GLEX AAL OM-B
Things out of the OM-B NOT for operational use!
Things out of the OM-B NOT for operational use!
Fichier Détails
| Cartes-fiches | 74 |
|---|---|
| Langue | Deutsch |
| Catégorie | Technique |
| Niveau | Autres |
| Crée / Actualisé | 09.06.2017 / 12.06.2017 |
| Lien de web |
https://card2brain.ch/box/20170609_glex_aal_omb
|
| Intégrer |
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max speed Flaps 6° speed?
210kt
max speed Flaps 16°?
210kt
max speed Flaps 30°?
185kt
max altitude to extend flaps or slats?
18'000ft
max gear retraction speed?
200kt
max gear extention speed?
200kt
max gear extended speed?
250kt/0.7M
max altitude to operate with gear extended?
20'000ft
tire limit ground speed?
183kt
turbulence penetration speed?
300kt/0.8M
Vmcg (Flaps 6° and 16°)?
80kt
Vmca (Flaps 6° and 16°)?
86kt
cowl anti-ice, GND ops: definition of icing conditions?
OAT 10°C and below, visible moisture
wing anti-ice, GND ops: definition of icing conditions?
OAT below 5°C
wing anti-ice, flight ops: definition of icing conditions?
TAT 10° of below (except SAT is below -40°C)
cowl anti-ice, flight ops: definition of icing conditions?
TAT 10°C or below (except SAT is below -40°C)
Min N2, when in icing condition?
76% N2
minimum ambient temperature for T/O?
-40°C
descision height for CAT II operation?
100ft
green CAT II below which altitude?
800ft
maximum head- and crosswind in CAT II operation?
15kt
no static ground operation in which N1 range?
between 66-80% N1
minimum oil temperature for starting?
- 40°C
minimum oil temperature before accelerating above idle?
+ 20°C
maximum permissible oil temperature?
+ 160°C
maximum oil consumption?
0.2 liter/h
oil replenishment ist prohibited below which OAT?
below - 12°C
max tailwind component for engine start?
20kt
T/O crosswind component exeeds 20kt, what has to be respected at thrust setting?
do not exceed 66% N1 below 30kt (no limits within 10° headwind)
when must the starter not be used concerning RPM of N2?
if above 42% N2
descriibe the three consecutive engine starts
- three consecutive ENG start cycles
- of three minutes each
- with 15s cooling between each cycles
thereafter allow a 15 minutes cooling period
what is the most common max fuel imbalance for all weigths on ground and in the air?
1'100lbs (600lbs only if more than 20'250lbs on GND and for T/O and LDG )
lowest fueltemperature for T/O?
5°C
max ENG ITT for continous operation?
860°C
