performance

 0    84 フィッシュ    jakubglowala8
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質問 English 答え English
requirements for CAT II / III
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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?
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2
cockpit oxygen for 3 and 2 crew members
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for 3 - min. 1150psi. for 2 - min. 842psi
for how long is the oxygen provided for crew?
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from FL410 to FL100 for 22min. continuous: cruise at FL100 for 98min
passengers oxygen time
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14 min and 12 min for emb 195ar
min. turn for EMB170 and EMB175
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emb170 - 11m; emb175 - 12m
min. turn for EMB190 and EMB195
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emb190 - 14m; emb195 - 15m
start limitations for APU
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1st/2nd attempt - 60s ON 60s OFF. 3rd attempt - 60s ON 5min OFF
how long on max. thrust
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5min AEO. 10min OEI
engine indications: red tick, green tick, hollow sector, cyan tick
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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)
caution range vibration
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4.5
engine starting duty cycle
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1 and 2 - 90/120 - 10s cool-down. 3 and 5 - 90/120 - 5min
engine dry motoring duty cycle
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1 - 90s - 5min cool-down. 1 to 5 - 30s - 5mim cool-down. after after 15 min cool-down period
fire handles close...
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fuel, hyd, bleed air
what is the maximum pitch for turn off fasten belts sign?
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max. 4,57 degrees (check in IRS status)
normal mode - functions:
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mach trim, auto-thrust compensation, AoA limiting, yaw damper and turn coordinator, rudder movements limiting
max. bank angle for 2 engines
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25° at V2+10.
max. bank angle for 1 engine
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15° at V2 and 25° at V2+10.
Lateral modes:
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ROLL, HDG, LNAV, LOC, BC, TRACK
Vertical modes:
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ALT, ASEL, FLCH, FPA, GS, GA
Autothrottle annunciations:
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TO, GA, SPDT, SPDE, OVSP
how to define point as flyover waypoint
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NAV - PATTERNS - FLYOVER - select waypoint
What is the difference between standard and simple-spacial procedure?
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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
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15° at or below 400ft AGL. 25° above 400ft AGL
performance limit codes: A B C D F M O P S T V
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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
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TDR 65,2 (planned takeoff weight) WAW R29
minima for CAT II
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DH 100ft. RVR 300m
minima for CAT III
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dh 50ft RVR 200m
emergency descent profile for 12 min OXYGEN
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descent to FL180. within 12 min descent to FL140. within next 30min descent to FL100
emergency descent profile for 14 min OXYGEN
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descent to FL220. within 14 min descent to FL140. within next 30min to FL100
method 1 and method 2
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method 1 - 1000ft clearance, within 5NM of the route. Method 2 - escaping routes 2000ft clearance. also 5nm.
three types of escape routes:
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direct diversion, simple and predefined escape routes
GCD -
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ground circle distance
RF -
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remaining fuel
ELDF -
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estimated landing fuel
EWAI -
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adjustment for engine and wing anti-ice on
cost index = 0, cost intex = 999
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=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
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- datalink - performance - econ speed
how to check optimum speed for holding
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- datalink - performance - econ speed
why there is no econ speeds below fL100?
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climb speed is assumed to be 250 kt
PTU - what is that?
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hydraulic pump in system 2 driven by hydraulic motor installed in system 1
Is automatic operation possible after the failure of one ice detector?
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Yes
ADSP/TAT - when are they heated?
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when engine is running or the airplane is airborne or manually on the ground
Emer/100%/norm. What is the mixture on norm?
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Emer/100%/norm. depends on cabin altitude W
How long is the APU gen available after rotating APU selector knob to OFF?
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1 minute
Igniters A cannot be deferred. Why?
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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?
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it's not possible to shut down the engine with thrust levers above 5° above IDLE
What does "starter cutout speed" mean?
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when is reached the SCV (starter control valve) is closed by FADEC
When does the ATTCS activate?
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difference between both N1 15%, oei on takeoff or go-around, windshear
minima for non precision approach
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MDH 250ft. RVR not less than 750m
N1 target
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+0,5% and -0,1%
bleed air for takeoff - altitude
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up to 500ft AGL
max OIL quantity and OPS time
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emb190- 14,6qt / 24h. emb170- 10,5 / 36h
minimum oil quantity
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emb190- 10qt. emb170- 8qt.
max. oil consumption [qt/h]
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emb190- 0,4. emb170- 0,2.
Resolution advisory RA and Traffic advisory TA - times:
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RA - 20s to 30s. TA - 35s to 45s
TCAS: Proximate traffic
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within 6,5nm and 1200ft above or below
from which systems the EGPWS receives inputs?
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ADS, FMS, GPS, IRS, radio altimeter and slat/flap control system
EGPWS database consists of...
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all hard surfaces runways greater than 3500ft in length
7 modes of GPWS
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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
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"sink rate sink rate" --- "whoop whoop pull up pull up"
2 mode of GPWS - Excessive Terrain closure rate - Aural alert and warning
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"terrain terrain" --- "whoop whoop pull up pull up"
3 mode of GPWS - Descent after take-off - Aural alert and warning
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"don't sink don't sink" ---
4 mode of GPWS - Unsafe terrain clearance - Aural alert and warning
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4 "too low - gear" - "too low - flap" "too low - terrain"
5 mode of GPWS - Descent below glideslope - Aural alert and warning
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"glideslope" --- "glideslope"
6 a b mode of GPWS - Advisory callout - Aural alert and warning
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6a - "minimums" "one thousand" 6b - "bank angle"
7 mode of GPWS - Windshear protection - Aural alert and warning
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"windshear, windshear, windshear"
pressurization dump button
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depressurize the cabin at 2000ft/min up to 12400ft
driftdown actions by PF:
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disengage autothrottle, thrust lever to TO/GA position, set altitude, set green dot speed, FLCH - when speed reaches green dot.
driftdown actions by PM:
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verifies thrust rate to continuous, inform ATC, turn fasten belts to ON
minimum speed target for OEI
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Vshaker + 3kt
max speed below FL100 in uncontrolled airspace
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minimum clean speed
how to disable or unable AUTOLAND in FMS?
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menu - misc - opr config - autoland on/off
altitude loss during go-around
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49ft
MLW - ERJ 170-100
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32800kg
MLW - ERJ 170-200
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34000kg
MLW - ERJ 190-100 AR
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44000kg
MLW - ERJ 190-100 STD
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43000kg
MLW - ERJ 190-200 LR
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45000kg
MLW - ERJ 190-200 AR
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45800kg
eng anti-ice - pressure:
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HP - emb170. LP - emb190
in which aircraft is 12 min oxygen system?
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in emb 190-200 AR
which aircraft don’t have autoland?
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LME, LMF and LNO, LNP
after landing sequence in emb170 - pitch:
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4 UP

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