# How Much Do You Actually Know About Landing An F-18 On An Aircraft Carrier?

Approved & Edited by ProProfs Editorial Team
The editorial team at ProProfs Quizzes consists of a select group of subject experts, trivia writers, and quiz masters who have authored over 10,000 quizzes taken by more than 100 million users. This team includes our in-house seasoned quiz moderators and subject matter experts. Our editorial experts, spread across the world, are rigorously trained using our comprehensive guidelines to ensure that you receive the highest quality quizzes.
| By Steven.e.shaw
S
Steven.e.shaw
Community Contributor
Quizzes Created: 1 | Total Attempts: 105
Questions: 10 | Attempts: 105

Settings

.

• 1.

### What is the total angular coverage of the IFLOLS?

• A.

1.0°

• B.

1.3°

• C.

1.7°

• D.

2.2°

C. 1.7°
Explanation
There are 12 cells on the IFLOLS, 10 yellow and 2 red. Each yellow cell has an angular coverage of .13°, and each red cell covers approximately .2°. For a 3.5° Basic Angle, the top of the top cell is angled at 4.28° and the bottom of the bottom red cell is angled at 2.58°.

Rate this question:

• 2.

### From where on the IFLOLS does the Basic Angle emanate

• A.

Between cells 5 and 6

• B.

Between cells 6 and 7

• C.

The center of cell 6

• D.

The center of cell 7

B. Between cells 6 and 7
Explanation
The IFLOLS is designed so the prescribed Basic Angle emanates from between cells 6 and 7. The datums are also aligned between cells 6 and 7. Like Paddles says, there's no centered ball.

Rate this question:

• 3.

### What is the Basic Angle under most normal conditions?

• A.

3.25°

• B.

3.5°

• C.

3.75°

• D.

4.0°

B. 3.5°
Explanation
Unless the natural winds are much stronger than 40 knots, or an aircraft malfunction requires a non-standard landing configuration, you will not typically see any Basic Angle other than 3.5°

Rate this question:

• 4.

### If you are able to maintain a centered ball, will your VSI differ between 25 knots of natural wind with no ship's movement, and 25 knots of ship's movement with no natural wind?

• A.

Yes

• B.

No

B. No
Explanation
Your VSI in both cases will be exactly the same because your closure to the ship is the same. In these examples the closure is entirely based on ship's speed OR wind speed. As you combine the two, things start to get more complicated

Rate this question:

• 5.

### Based on the table, if you are able to maintain centered ball, approximately where will you see the Velocity Vector on the pitch ladder with a 3.5° Basic Angle, 30 knots of natural wind, and no ship's movement?

• A.

-2.2°

• B.

-2.7°

• C.

-3.5°

• D.

-4.0°

C. -3.5°
Explanation
You will see the Velocity Vector at -3.5° because natural winds have no affect on where you will see the Velocity Vector on the pitch ladder. The Velocity Vector shows you only your flight path angle relative to the earth, and in this case, the ship is not moving. Like any normal field landing, if you are able to maintain a centered ball with a 3.5° Basic Angle the Velocity Vector angle will equal the Basic Angle.This makes the Velocity Vector especially useful for pilots because the only variable that will affect where you see the Velocity Vector on the pitch ladder is ship's speed. Notice in this video that even though the flight path angle through the air mass (represented by the hot air balloon) is shallowed out by windspeed, if the aircraft's flight path angle relative to the earth did not equal the Basic Angle (represented by the yellow line emanating from the carrier), the aircraft would not land in the correct spot on the flight deck.

Rate this question:

• 6.

### Based on the table, if you are able to maintain a centered ball, approximately where will you see the Velocity Vector on the pitch ladder with a 3.5° Basic Angle, 30 knots of ship's movement, and no natural wind?

• A.

-2.2°

• B.

-2.7°

• C.

-3.5°

• D.

-4.0°

B. -2.7°
Explanation
You will see the Velocity Vector at -2.7° on the pitch ladder because as the ship moves away from you, you will have to travel a greater horizontal distance over the earth to reach the touchdown point on the flight deck, decreasing your flight path angle relative to the earth.  Since the Velocity Vector shows you your flight path angle relative to the earth, you will see the Velocity Vector at -2.7° on the pitch ladder.The video below shows the same concept calculated for 25 knots of ship's speed.

Rate this question:

• 7.

### If you are at the top of the lens at the Start behind a non-moving ship with a 3.5° Basic Angle, where would you have to set the Velocity Vector on the pitch ladder to fly straight into the Round Down (hypothetically speaking)?

• A.

-4.2°

• B.

-4.6°

• C.

-5.0°

• D.

-5.4°

B. -4.6°
Explanation
A -4.64° flight path angle from a Full High Start behind a non-moving ship with a 3.5° Basic Angle will fly you straight into the Round Down.  This combination of conditions gives you the steepest angle you would ever need if you wanted to hit the back of the ship (which you should not want).  Any increase in ship's speed or decrease in Start altitude will only shallow the angle that will put you into the Round Down.The table below shows you the required flight path angles relative to the earth (where you will see the Velocity Vector on the pitch ladder) to maintain any cell at any ship's speed.  As you can see, with a 3.5° Basic Angle, there is almost no circumstance in which you would need to set the Velocity Vector to steeper than -4° or shallower than -2° on the pitch ladder.  Except in the most extreme circumstances, pilots should never allow the Velocity Vector below -4° or above -2° if they see a ball on the lens.

Rate this question:

• 8.

### What is the longest groove distance you could have in an F-18 in the normal full flaps landing configuration and still be within the optimum 15" to 18" groove length?

• A.

.3 NM

• B.

.5 NM

• C.

.7 NM

• D.

.9 NM

C. .7 NM
Explanation
Groove distance is based on closure between the aircraft and the ship. The greatest distance occurs with the greatest closure, which happens when aircraft is moving the fastest and the Recovery Headwind is the weakest. Minimum Recovery Headwind for Hornets is 15 knots, and the maximum approach speed in the normal full flaps landing configuration is 150 knots. With 135 knots of closure, an aircraft will cover .7 NM in 18".The table below show all the possible groove distances for the different allowable approach speed and recovery head wind combinations. As you can see the most common groove distance is .4 NM to .6 NM.These distances are important to know when flying a CV-1 approach because if you start flying the ball further away than you are used to from the day pattern, you are more likely to make unnecessarily large glidepath corrections, increasing the probability of an unsafe pass.  Therefore, you should not transition to the ball at night until inside .5 NM.

Rate this question:

• 9.

### Based on the table, if you are able to maintain a centered ball, approximately where will you see the velocity vector on the pitch ladder with a 3.5° Basic Angle, 15 knots of ship's movement, and 10 knots of natural wind?

• A.

-2.5°

• B.

-2.8°

• C.

-3.1°

• D.

-3.5°

C. -3.1°
Explanation
Because the Velocity Vector shows you your flight path angle relative to the earth, the only factor that affects where you will see the Velocity Vector on the pitch ladder is ship's speed. In this case, ship's speed is only 15 knots, which corresponds to a -3.1° glide path. Even though the 10 knots of natural wind contributes to 25 knots of Wind Over the Deck, it will have no affect on where you will see the Velocity Vector on the pitch ladder.

Rate this question:

• 10.

• A.

Yes

• B.

No