Resume the flight and immediately press 'a' to re-engage the autopilot. LNAV/VNAV should engage right away and after a short time the aircraft should stabilize itself at cruise altitude. We can now proceed with the pre-decent preparations. Pre-Descent VREF The reference approach speed (VREF) ...
Maximum Cruise Speed Mach 0.89 (950 km/h, 512 knots) at a cruise altitude of 35,000 ft (11,000 m) Maximum Range 5,240 NM(9,700 km) 7,065 NM(13,080 km) 8,555 NM(15,843 km) 6,006 NM(11,120 km) 7,370 NM(13,649 km) Takeoff distance in International StandardAtmosphere at...
VNAV– Commanding climb, cruise and descent performance (via our MCP only) Calculations based ontype specific performance data(can be configured by the user) Display and setting ofV-Speeds Setting ofN1 Limitsfor the MCP’s thrust management computer CLB/CRZ/DESPages HOLDFeature (time, distance, ...
then the SAI (Standby Altitude Indicator) comes partly to life... still a loooong wait, then finally the displays will flash themselves on and off, still waiting... then suddenly the 777 systems will come to life,But you will still need to set the current position C...
With a payload of 160,000 pounds (73,000 kg) and an initial cruise altitude of 28,000 ft (8,500 m), the C-17 has an unrefueled range of about 2,400 nautical miles (4,400 kilometres) on the first 71 aircraft, and 2,800 nautical miles (5,200 kilometres) on all subsequent ...
The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used. Descent: The Aircraft descends from the final cruise altitude at 250 KCAS to an altitude of 1,500 feet above the destination airport altitude. Throughout the descent, ...
Cruise speed Mach 0.80 (530 mph, 458 knots, 850 km/h at cruise altitude, i.e. 35,000 ft or 10.66 km) Range, loaded 7,222 km (3,900 NM) -200WL: 7,600 km (4,100 NM) 5,834 km (3,150 NM) 6,421 km (3,467 NM) Max. fuel 43,490 L (11,489 US gal) 42,680 L (11...
Assume the current autoflight guidance instructions are to climb to a cruise altitude of FL210 at an economy airspeed with an intermediate altitude constraint of FL190 at navigation waypoint “MARZY.” For a pilot (not shown) to ascertain these instructions, the pilot typically first looks at ...
When an aircraft is at cruise altitude or operating in cold climates while on the ground, the oil within the engine becomes cold. This significantly increases the viscosity of the oil. Higher viscosity oil may not always flow sufficiently through the oil distribution system, thereby creating issues...
Cruise Speed: Mach 0.80 (530 mph, 458 knots, 850 km/h at cruise altitude of 35,000 ft or 10.66 km)Range: 3,900 nmi (7,222 km) (4,100 nmi (7,600 km) with winglets)Service Ceiling: 42,000 ft (12,800 m) FlightFactor