IR - DA42 Flashcards
DA42
Stalling speeds (max weight)
V(S0) - 62kt
V(S1) - 66kt
DA42
V(X)
90kt
DA42
V(Y)
90kt
DA42
V(YSE)
85kt - BLUE LINE
= V(SSE) minimum control speed for training
DA42
V(MCA)
76kt (per Stapleford)
DA42
V(R)
80kt
DA42
Operating speed range in ice
118 - 156 kt
DA42
V(FE) - approach & landing
Approach - 133kt
Landing - 113kt
DA42
V(LE)
188kt
Extension AND extended
DA42
V(LOR)
152kt
Retraction speed
DA42
V(REF)
84kt (86kt flapless)
DA42
V(NO)
151kt
DA42
V(NE)
188kt
DA42
MTOM
1900kg
DA42
MLM
1805kg
DA42
MZFM
1765kg
DA42
Empty mass
1450kg
DA42
Max baggage
- Nose
- Cockpit
- Rear extension
Nose: 30kg
Cockpit: 45kg
Rear extension: 18kg
DA42
When does landing gear warner go off
Landing gear retracted and:
- Flaps in LDG position; or
- Power < 20%
DA42
Maximum load factor
3.8G
DA42
Max crosswind component
20kt Stapleford
(25kt pilots handbook)
DA42
Fuel types
Jet-A, Jet-A1 and some others
DA42
Total fuel useable (and total)
50 USG useable
[51 USG total]
DA42
Typical fuel flow rate
10 USG/hr
DA42
Max difference between fuel content in L and R tanks
5 USG
DA42
Fuel delivery method
Direct injection from common rail to each of the 4 cylinders.
DA42
Autopilot operation speed limits
90-180 kt
DA42
Autopilot operation height limits
200ft AGL in approach and departure
800ft AGL other phases
DA42
Critical Engine on DA42
Left
DA42
Max starter time
10 seconds
DA42
Engines
- # cylinders
- # stroke
- sump type
4 cylinder
4 stroke
Wet sump
DA42
Feathering rpm limit
Switching off engine master feathers the engine, but only if rpm is above 1300rpm.
Minimum En-route Altitude vs
Minimum Safe Altitude
MEA is min alt between two fixes ensuring terrain clearance and navaid coverage.
MSA is a more general term that allows you to determine an altitude for a phase of the flight to ensure terrain clearance.
DA42
Electrical system
28v DC
DA42
Backup batteries
30 minute backup for the ECU only
12V, 7.2 Ah batteries under each seat
DA42
Main battery voltage
24V, 13.6 Ah
Conditions conducive to windshear
Thunderstorms, Cb
DA42 anti-icing systems
[Labelled de-ice incorrectly!]
Pitot heat
Static heat
Windscreen (fluid)
Wing leading edge (fluid)
Propeller (fluid)
DA42
Landing gear operation
Hydraulic with electric pump