Semilla limitada ceo

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS CLEAN? ?G/?G.

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS OTHER CONFIGURATION? ?G/?G.

ENVIRONMENTAL ENVELOPE MAX T.O OR LANDING ALTITUDE. XXXXXFT/XXXXXft.

ENVIRONMENTAL ENVELOPE CELLING. Xxxxxxft.

ENVIRONMENTAL ENVELOPE MINIMUM TEMP FOR T.O AT 14100FT. XXXXC.

ENVIRONMENTAL ENVELOPE MAX TEMP FOR T.O AT 14100FT XXXXXXXC.

ENVIRONMENTAL ENVELOPE MIN TEMP FOR T.O AT -2000FT. XXXXXXC.

ENVIRONMENTAL ENVELOPE MAX TEMP FOR T.O AT -2000FT. XXXXXXC.

MAX RUNWAY SLOPE -xxx%/xxxx%.

MAX DEMO CROSSWIND FOR T.O OR LANDING. Xxxxkt.

MAX TAILWIND FOR T.O OR LANDING. Xxxxxkt.

FLAPS CONFIGURATION WITH TAILWIND GREATER THAN 10KT AT LANDING. FLAPS XXXXXXX.

The maximum wind for passenger door operation is? Xxxkt.

The maximum wind for FWD and AFT cargo door operation is? Xxxxxkt.

MAXIMUM CROSSWIND AT LANDING IN A RUNWAY COVERED WITH COMPACTED SNOW OAT AT OR BELOW -15C. Xxxxxkt.

MAXIMUM CROSSWIND AT LANDING IN A RUNWAY COVERED WITH DRY SNOW, WET SNOW, SLUSH, FROST, DAMP WET (UP TO 3MM-1/8”) Xxxxxkt.

MAXIMUM CROSSWIND AT LANDING IN A RUNWAY COVERED WITH DRY SNOW, WET SNOW (MORE THAN 3MM-1/8”), COMPACTED SNOW (OAT ABOVE -15), DRY SNOW OVER COMPACTED SNOW, WET SNOW OVER COMPACTED SNOW, SLIPPERY WET Xxxxxkt.

MAXIMUM CROSSWIND AT LANDING IN A RUNWAY COVERED WITH STANDING WATER OR SLUSH (MORE THAN 3MM-1/8” UP TO 13MM-1/2”). XXXXXKT.

MAXIMUM CROSSWIND AT LANDING IN A RUNWAY COVERED WITH ICE XXXXXKT.

COCKPIT WINDOW OPEN MAXIMUM SPEED Xxxxkt.

MAXIMUM FLAPS/SLATS SPEEDS CONF 1. Xxxkt.

MAXIMUM FLAPS/SLATS SPEEDS CONF 1+F. XXXXKT.

MAXIMUM FLAPS/SLATS SPEEDS CONF 2. XXXXKT.

MAXIMUM FLAPS/SLATS SPEEDS CONF 3 XXXXKT.

MAXIMUM FLAPS/SLATS SPEEDS CONF FULL. XXXXKT.

MAXIMUM OPERATING SPEED VMO. Xxxkt.

MAXIMUM OPERATING SPEED MMO. Mxxxxx.

MAXIMUM SPEEDS WITH THE LANDING GEAR EXTENDED VLE. XXXKT/MXXX.

MAXIMUM SPEEDS WITH THE LANDING GEAR EXTENDED VLO RETRACTION. XXXKT/MXXX.

MAXIMUM SPEED AT WHICH THE LANDING GEAR MAY BE EXTENDED VLO EXTENSION. XXXKT/MXXX.

MAXIMUM TIRE GROUND SPEED XXXKT.

MINIMUM CONTROL SPEED FOR LANDING (VMCL). Xxxkt.

MINIMUM CONTROL SPEED VMCG ON 30M NARROW RUNWAY. VMCG+XXXKT.

MINIMUM CONTROL SPEED VMCG ON 35M NARROW RUNWAY. VMCG+XXXKT.

MINIMUM CONTROL SPEED VMCG ON 40M NARROW RUNWAY. VMCG+XXXKT.

Do not exceed a taxi speed of ____kt during a turn when the takeoff weight is higher than 76 000 kg (167 550 lb).

WIPERS MAXIMUM OPERATING SPEED. Xxxkt.

Maximum taxi weight Xxxxxkg.

Maximum takeoff weight (brake release) xxxxxkg.

Maximum landing weight. xxxxxkg.

Maximum zero fuel weight xxxxxkg.

Minimum weight Xxxxxkg.

MAX TIME WITHOUT AIR CONDITIONING SUPPLY WITH PASSENGERS ON BOARD. Xxxxxmin.

The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System. True. False.

During ground operations and depending on the OAT, the flight crew must limit the time that the aircraft electric power supply is used, in normal avionics ventilation system configuration, as follows OAT ≤ 49 °C xx xxxxxxxxxx.

During ground operations and depending on the OAT, the flight crew must limit the time that the aircraft electric power supply is used, in normal avionics ventilation system configuration, as follows 49 °C < OAT ≤ 55 °C. XxxxH.

During ground operations and depending on the OAT, the flight crew must limit the time that the aircraft electric power supply is used, in normal avionics ventilation system configuration, as follows 55 °C < OAT ≤ 60 °C. XxxxH.

During ground operations and depending on the OAT, the flight crew must limit the time that the aircraft electric power supply is used, in normal avionics ventilation system configuration, as follows 60 °C < OAT ≤ 64 °C. XxxxH.

Maximum positive differential pressure. XxxPSI.

Maximum negative differential pressure Xxxpsi.

Safety relief valve setting Xxxpsi.

Minimum decision height ILS CAT II. XXXFT.

Minimum decision height ILS SA CAT II. XXXFT.

Minimum decision height ILS OTS CAT II. XXXFT.

Minimum decision height ILS CATEGORY III FAIL PASSIVE (SINGLE) XXXFT.

Alert height ILS CAT III FAIL OPERATIONAL (DUAL). Xxxft.

Minimum Runway Visual Range For CAT III without DH. XXXM.

Minimum decision height for CAT III with DH. Xxxxxft.

CAT II and CAT III fail passive autoland are only approved in configuration ____, and if engine-out procedures are completed before reaching _____ in approach. Xxx/xxxft.

MAX CROSSWIND FOR CAT II AND CAT III. XXXKT.

MAX HEADWIND FOR CAT II AND CAT III. XXXXKT.

MAX TAILWIND FOR CAT II AND CAT III. XXXKT.

Automatic landing is posible with a glide slope between Xxx/xxx.

Automatic landing is posible with an airport elevation at or below. Xxxxft.

Automatic landing is not allowed below Xxxxxftpressalt.

r three consecutive APU start attempts, the flight crew must wait ____ before a new start attempt. Xxxm.

Maximum APU N speed. XXXX%.

Maximum EGT for APU start (below 25 000 ft) XxxxC.

Maximum EGT for APU start (above 25 000 ft) XxxC.

Maximum EGT for APU running (with 5 s confirmation for shutdown) XxxC.

Maximum EGT for APU running (for immediate shutdown) XxxC/xxxC.

Max altitude to assist engine start with apu bleed. Xxxxft.

Max altitude for air conditioning and pressurization (single pack operation) Xxxxxft.

Max altitude for air conditioning and pressurization (dual pack operation) Xxxxxft.

Use of APU bleed air for wing anti-ice is permitted or not permitted?.

THRUST SETTING/EGT LIMITS TOGA ALL ENGINES OPERATIVE. XXXM/XXXC.

THRUST SETTING/EGT LIMITS TOGA ONE ENGINE INOPERATIVE. XXXM/XXXC.

THRUST SETTING/EGT LIMITS MCT XXXC.

THRUST SETTING/EGT LIMITS STARTING. XXXC.

Maximum engine N1 Xxx%.

Maximum engine N2. Xxx%.

Maximum continuous oil temperature. Xxxc.

Maximum transient oil temperature Xxxm/xxxc.

Minimum starting oil temperature. Xxxc.

Minimum oil temperature before takeoff. Xxxc.

Minimum oil quantity. Xxxqt+xxxqt/h.

Max oil pressure. Xxxpsi.

Min oil pressure xxxpsi.

How many start attempts includes a cycle of a standard automatic engine start.

For ground engine starts (automatic or manual), a ____ pause is required between successive cycles. Xxxxs.

Performing a standard automatic engine start, a ______ cooling period is required, subsequent to four failed cycles. Xxxmin.

The starter must not be run when N2 is above ___. Xxx%.

Maximum reverse should not be used below Xxxkt.

TFLEX cannot be higher than TMAXFLEX, equal to ISAXXXXC.

TFLEX cannot be lower than the xxxxx xxxxxxx.

TFLEX cannot be lower than the actual xxx.

Maximum operating altitude with slats and/or flaps extended. Xxxft.

The fuel system is certified with. JETA. JETA1. JETA2. JETB. JETB1. JP8. JP1. JP5. JP3. JP4.

The fuel system is certified with xxx/xxx/xxx/xxx/ etc.

MAX JETA1 TEMP. XXXC.

MIN JETA1 TEMP XXXC.

MAX JP8 TEMP XXXC.

MIN JP8 TEMP XXXC.

MAX N3 JET TEMP. XXXC.

MIN N3 JET TEMP XXXC.

MAX JETA TEMP. XXXC.

MIN JETA TEMP. XXXC.

MAX JP5 TEMP XXXC.

MIN JP5 TEMP Xxxc.

MAX RT FUEL TEMP. Xxxc.

MIN RT FUEL TEMP. Xxxc.

MAX TS1 FUEL TEMP XXXC.

MIN TS1 FUEL TEMP. XXXC.

MAX JETB TEMP. XXXC.

MIN JETB TEMP. XXXC.

MAX JP4 TEMP. XXXC.

MIN JP4 TEMP. XXXC.

If the wing fuel temperature exceeds 30 °C at engine start, the altitude must be limited to __________ until the center tank is empty. Xxxxxft.

If the wing fuel temperature exceeds 40 °C at engine start, the altitude must be limited to __________ until the center tank is empty. Xxxxxft.

If the wing fuel temperature exceeds 49 °C at engine start, the altitude must be limited to __________ until the center tank is empty. Xxxxxft.

FUEL IMBALANCE AT TO INNER TANK FULL - MAX ASYMMETRY _______. XXXKG.

FUEL IMBALANCE AT TO INNER TANK 3000kg - MAX ASYMMETRY _______. XXXKG.

FUEL IMBALANCE AT TO INNER TANK 1450KG - MAX ASYMMETRY _______. XXXKG.

FUEL IMBALANCE AT TO OUTER TANKS MAX ASYMMETRY _______. XXXKG.

FUEL IMBALANCE IN FLIGHT AND AT LANDING INNER TANK FULL - MAX ASYMMETRY _______. XXXKG.

FUEL IMBALANCE IN FLIGHT AND AT LANDING INNER TANK 4300KG - MAX ASYMMETRY _______. XXXKG.

FUEL IMBALANCE IN FLIGHT AND AT LANDING INNER TANK 2250KG - MAX ASYMMETRY _______. XXXKG.

FUEL IMBALANCE IN FLIGHT AND AT LANDING OUTER TANKS MAX ASYMMETRY _______. XXXKG.

MINIMUM FUEL QUANTITY FOR T.O. XXXXkg.

MAXIMUM BRAKE TEMPERATURE FOR T.O. Xxxc.

MAXIMUM NWS ANGLE WITH TOWBAR. Xxx.

If maximum one tire per gear is deflated (consider three gears) Maximum taxi speed during turn. Xxxkt.

If two tires are deflated on the same main gear (maximum one main gear) Maximum taxi speed. Xxxkt.

For the nosewheel steering (NWS) angle Maximum NWS angle. Xxx.

Ground alignment of the IRS is possible in latitudes between XXN/XXS.

In NAV mode, the IR will not provide valid magnetic heading and magnetic track angle. XXN/XXS.

MINIMUM FLIGHT CREW OXYGEN PRESSURE REF TEMP -10C/14F 2CM ___ 2CM+1OBS____ 2CM+2OBS____ XXX/XXX/XXX.

MINIMUM FLIGHT CREW OXYGEN PRESSURE REF TEMP 0C/32F 2CM ___ 2CM+1OBS____ 2CM+2OBS____ XXX/XXX/XXX.

MINIMUM FLIGHT CREW OXYGEN PRESSURE REF TEMP 10C/50F 2CM ___ 2CM+1OBS____ 2CM+2OBS____ XXX/XXX/XXX.

MINIMUM FLIGHT CREW OXYGEN PRESSURE REF TEMP 20C/68F 2CM ___ 2CM+1OBS____ 2CM+2OBS____ XXX/XXX/XXX.

MINIMUM FLIGHT CREW OXYGEN PRESSURE REF TEMP 30C/86F 2CM ___ 2CM+1OBS____ 2CM+2OBS____ XXX/XXX/XXX.

MINIMUM FLIGHT CREW OXYGEN PRESSURE REF TEMP 40C/104F 2CM ___ 2CM+1OBS____ 2CM+2OBS____ XXX/XXX/XXX.

MINIMUM FLIGHT CREW OXYGEN PRESSURE REF TEMP 50C/122F 2CM ___ 2CM+1OBS____ 2CM+2OBS____ XXX/XXX/XXX.

Maximum taxi speed on straight line Xxxkt.

When vacating a runway on high-speed taxiway: Dry: _____ Good:_____ Less than good:______ Turns of 90º or more (oversteering):_____ Turns 90º or less (dry or damp):_______ XXKT-XXKT/XXKT/XXKT/XXKT/XXKT.

Landing prohibited with RCAM.