Normal Ops Flashcards

1
Q

What is the minimum battery voltage for take-off?

A

The minimum batteries voltage allowed for takeoff is 24 VDC.
Replace battery if voltage is less than 22 VDC. If battery voltage is between 22 VDC and 24 VDC, recharge (in airplane) or replace the battery and rerun the battery test.

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2
Q

How long must you motor an engine if fuel has been introduced during engine start?

A

30 seconds. On subsequent start, it is acceptable to have flames out the tailpipe for a few seconds due to residual fuel.

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3
Q

How long must you wait until restarting an engine?

A

Before attempting ground restarts, wait 30 seconds after NG reaches zero (0) to enable a successful test of the NG
independent overspeed protection circuit.

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4
Q

What is the minimum bleed air pressure for starting engines?

A

Minimum bleed air pressure for sustaining a start is 22 PSI. A momentary drop below 22 PSI when the starter valve
opens is acceptable

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5
Q

How long must you wait if pusher test fails to try again?

A

5 minutes

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6
Q

When should you turn Engine AI to ON?

A

Icing conditions may exist when the total air temperature is 10°C or less and visible moisture is present in any form (clouds, fog with visibility of 1 mile or less, rain, snow, sleet, or ice crystals). In these conditions, turn ON engine anti-ice

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7
Q

If engine anti-ice is required and pressure altitude is greater than 3,000 feet, how long should you run the engines for with Engine anti ice on?

A

Consider operating with engine anti-ice ON
for a minimum of 3 minutes to stabilize engine temperatures before applying takeoff power, in order to reduce the possibility of an ENG 1 (2, 3, or 4) MGT HI (W) ACAWS event when takeoff power is applied.

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8
Q

On a normal takeoff, the takeoff data assumes that you will rotate at what rate?

A

3 degrees a second.

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9
Q

To avoid side slip control difficulties during an adjusted maximum effort climb, what should you limit your angle of bank to?

A

To avoid side slip control difficulties during an adjusted maximum effort climb, limit angle of bank to 20 degrees until airspeed is above 120 knots.

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10
Q

What is the procedure for a max effort take off after brake release?

A

After brake release, accelerate to rotation speed and execute a pitch up to 7 degrees pitch attitude (approximately 5 degrees per second rotation rate). When the airplane is airborne, as confirmed by the copilot, the pilot must immediately resume the 5 degrees per
second pitch rate to the target pitch attitude.

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11
Q

What is the flap retraction schedule for a normal climbout?

A

<100,000 lb
Raise flaps passing FUSS, (135 KIAS)

100,000 to 140,000 lb
Begin flaps retraction at 135 KIAS and
end at FUSS, (VOBS +25)

>140,000 lb
Raise flaps in 10% increments for each
5 kt increase in airspeed, beginning at
Minimum Flaps Retraction Speed (V
OBS+5) and ending at FUSS (VOBS +25)
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12
Q

How do you calculate FUSS on a max effort climb?

A

VOBS+45

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13
Q

What equipment must be operational before entering RVSM airspace?

A
CADC 1
CADC 2
SPTU 1
SPTU 2
Pilot PFD
Copilot PFD
One autopilot, including altitude hold
Altitude alert system
IFF, including Mode C
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14
Q

What are the RVSM altitude requirements?

A

With altitude hold engaged, the autopilot must maintain airplane altitude within ±65 feet of the assigned RVSM flight level during normal cruise (steady, level flight in non-turbulent conditions). The maximum difference between pilot and copilot flight level cannot exceed 200 feet.

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15
Q

How is a penetration descent made?

A

A penetration descent is made in two segments. The first from altitude down to 20,000 feet at speeds for maximum lift over drag with power levers at FLT IDLE and landing gear and flaps retracted. The second segment is from 20,000 feet to sea level at a constant 250 KIAS.

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16
Q

When should the approach checklist be completed by?

A

The Approach checklist will be completed prior to traffic pattern entry or before commencing any type of instrument approach.

17
Q

What should you set your radalt to?

A

Precision - 150
Non-precision- 250
Circling - 300

18
Q

What is the maximum pitch attitude during touchdown?

A

6 degrees

19
Q

What is the Power Lever limitation speed when touching down?

A

145KTS

20
Q

When should you consider high speed landing limitations

A

100% flaps landings at weight above 155,000 pounds.
50% flaps landings at weight above 130,000 pounds.
All 0% flaps landings.
Temperature at or below ISA +15 °C, all landings at field elevation greater than 4,000 feet MSL.
Temperature greater than ISA +15 °C, all landings at field elevation greater than 2,000 feet MSL.

21
Q

What are some high speed landing considerations?

A

Power level limitation speed (145), nose tire speed (139), PM should verbalize “4 Bs”,

22
Q

What is the maximum crosswind component for landing?

A

35 knots

23
Q

What is max crab angle when landing?

A

5 degrees

24
Q

What is the maximum effort performance based on?

A

First 500 feet of the runway. Assume max anti skid braking and full 4 eng reverse to the full stop

25
Q

If full anti skid braking is used, how much time must pass before retracting the gear or a subsequent application of brakes for landing

A

At least 15 minutes

26
Q

How much time must elapse after a full anti-skid braking application at weights above 130K?

A

65 minutes

27
Q

What conditions are conducive for wind shear?

A

Passage of cold fronts, temp change of 5.5C, if front is moving at 30KT or more, and if thunderstorms are present.

28
Q

What are some indications of wind shear?

A

+/- 20 knots of airspeeds, 500fpm altitude changes, 6 degrees of attitude changes, 1.5 dot GS deviation

29
Q

What is the wind shear recovery procedure?

A
  1. Set TAKEOFF power and level the wings.
  2. Pitch immediately to 15 degrees nose up, then adjust pitch to maintain approximately 10 knots above the stall warning caret.
    (If at high airspeed, ensure G limit is not exceeded.)
    WARNING
    In moderate or severe turbulence, more than 10 knots above the stall warning caret may be required to prevent inadvertent stick pusher activation.
  3. The pilot monitoring calls out radar altitude, airspeed, and sink rate, as appropriate.
  4. Do not change airplane configuration until the airplane is out of the alert and stabilized.
30
Q

What is the GCAS/TAWS Recovery?

A
  1. Set TAKEOFF power and level the wings.
  2. Pitch immediately to 15 degrees nose up, then adjust pitch to maintain approximately 10 knots above the stall warning caret.
    (If at high airspeed, ensure G limit is not exceeded.)
    NOTE
    When in visual conditions, establishing a pitch attitude in the HUD, where the climb dive marker is above the terrain/obstacle, will ensure terrain/obstacle clearance.
  3. The pilot monitoring calls out radar altitude, airspeed, and sink rate, as appropriate.
  4. If flaps are at 100%, ensure a positive rate of climb, and then set flaps to 50%.
  5. If gear is down, retract the landing gear after ground clearance is assured.
31
Q

What is the TAWS Tactical Recovery Procedure?

A

WARNING
In TACTICAL mode, the TAWS Warning alert envelope is based on a radius of turn at 45 degrees angle of bank. A
bank angle less than 45 degrees may be used at pilot discretion, while visually ensuring obstacle or terrain avoidance.

  1. Execute the GCAS/TAWS PULL UP Alert Recovery procedure, or
  2. Execute an immediate turn, using up to 45 degrees of bank, to establish a ground track that ensures obstacle or terrain avoidance.
32
Q

When do you complete the Approach Checklist when doing Touch and Gos?

A

The first TNG and then only if landing at a different airfield than already briefed

33
Q

What pitch does the FD command to fly to in a go around?

A

7 degrees.

34
Q

What is the Go Around procedure?

A
  1. Announce “Go-around” to the crew and press the G/A switch on the control wheel for go-around flight director guidance.
  2. Select TAKEOFF power, as necessary.
  3. Raise the nose to the flight director cue or higher, as necessary, and then direct the copilot to set/check flaps to 50%.
  4. Check that the side slip and side force is low, ensure positive rate of climb, and call for landing gear retraction.
  5. Complete flaps retraction and climbout in accordance with normal takeoff procedures.
35
Q

How long should the APU be on speed after landing before opening the bleed air valve?

A

1 min

36
Q

How long should LSGI be selected for before shutting down the engine?

A

2 minutes

37
Q

When must a no drop be called if checklists are incomplete?

A

If the run-in checklist is not done by the

“Standby drogue” call for HE towplate or 5 second call during other drops.

38
Q

What is the standard holding speed?

A

170KTS