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Aircraft > DA40 > Flashcards

DA40 Flashcards

1
Q

WARNING means:

A

non-observation of the corresponding
procedure leads to an immediate or important degradation
in flight safety

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2
Q

CAUTION means:

A

the non-observation of the corresponding
procedure leads to a minor or to a more or less long term
degradation in flight safety

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3
Q

NOTE means

A

draws the attention to any special item not directly related to
safety but which is important or unusual.

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4
Q

Span

A

11.95

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5
Q

Length

A

8.01 m

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6
Q

Height

A

1.97m

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7
Q

Wing Area

A

13.54 m²

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8
Q

Aspect ratio

A

10.53

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9
Q

Dihedral

A

5 °

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10
Q

Leading edge sweep

A

1°

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11
Q

Tail: Angle of incidence

A

-3.0° relative to longitudinal axis of airplane

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12
Q

Landing Gear

Track

A

2.97 m

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13
Q

vA means

A

Maneuvering Speed. Full or abrupt control surface movement is not permissible
above this speed

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14
Q

vNE

A

Never Exceed Speed in smooth air. This speed must not be exceeded in any
operation.

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15
Q

vNO

A

Maximum Structural Cruising Speed. This speed may be exceeded only in
smooth air, and then only with caution.

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16
Q

vA speeds

A

108 KIAS
(above 980 kg / 2161 lb
up to 1150 kg / 2535 lb)

94 KIAS
(780 kg / 1720 lb
up to 980 kg / 2161 lb)

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17
Q

vFE speeds

A

LDG: 91 KIAS

T/O: 108 KIAS

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18
Q

vNO

A

129

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19
Q

vNE

A

178

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20
Q

White arc

A

49 KIAS - 91 KIAS

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21
Q

Green arc

A

52 KIAS - 129 KIAS

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22
Q

Yellow arc

A

129 KIAS - 178 KIAS

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23
Q

Red line

A

178 KIAS

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24
Q

Engine manufacturer

A

Textron Lycoming

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25
Q

Engine designation

A

IO-360 M1-A

26
Q

Max. take-off RPM

A

2700 RPM

27
Q

Max. continuous RPM

A

2400 RPM

28
Q

Manifold pressure limitations

Maximum

A

FULL throttle

29
Q

Oil pressure

Minimum (IDLE)

A

25 PSI / 1.72 bar

30
Q

Oil Pressure

Maximum

A

98 PSI / 6.76 bar

31
Q

Oil quantity
Minimum
Maximum

A

4 qts

8 qts

32
Q

Oil temperature

Maximum :

A

245 °F (118 °C)

33
Q

Cylinder head temperature

Maximum

A

500 °F (260 °C)

34
Q

Oil specification

A

Airplane engine oil should be SAEJ1899 (MIL-L-22851) Standard
(ashless dispersant type). First 50 hours of operation of a new or newly
overhauled engine, or after replacement of a cylinder, airplane engine oil should be SAEJ1966 (MIL-L-6082) Standard (straight mineral type).

35
Q

Maximum take-off mass (Normal Category)

A

1200kg

36
Q

Maximum take-off mass (Utility Category)

A

980kg

37
Q

Maximum landing mass

A

1150kg

38
Q

Max. load in standard baggage compartment

A

30 kg

39
Q

Max. load in extended baggage compartment (OÄM 40-163)

Max. load in forward part :

A

45kg

40
Q

Max. load in extended baggage compartment (OÄM 40-163)

Max. load in aft part

A

18kg

41
Q

Max. load in extended baggage compartment (OÄM 40-163)

Max. total load forward + aft

A

45kg

42
Q

Normal category load limits, clean at Va and Vne

A

At Va:
+3.8, -1.52

At Vne:
+3.8, -0.

43
Q

Normal category load limits, flaps extended:

A

+2.0, -0. At both VA and Vne

44
Q

Utility category load limits to VA and Vne, clean:

A

VA:
+4.4, -1.76
Vne:
+4.4, -1.0

45
Q

Utility category load limits with flaps extended

A

Same as normal

+2.0, -0

46
Q

Conditions of utility category use:

A

2 people, both in front seats, can do manoeuvres up to 90° aob

47
Q

The maximum demonstrated operating altitude is

A

16,400 ft (5,000 m)

48
Q

Fuel Grade

A

AVGAS 100LL / AVGAS 100/130LL or

AVGAS 100 / AVGAS 100/130

49
Q

Total fuel

Usable and unusable

A

2 X 25.5 USG tanks total
2 X 0.5 USG unusable
Total 51 total, 50 usable

50
Q

Max permissible difference between fuel tanks

A

8 gallons

51
Q

Twilight zone of tanks

A

Between 16 and 19 gallons

52
Q

Power on battery only time - essential bus on
Main battery ?
Emergency battery ?

A

30 mins main

1.5hrs Emergency

53
Q

Warm Start Oil Temp

A

90 – 120°

54
Q

Hot Start Oil Temp

A

above 120°

55
Q

Normal start temperature

A

Below 90°

56
Q

Magnetos check drops

A

Max 2 sec on L/R Mag

Check – Max. 175 ea, Max diff. 50

57
Q

Run-up

A 
1Area Clear
2 Parking Brake Set
3 Fuel Selector Switch to Fullest Tank / Record
    Set Fuel Scheduler and SARTIME
4 MFD Set to Engine Page
5 Engine Gauges Check
6 Throttle 2000 RPM
7 Propeller Cycle 3 Times (max. 500 RPM Drop)
8 Magnetos Max 2 sec on L/R Mag
    Check – Max. 175 ea, Max diff. 50
9 Alternate Air Check
10 Alternator Check Load
11 Circuit Breakers Checked
12 Throttle Idle 600-900 RPM
13 Throttle 1200 RPM
14 MFD Set to MAP page with TAS Display On
58
Q

Pre-Takeoff

A 
1 Trim Set for T/O
2 Mixture Rich
3 Propeller High RPM
4 Flaps T/O
5 Fuel Pump On
6 Magnetos Both
7 Canopy and Rear Door Closed & Locked
8 Flight Controls Free & Correct
9 Performance Brief Complete
59
Q

Line-Up

A

1 HSI / Compass Aligned
2 Take-off clearance Received
3 Lights On as Required
4 Pitot Heat On

60
Q

After Takeoff

A

1 Flaps Up
2 Fuel Pump Off, Check Fuel Pressure
3 Transponder Verify ALT
4 Lights As Required

61
Q

Pre Landing

A 
1 Fuel Selector L / R Tank
    Contents Sufficient
    Pump On
2 Mixture Full Rich
3 Brakes Check Pressure
    Park Brake Off
4 Security Seatbelts Fastened
    Hatches Secure
62
Q

Finals

A

1 Propeller High RPM
2 Flaps LDG
3 Landing Clearance Received / Not Required
4 Airspeed Vref

Aircraft (1 decks)

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