DA42

Question 1

Span, length, height?

Answer 1

13.42m, 8.59m, 2.49m

Question 2

Dihedral? Leading edge sweep?

Answer 2

5 degrees, 1 degree

Question 3

Landing gear track? wheelbase?

Answer 3

2.894m, 1.735m

Question 4

Engines?

Answer 4

Textron Lycoming (LH) IO-350-M1A, (RH) LIO-350-M1A

Question 5

Va?

Answer 5

> 1542kg, 126 kias
up to 1542kg, 120 kias

Question 6

Vfe?

Answer 6

app, 137 kias
ldg, 111 kias

Question 7

Vle?

Answer 7

194 kias

Question 8

Vlor?

Answer 8

156 kias

Question 9

Vmca?

Answer 9

65 kias

Question 10

Vne?

Answer 10

194 kias

Question 11

Von?

Answer 11

155 kias

Question 12

Vsse?

Answer 12

80 kias

Question 13

Vyse?

Answer 13

90 kias

Question 14

Max cont RPM?

Answer 14

2700

Question 15

Manifold pressure limitations?

Answer 15

Take off - FULL throttle
AEO - 5 minutes
OEI - No limit

Question 16

Max continuous power?

Answer 16

160 HP

Question 17

Prop diameter

Answer 17

72.05”

Question 18

MRampW

Answer 18

1795

Question 19

MTOW

Answer 19

1785

Question 20

MLW

Answer 20

1700

Question 21

MZFW

Answer 21

1650

Question 22

Max load in nose baggage

Answer 22

30

Question 23

Max load in cockpit baggage

Answer 23

45

Question 24

Max load in baggage extension

Answer 24

18

Question 25

Max combined cockpit and extension

Answer 25

45

Question 26

Approved manoeuvres

Answer 26

• All normal flight manoeuvres
• Stalling (except power on stalls with a fuel imbalance)
• Lazy eights, chandelles, steep turns and similar manoeuvres in which a aob not more than 60 degrees is attained

Question 27

G limits?

Answer 27

Positive: 3.8, with flaps (app/ldg) 2.0
Negative: -1.52 (at Va), 0 (at Vne)

Question 28

Max operating alt

Answer 28

18,000ft PA

Question 29

Fuel quantity, max permissible difference

Answer 29

Main tanks: 2x 25.5 usg
Aux tanks: 2x 13.7 usg
(1.0 unusable per main tank 0.5 unusable per aux tank)

5 usg difference