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Treatise > Normal Procedures > Flashcards

Normal Procedures Flashcards

1
Q

If the Aircraft will not accept external power and the ground power unit checks good, _______ may actuate necessary relays to allow the aircraft to accept external AC power. (TO 1T-38C-1TO: 2-2)

A

Cycling the battery switch OFF then ON

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2
Q

Upon initial inspection of the nose gear tire, you see one cord on the nose tire sidewall. Is this acceptable?

A

No, 0 cords may be visible on the nose tire sidewall. (TO 1T-38C-1TO: 2-7)

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3
Q

Upon initial inspection of the hydraulic fluid indicator, you see that the fluid is above the upper line. Is this acceptable? (TO 1T-38C-1TO: 2-9)

A

Yes, fluid level above the upper line is acceptable for flight.

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4
Q

tire px check is good for

A

6 hours

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5
Q

Do not operate the seat adjust switch for more than _____ minute(s) during any 8-minute period.

A

1 minute. (TO 1T-38C-1TO: 2-13)

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6
Q

If battery voltage is less than ____ VDC, the EED display powers up at full brightness regardless of switch position and reverts to selected brightness when the first generator comes on line. (TO 1T-38C-1TO: 2-16)

A

22 VDC

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7
Q

During engine start, if EGT does not begin to rise within 12 seconds after the first indication of fuel flow, _______. (TO 1T-38C-1TO: 2-18)

A

Abort the start, maintain airflow on the engine for 2 minutes

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8
Q

If unsafe gear indication occur after engine start (Stall Warning, Break-X, loss of AoA Symbol), what action should be taken? (TO 1T-38C-1TO: 2-18)

A
  1. Do not touch the gear lever
  2. Shut down the engines as soon as possible
  3. Have the gear pins installed
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9
Q

Sufficient cooling airflow for the pitot static system is generated at _____ knots. (TO 1T-38C-1TO: 2-18)

A

25 knots

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10
Q

During the TAKE OFF TRIM test, ensure at least _____ of stick travel before repositioning the trim.

A

½ inch. (TO 1T-38C-1TO: 2-19)

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11
Q

The flap system should indicate 60% +/- _____% during the Before Taxi Checklist. (TO 1T-38C-1TO: 2-19)

A

+/- 5%

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12
Q

Nosewheel tires are severely damaged when maximum rudder deflection turns are attempted at ground speeds in excess of ______ knots. (TO 1T-38C-1TO: 2-27)

A

10 knots

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13
Q

To prevent possible damage to the canopy downlock mechanism, what canopy configurations should be used to the max extent practical? (TO 1T-38C-1TO: 2-27)

A

Both canopies open or both canopies closed

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14
Q

Allow a minimum of ___ minutes before takeoff behind a large type aircraft or helicopter, and ____ minutes behind a heavy type aircraft. (TO 1T-38C-1TO: 2-29)

A

2 minutes, 4 minutes

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15
Q

A crosswind component of over ___ knots may reduce the interval time for wake turbulence.

A

5 knots. (TO 1T-38C-1TO: 2-29)

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16
Q

The takeoff should be aborted if either afterburner fails to light within ___ seconds or if the light off is abnormal. (TO 1T-38C-1TO: 2-29)

A

5 seconds

17
Q

Wheel braking is limited to cautious braking from _____ to _____ KCAS, with optimum braking below ______ KCAS. (TO 1T-38C-1TO: 2-32)

A

130 to 100 KCAS, 100 KCAS

18
Q

Variation in landing technique could increase landing distance as much as _____% from that computed from the landing distance chart. (TO 1T-38C-1TO: 2-32)

A

50%

19
Q

If a tire skid(s) is detected, what immediate action should be taken? (TO 1T-38C-1TO: 2-32)

A

Immediately release both brakes and cautiously re-apply

20
Q

How do you accomplish a Minimum Roll Landing? (TO 1T-38C-1TO: 2-32)

A
  1. Flying 10 knots below final approach speed (Green Speed)
  2. Attempt to land with a 12o NH attitude
  3. Just prior to loss of elevator authority, lower the nosewheel and apply optimum braking
  4. For wet runways, firm touchdown will reduce effects of hydroplaning
21
Q

Fuel required for a Closed Pattern is approx. _____ pounds. (TO 1T-38C-1TO: 2-33)

A

150 pounds

22
Q

Define Optimum Braking. (TO 1T-38C-1TO: 2-34)

A

A single, smooth application, increasing as airspeed decreases.

23
Q

When executing a go-around, can runway contact be made if conditions do not permit an aerial go-around? (TO 1T-38C-1TO: 2-35)

A

Yes. Do not try to hold the aircraft off the runway if conditions do not permit an aerial go-around. If touchdown is made, lower the nose slightly to accelerate and establish the takeoff attitude.

24
Q

Before engine shutdown, operate the engines at ____% or below for 1 minute to allow for engine cooling.

A

70%. (TO 1T-38C-1TO: 2-36)

25
Q

For an Instrument Climb, power settings between ____ and ____ % RPM will provide comfortable climb rates at 300 KCAS for intermediate level-offs. (TO 1T-38C-1TO: 2-38)

A

90-95% RPM

26
Q

If conditions require a MAX thrust climb, maintain 2o to 5o climb until reaching recommended climb Mach, then rotate to approx. _____ to _____ o nose high climb. (TO 1T-38C-1TO: 2-38)

A

20-25o NH

27
Q

Hold at airspeeds between ____ and ____ KCAS. (TO 1T-38C-1TO: 2-38)

A

250-265 KCAS

28
Q

A Radar Approach requires approx. ___ pounds of fuel. (TO 1T-38C-1TO: 2-40)

A

325 pounds

29
Q

Crossfeeding is recommended when fuel differences exceed ____ pounds. (TO 1T-38C-1TO: 2-42)

A

200 pounds

30
Q

Crossfeed is not recommended under what conditions? (TO 1T-38C-1TO: 2-43)

A
  1. Fuel Quantity failure
  2. Fuel Leak
  3. Low Altitude (BEO)
  4. Low Fuel (BEO)
31
Q

Under low fuel conditions, how should fuel balance be managed? (TO 1T-38C-1TO: 2-42)

A

Differential power settings

32
Q

The FULL line on the Oil Dipstick equates to ____ pints of oil. (TO 1T-38C-1TO: 2-45)

A

8 pints

33
Q

Each ADD line on the Oil Dipstick is equivalent to ____ pint of oil consumption. (TO 1T-38C-1TO: 2-45)

A

1 pint

34
Q

For a standard instrument ride (1.2 hours), ensure no greater than ____ of a pint have been depleted from the oil system. (TO 1T-38C-1TO: 2-45)

A

¾ of a pint

35
Q

The oil system levels should be checked with ___ minutes of engine shutdown. (TO 1T-38C-1TO: 2-45)

A

15 minutes

36
Q

The tire pressure of the main wheel tire is ____ PSI while the nose wheel is ____ PSI.

A

265 psi, 75 psi

Treatise (12 decks)

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