performance

requirements for CAT II / III

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?

2

cockpit oxygen for 3 and 2 crew members

for 3 - min. 1150psi. for 2 - min. 842psi

for how long is the oxygen provided for crew?

from FL410 to FL100 for 22min. continuous: cruise at FL100 for 98min

passengers oxygen time

14 min and 12 min for emb 195ar

min. turn for EMB170 and EMB175

emb170 - 11m; emb175 - 12m

min. turn for EMB190 and EMB195

emb190 - 14m; emb195 - 15m

start limitations for APU

1st/2nd attempt - 60s ON 60s OFF. 3rd attempt - 60s ON 5min OFF

how long on max. thrust

5min AEO. 10min OEI

engine indications: red tick, green tick, hollow sector, cyan tick

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

4.5

engine starting duty cycle

1 and 2 - 90/120 - 10s cool-down. 3 and 5 - 90/120 - 5min

engine dry motoring duty cycle

1 - 90s - 5min cool-down. 1 to 5 - 30s - 5mim cool-down. after after 15 min cool-down period

fire handles close...

fuel, hyd, bleed air

what is the maximum pitch for turn off fasten belts sign?

max. 4,57 degrees (check in IRS status)

normal mode - functions:

mach trim, auto-thrust compensation, AoA limiting, yaw damper and turn coordinator, rudder movements limiting

max. bank angle for 2 engines

25° at V2+10.

max. bank angle for 1 engine

15° at V2 and 25° at V2+10.

Lateral modes:

ROLL, HDG, LNAV, LOC, BC, TRACK

Vertical modes:

ALT, ASEL, FLCH, FPA, GS, GA

Autothrottle annunciations:

TO, GA, SPDT, SPDE, OVSP

how to define point as flyover waypoint

NAV - PATTERNS - FLYOVER - select waypoint

What is the difference between standard and simple-spacial procedure?

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

15° at or below 400ft AGL. 25° above 400ft AGL

performance limit codes: A B C D F M O P S T V

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

TDR 65,2 (planned takeoff weight) WAW R29

minima for CAT II

DH 100ft. RVR 300m

minima for CAT III

dh 50ft RVR 200m

emergency descent profile for 12 min OXYGEN

descent to FL180. within 12 min descent to FL140. within next 30min descent to FL100

emergency descent profile for 14 min OXYGEN

descent to FL220. within 14 min descent to FL140. within next 30min to FL100

method 1 and method 2

method 1 - 1000ft clearance, within 5NM of the route. Method 2 - escaping routes 2000ft clearance. also 5nm.

three types of escape routes:

direct diversion, simple and predefined escape routes

GCD -

ground circle distance

RF -

remaining fuel

ELDF -

estimated landing fuel

EWAI -

adjustment for engine and wing anti-ice on

cost index = 0, cost intex = 999

=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

- datalink - performance - econ speed

how to check optimum speed for holding

- datalink - performance - econ speed

why there is no econ speeds below fL100?

climb speed is assumed to be 250 kt

PTU - what is that?

hydraulic pump in system 2 driven by hydraulic motor installed in system 1

Is automatic operation possible after the failure of one ice detector?

Yes

ADSP/TAT - when are they heated?

when engine is running or the airplane is airborne or manually on the ground

Emer/100%/norm. What is the mixture on norm?

Emer/100%/norm. depends on cabin altitude W

How long is the APU gen available after rotating APU selector knob to OFF?

1 minute

Igniters A cannot be deferred. Why?

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?

it's not possible to shut down the engine with thrust levers above 5° above IDLE

What does "starter cutout speed" mean?

when is reached the SCV (starter control valve) is closed by FADEC

When does the ATTCS activate?

difference between both N1 15%, oei on takeoff or go-around, windshear

minima for non precision approach

MDH 250ft. RVR not less than 750m

N1 target

+0,5% and -0,1%

bleed air for takeoff - altitude

up to 500ft AGL

max OIL quantity and OPS time

emb190- 14,6qt / 24h. emb170- 10,5 / 36h

minimum oil quantity

emb190- 10qt. emb170- 8qt.

max. oil consumption [qt/h]

emb190- 0,4. emb170- 0,2.

Resolution advisory RA and Traffic advisory TA - times:

RA - 20s to 30s. TA - 35s to 45s

TCAS: Proximate traffic

within 6,5nm and 1200ft above or below

from which systems the EGPWS receives inputs?

ADS, FMS, GPS, IRS, radio altimeter and slat/flap control system

EGPWS database consists of...

all hard surfaces runways greater than 3500ft in length

7 modes of GPWS

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

"sink rate sink rate" --- "whoop whoop pull up pull up"

2 mode of GPWS - Excessive Terrain closure rate - Aural alert and warning

"terrain terrain" --- "whoop whoop pull up pull up"

3 mode of GPWS - Descent after take-off - Aural alert and warning

"don't sink don't sink" ---

4 mode of GPWS - Unsafe terrain clearance - Aural alert and warning

4 "too low - gear" - "too low - flap" "too low - terrain"

5 mode of GPWS - Descent below glideslope - Aural alert and warning

"glideslope" --- "glideslope"

6 a b mode of GPWS - Advisory callout - Aural alert and warning

6a - "minimums" "one thousand" 6b - "bank angle"

7 mode of GPWS - Windshear protection - Aural alert and warning

"windshear, windshear, windshear"

pressurization dump button

depressurize the cabin at 2000ft/min up to 12400ft

driftdown actions by PF:

disengage autothrottle, thrust lever to TO/GA position, set altitude, set green dot speed, FLCH - when speed reaches green dot.

driftdown actions by PM:

verifies thrust rate to continuous, inform ATC, turn fasten belts to ON

minimum speed target for OEI

Vshaker + 3kt

max speed below FL100 in uncontrolled airspace

minimum clean speed

how to disable or unable AUTOLAND in FMS?

menu - misc - opr config - autoland on/off

altitude loss during go-around

49ft

MLW - ERJ 170-100

32800kg

MLW - ERJ 170-200

34000kg

MLW - ERJ 190-100 AR

44000kg

MLW - ERJ 190-100 STD

43000kg

MLW - ERJ 190-200 LR

45000kg

MLW - ERJ 190-200 AR

45800kg

eng anti-ice - pressure:

HP - emb170. LP - emb190

in which aircraft is 12 min oxygen system?

in emb 190-200 AR

which aircraft don’t have autoland?

LME, LMF and LNO, LNP

after landing sequence in emb170 - pitch:

4 UP