B767 LPE

Maximum Taxi Weight (XXX,XXX kgs).

MTOW (XXX,XXX kgs).

MLW (XXX,XXX kgs).

MZFW (XXX,XXX kgs).

Runway slope. +-2%. +-1%. +-1.5%.

Maximum operating altitude. 43,100 ft. 41,300 ft. 41,900 ft.

Maximum T.O. and Landing altitude. 9,500 ft. 9,000 ft. 8,500 ft.

# Max T.O. and Landing TW. 15 kts. 10 kts. 12 kts.

#Severe turbulent air penetration speed: 290 KIAS / .78 Mach, whichever is lower. 300 KIAS / .80 Mach, whichever is lower. 280 KIAS / .76 Mach, whichever is lower.

#Use of HF radios is permitted during refueling operations. True. False.

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

Max. allowable in-flight difference between Captain and First Officer altitude displays for RVSM operation is: 200 ft. 150 ft. 100 ft.

Max. allowable on the ground differences between Captain and First Officer altitude displays for RVSM operation SEA LEVEL: 40 ft between altitude displays / 75 between altitude display & field elevation. 20 ft between altitude displays / 75 between altitude display & field elevation. 25 ft between altitude displays / 75 between altitude display & field elevation.

#Avoid weather radar operation in a hangar. True. False.

#After takeoff, the autopilot must not be engaged below: 200 ft AGL. 100 ft AGL. 150 ft AGL.

#Do not use the autopilot below ________ at airport pressure altitude above 8,400 ft. 100 ft RA. 200 ft RA. 250 ft RA.

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

#Max. HW for CAT II / III. 25 kts. 20 kts. 15 kts.

#Max. TW for CAT II / III. 15 kts. 10 kts. 20 kts.

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

Min. inflight fuel tank temperature. 3°C above the freeze point of the fuel being used. 5°C above the freeze point of the fuel being used. 7°C above the freeze point of the fuel being used.

Max. fuel temperature (JET A). 49°C. 47°C. 46°C.

Center tank may contain up to 10,000 kgs of fuel with less than full main tanks provided that. center tank fuel + ZFW does not exceed MZFW and center of gravity limits are observed. No limitation. center tank fuel + ZFW does not exceed MZFW and center of gravity limits are Alternate T1.

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

#Reverse thrust is for ground only. True. False.

#Max. altitude with flaps extended is. 20,000 ft. 25,000 ft. 22,500 ft.

#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. True. False.

Largo del B767-300ER. 54.94m. 58.32m. 51.54m.

Envergadura B767-300ER. 50.88m. 54.94m. 48.75m.

Ancho requerido para viraje 180°. 44.6m. 40m. 38.5m.

Pitch en despegue para Tailstrike. 9.6 degrees. 10 degrees. 11.5 degrees.

Master Warning inhibit. Lift off until 400 ft AGL or 20 secs. Lift off until 200 ft AGL or 20 secs. Lift off until 400 ft AGL or 25 secs.

Master Caution inhibit. 80 knots until 400 ft AGL or 20 secs. 80 knots until 200 ft AGL or 20 secs. 80 knots until 400 ft AGL or 25 secs.

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. -47. -49. -44.

B767 min. fuel temperature (JET A1). -44. -47. -49.

L and R fuel tanks capacity (each). 18,267 kg. 16,342 kg. 17,963 kg.

Center tank capacity. 36,349 kgs. 40,873 kgs. 38,764 kgs.

Fuel jettison rate. 1,200 kg / min. 1,000 kg / min. 600 kg / min.

Fuel jettison rate (CTR TK pumps only). 600 kg / min. 1,000 kg / min. 1,200 kg / min.

Normal bleed pressure. 25 PSI. 20 PSI. 50 PSI.

Max. bleed pressure. 50 PSI. 30 PSI. 40 PSI.

Landing gear max. extension / retraction speeds (Normal sys). 270 kts / .82M. 250 kts / .80M. 290 kts / .78M.

Landing gear max. extension / retraction speeds (ALTN sys). 250 kts / .75M. 270kts / .80M. 290 kts / .78M.

Max. speed with Landing gear extended in flight. 270 kts / .82M. 250 kts / .75M. 290 kts / .78M.

Max. tire speed. 235 MPH. 230 MPH. 225 MPH.

Parking brake time (3,000 PSI). 8 hours. 10 hours. 6 hours.

Min. brake accumulator pressure. 950 PSI. 850 PSI. 900 PSI.

BTM (cyan number and box). 0 - 2. 2 - 4. 0- 1.

BTM (cyan number and white box). 3 - 4. 2 - 4. 3 - 5.

BTM (white number and box). 5 - 9. 4 - 8. 3 - 8.

Tire pressure main gear. 200 - 210 PSI. 175 - 185 PSI. 185 - 195 PSI.

Tire pressure nose gear. 175 - 185 PSI. 195 - 200 PSI. 200 - 210 PSI.

Hottest brake indication (BTM). 10 - 15 minutes after complete stop. 15 - 20 minutes after complete stop. 20 - 25 minutes after complete stop.

AC electrical Voltage. 115V. 200V. 100V.

AC electrical frequency. 400 Hz. 450 Hz. 420 Hz.

IDG / APU / External KVA. 90 KVA. 110 KVA. 400 KVA.

HDG KVA. 5 KVA. 90 KVA. 55 KVA.

IDG Max. oil temperature. 185° C. 155° C. 145° C.

DC electrical voltage. 28 V. 90 V. 115 V.

Main TRU load limit. 120 A. 90 A. 200 A.

HDG load limit. 50 A. 40 A. 90 A.

Battery voltage. 23.5 V. 24 V. 25.5 V.

STBY power capacity time. 90 min. 110 min. 60 min.

HYD normal range. 2400 - 3100 PSI. 2500 - 3000 PSI. 2500- 3050PSI.

HYD max. PSI. 3500 PSI. 3100 PSI. 3000 PSI.

Fuel penalty RAT extended. 2%. 10%. 8%.

RAT stall speed. 130 kts. 140 kts. 120 kts.

RAT deploys when N2 of both engines are below. 42%. 40%. 30%.

HYD normal level. 1.00. 0.75. 1.10.

HYD refill level. 0.75. .50. 0.70.

HYD overfull level. 1.22. 1.30. 1.32.

Engines thrust output (each). 60,200 lbs. 62,000 lbs. 62,200 lbs.

Max. N1 rpm. 117.50 %. 112.50 %. 101.50 %.

Max. N2 rpm. 117.50 %. 112.50 %. 101.50 %.

Max. EGT start up (unlimited). 750°C. 725°C. 745°C.

Max. EGT MCT. 925°C. 955°C. 965°C.

Max. EGT Takeoff. 960°C. 950°C. 925°C.

Max. EGT startup (transient 40 secs). 870°C. 750°C. 925°C.

Max. oil temperature (period of 15 minutes max.). 175°C. 160°C. 180°C.

Max. oil temperature (continuous operation). 160°C. 175°C. 180°C.

Max. oil comsumption. 0.5 Liters per hour. 0.3 Liters per hour. 0.2 Liters per hour.

Min. oil pressure. 10 PSI. 12 PSi. 8 PSI.

Estimated fuel comsumption for planning (flight / holding ). 4,400 kg per hour / 4,800 kg per hour. 4,000 kg per hour / 4,800 kg per hour. 4,000 kg per hour / 4,400 kg per hour.

FF increase using Engine Anti Ice. 160 kg per hour. 230 kg per hour. 220 kg per hour.

FF increase using Total Anti Ice. 230 kg per hour. 200 kg per hour. 250 kg per hour.

APU start limits. Max. 3 consecutive starts within 60 minutes. Max. 5 consecutive starts within 45 minutes. Max. 3 consecutive starts within 45 minutes.

APU may not start above (not a limitation). 35,000 ft. 30,000 ft. 33,000 ft.

Max. APU bleed altitude. 17,000 ft. 15,000 ft. 22,000 ft.

Max. APU electrical altitude. 43,100 ft. 35,000 ft. 33,000 ft.

Average APU FF on ground. 115 kg per hour. 90 kg per hour. 105 kg per hour.

Flaps UP acceleration limit. +2.5g to -1.0g. +2.0g to -1.0g. +2.0g to 0.0g.

Flaps DN acceleration limit. +2.0g to -1.0g. +2.5g to -1.0g. +2.0g to 0.0g.

Cargo fire agent protection duration. 195 min. 120 min. 60 min.

Water tanks capacity (total). 564 lt. 530 lt. 510 lt.

Waste tanks capacity (total). 530 lt. 564 lt. 540 lt.

Max. thrust reduction for assumed temperature T.O. 25%. 20%. 15%.