
94
How many alternators are there?
2
95
1 Main battery __ Volts & __ Amps hour
24 V
13.6 Ah
96
ECU backup batteries are connected...
automatically
97
Emergency battery location & duration
Behind pilot G1000 & 1.5 hours
98
External Power Unit location (EPU)
in front of nose gear
99
How many IAU are there?
2
100
AHRU alignment time and max bank
less than 1 min
up to 20º in air
101
ELT frequencies in MHz
121.5
243
406
102
Red terrain is
Yellow terrain is
higher
up to 1000 ft below
103
Deice is applied to...
Wings leading edge
All empennages
Propellers
Canopy
104
De-ice modes working & duration
0. Windshield
1. NORM
2. HIGH
3. MAX
0. 1 pump for 5 s (both are able to)
1. 30 s ON, 90 s OFF | 2.5 h
2. 1 pump continuously | 1 h
3. 2 pumps for 2 min | 0.5 h
105
De-ice alternate uses pump number _
2
106
Autopilot model
KAP 140
107
KAP 140 annunciators are on
Pitch
Roll
108
There are _ fuel chambers per wing and _ more behind the engine with auxiliary tanks
3
1
109
Aux pumps should be turned on when quantity is at or below
17 USG (one wing)
110
"L/R AUX FUEL E" appears because...
Auxiliar tank is empty, but pump is still on
111
Engine temperature limits
Engine start
Takeoff
-5 ºC
+5 ºC
112
Length x Width x Height
8.56 x 13.55 x 2.49 m
113
Callout oil on engine start
ENGINE OIL OUT OF RED
114
Emergency before Rotation
Power
Brakes
Report
115
Emergency with Runway available
Speed
Flap
Nose
*Land ahead
Brakes
Report
Secure
116
Emergency without Runway available
Speed
Rudder
Flap
Gear
VMC (req. pattern)
IMC (req. vectors)
*restart if possible
Secure
117
EF: Fly
Directional control
Airspeed
118
EF: Performance
Power live engine (cruise / climb)
Flaps
Gear
119
EF: Feather
Identify
Verify
Feather
120
EF: Cause
Air
Fuel
ECU
Brakes
Parameters
121
EF: Prepare
Selector
Alternator
Engine Master
122
EF: Start
Windmill
With starter
Say START
123
EF: Secure
Master
Pump
Alternator
Selector
124
Secure (briefing)
Master
Pump
Alternator
Selector
Electric
125
Oil Temperatures
-30 ºC
50 ºC
135 ºC
140 ºC
126
Stabilized
1000 ft AAL
No grand deflections needed
Vref +15 / -5 kt
Landing configuration
Power adjusted
127
Amount of batteries
1 Main
4 Backup
1 Emergency
