Takeoff

Question 1

Which is considered a greater problem? An aborted takeoff with a tire failure or landing with a failure tire?

Answer 1

Aborted takeoff with a tire failure

Question 2

The effects of a tire failure are most pronounced at ____ and ____.

Answer 2

Heavy gross weight and speeds below 100 KCAS

Question 3

During heavy gross weight aborts, the nose will lower at approximately ____.

Answer 3

120 KCAS

Question 4

What should you anticipate following a high speed, heavy weight abort?

Answer 4

Extremely hot brakes, or brake failure, and possibility of tire fire

Question 5

When should you lower flaps during a high speed abort situation?

Answer 5

Once reaching full aft stick

Question 6

What should you do just prior to a barrier engagement?

Answer 6

Release brakes momentarily

Question 7

For MA-1/MA-1A what is the minimum engagement speed?

Answer 7

60 knots

Question 8

What is the designed dynamic limit for MA-1/MA-1A?

Answer 8

150 knots

Question 9

Expect nose or main gear failure above ___ knots for a MA-1/MA-1A engagement.

Answer 9

120

Question 10

Aircraft with ___ or ___ may not engage successfully with MA-1/MA-1A.

Answer 10

Centerline pylon or external stores, or speed brake open

Question 11

What is the maximum speed for BAK-15 engagement?

Answer 11

200 knots

Question 12

How long should it take for a BAK-15 to be raised after calling “barrier, barrier, barrier”?

Answer 12

5-7 seconds

Question 13

If you experience canopy entanglement after BAK-15 engagement, what should you consider?

Answer 13

Do not jetison canopy. Consider using canopy breaker tool if egress is required.

Question 14

What is the definition of SETOS?

Answer 14

Minimum speed at which the aircraft will take off and be able to fly out of ground effect with a minimum of 100 fpm rate of climb

Question 15

How much does SEROC increase with each additional knot above SETOS depending on temperature / pressure altitude?

Answer 15

8 to 50 fpm

Question 16

How much climb should you use on an engine failure during takeoff, takeoff continued?

Answer 16

Only that which is needed to avoid obstacles until the airspeed reaches 200 and flaps are retracted

Question 17

Why is gear retracted at SETOS + 10 on an engine failure during takeoff, takeoff continued?

Answer 17

Gear door drag is not a factor during retraction above this speed

Question 18

What could be exceeded before reaching SETOS + 10 on an engine failure during takeoff, takeoff continued?

Answer 18

Nosewheel tire limit

Question 19

On an engine failure during takeoff, takeoff continued, if left engine is inop but windmilling, will gear doors retract? How long will it take for gear retraction?

Answer 19

Gear doors may not completely close

Gear retraction may require up to 1 minute

Question 20

On an engine failure during takeoff, takeoff continued, if unable to retract the landing gear, best level flight/climb capability is obtained at what airspeed?

Answer 20

200 KCAS with 60% flaps

220 KCAS with flaps up

Question 21

On an engine failure during takeoff, takeoff continued, at high gross weight with the landing gear extended, flap retraction should not be initiated prior to ___.

Answer 21

220 KCAS

Question 22

As a guide, what is the formula for landing distance with full flaps?

Answer 22

(Fuel + 2500) * 2 + TD point

Question 23

If unable to raise the landing gear, aircraft will consume approximately ___ lbs per NM

Answer 23

10 to 15

Question 24

When configured with gear down and full flaps, the aircraft will burn approximately how much gas per minute at low altitudes and airspeeds below 220

Answer 24

60 lb/min