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LAT DA42 > Pitch & Power / V Speeds > Flashcards

Pitch & Power / V Speeds Flashcards

1
Q

Normal Cruise Level

A

130kt
70 %
0°

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2
Q

Long Range Cruise Level

A

120kt
60%
+1°

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3
Q

Max Endurance Cruise

A

115kt
55%
+2°

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4
Q

Vp Clean Level

A

110kt
50%
+2°

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5
Q

Vp App Level Gear Up

A

100kt
50%
-1°

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6
Q

Vp App Level Gear Down

A

100kt
70%
-1°

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7
Q

Vp App Descent Gear Down

A

100kt
30%
-4°

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8
Q

Va App Gear Down

A

85kt
25%
-3°

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9
Q

Va App Level Gear dow

A

85kt
65%
+1°

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10
Q

Va LDG Descent Gear down

A

80/82kt (>1700kg)
45%
-4°

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11
Q

Vp Clean Level Gear down

A

110kt
75%
+2°

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12
Q

Vp Clean Descent Gear Down

A

110kt
30%
-1°

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13
Q

Va Clean Descent Gear Down

A

90/91kt (>1700kg)
25%
0°

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14
Q

OEI

Vp Clean Level

A

100kt
95%
+1°

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15
Q

OEI

Vp App Level

A

90
100%
0°

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16
Q

OEI

Vp App Descent

A

90kt
45%
-4°

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17
Q

OEI

Vp App Descent Gear Down

A

90kt
75%
-4°

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18
Q

OEI

Va App Descent Gear Down

A

85kt
60%
-4°

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19
Q

VLO Gear Down

A

Max 188kt

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20
Q

VLO Gear Up

A

Max 152kt

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21
Q

VLE

A

Max 188kt

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22
Q

VFE Flaps App

A

Max 133kt

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23
Q

VFe Flaps LDG

A

Max 113kt

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24
Q

Maximum demonstrated crosswind component (including gusts)

A

20kt

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25
Q

Maximum tailwind component

A

5kt

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26
Q

VR

A

76kt

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27
Q

VMCA

A

71kt (red linke)
Minimum control Speed. The minimum speed at which it is possible to maintain directional control of the airplane in the air, wirth one engine wind milling and the other engine at T/O power (at MTOM, CG max. aft)

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28
Q

VMCA ICE

A

75kt

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29
Q

VSSE

A

85kt

The recommended safe one engine inoperative speed provides a margin above VMCA

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30
Q

VX

A

not published

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31
Q

VY

A

82kt

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32
Q

VYSE

A

85kt

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33
Q

VA

A

> 1542kg 123kt

<1542kg 117kt

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34
Q

VNO

A

151kt

35
Q

VNE

A

188kt (red radial)

36
Q

VS1

A

69kt

Stall speed in a specific configuration (gear + flaps up, 0° bank, at MTOM)

37
Q

VS0

A

62kt

Stall speed in the landing configuration (gear down, flaps LDG, 0° bank, at MLM)

38
Q

Autopilot maximum airspeed

A

180kt

39
Q

Autopilot minimum airspeed

A

90kt

40
Q

Fuel on board

A

25 USG each wing + 1 USG not usable

94.6l + 4l

41
Q

Aux fuel tanks

A

13.7 USG each wing

52l

42
Q

RPM Limitation

A

2300 RPM

43
Q

Max overspeed

A

2500 RPM for 20 sec

44
Q

MTOM

A

1785kg

45
Q

MLM

A

1785kg

46
Q

Maximum operating altitude

A

18000ft

47
Q

Maximum zero fuel mass

A

1730kg

48
Q

Max load at VA

A

+3.8

-1.52

49
Q

Minimum RWY length for T/O and landing

A

700m

50
Q

Minimum RWY length for T/G

A

850m

51
Q

Company operational limits

A

Visibility 1500m

Ceiling 300ft

52
Q

Engine Start Procedure

A

Power levers …………………………………………… IDLE ……………………………………………………. Strobe lights / Position lights …………………….. ON ……………………………………………………… Propeller area …………………………………………. CLEAR ………………………………………………..
Engine master (L/R) ………………………………… ON ……………………………………………………… Annunciations / Engine / System page ………. CHECKED …………………………………………… Glow annunciation …………………………………… OFF ……………………………………………………. Start key…………………………………………………. START …………………………………………………
Oil pressure ……………………………………………. CHECKED …………………………………………… Annunciations / Engine / System page ………. CHECKED …………………………………………… Strobe lights ……………………………………………. OFF …………………………………………………….

53
Q

Engine Failure / Fire during T/O

A

1Power…………………………………………….OFF 1
2Brakes…………………………………………APPLY 2
3ATC………………………………………….INFORM 3
If necessary:
4Engine Masters (2)…………………………….OFF 4
5Fuel selectors (2)………………………………OFF 5
6Electric Master………………………………….OFF 6
In case of fire:
7Cabin heat & defrost…………………………..OFF 7

54
Q

Engine Failure / Fire in Flight

A

1 PPAA

Above safe altitude
7Alternator (dead engine)……………………..OFF 7
8Fuel selector (dead engine)…………………..OFF 8
In case of fire:
9Cabin heat & defrost…………………………..OFF 9
10Canopy…………………….UNLATCH if necessary 10

Max airspeed 117 KIAS

55
Q

Landing with defective brakes

A 
After touchdown (if necessary): 
1Engine Masters (2)..................................OFF 1 
2Fuel selectors (2)....................................OFF 2
3Electric Master........................................OFF 3
56
Q

Landing Gear Up Landing

A

1Approach…………………………………..NORMAL 1

 If time/situation allows: just before touchdown: 
2Power lever...........................................IDLE 2 
3Engine Masters (2)..................................OFF 3 
4Fuel selectors (2)....................................OFF 4

Immediately after touchdown:
5Electric Master………………………………….OFF 5

57
Q

Spannweite

A

13.55m

58
Q

Länge

A

8.56m

59
Q

Batterien

A 
24V 10 Ah Main battery
2x 12V 1.3 Ah Alternator excitation
Emergency Battery (standby gyro and flood flood light) for 1.5h
ECU backup battery
ELT battery
60
Q

Single engine rate of climb

A

approx. 150 FPM

Gear Down minus approx. 200 FPM

Windmilling Propeller minus approx. 200 FPM

61
Q

PPAA T/O bis Power Reduction

A
  • 80% Performance

ENGINE FAILURE

1) pitch 5°
2) T/O power set
3) gear up
4) speed 85kt
5) X engine failed
6) X power Lever idle
7) X engine master off

No PPAA calls

On safe altitude perform emergency checklist

62
Q

Least drag OEI

A

2° bank towards operative engine + rudder

Slip indicator 1/2 displacement towards operative engine

63
Q

PPAA in flight

A

ENGINE FAILURE
autopilot off

POWER
1) max power set

PERFORMANCE

1) gear up
2) flaps up
3) minimum speed 85kt
4) target speed 100kt

ANALYSIS
1) X engine failed

ACTION

    • troubleshooting if time permits –
      1) X power Lever idle
      2) X engine master off
      3) X Alternator off
      4) X fuel selector off
64
Q

PPAA Engine Problem in flight

A

ENGINE PROBLEM
autopilot off

POWER
1) (other engine) power lever max

PERFORMANCE

1) gear up
2) flaps up
3) minimum speed 85kt
4) target speed 100kt

ANALYSIS
– call out the problem –
DECISION: shut down X engine

ACTION

1) X power Lever idle
2) X engine master off
3) X Alternator off
4) X fuel selector off

65
Q

PPAA Approach

A

after starting final approach (leaving intermediate approach altitude or circuit altitude

ENGINE FAILURE

1) autopilot off
2) power as required
3) flaps APP
4) Va App OEI 85kt
5) gear up – if necessary –
6) X engine failed
7) X power lever idle
8) X engine master off

66
Q

OEI go around

A

avoid a go-around by all means!

1) Go-around
2) Power (check slip indication)
3) (if not already set) Flaps APP
4) Gear up (if terrain clearance assured, even before pos. ROC)
5) Flaps UP
6) – Rotate smoothly to 5° ANU –
7) FD off

67
Q

Threshold height

A

Between 50ft and 35ft on instrument runways

68
Q

HASELL Check

A 
Height
Airframe
Security
Engine
Location
Lookout
69
Q

Steep Turns

A

45° bank, 115kt

60% load; speed 115 KIAS, 1° ANU. During turn increase power 5-10%

Tolerance: ± 100 ft, ± 5 KIAS

70
Q

Clean stall

A

Level flight, wings level, clean, power to idle

STALL, reduce AoA
Simultaneously set full power smoothly
Level the wings
Start pitch-up to approx. 8° ANU earliest at VYSE 85 KIAS
When a steady climb is established announce “Go around” and follow standard go-around procedure

70
Q

Clean stall

A

Level flight, wings level, clean, power to idle

STALL, reduce AoA
Simultaneously set full power smoothly
Level the wings
Start pitch-up to approx. 8° ANU earliest at VYSE 85 KIAS
When a steady climb is established announce “Go around” and follow standard go-around procedure

71
Q

Landing Stall

A

Slight descent, wings level, landing configuration, at an imaginary RWY altitude power idle and flare

STALL, reduce AoA
Simultaneously smoothly set full power
Level the wings
Start pitch-up to approx. 3º-5º ANU earliest at 75 KIAS (1.2 VS0)
When a steady climb is established announce “Go around” and follow standard go-around procedure
Observe maximum flap / landing gear retraction speeds

72
Q

Go Around

A

1) Go-around
2) Power
3) Flaps APP (expeditiously, but min. 76 KIAS)
4) Gear up (after positive ROC checked)
5) Flaps UP (at min. 82 KIAS

73
Q

ADDNAR planning

A

Planned flight time < 6h
Additional fuel: 15min holding at 15000ft overhead dest = 2USG (DA42)

Weather req (Eta ± 1h)
Ceiling >= 2000ft or circling height + 500ft
Visibility >= 5km
2 separate RWYs with desperate approach procedures
Min 1 non GNSS approach

74
Q

Alternate approach limits

A

CAT 1 - NPA
NPA - NPA + 200ft, Vis + 1000m
Circling - circling

75
Q

Route MORA

A

10NM to both sides from the centerline and beyond radio fix

Obstacle clearance 1000ft to 5000ft, 2000ft above

76
Q

Wake turbulence separation departure full RWY

A

Same RWY or parallel < 760m (2500ft)
Medium / Light 2min
Heavy / Light 2min
Super / Light 3min

77
Q

Wake turbulence Separation Departure intermediate part of RWY

A

Same RWY or parallel < 760m (2500ft)

Medium / Light 3min
Heavy / Light 3min
Ssuper / Light 4min

78
Q

Wake turbulence landing seperation

A

Medium / Light 5NM
Heavy / Light 6NM
Super / Light 8NM

79
Q

Mass Parameters / Categories

A 
MTOM
Light <= 7000kg
Medium > 7000kg <= 136000kg
Heavy > 136000kg
Super A380
80
Q

Stabilized

A

IMC 500ft AAE

VMC 300ft AAE

81
Q

MISAP climb gradient on charts

A

2.5% or as published

82
Q

Anti Ice System

A

30l fluid, min 22l

Normal mode
2 pumps, 30s, 90s pause, ~2.5h

High mode
1 pump continously, ~1h

Max button
2 pumps 2min, ~30min

Alternate mode
RH bus, pump #2, only high mode

Windshield spray 5sec

LAT DA42 (1 decks)

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