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KC-130J NATOPS > Ch 4 - Limitations > Flashcards

Ch 4 - Limitations Flashcards

1
Q

Fuel Weight: Tank 1 and 4 (each)

A

8310 lbs

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2
Q

Fuel Weight: Tank 2 and 3 (each)

A

7650 lbs

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3
Q

Fuel Weight: L and R Auxiliary (each)

A

5810 lbs

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4
Q

Fuel Weight: L and R External (each)

A

8900 lbs

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5
Q

Fuel Weight: Fuselage Tank

A

24,390 lbs

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6
Q

Fuel Weight: Total Internal and External (with fuselage tank)

A

85,730 lbs

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7
Q

Fuel Weight: Total Internal and External (without fuselage tank)

A

61,340 lbs

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8
Q 
Avoid abrupt or full rudder deflection with flaps lever positioned \_\_\_\_\_
or greater (high rudder boost) and airspeed \_\_\_\_\_ or greater
A

15%, 210 KIAS

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9
Q

With FLAP extension, maximum load factor is _____ in symmetrical maneuvers and _____ in unsymmetrical maneuvers

A

2.0 g and 1.5g

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10
Q

Prohibited Maneuvers

A
  1. Aerobatics and spins.
  2. Practice stalls with power above 1,000 HP.
  3. Practice asymmetric power stalls.
  4. Intentional zero or negative G maneuvers lasting longer than 7 seconds.
  5. Sustained airspeed below stick pusher speed.
  6. Intentionally maneuvering the aircraft into a sideslip for a LEFT/RIGHT RUDDER alert.
  7. Abrupt longitudinal control inputs at high speeds (faster than 1.0 g per second load factor increase or decrease).
  8. Rapid roll reversals (roll rate shall be zero momentarily before applying full aileron in the opposite
    direction).
  9. At airspeeds above 150 KIAS, moderate to large rudder input held until sideslip peaks followed by opposite rudder (past neutral) or a series of large alternating rudder inputs tending to produce successively larger
    sideslip angles.
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11
Q

If bleed air is available from another operating engine, a starter assisted air start can be accomplished at any airspeed less than approximately ___ KIAS (NG below ___). If bleed air is not available or if the engine starter is not functional, maintain NG between _____. If the propeller is windmilling at ___ NP, NG will stabilize at ___ at speeds as low as _____. If the propeller is feathered, speed as high as 200
to 250 KIAS may be required to achieve the required 15 percent NG.

A

250 KIAS, 29%, 15 and 29%, 100%, 15%, 110-130 KIAS

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12
Q

Propeller Aux Pump Operating Limits:

  • Static Prop Feathering: ___ cycles
  • What is a cycle:
  • Feathering command limitations:
  • What is counted for feathering command:
A

-2 cycles
-A cycle is counted each time the aux feather pump is used to drive the propeller from feather to reverse to feather.
-Feathering is limited to four commands
-A feather command is counted each time the FIRE handle is pulled or the
PROPELLER CONTROL switch is placed to FEATHER.

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13
Q

Takeoff Crosswind and Tailwind Restrictions

A

If the aircraft is not pointed into the wind ±45° (i.e., wind is from 045° to 315°) and wind is greater than 15 but less
than 35 knots, the limitation is 2,500 HP max until indicated speed is greater than 35 knots.

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14
Q

Windmilling Propeller Limitation: Do not allow the engine to turn at less than ___ NG for greater than ___ , or greater than ___ NG for
___ with a propeller feathered (propeller is visibly rotating at less than one half revolution per second) with
oil supplied (FIRE handle in). Slow rotation of the engine causes oil to pool in the sumps and subsequent restart may result in an engine fire. An airspeed of ___ should ensure the gas generator rotor is turning fast enough
(greater than ___ NG) to ensure the power section lube scavenge pump is rotating fast enough for the pump to scavenge the center sump.

A

7%, 3 min, 7%, 20 min, 165 KIAS, 7%

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15
Q

To ensure sufficient liferaft capacity, no more than ___ persons, including crewmembers, should be carried on
extended over-water flights that operate more than ___ nautical miles from the nearest shore line.

A

80, 50

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16
Q

Define high strength airfields

A

High strength airfields are paved runways considered to be either R/rigid (concrete paved) or F/flexible (asphalt paved).

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17
Q

Define marginal strength airfields

A

Marginal strength airfields are temporary airfields which include minimally surfaced and unsurfaced runways such as dirt, grass, gravel, coral, etc.

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18
Q

Define substandard airfields

A

Substandard airfields may be either paved or unpaved, and are those which have unusually rough, undulating, pitted, or rutted runways.

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19
Q

With a feathered propeller (less than one half revolutions per second), and no oil supply (FIRE handle pulled),
maximum time before an air start is up to ___. If the engine can be restarted before these time limits expire, the
engine should be operated for a minimum of ___ at FLIGHT IDLE to circulate the oil.

A

6 hours, 20 minutes

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20
Q

APU Door Operation

A

9-18 sec

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21
Q

APU Start Light on speed

A

35 sec

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22
Q

APU Normal RPM

A

98-105%

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23
Q

APU Maximum RPM

A

110%

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24
Q

APU EGT

A

260 to 680 °C normal, 710 °C maximum

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25
Q

APU Limits: Bleed Air Pressure

A

40 to 50 psi

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26
Q

APU Limits: Bleed Air Pressure check, 30-15 PSI

A

Not less than 22 seconds

27
Q

APU Limits: Voltage

A

108-117

28
Q

APU Limits: Load

A

0-100

29
Q

Fuel Boost Pump Pressure: Auxiliary

A

28 to 40

30
Q

Fuel Boost Pump Pressure: External

A

28 to 40

31
Q

Fuel Boost Pump Pressure: Main

A

15 to 24

32
Q

Fuel Boost Pump Pressure: Transfer

A

28 to 40

33
Q

What is considered fuel unbalanced

A

> 1,000 lb between symmetrical pair

>1,500 lbs between wings

34
Q

When is emergency fuel allowed and for how long?

A

Emergency fuel shall be used only to allow the aircraft to proceed to a base where primary fuel is available. Aviation
fuels used as emergency fuels are restricted to one-time flight of not more than 6 hours.

35
Q

Autopilot Limitations:

A

Do not operate with the autopilot engaged during the following situations:
1. Takeoff and landing.
2. At airspeeds above maximum recommended airspeed VH.
3. ILS coupled approach below 200 feet HAT (CAT I), 100 feet HAT (CAT II), below MDA on a non-precision
approach, or when flying over the localizer transmitter.
4. During IPRA coupled approach below 200 feet HAT.
Note
During approach with any engine(s) inoperative, do not operate with the
autothrottles engaged. An autopilot coupled approach can be flown with
the engine(s) inoperative if manual, symmetric power changes are made.
5. At or below 500 feet AGL for nonapproach operations.
6. In RVSM airspace, unless the autopilot, in ALT HOLD mode is able to maintain altitude within ±65 feet of
ATC assigned flight level (steady, level flight in non-turbulent conditions) at all times during normal cruise.
7. At gross weights above 164,000 lbs for any of the following:
a. Below 1,000 feet AGL.
b. During configuration changes.
c. During approach operations.

36
Q

Windmilling Prop Limit NG <7% with fire handle IN

A

3 minutes or accelerate to greater than 7% (165 KIAS) or pull the fire handle

37
Q

Windmilling Prop Limit NG >7% with fire handle IN

A

20 minutes or pull the fire handle

38
Q

Windmilling Prop Limit Prop windmilling at 100% with fire handle IN

A

5 minutes or pull the fire handle

39
Q

If the propeller is windmilling (greater than one half revolution per second) with oil supplied (FIRE handle in) the engine should be started before ___ minutes and the engine operated at flight idle for at least 5 minutes to scavenge the oil sumps. If any of the time limits are exceeded maintenance action is required. If a greater emergency exists and the engine must be restarted, recommend flight idle for 5 minutes to scavenge the
pooled oil.

A

5, 5

40
Q

AFCS IAS Hold Accuracy?

A

±3 KIAS

41
Q

AFCS VS Hold Accuracy?

A

±70 fpm at 1,000 fpm

42
Q

AFCS ALT SEL Accuracy

A

±40 feet with ±75 foot overshoot at 1,000 fpm (ALT Hold 40 as well)

43
Q

Airspeed indicators must agree within:

A

±6 KCAS

44
Q

Static reading at field elevation must agree within:

A

±50 feet of field elevation

45
Q

HUD/PFD, and standby compass headings must agree within:

A

±5

46
Q

Oil Quantity White Readout

A

4 to 14.1 gallons

47
Q

Cabin altimeter (zero differential at field elevation)

A

±500 feet of actual field pressure altitude

48
Q

Hydraulic System Pressure White Readout

A

2,900 to 3,200 psi

49
Q

Emergency Brake Pressure White Readout

A

2,900 to 3,300 psi

50
Q

Oxygen Quantity White Readout

A

5 to 25.0 liters

51
Q

Oxygen Regulator Pressure for Continuous Breathing

A

270 to 340 psi

52
Q

Oxygen Regulator Pressure for No Flow

A

270 to 455 psi

53
Q

Outflow valve differential control

A

14.3° ±0.2° in. Hg

54
Q

Safety valve

A

15.0° ±0.3° in. Hg (do not exceed 16.0 in. Hg)

55
Q

Negative pressure relief

A

-0.76 in. Hg

56
Q

Negative pressure limit

A

Do not exceed -1.6 in. Hg

57
Q

Max Cabin Differential Pressure

A

15.2 in. Hg

58
Q

Max % of load for AC Gen and Ess and Main DC Buses

A

0-125%

59
Q

Starting MGT of ___ C for a maximum of ___ sec is permitted. If exceeded, over temperature inspection required

A

807, 2

60
Q

Engine starts prohibited when oil temperature is ___ C or below

A

-40

61
Q

Prior to start maximum MGT is ___ C

A

175

62
Q

Transient operations up to ___% during transition from flight idle to ground idle is acceptable

A

112

63
Q

Takeoff permitted with an oil temperature of ___ C

A

45

64
Q

Maximum horsepower for normal operation is limited to _____

A

4840 HP

KC-130J NATOPS (4 decks)

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