Daily/Turnaround Inspectipns

Question 1

How long is the daily inspection good for?

Answer 1

A. 72 hours commencing from the date and time the inspection was completed.

Question 2

How long is a turnaround inspection good for?

Answer 2

A. 24 hours commencing from the date and time the inspection was completed.

Question 3

What would avoid a daily/turnaround inspection within a 72 hour period?

Answer 3

A. Maintenance, other than servicing; maintenance control shall determine if a complete daily or turnaround inspection or portion thereof is required.

Question 4

If the ambient temperature on the ground it’s 20°F or lower, and the fluid level in the hydraulic reservoir is below refill, what is the reservoir service to and why?

Answer 4

A. Service the reservoir just to about RFL indication. This will prevent the reservoir from being too full at a warmer location.

Question 5

A turn around/post flight inspection is conducted between flights to ensure what?

Answer 5

A. The integrity of the aircraft for flight, verify proper servicing, and to detect degration that may have occurred during the previous flight.

Question 6

Within what timeframe should you service engine oil’s?

Answer 6

A. within 5 to 30 minutes after engines have shut down

Question 7

If oil is not serviced before 30 minutes what must happen?

Answer 7

A. A work order or a MAF must be issued to operate engines and perform oil servicing.

Question 8

What does it mean if your drains from the press to test button?

Answer 8

A. There is a fuel leak between the inner and outer wall of one or more tanks.

Question 9

If the sonobuoy switch on the WBD ground maintenance panel is not set to off, what could happen?

Answer 9

A. It is possible for a sonobuoy to be launched.

Question 10

What fault code can you clear on the WBD without issuing a MAF?

Answer 10

A. 32, 54, and 44

Question 11

If the sonobouy launching system is not depressurized during 48 hour window, what may occur?

Answer 11

A. The sonobouy rotary launcher launch tank burst disk may rupture doe to an increase in pressure.

Question 12

Without the downlock pins installed on the ground, what may happen?

Answer 12

A. The landing gear could retract and cause injuries to persons and damage to the equipment.

Question 13

The tires should be checked how long after the planes land? Can tires be checked when they are hot?

Answer 13

A. 2 hours.

B. Yes, following AMM II guidelines.

Question 14

What is the pressure for the main and nose tires

Answer 14

A. 224 +/- 5 for the main and 208 +/- 5 for the nose.

Question 15

What is the correct procedure for checking the IDG oil level?

Answer 15

A. Open the fan cowling ensuring the leading edge flaps are deactivated in the retracted position.

B. Make sure the engines have been shut down for a minimum of 5 minutes.

C. Make sure no click is felt when pulling the IDG Disconnect Reset and ensure the ring returns to the max inward position.

D. Push the PUSH-TO-VENT valve for a minimum of 15 seconds. Oil level should be above the low oil level line.

Question 16

How many times may you reset the Differential Pressure Indicator (DPI) before the UDG has to be replaced?

Answer 16

A. Once.

Question 17

How do you check the brake indicators of wear?

Answer 17

A. Ensure brakes are set and verify indicator pins are extended pass the guides. If pins are level or below the face of the guide, brakes must be replaced.

Question 18

How many proximity sensors are there in the weapons bay door area?

Answer 18

A. 8

Question 19

What do you check the tires for?

Answer 19

A. Inspection for contamination, cuts, wear, and bulges and refer to AMM task for tire inspection.

Question 20

What is the limit for the pad bolt head and the outside pad edge before the pad mush be changed?

Answer 20

A. 0.06 inches or less

Question 21

What should you look for on the wing bomb rack units that is not currently updated in the AMM chapter 5, and where can the information be found?

Answer 21

A. It is recommended to inspect the BRU Swaybrace Springs for cracks and damage during the scheduled BRU inspection tasks. BRU swaybrace leaf spring failure guidance and disposition in maintenance control P-8A deviation binder.

Question 22

When performing a Daily/Turnaround inspection, a squadron plane captain noticed a particular part of the engine fan was sticking up from its normal position. Which portion of the engine was this? The plain captain simply pushed this part back down, and did not tell anyone. Would you consider his/her actions acceptable behavior? What could have happened because of the action that this plain captain took?

Answer 22

A. The platform

B. No, use integrity and immediately inform the FLC or maintenance control. Always have a questioning attitude.

C. The platform was not seated correctly, and it could become dislodged or cause catastrophic engine failure.

Question 23

Recently, there have been documented issues with the in-flight recording system which are induced by placing what switch to the “off” position? What position should we leave the switch in?

Answer 23

A. The Cockpit Voice Recorder Auto/Off position switch.

B. Leave the switch in “auto.”

Question 24

If the first aid kits are not at their assigned location, where can they typically be found?

Answer 24

A. In the cubbies under the vacuum.

Question 25

When you look at the CMDS blank off plate, what should the hardware look like?

Answer 25

A. Flush with the CMDS blank off plate surface.

Question 26

What chapter of the AMM II is the Daily/Turnaround inspection found in?

Answer 26

A. AMM II chapter 05 time limits / Maintenance checks.

Question 27

If you are examining the sonobouy chute and you see a sonobouy, what is wrong and what should you do?

Answer 27

A. The SRL and SSL gate valve is stuck, and the door is open. Inform the FLC, Maintenance control, and the ordnance shop.

Question 28

What is a common discrepancy in regard to the DIRCM?

Answer 28

A. The mesh vents are often torn or degraded.

Question 29

What is the process of swapping the PCMCIA card? Who can Sign the work order or MAF off?

Answer 29

A. Ensure the card is removed, turned into Maintenance control, and replaced with a blank card.

B.remove power from the FLIGHT RECORDER AC and the FLIGHT RECORDER DC. Open the access panel for the MFDAU by pushing down on the latch. Push the button below the slot to eject the PCMCIA Card. Turn the old card into maintenance control. To install the new card, align the PCMCIA Card with the slot, with the directional arrow in the right side. Carefully push the card into the slot. Make sure that you fully engage the card in the slot. Close and latch the access door. Do the replacement conformation. Close the FLIGHT RECORDER AC and the FLIGHT RECORDER DC circuit breakers. Wait five minutes. In the flight compartment. , push the MENU button on an FMCS MCDU. Push the NEXT button. Push ACMS LSK. Push the VERSIONS AND STATUS LSK. Push the DEVICES INTERFACES LSK. Push the PCMCIA STATUS LSK. Make sure that you see three yes’s followed by three no’s. Put the airplane back to it usual condition.