Term
| As a general rule to estimate fuel required: |
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Definition
1st hour = 1500 pounds
2nd hour = 1200 pounds
3rd hour = 1200 pounds
subsequent hours = 1100 pounds |
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Term
| As a general rule to find time for a trip, take the trip distance and divide by ____________ KTS. |
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Definition
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Term
| The minimum fule required for a 45-minute reserve/hold is approximately _________ pounds. |
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Definition
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Term
| Approach climb gradient is computed at _______ climb gradient of 2.1% since a safety factor of airspeed and altitude has already been obtained. |
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Definition
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Term
| Configuration for Approach Climb is landing gear _______, flaps ______ degrees and take off thrust on ____ engine. |
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Definition
Landing gear - UP
Flaps - 20 degrees
T/O Thrust - 1 engine |
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Term
| ______ climb gradient is the climb gradient that the airplane can actually achieve under ideal conditions with a test pilot. |
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Definition
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Term
| First segment climb ends at _________. |
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Definition
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Term
| Maximum takeoff weight limit is determined by selecting the lowest of these 4 limits: |
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Definition
- Cerified takeoff weight limit
- climb or brake energy weight limit
- takeoff distance weight limit
- obstacle clearance weight limit |
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Term
| Landing distance is based in part on a ________ runway. |
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Definition
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Term
| To account for human variables among others, net climb gradient is the gross climb gradient reduced by _____ % during takeoff phase. |
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Definition
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Term
| Second segment starts at the end of _________, andis flown at a speed of _____, which provides a climb gradient of _________. |
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Definition
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Term
| For FAR Part 25 aircraft certification, required second segment climb performance is _______%. |
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Definition
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Term
| Vmca (Minimum Control Speed Air) is the flight speed at which the aircraft is controllable with _______ when one engine suddenly becomes inoperative and the remaining engine is operating at _________. |
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Definition
5 degrees of bank
Takeoff Thrust |
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Term
| The maximum takeoff weight is _____ pounds. |
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Definition
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Term
| Critical engine failure speed (V1) is the speed at which, due to engine failure, the pilot is assumed to elect to ____________ the takeoff. |
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Definition
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Term
| If engine failure occurs at V1, the distance to continue the takeoff to 35 feet does not exceed _________; or, the distance to bring the aircraft to a full stop does not exceed the _______ distance available. |
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Definition
Usable Takeoff Distance
Accelerate Stop |
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Term
| The close in flight path chart uses _______ and ________ to determine net climb gradient. |
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Definition
-Obstacle Height Above Runway
-Obstacle horizontal distance from reference zero |
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Term
| The close in takeoff path chart will give you _________ net climb gradient required to clear an obstacle. |
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Definition
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Term
| Second Segment climb gradient is a function of: |
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Definition
- Temperature
- Altitude
- Gross Weight
- Wind
- Anti-Ice Systems |
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Term
| Critical Engine Failure speed is a factor of: |
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Definition
- Temperature
- Gross Weight
- Wind
- Runway Gradient
- Anti-Ice Systems; Anti-Skid |
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Term
| Vr and V2, at Takeoff flaps 8 degrees, are a function of airplane ______ only. |
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Definition
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Term
| ______ is the only factor used to determine a normal landing approach speed (Vref- no gusts reported). |
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Definition
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Term
| Wet runway correction factor for FAR Part 91 aircraft is actual dry runway landing distance multiplied by _____; FAR Part 121/135 operations, multiply factored landing distance by _____. |
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Definition
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Term
| Minimum turn around time is _____ to allow the brakes to cool after landing. Longer time may be necessary if _________ action was needed. |
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Definition
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Term
| ENGINE FAILURE DURING TAKEOFF/BELOW V1-ABORTED TAKEOFF: |
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Definition
1.THRUST LEVERS - IDLE
2.WHEEL BRAKES - APPLY
3.SPOILERS - EXTEND
4.DRAG CHUTE OR THRUST REV. - DEPLOY IF NECESSARY |
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Term
| ENGINE FAILURE DURING TAKEOFF ABOVE V1: |
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Definition
1.RUDDER/AILERONS - AS REQUIRED FOR DIRECTIONAL CONTROL
2.ACCELERATE TO Vr KEEP NOSE WHEEL ON RUNWAY.
3.ROTATE AT Vr;CLIMB AT V2 AT POSITIVE RATE OF CLIMB
4.LANDING GEAR - UP
5.ACCELERATE TO V2+30 AND RETRACT FLAPS |
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