AOM

PPU -

Power Push Unit

Mooring -

kotwiczenie

Fuel Nozzle -

dysza paliwowa

Fuel transfer from RH to LH tank (selector)

LOW 1

Fuel transfer from LH to RH tank (selector)

LOW 2

Tire pressure

MAIN: between 157 and 167 psi. NOSE: 131 and 141 psi

Digital oxygen pressure CYAN on MFD

minimum for 2 crew members

LNAV mode activation

when is armed, will automatucally engage when passing 200ft during climb. Or after pressing NAV button, when the airplane is above 200ft

Bank angle command during localizer capture

to 35°

Autoland limits

decision height 50ft, RVR 200m

Retard mode engagement

at or below 30ft

useage of CPDLC - altitude

above FL200

time for crew to response to CPDLC message

100 seconds

CPDLC connection terminated after landing - when?

2 minutes after the airplane door open or pakring brakes set

Manual IDG disonnection by selecting IDG knob to DISC position for...

for 1 second

Which circuit breakers can flight crew reset?

Electronic in SPDAs and Thermal in Cockpit

INHIB button - cockpit doors

inhibits the emerg entry for 500s. not pressed will open the door in 30s.

EMB 190 STD, EMB 195 LR, EMB 195 LR (SP-LNO, SP-LNP), EMB 195 AR - passenger seats + attendants

EMB 190 STD - 106+4, EMB 195 LR - 112+4, EMB 195 LR (SP-LNO, SP-LNP) - 118+3, EMB 195 AR - 118+4

EMB 170, EMB 175, EMB 175 LR - passenger seats + attendants

EMB 170 - 76+2, EMB 175 - 88+2, EMB 175 LR - 82+3

CAT III decision height

50 ft

Minimum use height of autopilot without auto land

50 ft

EMB 190 - Max headwind, max tailwind, max crosswind

Max headwind - 37kt, max tailwind - 10kt, max crosswind - 16kt

EMB 170 - Max headwind, max tailwind, max crosswind

Max headwind - 25kt, max tailwind - 10kt, max crosswind - 12kt

CAT II / IIIA approach and landing must be performed with flaps:

flaps 5

AUTOLAND - The maximum and minimum glide slope angles are:

3.25 degrees and 2.5 degrees

The maximum airport elevation for autoland operation is

7340 ft

EMB 190 and EMB 170 - AUTOLAND - Runway slopes

EMB 190 - -1% to +1%. EMB 170 - -0.8% to +0.8%

Wind limitations for autoland

headwind - 25kt. crosswind - 15kt. Tailwind - 10kt

Autoland 1 must be performed with flaps:

flaps 5

Minimum equipemnt for RVSM

2 Air Data Systems, 1 Autopilot with altitude hold mode, 1 Altitude alerter, 1 transponder

Before takeoff the maximum difference among the three altimeters indication must not exceed:

75ft

during cruise when altitude maximum difference between PFD 1 and PFD 2 exceeds

180ft

Airplane allowed for steep approach operations

EMB 190-100

The steep approach to landing may be performed with an approach flight path angle up to

5.5°

The steep approach operations in contaminated runways

from 4.5° to 5.4°

2 limitations for steep approach operations

2 operating engines and only CAT I approaches

Minimum use height of autopilot during steep approach operations

167ft

Maximum airport altitude for steep approach operations

10000ft

Flaps position for steep approach operation

FULL

Max tailwind and crosswind component for steep approach

tailwind - 5kt. crosswind - 25kt

Max. runway slope for steep approach operations

-2% to +2%

When anti-ice AUTO mode is inoperative, the crew must set the selector to ON when:

icing conditions exists, TAT below 10°C with visible moisture

Maximum airspeed for windshield wiper operation

253kt

MTOW for EMB170 STD, EMB175 STD, EMB 175 LR

EMB170 STD - 37t, EMB175 STD - 37,5t, EMB 175 LR - 38,8t

MTOW for EMB190 STD, EMB190 AR, EMB 195 LR, EMB 195 AR

EMB190 STD - 48t, EMB190 AR - 52t, EMB 195 LR - 51t, EMB 195 AR - 52t

MLAW for EMB170 STD, EMB175 STD, EMB 175 LR

EMB170 STD - 33t, EMB175 STD - 34t, EMB 175 LR - 34t

MLAW for EMB190 STD, EMB190 AR, EMB 195 LR, EMB 195 AR

EMB190 STD - 43t, EMB190 AR - 44t, EMB 195 LR - 45t, EMB 195 AR - 46t

Speed to open the direct vision window

160 kt

Vlo and Vle for EMB 170

250kt

Maximum Tire ground speed

195kt

Max turbulent speed

below 10000ft - 250kt. Above 270kt/0.76Mach

Mmo

0.82 Mach

Vmo

320kt

Minimum runway elevation

-1000ft

Maximum runway elevation

EMB 190 - 10000ft. EMB 170 - 8000ft

Max operating altitude

41000ft

Max ISA deviation

ISA + 35°C

temperatures on the ground - range

-54°C and 52°C

temperatures in the air - range

-65°C and -21,5°C

Min temperature for landing for necessary maintenance inspection

-40°C

Max takeoff and landing tailwind component

10kt

Maximum demonstrated crosswind component for landing

28kt

Due to engine compressor stall possibility, static takeoff is not recommended with crosswind component greater than

30kt for EMB 190. 25kt for EMB170

max wind for ground-handling activities

40kt

Max wind for passenger door opening

65kt

Max wind for cargo door opening and closing

40kt and 65kt

Max crosswind for dry and wet runway

Dry - 38kt. wet - 31kt

Max crosswind for runway with frost

31kt

Max crosswind for compacted snow/winter (condition 4)

20kt

Max crosswind for runway with standing water/slush/wet or dry snow

18kt

Max crosswind for winter (condition 3)

15kt

Max crosswind for wet runway and slippery

15kt

Max crosswind for runway with ice

12kt

Max positive and negative load factor

Positive - 2,5g (flaps up) and 2,0g (flaps). Negative - 1,0g (flaps up) and 0g (flaps)

max flaps position for towbarless towing

position 2

Runway slope limits

-2% to 2%

Max water depth on the runway

EMB190 - 25,4mm. EMB170 - 19mm.

Unusable fuel

EMB190 - 92kg. EMB 170 - 68kg

Usable fuel

EMB190 - 13100kg. EMB 170 - 9428kg

Max. fuel capacity

EMB190 - 13192kg. EMB 170 - 9496kg

Lowest temperature of Jet A1

-44°C

APU - max. altitude to start

30.000ft

Time of APU to operate in amber range of temperature

no limit

APU - max. operating altitude

33.000ft

CF34-10E5 - N2 minimum limit

59,3

CF34-10E5 - max ITT temp. on the ground and in flight

on the ground - 740°C and in flight - 875°C

CF34-10E5 - minimum oil pressure

25 psi

CF34-8E5 - Max N1 and Min, Max N2

N1 - max. 99,5%. N2 - min. 58,5%, max. 99,4%

CF34-8E5 - max. ITT temp. for start

815°C

CF34-8E5 - limits of oil pressure

min. 25psi and max. 95psi

TAS, TAT and SAT information are only valid above what speed?

60kt

Maximum latitude of stationary alignment of IRS

78° N and S

Maximum differential pressure and overpressure

8,4psi and 8,8psi

Maximum differential negative pressure

-0,5psi

Maximum differential pressure for take-off and landing

0,2 psi

Maximum altitude for flaps extended

20,000ft

Minimum use height of autopilot

cruise or descent - 1000ft. Approach - 50ft

Difference between the charts and the FMS information

up to 3°

MEMORY ITEMS - cargo forward (aft) smoke

Associated cargo fire extinguising button - PUSH

THR Hold - when is it operating?

above 60kt and to 400ft

MEMORY ITEMS - smoke evacuation

Crew oxygen masks - DON, 100%; Crew communication - establish; pressurization dump button - PUSH IN

MEMORY ITEMS - Smoke, fire or fumes

crew oxygen masks - DON, 100%; crew communication - Establish

MEMORY ITEMS - Dual engine failure

Airspeed - 265kt (250kt - emb170) MIN; RAT manual deploy lever - PULL

MEMORY ITEMS - engine abnormal start

Affected engine: START/STOP selector - STOP

MEMORY ITEMS - engine fire, severe damage or separation

autothrottle - disengage; N1 (operating engine) - at least 5% above N1 idle; affected engine: thrust lever - IDLE; start/stop selector - STOP; fire extinguising handle - PULL

MEMORY ITEMS - Engine fire (on ground)

affected engine: thrust lever - IDLE; start/stop selector - STOP; fire extinguising handle - PULL

MEMORY ITEMS - gear lever can not be moved up

If climb performance is required to clear obstacles: DN LOCK REL button - PRESS AND HOLD; landing gear lever - UP; DN LOCK REL button - RELEASE

MEMORY ITEMS - Jammed control column (pitch)

Elevator Disconnect Handle - PULL

MEMORY ITEMS - Jammed control wheel (roll)

Aileron Disc Handle - PULL

MEMORY ITEMS - pitch trim runaway

A/P Disc button - PRESS AND HOLD; Pitch trim systems 1 and 2 cutout button - OFF (push in)

MEMORY ITEMS - rejected takeoff

thrust levers - IDLE; reverse thrust - as required; brake pedals (if autobrake is not armed) - MAX APPLY; EMERG/PARKING brake - as required; (if required) EMERG evacuation proxedure - Accomplish

MEMORY ITEMS - roll (yaw) trim runaway

a/p disc button - PRESS AND HOLD

MEMORY ITEMS - Steering runaway

Steer Disc Switch - PRESS; use differential braking and rudder to steer the airplane

MEMORY ITEMS - Windshear prevention/recovery

thrust levers - MAX; Go Around button - PRESS

MEMORY ITEMS - battery 1 (2) overtemperature

Associated battery - OFF

MEMORY ITEMS - APU fire

APU Emergency stop button - PUSH IN

minimum pressure to dispatch in crew oxygen cylinder

green - 1150psi. amber - 842psi

Where is the ELT istalled?

impact switch in the rear rack and antenna on the top rear

The Embraer FBW system is composed of:

9 x ACEs (Actuator Control Electronics) and 4x FCMs (Flight Control Modules)

Nine ACEs consist of:

3x Primary, 2x Slat/Flap, 1x horizontal stabilizer, 3x spoiler

What controls P-ACE?

rudder and the elevator surfaces

What controls SF-ACE?

slat and flap surface

What controls HS-ACE?

horizontal stabilizer surface

How long does it take to perform Electrical PBIT and Hydraulic PBIT?

Electrical - 3 minutes. Hydraulic - 1 minute

Hydraulic fluid temperature indications

temp - 100°C - HYD HI TEMP. temp - 125°C - shutoff valve islotes the EDP. temp - 145°C - HYD OVERHEAT

After what conditions the ice detectors inhibits the MCDU setting of anti-ice

above 1700ft or 2 min after liftoff

The wing anti-ice system test during flight

10 min after takeoff or at 10000ft AGL (whichever occurs first). It takes 60 seconds.

How many cabinets are in the MAUs?

MAU 1 has 20 slots. MAU 2 and MAU 3 - each has 16 slots

What is the Vfs speed?

Takeoff final segment speed

Margin of green dot

1,3g over stock shaker speed or 40° of bank angle for wings leveled

miscompare annunciators for pitch and roll

pitch > 5° roll > 6°

miscompare annunciator for speed

IAS > 5kt

miscompare annunciator for altitude

ALT > 200ft

miscompare annunciator for heading

HDG > 6°

When will the autobrake start acting?

2 seconds after WOW detects on the ground

FADEC will not allow fuel flow if ITT is above...

120°C

When will ATTCS automatically command RSV?

diference between both N1 is greater than 15% or one engine failure during takeoff/go-around or windshear detection

When approach idle?

in flight, altitude less than 15000ft and flaps 1 or greater or landing gear

when final approach idle?

altitude lower than 1200ft AGL, landing gear and landing flaps

altitude of windshear detection activation

between 10ft and 1500ft

Resolution advisory and traffic advisory

20s to 30s and 35s to 45s

Proximate traffic TCAS

within 6,5nm and 1200ft above or below

net/gross climb gradient

Net - demonstrated gross gradient reduced by 0,8% during takeoff and 1,1% during enroute

If the message ENG REF ECS DISAG is displayed after the Bleed and Pack buttons are pushed IN, what will you do?

smoothly advance thrust levers to increase bleed pressure to min 13 psig

to which altitude packs off/on during takeoff

up to 500ft AGL

speeds for CAT II / III

Vref = Vac = Vap

How to enable Autoland function on MCDU

MENU -> MISC -> OPR CONFIG -> AUTOLAND ENABLED

Autobrake for CAT II/III

not less than MED

is Autopilot required for LNAV/VNAV approach?

only if non-SBAS

How many static discharges are on the aileron and winglet?

aileron - 3 ; winglet - 6

How many static discharges are on the rudder, elevator, stabilizers on E190 and E170

E190 - 4 on rudder, 3 on elevator, 3 on horziontal stabilizer and 1 on vertical. E170 - 4 on rudder, 4 on elevator and 1 on vertical stabilizer

minimum batteries temperature for start

-20°C

Engine start in cold conditions - case with engine oil

if the oil is between -20 and -40 after start oil pressure may drop. if it not increase after 2 min - SHUT DOWN

takeoff during icing conditions

set takeoff thrust at 54% n1 for 30s before takeoff roll

ICE CONDITION AFTER LANDING SEQUENCE

leave the flaps extended

autopilot disengaged during CAT II approach

above 1000ft try to reengage it, if disengage agaij - GO AROUND. below 1000ft perfom GO AROUND

Autoland - callouts and heights

1500ft - check for Autoland 1. 1000ft - stabilization. 800ft - autotrim. 500ft - stabilziation. 100ft above minimums - approaching minimums. 150ft - ALIGN on FMA. 50ft - FLARE on FMA. 30ft - RETARD. If no D-ROT or NO ROLLOUT continue landing manually

RNP value for remote/oceanic, en-route, temrinal, approach, missed approach

remote/oceanic - 4, en-route - 2, temrinal - 1, approach - 0,3, missed approach - 1

maximum rate of descent at touchdown during overweight landing

360 ft/min

during windshear escape maneuver how far will you maintain configuration (gear and flaps)?

until 1500ft AGL or after Windshear label is removed

what pitch during windshear escape maneuver?

20° or PLI

upset recovery conditions:

pitch up 25°, pitch down 10°, bank more than 45°

depresurization, oxygen profile

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

green dot

provides the minimum speed for the current configuration

how to disarm slide

all small handles up

fire detection class of cargo compartment

class C