Section One Limitations for Boeing 777
Quiz yourself by thinking what should be in
each of the black spaces below before clicking
on it to display the answer.
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| B777 airplanes are category __ for instrument approaches except for circling, which is category __. | show 🗑
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| show | 8,400 feet
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| show | +/- 2%
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| Maximum UNRESTRICTED takeoff / landing tailwind component: | show 🗑
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| show | 15 knots
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| Restrictions for 15 knot tailwind takeoffs are:________________ | show 🗑
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| show | 1. Landing weights are verified by reference to Section 5.2. Antiskid and Thrust Reversers are fully operational.3. Flaps 30 landing.4. Auto spoilers are used (unless correction is taken.)5. Braking action reported at least GOOD.
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| Flight maneuvering load acceleration limits (flaps up): | show 🗑
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| show | +2.0g to 0.0g
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| Flap 1 placard speed: | show 🗑
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| show | 235 kias
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| show | 215 kias
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| show | 195 kias
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| Flap 25 placard speed: | show 🗑
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| Flap 30 placard speed | show 🗑
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| Maximum Landing Gear Operating Speed (VLO/MLO): | show 🗑
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| Maximum Landing Gear Extended Speed (VLE/MLE): | show 🗑
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| show | deliberately exceeded
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| show | 0.87 mach
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| show | 330 kias
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| Note: All airspeed markings and placards in the airplane are shown as ___ values, based on the primary static pressure source. | show 🗑
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| The ____ corrects for static source position error and essentially displays knots ___ inflight. | show 🗑
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| Vmo, Mmo, Vle, or flap placard speed (whichever is lower) is indicated by the _______________________________________. | show 🗑
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| ___ is defined as the speed above which maneuvers involving full application of rudder, ailerons, or elevator, or maneuvers involving angles of attack near stall, SHOULD BE AVOIDED. | show 🗑
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| show | 43,100 feet
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| Turbulent Air Penetration Speed (in severe turbulence) below 25,000 feet: | show 🗑
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| Turbulent Air Penetraion Speed (in severe turbulence) at and above 25,000 feet: | show 🗑
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| In severe turbulence, maintain a minimum of __ knots above the minimum maneuvering speed (top of the amber band) when below 0.82 mach. | show 🗑
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| The crosswind guidelines (takeoff and landing) were derived through flight test data, engineering analysis, and piloted simulation evaluations. Therefore, the use of these guidelines should be based on the ________ and the _____________. | show 🗑
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| show | 148 feet (45 meters)
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| Engine surge can occur with a strong crosswind component if takeoff thrust is set prior to brake release. Therefore, ______ takeoffs are strongly advised when crosswinds exceed ___ knots. | show 🗑
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| show | ... the chart in Section 1.
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| Recommended LANDING crosswind component guidelines (not Autoland) - DRY: | show 🗑
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| show | 40 knots
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| show | 20 knots
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| show | 35 knots
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| Landing on untreated snow should only be attempted when ___ _____ is present. | show 🗑
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| Landing crosswind guidelines are valid for __________________. | show 🗑
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| show | 5 knots
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| show | weights and C.G.
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| LAHSO required runway length (feet) for elevations , 2,000 ft: | show 🗑
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| show | 8,700
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| Maximum RAMP weight: | show 🗑
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| Maximum TAKEOFF weight: | show 🗑
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| show | 460,000 pounds
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| show | 430,000 pounds
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