DA42 Specific

Question 1

What is the maximum zero fuel weight?

Answer 1

1250 kg

Question 2

Maximum ramp weight?

Answer 2

1793kg

Question 3

Maximum take off weight?

Answer 3

1700kg

Question 4

Maximum landing weight?

Answer 4

1700kg

Question 5

Max demonstrated cross wind component?

Answer 5

20kts

Question 6

Max tail wind component?

Answer 6

10kts

Question 7

VNE?

Answer 7

194kt

Question 8

VNO?

Answer 8

155kts

Question 9

VSO?

Answer 9

57kts

Question 10

VS1?

Answer 10

64kts

Question 11

VLE?

Answer 11

194kts

Question 12

VLO?

Answer 12

194kts

Question 13

VLR?

Answer 13

156kts

Question 14

Va?

Answer 14

126kts

Question 15

Vy?

Answer 15

79kts

Question 16

Vx?

Answer 16

79kts

Question 17

Vyse?

Vxse?

Answer 17

82kts

Question 18

VMCA?

Answer 18

70kts

Question 19

Vtoss?

Answer 19

75kts

Question 20

What is the minimum altitude to engage/disengage autopilot?

Answer 20

200ft AGL

Question 21

What powers the aircraft compass and attitude system?

Answer 21

AHRS left hand bus bar

Question 22

What powers the standby attitude indicator?

Answer 22

Battery back up (1.5hrs use)

Question 23

How many battery’s are fitted in the aircraft?

Answer 23

1 10 amp/hr 24 volt lead acid battery

1 emergency power pack X 10 3v backup batteries X2 ECU backup

Question 24

What type of engines are on the DA42 twin star?

Answer 24

Thielert diesel TAE 125-o2.

4 cylinders alt air liquid cooled, turbo charged, reduction gear

135hp at 2300rpm (sea level)