B767 LATAM V2

Maximum Taxi Weight (XXX,XXX kgs).

MTOW (XXX,XXX kgs).

MLW (XXX,XXX kgs).

MZFW (XXX,XXX kgs).

Runway slope.

Maximum operating altitude.

Maximum T.O. and Landing altitude.

# Max T.O. and Landing TW.

#Severe turbulent air penetration speed:

#Use of HF radios is permitted during refueling operations.

#FLCH use on final approach below 1000 fet AFE is permitted.

Max. allowable in-flight difference between Captain and First Officer altitude displays for RVSM operation is:

Max. allowable on the ground differences between Captain and First Officer altitude displays for RVSM operation SEA LEVEL:

#Avoid weather radar operation in a hangar.

#After takeoff, the autopilot must not be engaged below:

#Do not use the autopilot below ________ at airport pressure altitude above 8,400 ft.

#Use of aileron trim with the autopilot engaged is prohibited.

#Max. HW for CAT II / III.

#Max. TW for CAT II / III.

#Flight crew shall not blank engine vibration display during T.O.

Min. inflight fuel tank temperature.

Max. fuel temperature (JET A).

Center tank may contain up to 10,000 kgs of fuel with less than full main tanks provided that.

Intentional dry running of a center tank fuel pump is prohibited.

#Reverse thrust is for ground only.

#Max. altitude with flaps extended is.

#Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll or yaw as they may result in structural failure at any speed, including below VA.

Largo del B767-300ER.

Envergadura B767-300ER.

Ancho requerido para viraje 180°.

Pitch en despegue para Tailstrike.

Master Warning inhibit.

Master Caution inhibit.

Max. speed Flaps 1 (XXX kts).

Max. speed Flaps 5 (XXX kts).

Max. speed Flaps 15 (XXX kts).

Max. speed Flaps 20 (XXX kts).

Max. speed Flaps 25 (XXX kts).

Max. speed Flaps 30 (XXX kts).

JET A1 min. temperature.

B767 min. fuel temperature (JET A1).

L and R fuel tanks capacity (each).

Center tank capacity.

Fuel jettison rate.

Fuel jettison rate (CTR TK pumps only).

Normal bleed pressure.

Max. bleed pressure.

Landing gear max. extension / retraction speeds (Normal sys).

Landing gear max. extension / retraction speeds (ALTN sys).

Max. speed with Landing gear extended in flight.

Max. tire speed.

Parking brake time (3,000 PSI).

Min. brake accumulator pressure.

BTM (cyan number and box).

BTM (cyan number and white box).

BTM (white number and box).

Tire pressure main gear.

Tire pressure nose gear.

Hottest brake indication (BTM).

AC electrical Voltage.

AC electrical frequency.

IDG / APU / External KVA.

HDG KVA.

IDG Max. oil temperature.

DC electrical voltage.

Main TRU load limit.

HDG load limit.

Battery voltage.

STBY power capacity time.

HYD normal range.

HYD max. PSI.

Fuel penalty RAT extended.

RAT stall speed.

RAT deploys when N2 of both engines are below.

HYD normal level.

HYD refill level.

HYD overfull level.

Engines thrust output (each).

Max. N1 rpm.

Max. N2 rpm.

Max. EGT start up (unlimited).

Max. EGT MCT.

Max. EGT Takeoff.

Max. EGT startup (transient 40 secs).

Max. oil temperature (period of 15 minutes max.).

Max. oil temperature (continuous operation).

Max. oil comsumption.

Min. oil pressure.

Estimated fuel comsumption for planning (flight / holding ).

FF increase using Engine Anti Ice.

FF increase using Total Anti Ice.

APU start limits.

APU may not start above (not a limitation).

Max. APU bleed altitude.

Max. APU electrical altitude.

Average APU FF on ground.

Flaps UP acceleration limit.

Flaps DN acceleration limit.

Cargo fire agent protection duration.

Water tanks capacity (total).

Waste tanks capacity (total).

Max. thrust reduction for assumed temperature T.O.