DA42 NG General

Question 1

What is the DA42 NG wingspan?

Answer 1

13.42m

Question 2

What is the length of the DA42 NG?

Answer 2

8.56m

Question 3

What is the height of the DA42 NG?

Answer 3

2.49m

Question 4

What engines does the DA42 NG use?

Answer 4

Austro E4-C

Question 5

What is the max continous RPM and load?

Answer 5

2300rpm and 92% load

Question 6

What are the min and max oil quantities?

Answer 6

5-7 litres

Question 7

What is the minimum altitude for intentional engine shutdown?

Answer 7

3000ft AGL

Question 8

List the manoeuvres that the DA42 NG is approved for

Answer 8

Stalling (not dynamic stalling), lazy eights, chandelles and steep turns (no more than 60 degrees)

Question 9

What manoevres are expressly not permitted in the DA42 NG?

Answer 9

Bank angles of more than 60 degrees, stalling with OEI or asymmetric power and intentional negative g manoevres

Question 10

What are the max load factors?

Answer 10

+3.8 to -1.52 with flaps retracted

+2.0 to 0.0 with APP or LDG flaps

Question 11

What is the max operating altitude?

Answer 11

18000ft pressure altitude

Question 12

Can the DA42 NG be flown into known or forecast thunderstorms?

Answer 12

No

Question 13

What is the total fuel capacity?

Answer 13

52 USG

Question 14

What is the total usable fuel capacity?

Answer 14

50 USG

Question 15

What is the max fuel imbalance?

Answer 15

5 USG

Question 16

What fuel does the DA42 NG use?

Answer 16

Jet - A1

Question 17

What are the min and max autopilot airspeed?

Answer 17

90-180 KIAS

Question 18

When must the autopilot be disengaged?

Answer 18

Below 200ft AGL on app or departure
Below 800ft AGL on all othe phases of flight
During single engine operation

Question 19

What is the max engine restart speed?

Answer 19

100KIAS or the airspeed for a stationary propeller

Question 20

What type of construction is the DA42 NG?

Answer 20

A composite, semi monocoque structure made of carbon fibre reinforced plastic and glass fibre reinforced plastic

Question 21

What type of cooling is used in the DA42 NG engines?

Answer 21

Liquid

Question 22

What type of aspiration does the austro engine have?

Answer 22

A turbocharger

Question 23

What is the max power of the DA42 NG?

Answer 23

166HP

Question 24

Describe the propeller of the DA42 NG?

Answer 24

A 3 bladed constant speed propeller made of wood composite with fibre reinforced plastic coating

Question 25

What is the max time that max power can be set?

Answer 25

5 mins

Question 26

What direction does each propeller rotate?

Answer 26

Clockwise

Question 27

Which engine is the critical engine?

Answer 27

Left engine

Question 28

Describe the CSU

Answer 28

Single acting, controlled by ECU and driven by oil pressure

Question 29

When will the propellers feather?

Answer 29

When the engine master is off and prop speed above 1300rpm

Question 30

What type of brakes are used?

Answer 30

Hydraulic disc brakes

Question 31

When is the landing gear warning system activated?

Answer 31

When airbourne and either power lever below 25%

Question 32

How is the landing gear operated?

Answer 32

Via a electrically powered hydraulic pump

Question 33

What is the minimum flight mass?

Answer 33

1450kg

Question 34

What is the maximum takeoff mass?

Answer 34

Without MAM 42-678 = 1900kg | With MAM 42-678 = 1999kg

Question 35

What is the maximum zero fuel mass?

Answer 35

Without MAM 42-659 = 1765kg | With MAM 42-659 = 1835kg

Question 36

What is the maximum landing mass?

Answer 36

Without MAM 42-659 = 1805kg | With MAM 42-659 = 1999kg

Question 37

What is the max load in nose baggage area?

Answer 37

30kg

Question 38

What is the max load in the cabin baggage area?

Answer 38

45kg

Question 39

What is the max load in the cabin baggage extension area?

Answer 39

18kg