B767 Exam Questions and Answers 100% Pass

B767 Exam Questions and Answers 100% Pass ABORTED ENGINE START - FUEL CONTROL switch (affected side) . . . CUTOFF CABIN ALTITUDE - Oxygen Masks - ON/100% Dual Engine Failure - ENGINE START SELECTORS (Both) . . . FLT THRUST LEVERS (Both). . . . . . . . . Idle FUEL CONTROL SWITCHES (Both) . . . . . . . . . . . . . . . . . CUTOFF, THEN RUN If engine appears stalled or EGT approaches the Standby Engine Indicator placard limit: 2 100% Pass Guarantee Katelyn Whitman, All Rights FUEL CONTROL SWITCH (Affected engine). . . . . . . . . . . . . . . . . CUTOFF, THEN RUN If engine appears stalled again or EGT approaches the Standby Engine Indicator placard limit, repeat as needed. ENGINE FIRE/Eng Severe Damage or Sep. - A/T ARM switch ... OFF Thrust lever (affected side) .... Confirm .... Idle ENGINE LIMIT OR SURGE OR STALL - 1. A/T ARM SWITCH- OFF 2. THRUST LEVER- (AFFECTED SIDE) CONFIRM- RETARD UNTIL INDICATIONS REMAIN WITHIN NORMAL LIMITS OR THE THRUST LEVER IS AT IDLE MAIN CARGO FIRE - Oxygen Masks .... On/100% Rapid Decompression - Oxygen Masks .... On/100% 3 100% Pass Guarantee Katelyn Whitman, All Rights Smoke/Fire/Fumes - Oxygen Masks .... On/100% Limitations - Weight - Ramp/Taxi .... 409,000 Max TO Wt .... 408,000 Max Landing Wt .... 326,000 Zero Fuel Wt .... 309,000 Limitations - Speeds - Normal Taxi Speed .... 20 knots Long-Straight Taxi Speed .... 30 knots Turns, dry surface .... 10 knots Limitations - Tailwind - Takeoff, Landing, Autoland ..... 15 knots Autoland Headwind - 25 knots Limits - Crosswind Takeoff - 30 ... good-25 ... good to medium-20 ... medium-17 ... medium to poor-15 ... poor-13 Limits - Crosswind Landing - 30 ... good-30 ... good to medium-30 .... medium-25 ... medium to poor-17 ... poor-15 4 100% Pass Guarantee Katelyn Whitman, All Rights Max Operating Altitude - 43,100 Maximum depth of dry snow for takeoff - 4 inches Maximum depth of slush, wet snow, or standing water - Half and inch Minimum runway width for 180 degree turn - 146 feet Max Runway Slope - +/- 2% Maximum Fuel Imbalance Between Main Tanks - 2,500 when total main tank fuel is less than 48,000 lb 1,500 when total main tank fuel is greater than 48,000lb The center tank may contain up to _________ of fuel with less than full main tanks provided center tank fuel weight plus actual zero fuel weight does not exceed the maximum zero fuel weight, and center of gravity limits are observed. - 22,050 lbs