Checkout ?'s

Question 1

What type of engine is in the DA40?

Answer 1

IO-360-M1A

Question 2

What is the maximum takeoff power produced?

Answer 2

2700 RPM

Question 3

What is the specified maximum continuous power?

Answer 3

2400

Question 4

What are the maximum and minimum quantities of oil to be used in the DA40?

Answer 4

Maximum= 8 quartz
Minimum= 4 quartz

Question 5

What type and grade of oil must be used after the first 50 hours of operation?

Answer 5

SAEJ1899 (Ash-less Dispursant)

Question 6

What is the DA40 maximum takeoff weight?

Answer 6

Normal Category= 2535

Utility Category= 2161

Question 7

​What is the wingspan of the DA40?

Answer 7

39’ 2”

Question 8

​Oil pressure normal range?

​Oil pressure maximum?

Oil pressure minimum?

Answer 8

Normal= 55-95psi

Maximum= 98psi

Minimum = 25psi

Question 9

Oil temperature maximum?

Answer 9

245 degrees

Question 10

Oil pressure minimum for run-up

Answer 10

56psi

Question 11

Cylinder Head Temperature (CHT) maximum?

Answer 11

500 degrees F

Question 12

Fuel pressure minimum?

Fuel pressure maximum?

Answer 12

Minimum= 14psi

Maximum= 35psi

Question 13

Voltage minimum?

Voltage normal range?

Voltage maximum?

Answer 13

Minimum= 24 volts

Normal= 25-30 volts

Maximum= 33 volts

Question 14

What is the maximum ramp weight?

Answer 14

2544 lbs

NOTE
In some countries the beginning of a flight is defined by starting the engine. In those countries a maximum ramp mass (9 lbs) above the maximum takeoff mass is approved. At the time of lift-off the maximum permitted takeoff mass (2535 lbs) must not be exceeded.

Question 15

What is the maximum landing weight?

Answer 15

Original MLG strut= 2407 lbs

Modified MLG strut= 2535 lbs

Question 16

What is the maximum allowable weight in the baggage compartment?

Answer 16

Standard baggage compartment= 66 lbs

Baggage tube= 11 lbs