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P-8A PC TAINING > P-8A PC > Flashcards

P-8A PC Flashcards

1
Q

How long is a Daily Inspection good for?

A

72 hours or 24 hours after first flight

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2
Q

How long is a Turn Around good for?

A

24 hours, not to exceed the Daily

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3
Q

What chapter can you find the publications for Daily/Turnaround inspection?

A

Chapter 05 of IETMS

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4
Q

When is the aircraft washed?

A

Every 90 days during an SMI inspection

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5
Q

Where do you find the procedures to wash the aircraft?

A

IETMS: Chapter 12 or Special Inspection 90 day PC task card

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6
Q

What pin must be installed before towing the aircraft?

A

Nose wheel steering pin

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7
Q

What is locked out by installing the nose wheel steering pin?

A

Hydraulics

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8
Q

Why is it necessary to install the nose wheel steering pin before towing the aircraft?

A

If the hydraulic system gets pressurized while the nose landing gear is turned, movement can occur

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9
Q

What is the maximum turning radius of the nose wheel while pulling?

A

78 degrees

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10
Q

What is the maximum turning radius of the nose wheel during pushback?

A

75 degrees

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11
Q

How is the nose wheel turning radius indicated?

A

Placard located on NLG (the red line on the nose landing gear doors only indicates 78 degrees)

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12
Q

What is required to turn the nose wheel past 78 degrees?

A

Torsion link on the nose wheel needs to be disconnected

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13
Q

What is required to turn past 90 degrees?

A

Torsion link and taxi light assembly needs to be disconnected

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14
Q

Do all aircraft have taxi lights on the nose wheel?

A

No (168400’s-168800’s do have nose taxi lights; 168900’s and up do not)

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15
Q

What is the procedures if you need the torsion link and/or taxi light disconnected?

A

Notify Maintenance Control, and they will issue MAFs and notify the appropriate work centers

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16
Q

What must you do before and after a plane move?

A

Do a brief before and debrief after

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17
Q

How many additional people would you need to tow the P-8 if brakes cannot be charged? Who?

A

You would use 2 chock walkers until brakes are charged

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18
Q

How many personnel are required for a plane move in and out if the hangar/wash rack?

A

8

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19
Q

Why do you need to know the frequency to Ground(Tower)?

A

In case of emergency

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20
Q

What is the frequency for Ground?

A

336.4

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21
Q

What is the frequency for Maintenance?

A

361.3

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22
Q

What is the frequency for Ground (flight ops)

A

340.2

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23
Q

What breaker has to be pulled to establish COMMS with Base when media is NOT loaded?

A

COMMS 3 for Alt UHF radio

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24
Q

What safety precaution should be taken when performing HF checks?

A

A safety observer should be outide the aircraft safety diamon to ensure no one touches the skin

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25
Q

What do you annotate on the A-sheet?

A

-PC signature
-Oil ounces added
-Oxygen pressure for Crew and Passenger
-Fuel Load
-Fuel Type
-PCMCIA S/N

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26
Q

What do you annotate on a Daily Check if you find a Discrepancy?

A

JCN/MCN and system reason, prior to signing off

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27
Q

When do we change the PCMCIA Card?

A

POST flight, and again in preflight

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28
Q

What are the three lights on the MFDAU?

A

-FDAU fail
-FDAU Caution
-Digital Flight recorder Fail

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29
Q

How long does it take the PCMCIA card to initialize?

A

3-5 minutes

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30
Q

What SIX conditions do you check for on the internal RCDR status page?

A

-Media Installed - YES
-RCDR Ready - YES
-Write Enable - YES
-Media Low - NO
-Media Full - NO
-Write Fail - NO

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31
Q

In what publication do we find hand signals?

A

NA 00-80T-113

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32
Q

How long after landing should you wait before checking tire pressures? Why?

A

2 hours because they need to cool to get an accurate reading

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33
Q

What is the form number for the Aircraft Inspection and Acceptance Record (A-Sheet)?

A

4790/141

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34
Q

What is the form number for the DTA?

A

4790/38

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35
Q

What is the form number for the PC Designation?

A

4790/158

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36
Q

What is procedure 1 of the Daily inspection?

A

Record outside air temperature for use later

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37
Q

Which flight controls are you inspecting for cracks, corrosion, and loose or missing hardware?

A

Flaps, Ground and Flight Spoilers, Ailerons, Slats, and Krueger Flaps

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38
Q

When inspecting the weapons bay and weapons are not loaded, what do you have to ensure?

A

the power switch is set to off and BRU hooks are open

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39
Q

What do you wipe the strut and actuator cylinders with?

A

DMS3-32 (type II)(also known as Aero 40)

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40
Q

Can you service a disconnected IDG?

A

No

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41
Q

Can you check IDG oil on a disconnected IDG?

A

No, you will not get an accurate reading

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42
Q

What lights are required to operate for flight?

A

All exterior lights and all emergency lights. (emergency lights, wing tip strobes, red and green position lights, Anti-collision lights, retractable and fixed wing landing lights, taxi lights, runway turnoff lights, and wing illumination lights)

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43
Q

How many DC volts are you looking for on the DC meter?

A

22-30

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44
Q

During the Turnaround Inspection, what condition are you looking for when inspecting the 12 person life raft?

A

That it is secure

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45
Q

Why must you use your body weight on the seat when adjusting the recline function?

A

If you don’t have body weight in the seat while moving it, damage can occur

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46
Q

Where is the PCMCIA card installed?

A

MFDAU (Multi-function Data Acquisition Unit)

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47
Q

What does PCMCIA card stand for?

A

Personal computer memory card international association

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48
Q

What are the servicing limits for the Hydraulic System?

A

The reservoir gauges must not pass the full mark or below the RF line

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49
Q

What should the brake precharge be?

A

1000 psi nominal pressure, or according to chart

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50
Q

What two types of power does the APU provide?

A

Pneumatic and electrical

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51
Q

What type of hydraulic fluid is used on the P-8?

A

Skydrol

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52
Q

How many hydraulic systems are there on the P-8? What are they called?

A

-System A
-System B
-Standby

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53
Q

What breakers need to be pulled before removing the PCMCIA?

A

Flight recorder AC (C9) and DC (C10) on the P18-2 panel

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54
Q

What is operated by hydraulic power?

A

-Flight controls
-UARRSI Door
-Nose Wheel Steering
-Brakes
-Landing Gear
-Weapons Bay Doors
-Thrust Reversers
-Power Transfer Unit (PTU)
-Autopilot Actuators

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55
Q

How do you service the standby reservoir?

A

Through servicing Hyd System B

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56
Q

What are the Hydraulic % limits on the flight station CDU?

A

76%-106% (at and below 76% reads RF(refill)/at and above 106% still reads 106%) (100% is full. 101%-106% is overfill)

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57
Q

Can you get an accurate yd pressure reading on the flight station CDU if flaps are down?

A

No, it will not be accurate if flaps are extended

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58
Q

Which hydraulic system is used to change the brake accumulator?

A

Hydraulic system B

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59
Q

Where is the brake accumulator located?

A

Starboard side wheel well aft bulkhead

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60
Q

What are the 2 ways to service the P-8 hydraulic systems?

A

-Hand pump in the wheel well
-Skydrol Servicing Unit (SSU)

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61
Q

What is the preferred method to service the Hydraulic Systems on the P-8 according to the ULSS?

A

Hand pump

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62
Q

Can you drop flaps using electric hydraulic pumps with a 1000 lbs of fuel in each Main tank?

A

No, because you need a minimum of 1675 lbs of fuel to use the Hydraulic pumps or else you will cause damage to the Hydraulic system. Hydraulic cooling.

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63
Q

How do you properly open the weapons bay door (from what location)?

A

From the ground maintenance panel

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64
Q

Can we open the weapons bay door from the flight station? Why or why not?

A

Using flight station commands a higher rate flow for the hydraulic system that the electric pumps cannot provide. The flight station switch may only be used with engines online (engine driven hyd pumps) or with a hydraulic power cart. It can damage the pumps.

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65
Q

What pin must be removed before clearing WBDDS (weapons bay) faults?

A

Weapons bay door pin

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66
Q

How many fire bottles does the APU have?

A

1

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67
Q

What is the procedure of the DC boost pump on APU startup?

A

A dc-operated APU fuel boost pump is installed to ensure positive fuel pressure to the APU fuel control unit. During APU start and operation, the pump operates automatically when the aircraft fuel system pressure sensors detect low fuel pressure. The pump shuts off automatically when an ac fuel pump pressurizes the fuel manifold. If the ac and dc fuel pumps are not operating fuel is suction fed from the No. 1 tank.

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68
Q

APU oil:

A

Full:5.7
Add: 4.3
Low: 3.8

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69
Q

What is done prior to starting the APU?

A

Verify in ADB power can be applied.

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70
Q

What type of landing gears are found on a P-8?

A

Tricycle type with air/oil shock struts

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71
Q

How do you identify brakes are worn?

A

When one of the four brake wear indicator pins are flush when brakes are set.

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72
Q

When are tires required to be replaced?

A

If it has a soft spot, bulge, crack or cut showing cord, flat spot showing cord, tread worn beyond limits, tire pressure drops 10% below nominal pressure.

73
Q

How many shimmy dampers are located on the P-8? Where are they located?

A

Two, one on each Main landing gear
The nose wheel steering acts as the shimmy dampener on the nose

74
Q

What are the brakes on the P-8 made of?

A

Carbon fiber

75
Q

What is the purpose of the retention cable?

A

It holds the brakes on the mains together

76
Q

Where are the emergency tire deflator kit located?

A

On front of w/c 120 (airframes)

77
Q

What pins are installed/removed for engine turns?

A

Installed: both MLG and NLG
Removed: Nose wheel steering, Weapons bay, both Thrust Reversers, ALE-47, Aft bailout door

78
Q

Are chocks installed during turns?

A

Yes

79
Q

When is it recommended to Wipe Struts?

A

After flight, prior to fueling

80
Q

What are the tire pressure limitations?

A

Mains: 224 +/- 5 PSI (no action required)
Nose: 208 +/- 5 PSI (no action required)

81
Q

What is the purpose of the Frangible fittings? Where are they located?

A

IF a damaged tire is retracted into the wheel well, it will hit the frangible fitting, which will break and remove hydraulic pressure from the MLG actuator. They are located adjacent to MLG wheel well on both poet and starbord side.

82
Q

How can you tell if a torque trip indicator is tripped?

A

The center is extended, not flush.

83
Q

What is the hight of the P-8?

A

42’9”

84
Q

What is the wingspan of teh P-8?

A

123’6”

85
Q

How long is the P-8?

A

129’6” without the MAD Boom
131’2” with the MAD Boom

86
Q

What does the SPDS CDU stand for?

A

Secondary power distribution System Control Display Unit

87
Q

How many degrees do the flaps extend to?

A

40 degrees

88
Q

how many spoilers are located on the P-8?

A

12, 6 on each wing

89
Q

How many BRU stations are located on the P-8?

A

11

90
Q

Where is BRU 3 and 4 located on the P-8?

A

On the belly

91
Q

How many MWS sensors are on the P-8?

A

6

92
Q

How many static Wicks are on the P-8?

A

19 (wings: 4 on each, horizontal stab: 3 per side, vertical stab: 5)

93
Q

How many potable fire extinguishers are on the P-8?

A

6

94
Q

How many walk around oxygen bottles are on the P-8?

A

6

95
Q

How many life rafts are on the P-8?

A

2

96
Q

How many LPU’s should be on the P-8?

A

12 minimum

97
Q

How many Survival Suits (Viking suits) are on the P-8?

A

21 or 22 (depending on if ere are 5 or 6 MCW’s)

98
Q

How can you tell if Crew and Passenger Oxygen is in limits per IETMS?

A

Compare PSI with OAT in Oxygen servicing limits chart

99
Q

Where can you find the OAT?

A

Flight Station center CDU

100
Q

Can you use the same solution to clean inner and outer flight station windows? What is the solution?

A

No.
Inside: lint free, Castile soap and deionized water
Outside: lint free, 50/50 mis of alcohol/deionized water

101
Q

Who id the 8th person required for moving a plane into the hangar?

A

An e-6 Safe for flight or a Maintenance Chief

102
Q

What is the procedure for a tow bar separation while pulling?

A

The driver would pull off at a 45 degree angle and the director would signal the brake rider to slowly apply brakes.

103
Q

What is the procedure for tow bar separation while pushing?

A

The director would signal the driver to apply brakes, and then signal the brake rider to slowly apply brakes.

104
Q

Why do we tow the P-8 10 feet in a straight line after a turn?

A

To release torsional loads on the main mounts.

105
Q

What happens when one one horn blows?

A

All horns blow

106
Q

How fast do we tow the aircraft?

A

No faster than the slowest wing/tail walker

107
Q

What is the correct position for the wing walker?

A

Five feet aft and outboard of the wing tip. always face the direction of the plane’s movement.

108
Q

What is the brake pressure required for towing, as per IETMS?

A

2850 psi minimum-3150 psi maximum

109
Q

Approximately how many brake applications would you get from 3000 psi?

A

Approximately 6 brake applications from 3000 psi

110
Q

How long does a fully charged brake accumulator keep the parking brake pressurized?

A

8 hours

111
Q

What would you do if you were towing the aircraft and thunderstorm condition 1 occurred?

A

The director would signal the driver and the brake rider to apply brakes, and everyone would board the plane and stay inside until T1 has been removed.

112
Q

When would you tow the P-8 from the main landing gear?

A

If your are towing with two flat tires on one main gear
Towing on soft ground
Towing up inclines more than 5 degrees

113
Q

Which lights will be on while radar is running?

A

Position red and green lights
Wing tip strobes
Anti-collision lights

114
Q

What is the frequency to Base (Maintenance Control) and Ground (Tower)?

A

361.3 Base
128.6 Ground

115
Q

Why do you need to know the frequency to Ground (Tower)?

A

In case of emergency

116
Q

What breaker has to be pulled to establish COMMS with Base when media is NOT loaded?

A

COMMS 3 for Alt UHF radio

117
Q

What safety precaution should be taken when performing HF checks?

A

A safety observer should be outside the aircraft safety diamond to ensure no one touches the skin.

118
Q

Safe distances for equipment during refuel/defuel operation
Adjacent aircraft engineer APU

A

50 ft (15 m)

119
Q

Safe distances for equipment during refuel/defuel operation
Fuel service equipment

A

measured from engine or exhaust system 10 ft (3.0 m) from fuel vent

120
Q

Safe distances for equipment during refuel/defuel operation
Ground power Units

A

20 ft (6m)

121
Q

Safe distances for equipment during refuel/defuel operation
Aircraft servicing equipment

A

Measured from the engine or exhaust system 10 ft (3.0)

122
Q

Safe distances for equipment during refuel/defuel operation
Electrical equipment that is likely to cause arcs or sparks

A

50 ft (15 m)

123
Q

Safe distances for equipment during refuel/defuel operation
Photographic equipment

A

10 ft (3.0 m)

124
Q

Safe distances for equipment during refuel/defuel operation
Battery powered equipment

A

10 ft (3 m) from fuel servicing equipment or fuel spills

125
Q

Safe distances for equipment during refuel/defuel operation
Open flames, heat sources, lighted smoking material, and any other potential ignition sources

A

50 ft (15 m)

126
Q

What is your primary job as a Plane Captain?

A

You are the first line of inspections and last line of inspections. You are to help find any discrepancies to ensure nothing was missed and they are safe to release.

127
Q

When are fuel samples required?

A

Prior to first flight of the day

128
Q

How long are fuel samples good for?

A

24 hours

129
Q

How long after fueling or moving the aircraft should you wait before sampling fuel? Why?

A

2 hours, to allow any containants to settle to the bottom of the tank.

130
Q

Who can sign for inspecting fuel samples?

A

310/110 shift supervisor
CDI
CDQAR
Qualified Aircrew

131
Q

How many fuel sample points are there on a P-8?

A

6

132
Q

Can you use the same jar for all fuel sample points?

A

No

133
Q

What do you do if a sample is bad?

A

Retain sample, drain 1 gallon, and then take another sample.

134
Q

What if the second sample is bad?

A

Notify Maintenance Control
Initiate downing MAF
Give both samples to QA

135
Q

How do you annotate a fuel sample in ADB if first sample had dirt, and second sample was good?

A

1D/2A

136
Q

In what publication do we find fuel sampling procedures?

A

NA 01-1A-35
NA 00-80T-109
IETMS
NAMP

137
Q

What is done prior to taking fuel samples or handling any hazmat?

A

Check the SDS

138
Q

Why do we check the SDS?

A

It lists hazards, required PPE, and first aid

139
Q

Where can you find the SDS?

A

In the hangar outside of QA.

140
Q

Where can you find the Fuel spill kit(s)?

A

Outside of QA
Outside Supply
Outside X51

141
Q

What is the 3% limit during fueling?

A

Air to fuel ratio to allow room for expansion.

142
Q

How do you transfer fuel using boost pumps?

A

Turn on the pump in the flight station you want to draw fuel from. Then go to the defueling statin outside on the starboard wing, open the panel and move the switch down, then go to refueling station open panel and select which tank you want fuel to go to.

143
Q

What is the proper PPE used for fuel samples and during refueling?

A

Splash proof goggles
Rubber gloves
Sleeves rolled down
Face shield
Apron

144
Q

What fuels are used on a P-8 and what are the NATO codes PER NATOPS?

A

JP-5 (F44)
JP-8 (F34)
Jet A++ (F24)
Jet-A1(F35)
Jet A (no NATO code)
J8+100 (F37) (emergency fuel)
A++100(F27) (emergancy fuel)

145
Q

What is the mas pressure for refueling?

A

55 psi

146
Q

What pressure do you drop to after you hit 90% of max fuel load in fwd and aft aux tanks?

A

90 psi

147
Q

What is the ratio fwd/aft when filling AUX tanks?

A

1/3 FWD, 2/3 AFT (example: 2k fwd, 4k aft for a total of 6k in AUX tanks)

148
Q

How many fuel tanks are located on the P-8?

A

10

149
Q

What are the tank groups on the P-8?

A

Main 1
Main 2
Center
Forward tank group (FTG)
Mid tank group (MTG)
Aft integral group (AIG)

150
Q

Can you fuel the P-8 on battery power only? if yes what are the limitations?

A

Ues,you only have 30 seconds after the fuel panel is open to hook up and begin refueling. if not the fuel valve will close and you have o close the oanel and reset the fuel valve.

151
Q

How many fuel pumps are located on the P-8?

A

7, 2 AC powered boost pumps in each main and center tank and one DC in main 1

152
Q

What must you ensure about the hose when refueling?

A

Make sure there is no tension on the hose. The hose MUST hang freely with no force on it, Tension can cause damage to the fuel receptacle and cause the hose to disconnect. Injuries and damage to equipment can occur.

153
Q

Can you start the APU during refueling operations?

A

Yes, as long as it is the initial start or restart after normal shutdown.

154
Q

Can you restart the APU if it fails during refueling operations?

A

No, wait until refueling is complete. If you dont wait damage to the APU or injury to personnel can occur.

155
Q

Which tanks must be full before filling thr FWD and AFT aux tanks?

A

Main 1
Main2
Center

156
Q

If the center tank contains more than 1,000 lbs do you fill main 1and main 2 fully?

A

Yes

157
Q

What type engines are on the P-8?

A

CFM56-7B turbofan engine

158
Q

What is the engine inlet hazard area?

A

idle: 10 ft radius from inlet and 4 ft aft of inlet. (increases 20% when winds are over 25 kts)
Breakaway: 14 ft radius from inlet and 5 ft aft of inlet

159
Q

What is the start procedure with an air start unit?

A

Pre-op all SE being used. Guide the lineman into the safety diamond. Hook up the 108, start it up and make sure power is available. Then hook up the huffer and position it correctly behind stbd wing with exhaust facing away from the aircraft. Make sure the hose is fully laid out with no kinks and make sure there is no damage, then power up unit. Then the pilot will tell you they have electrical power. Pilot will tell you to apply bleed are, then turn up engine one, after engine one is up tell your lineman to shut down and disconnect huffer and 108 and push them out of the safety diamond. Guide lineman in and out of safety diamond, then start engine two.

160
Q

What type of oil is used to service the engines?

A

MIL-PRF 23699 Mobil Jet II
Turbonycoil600

161
Q

When can you get an accurate oil servicing reading?

A

5 to 30 minutes after engine shut down.

162
Q

Why do we wait 5 minutes prior to servicing oil?

A

To allow pressure to decrease from engines.

163
Q

What conditions would we not service oil?

A

T-1 or missed the 5-30 minute window.

164
Q

How do you annotate the oil consumption sheet in ADB if oil is not serviced?

A

“NOT SERVICED”

165
Q

How do you annotate the Turnaround if oil is not serviced?

A

“SERVICING NOT REQUIRED”

166
Q

How do you annotate BLOCK 6 of the A sheet if oil is not serviced?

A

Put “0” ounces of oil added

167
Q

What instruction do we follow that explains how to properly annotate/calculate oil consumption?

A

Oil analysis and Consumption Monitoring Program NAMPSOP (found on CPRG Sharepoint)

168
Q

Do we service engine oil after ground maintenance turns? Why?

A

No. Ground maintenance turns do not usually heat engine oil enough to get an accurate reading on servicing gauge, and oil consumption is based on flight hours.

169
Q

When do you stop servicing engine oil?

A

When you reach the lower fill mark on the servicing gauge.

170
Q

How do we know if there is sufficient engine oil for flight when we cannot get an accurate reading on the servicing gauge?

A

The oil qty on the flight station CDU (note: Max reading is 19 Qts)

171
Q

Why does engine 2 hold more oil than engine 1?

A

Due to the dihedral of the wing

172
Q

What is required to be locked out prior to opening the engine cowling doors during the daily inspection?

A

Standby hydraulics and leading edge.

173
Q

How do you know if an IDG was disconnected?

A

A click is felt when pulling IDG disconnect reset ring

174
Q

What is the emergency procedure for an APU fire during refueling? (Ref. A1-P8AAA-NFM-000)

A

Stop fueling operations
Perform an emergency shutdown of the APU if it does not shut down automatically
Notify personnel on board the airplane, airport fire services, and maintenance

175
Q

What is the emergency procedure during APU fire if crewmember(s) are inside the aircraft? (Ref. A1-P8AAA-NFM-000)

A

APU fire switch–Pull, rotate to the stop, and hold for 1 second
APU switch–OFF

176
Q

What is the emergency procedure during APU fire is crewmember(s) outside the aircraft? (Ref. A1-P8AAA-NFM-000)

A

Proceed to APU Ground control Panel in right wheel well
HORN CUTOUT switch–Push
Fire Warning light–Confirm illuminated
APU Fire Control handle–Pull down
BOTTLE DISCHARGE–Push left

177
Q

Where is the Battery Thermal Runaway Spill Kit?

A

Outside w/c 220

178
Q

Where is the AED?

A

Duty Office

179
Q

What is the emergency procedure for a fuel spill? (Ref. A1-P8AAA-NFM-000)

A

Stop fueling operations
Secure APU
Notify fire department and maintenance control

P-8A PC TAINING (2 decks)

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