LIMITACIONES EMBRAER 190

EMBRAER 190. MAX RAMP WEIGHT. 110230 LBS. 112245 LBS. 111245 LBS.

EMBRAER 190. MAX TAKE OFF WEIGHT. 110230 LBS. 94798 LBS. 102130 LBS.

EMBRAER 190. MAX ZERO FUEL WEIGHT. 110230 LBS. 94798 LBS. 89948 LBS.

EMBRAER 190. MAX. LANDING WEIGHT. 110230 LBS. 94798 LBS. 97498 LBS.

MAXIMUM ALTITUD FOR FLAPS EXTENSION AND OPERATION. 21000 FT. 22000 FT. 20000 FT.

ALTERNATE CENTER OF GRAVITY IN EMBRAER 190 IS. 12%. 22%. 17%.

VLo FOR GEAR RETRACTION. 235 KIAS. 265 KIAS. 235 GS.

VLo FOR GEAR EXTENSION. 235 KIAS. 265 KIAS. 210 KIAS.

VLE. MAX SPEED WITH LANDING GEAR EXTENDED AND LOCKED. 253 KIAS. 265 KIAS. 210 KIAS.

WHAT IS VLo?. is the maximum speed at which the landing gear can be safely extended and retracted. is the maximum speed at which the airplane can be safely flown with the landing gear extended and locked. is the maximum maneuver speed with the airplane full configurated for landing.

WHAT IS VLe?. is the maximum speed at which the landing gear can be safely extended and retracted. is the maximum speed at which the airplane can be safely flown with the landing gear extended and locked. maximum operatin speed in turbulence condition.

MAXIMUN SPEED TO OPEN THE DIRECT VISION WINDOW?. M.82. 160 KIAS. 210 KIAS.

MAX. N1 ROTATION SPEED. 108%. 100%. 89.5%.

Vmo. UP TO 8.000FT. 320 KIAS. M.82. 300 KIAS.

Vmo. FROM 10000 ft AND UP TO 29000 ft. M.82. 300 KIAS. 320 KIAS.

VFe. FLAPS 1. 230 KIAS. 210 KIAS. 320 KIAS.

VFe. FLAPS 2. 230 KIAS. 215 KIAS. 320 KIAS.

VFe. FLAPS 3. 230 KIAS. 215 KIAS. 200 KIAS.

VFe. FLAPS 4. 180 KIAS. 215 KIAS. 320 KIAS.

VFe. FLAPS 5. 180 KIAS. 215 KIAS. 190 KIAS.

VFe. FLAPS FULL. 180 KIAS. 165 KIAS. 190 KIAS.

MAXIMUM TIRE GROUND SPEED. 180 KIAS. 195 KIAS. 195 KTS.

Maximum Takeoff and Landing Tailwind Component. 38 KT. 10 KT. 25 KT.

MAXIMUM RECOMMENDED CROSSWIND (Dry Runway). 38 KTS. 31 KTS. 25 KTS.

MAXIMUM RECOMMENDED CROSSWIND (Wet Runway). 38 KTS. 31 KTS. 10 KTS.

MAXIMUM RECOMMENDED CROSSWIND (Runway with Compacted Snow). 38 KTS. 31 KTS. 20 KTS.

MAXIMUM RECOMMENDED CROSSWIND (Runway with Standing Water/Slush/Wet Snow/Dry Snow). 25 KTS. 18 KTS. 20 KTS.

MAXIMUM RECOMMENDED CROSSWIND Runway with Ice (including wet ice). 25 KTS. 18 KTS. 12 KTS.

YOU SHOULD AVOID A STATIC TAKEOFF WITH A CROSWIND COMPONENT GREATER THAN. 25 KTS. 18 KTS. 38 KTS.

¿Are the Pilots are authorized to deviate from their current Air Traffic Control (ATC) clearance to the extent necessary to comply with an EGPWS warning.?. true. false.

The Terrain Display is intended to be used as a first aid of navigation and terrain avoidance maneuver. true, the terrain dysplay provides the accuracy and/or fidelity on which to solely base terrain avoidance maneuvering. false, The Terrain Display is intended to be used as a situational tool only and may not provide the accuracy and/or fidelity on which to solely base terrain avoidance maneuvering.

DURING SINGLE ENGINE OPERATION, TCAS MUST BE SET TO: TA MODE. TA/RA. STBY.

Deviation from the ATC assigned altitude is authorized only to extent necessary to comply with a TCAS Resolution Advisory (RA). TRUE. FALSE.

Maximum usable fuel quantity per wing tank. 41440 LBS. 14440 LBS. 114440 LBS.

Maximum fuel capacity is. 29083 LBS. 28183 LBS. 92380 LBS.

Unusable fuel quantity per wing tank. 101.5 LBS. 100 LBS. 10.5 LBS.

minimum fuel tank temperature. -40 ºC. 32ºF. 15ºC.

WICH IS THE NORMAL POSITION OF THE CROSSFEED SELECTOR KNOB BUTTON DURING TAKEOFF AND LANDING. OFF. AUTO. ON.

WICH IS THE MINIMUM TEMPERATURE TO START THE APU. -54ºC. 0ºC. 15ºF.

WICH IS THE MAXIMUM ALTITUD TO START THE APU. 30000 FT. 41000 FT. 21000 FT.

WICH IS THE MAXIMUM OPERATING ALTITUD OF THE APU. 30000 FT. 33000 FT. 21000 FT.

THE APU CAN PROVIDE ELECTRICAL ENERGY (AC) TO THE AIRPLANE UP TO. 30000 FT. 33000 FT. 15000 FT.

THE APU CAN PROVIDE BLEED AIR PRESSURE UP TO. 21000 FT. 33000 FT. 15000 FT.

THE APU CAN ASSIST AN ENGINE AIR START UP TO. 21000 FT. 33000 FT. 15000 FT.

THE MAXIMUM ROTOR SPEED OF THE APU IN % IS. 59.3%. 108%. 100%.

there is automatic shutdown of APU in flight, if EGT exceeds the limits. true. false.

the APU can only operate for 30 minutes in a temperature range between 662ºC and 717ºC in amber range. true, the APU on ground or in flight if the amber range between 662°C and 717°C is reached must be turned off. false, There is no time limitation for operating the APU on ground or in flight in the amber range between 662°C and 717°C.

what is the cooling period of the APU during the first and second start attempt. 10 seconds off. 60 seconds off. 5 minutes off.

after the third start attempt. what is the cooling period required for a new try ??. 10 seconds off. 60 seconds off. 5 minutes off.

The use of predictive EGPWS functions should be manually inhibited when landing to an airport that is not in the EGPWS airport database to avoid unwanted alerts. true. false.