Question  |
Answer |
requirements for CAT II / III start learning
|
|
2 IRS, 2 FD, 2 PFD, 1 RA (2x for CAT III), 1 wiper, 2 ILS, 1 VHF, 1 EGPWS, 2 ADS, 1 AP, Rud + spoil., ((for CAT III - Autoland)
|
|
|
how many MCDU is required for CPDLC? start learning
|
|
|
|
|
cockpit oxygen for 3 and 2 crew members start learning
|
|
for 3 - min. 1150psi. for 2 - min. 842psi
|
|
|
for how long is the oxygen provided for crew? start learning
|
|
from FL410 to FL100 for 22min. continuous: cruise at FL100 for 98min
|
|
|
|
start learning
|
|
14 min and 12 min for emb 195ar
|
|
|
min. turn for EMB170 and EMB175 start learning
|
|
emb170 - 11m; emb175 - 12m
|
|
|
min. turn for EMB190 and EMB195 start learning
|
|
emb190 - 14m; emb195 - 15m
|
|
|
start limitations for APU start learning
|
|
1st/2nd attempt - 60s ON 60s OFF. 3rd attempt - 60s ON 5min OFF
|
|
|
|
start learning
|
|
|
|
|
engine indications: red tick, green tick, hollow sector, cyan tick start learning
|
|
red tick - max. N1. green tick - max. for current mode. sector - actual and requested N1. cyan tick - min. N1. icing conditions, gear down ot flaps extended (<1200ft)
|
|
|
|
start learning
|
|
|
|
|
engine starting duty cycle start learning
|
|
1 and 2 - 90/120 - 10s cool-down. 3 and 5 - 90/120 - 5min
|
|
|
engine dry motoring duty cycle start learning
|
|
1 - 90s - 5min cool-down. 1 to 5 - 30s - 5mim cool-down. after after 15 min cool-down period
|
|
|
|
start learning
|
|
|
|
|
what is the maximum pitch for turn off fasten belts sign? start learning
|
|
max. 4,57 degrees (check in IRS status)
|
|
|
|
start learning
|
|
mach trim, auto-thrust compensation, AoA limiting, yaw damper and turn coordinator, rudder movements limiting
|
|
|
max. bank angle for 2 engines start learning
|
|
|
|
|
max. bank angle for 1 engine start learning
|
|
15° at V2 and 25° at V2+10.
|
|
|
|
start learning
|
|
ROLL, HDG, LNAV, LOC, BC, TRACK
|
|
|
|
start learning
|
|
ALT, ASEL, FLCH, FPA, GS, GA
|
|
|
Autothrottle annunciations: start learning
|
|
|
|
|
how to define point as flyover waypoint start learning
|
|
NAV - PATTERNS - FLYOVER - select waypoint
|
|
|
What is the difference between standard and simple-spacial procedure? start learning
|
|
in simple-spacial turn to a NAVAID or heading is required before reaching 1000’
|
|
|
max bank angle during turn to navaid or heading in simple-spacial procedure start learning
|
|
15° at or below 400ft AGL. 25° above 400ft AGL
|
|
|
performance limit codes: A B C D F M O P S T V start learning
|
|
A - max AFM weight. B - brakes. C - climb. D - dry runway weight. F - field. M - MEL. O - obstacle. P - policy. S - structural. T - tires. V - Vmcg
|
|
|
AeroData ACARS freeText for takeoff start learning
|
|
TDR 65,2 (planned takeoff weight) WAW R29
|
|
|
|
start learning
|
|
|
|
|
|
start learning
|
|
|
|
|
emergency descent profile for 12 min OXYGEN start learning
|
|
descent to FL180. within 12 min descent to FL140. within next 30min descent to FL100
|
|
|
emergency descent profile for 14 min OXYGEN start learning
|
|
descent to FL220. within 14 min descent to FL140. within next 30min to FL100
|
|
|
|
start learning
|
|
method 1 - 1000ft clearance, within 5NM of the route. Method 2 - escaping routes 2000ft clearance. also 5nm.
|
|
|
three types of escape routes: start learning
|
|
direct diversion, simple and predefined escape routes
|
|
|
|
start learning
|
|
|
|
|
|
start learning
|
|
|
|
|
|
start learning
|
|
|
|
|
|
start learning
|
|
adjustment for engine and wing anti-ice on
|
|
|
cost index = 0, cost intex = 999 start learning
|
|
=0 - max range cruise speed (time is not value). =999 - max aircraft speed (fuel is not value)
|
|
|
how to check max flight level for current configuration start learning
|
|
- datalink - performance - econ speed
|
|
|
how to check optimum speed for holding start learning
|
|
- datalink - performance - econ speed
|
|
|
why there is no econ speeds below fL100? start learning
|
|
climb speed is assumed to be 250 kt
|
|
|
|
start learning
|
|
hydraulic pump in system 2 driven by hydraulic motor installed in system 1
|
|
|
Is automatic operation possible after the failure of one ice detector? start learning
|
|
|
|
|
ADSP/TAT - when are they heated? start learning
|
|
when engine is running or the airplane is airborne or manually on the ground
|
|
|
Emer/100%/norm. What is the mixture on norm? start learning
|
|
Emer/100%/norm. depends on cabin altitude W
|
|
|
How long is the APU gen available after rotating APU selector knob to OFF? start learning
|
|
|
|
|
Igniters A cannot be deferred. Why? start learning
|
|
Igniters B are connected to SPDA 2. In case of failure, setting the knob to OVRD at least energizes the igniter A.
|
|
|
"N1 5% above N1 idle" - why such memory item is needed? start learning
|
|
it's not possible to shut down the engine with thrust levers above 5° above IDLE
|
|
|
What does "starter cutout speed" mean? start learning
|
|
when is reached the SCV (starter control valve) is closed by FADEC
|
|
|
When does the ATTCS activate? start learning
|
|
difference between both N1 15%, oei on takeoff or go-around, windshear
|
|
|
minima for non precision approach start learning
|
|
MDH 250ft. RVR not less than 750m
|
|
|
|
start learning
|
|
|
|
|
bleed air for takeoff - altitude start learning
|
|
|
|
|
max OIL quantity and OPS time start learning
|
|
emb190- 14,6qt / 24h. emb170- 10,5 / 36h
|
|
|
|
start learning
|
|
emb190- 10qt. emb170- 8qt.
|
|
|
max. oil consumption [qt/h] start learning
|
|
emb190- 0,4. emb170- 0,2.
|
|
|
Resolution advisory RA and Traffic advisory TA - times: start learning
|
|
RA - 20s to 30s. TA - 35s to 45s
|
|
|
|
start learning
|
|
within 6,5nm and 1200ft above or below
|
|
|
from which systems the EGPWS receives inputs? start learning
|
|
ADS, FMS, GPS, IRS, radio altimeter and slat/flap control system
|
|
|
EGPWS database consists of... start learning
|
|
all hard surfaces runways greater than 3500ft in length
|
|
|
|
start learning
|
|
1. Excessive descent rate 2. Excessive Terrain closure rate 3. Descent after take-off 4. Unsafe terrain clearance 5. Descent below glideslope 6. Advisory callout 7. Windshear protection
|
|
|
1 mode of GPWS - Excessive descent rate - Aural alert and warning start learning
|
|
"sink rate sink rate" --- "whoop whoop pull up pull up"
|
|
|
2 mode of GPWS - Excessive Terrain closure rate - Aural alert and warning start learning
|
|
"terrain terrain" --- "whoop whoop pull up pull up"
|
|
|
3 mode of GPWS - Descent after take-off - Aural alert and warning start learning
|
|
"don't sink don't sink" ---
|
|
|
4 mode of GPWS - Unsafe terrain clearance - Aural alert and warning start learning
|
|
4 "too low - gear" - "too low - flap" "too low - terrain"
|
|
|
5 mode of GPWS - Descent below glideslope - Aural alert and warning start learning
|
|
"glideslope" --- "glideslope"
|
|
|
6 a b mode of GPWS - Advisory callout - Aural alert and warning start learning
|
|
6a - "minimums" "one thousand" 6b - "bank angle"
|
|
|
7 mode of GPWS - Windshear protection - Aural alert and warning start learning
|
|
"windshear, windshear, windshear"
|
|
|
pressurization dump button start learning
|
|
depressurize the cabin at 2000ft/min up to 12400ft
|
|
|
|
start learning
|
|
disengage autothrottle, thrust lever to TO/GA position, set altitude, set green dot speed, FLCH - when speed reaches green dot.
|
|
|
|
start learning
|
|
verifies thrust rate to continuous, inform ATC, turn fasten belts to ON
|
|
|
minimum speed target for OEI start learning
|
|
|
|
|
max speed below FL100 in uncontrolled airspace start learning
|
|
|
|
|
how to disable or unable AUTOLAND in FMS? start learning
|
|
menu - misc - opr config - autoland on/off
|
|
|
altitude loss during go-around start learning
|
|
|
|
|
|
start learning
|
|
|
|
|
|
start learning
|
|
|
|
|
|
start learning
|
|
|
|
|
|
start learning
|
|
|
|
|
|
start learning
|
|
|
|
|
|
start learning
|
|
|
|
|
|
start learning
|
|
|
|
|
in which aircraft is 12 min oxygen system? start learning
|
|
|
|
|
which aircraft don’t have autoland? start learning
|
|
|
|
|
after landing sequence in emb170 - pitch: start learning
|
|
|
|
|
