Limits DA 40
SAT
SAT
Fichier Détails
| Cartes-fiches | 94 |
|---|---|
| Langue | Deutsch |
| Catégorie | Technique |
| Niveau | École primaire |
| Crée / Actualisé | 28.12.2014 / 14.05.2024 |
| Lien de web |
https://card2brain.ch/box/limits_da_40
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| Intégrer |
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Engine
Austro Engine
MAX RP; take-off + Time
2300 RPM for 5 min
MAX RP; continuous + Load %
2100 RPM
Max. overspeed RPM + time
2500 RPM max. 20 sek.
Fuel temperature Min und Max
Min: -25 Grad max: 60 Grad
Oil specification:
Shell Helix Ultra 5 W30 and Shell Helix Ultra 5 W40
Max. restart altitude: for immediate restart
16'400 ft for immediate restart
Max. restart altitude: for restarts within 2 minutes
10'000 ft
Max Bank DA 40 vom Hersteller zertifizeirt
60 Grad Bank
G-load: + and -
max. 3.8 g at Vo max. -1.52 at Vo
Max Wind:
Crosswind and Tailwind
Crosswind: 25 kt Tailwind: 5 kt
Max. Altitude DA 40 nach Hersteller
16'400 ft
Flight int forecast icing and thunderstorms are
prohibited
T/O and landing (nach Hersteller ) auf ?
T/O and landing (nach Hersteller ) on paved and unpaved surfaces
Fuel in DA 40
1. Jet A
2. Jet A1
3. TS-1
Total fuel quantity and Usable fuel
Total fuel quantity: 2x 15.0 US gal (2x 56.8 Liter)
Usable fuel: 2x 14.0 US gal (2x 53.0 Liter)
Engine Start: when we use externaö power for the first engine start of teh day
OAT is below -10 Grad
Fuel cooler inlet baffle muss man installieren (Maintenace)
Beloe -20 Grad
Door locking during flighT?
must not be key locked during operation of teh airplane
MTOM
1280 kg, 2822 lbs
MLM
Maximum Landing Mass 1280kg; 2822 lbs
Minimum flight mass
940 kg; 2072 lbs
maximum zero fuel mass
1200 kg; 2646 lbs
Max. load in baggage compartment (behind rear seats)
45 kg; 100 lb
Max. load in extended baggage compartment
18 kg
Max. lod in cockpit baggage compartment and extended baggage compartment
45 kg
With ventilation inlet baffle installed: max OAT for Take-off:
With ventilation inlet baffle installed: max OAT for Take-off: 15°C
SPatiail disorientation
Force which are produced by acceleration can deceive the hunan body's sensory system
Flightpath
Direction of movement of the aircraft
Attitude
Angle between longitudinal axis and horizon
Aviodance in Training flights (Below10'000 ft and 250 kts)
Over 5 NM: Recognition => be aware
1-5 NM: Warning => Periodic observation
Below 1 NM: ALARM => Obervation and quick judgment
Ckecks before starting inflight excercises:
HASELL
H: HEIGHT => Height above ground
A: Airframe => Flaps up, Doors/Windows closes, gear up
S: Security => looses item secured + LANDING LIGHTS ON
E: Engine => if necessary fuel pump + check engine instruments
L: Location => a suitable area for and a emergency landing
L: LOOKOUT => oberservation - clear the area
Procedure for ectending/retraction of flaps
1. Ckeck speed below FFE T/O = 110kts
2. Flaps take-off
3. check for teh flaps indicator => Flaps take-off
4. Call out the next target speed => VP T/O
Ablauf Flaps setzten
First Hand Second Hand Eyes:
Flaps 0-T/O Add forward pressure Check ALT/VSI
Flaps T/O -LDG Add forward pressure Check ALT/ VSI
Ablauf Power handling
First Hand Second Hand Eyes:
Throttle Increase Add forward pressure Ckeck ALT/VSI
Throttle Decrease Add back pressure Ckeck ALT/VSI
In Climb ( full power/low Speed) Th epropeller moment is larger: What do you make
rudder input right
In descent (low pressure/high speed) the aerodynamic moment is larger ==> what do you make ?
rudder input left
Taxi speed: wie gibt man am besten speed
1. more energy to start taxi 2. after it roles, reduces speed
When you breaking during taxi, what do you must look for
that during the breaking action the nose wheel would be in neutral position
What happens with the parking break, when teh break is let on for a longer period?
The hydraulic pressure of the break may descries which reduces the effectively of the break
