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CC130J > Limitations > Flashcards

Limitations Flashcards

1
Q

What are the maximum normal and maximum alternate take-off weight limits?

A

164 000 and 175 000

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2
Q

What are the recommended, normal and alternate landing weight limits?

A

162 286, 164 000 and 175 000

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3
Q

What are the max fuel tank weights for taxi and take-off?

A

No 1, 4 - 8310
No 2,3 -7660
Aux - 5810
Total: 43 560

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4
Q

Describe Primary Fuel Management?

A

No 1 and 4 contains, 500-1000 more than tanks 3 and 4 except when total fuel is less than 6000.
No 1 and 4 have at least 7060 and 2, and 3 have at least 6400 with any usable fuel in the auxes

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5
Q

If severe turbulence is unavoidable what is the recommended airspeed?

A

Flight should be in the range of 65 KIAS above power off stall flaps up speed not to exceed 181 KIAS.

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6
Q

What are the flap speeds?

A 
20% - 210
30% - 200
40% - 190
50% - 183
60% -165
70% - 155
80%- 150
90% - 145
100 % - 145
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7
Q

What is the landing gear speed?

A

168

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8
Q

What is the landing light extended speed?

A

250

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9
Q

What is the ramp open speed?

A

250

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10
Q

What is the paratroop Air Deflectors Open Speed?

A

150

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11
Q

What is the inoperative windshield anti-icing below 10,000 feet speed?

A

187

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12
Q

What is the max HP in order to move the aircraft with an obstructed gear?

A

2585HP

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13
Q

Nose gear speed is limited to what beyond 20 degrees?

A

5 knots

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14
Q

What are the maximum tire speeds?

A

Nose - 139

Main - 174

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15
Q

What is the minimal CBR value for a marginal strength airfield?

A

CBR value of 3 is the minimum but consideration should be given to values of 6 or less.

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16
Q

What maneuvers are prohibited?

A

The following maneuvers are prohibited:

  • Aerobatics and spins.
  • Intentional zero or negative G maneuvers lasting longer than 7 seconds.
  • Practice stalls with power above 1,000 HP.
  • Practice asymmetric power stalls.
  • Sustained airspeed below the stick pusher speed.
  • Intentionally maneuvering into a sideslip resulting in a LEFT/RIGHT RUDDER alert.
  • Abrupt longitudinal control inputs at high speeds (faster than 1.0 G per second load factor increase or decrease).
  • Rapid roll reversals (roll rate must be zero momentarily before applying full aileron in the opposite direction).
  • At airspeeds above 150 KIAS, moderate to large rudder input held until sideslip peaks followed by opposite rudder (past neutral) or series of moderate to large alternating rudder inputs tending to produce successively larger sideslip angles.
17
Q

What are the crosswind take-off limitations?

A

Airplane not pointed into the wind ±45° and crosswind component >15 but <35 knots:

2,500 HP max until the airplane speed is >35 knots.

Airplane not pointed into the wind ±45° and crosswind component >35 knots:

Takeoff is not permitted

18
Q

When does the APU start light extinguish?

A

50%

19
Q

APU should be on speed for how long prior to introducing a bleed air load?

A

1 minute, if below 0C, 4 minutes

20
Q

What is the APU duty cycle?

A

1 minute on 4 minutes off

21
Q

What is the maximum continuous APU EGT?

A
  1. If EGT exceeds 710 °C for longer than 3 seconds, the APU OVRTEMP (C) ACAWS message alerts the crew to reduce APU loading
22
Q

What are the fuel balance limits?

A

a. 1,000 pounds between tanks of a symmetrical pair (main or external).
b. 1,500 pounds between left and right wings except as stated in items c and d.
c. One auxiliary tank full and the other auxiliary tank empty, provided all other tanks are symmetrically fueled or unbalanced toward the opposite side within the above limits

23
Q

What are the fuel freezing limitations?

A

To avoid fuel freezing, fuel temperature should not be lower than 6 °F (3.3 °C) above the freeze point defined in
Figure 1-4. The fuel temperature should be considered to be equal to the TAT. If the TAT drops below the above limit,
the airplane should be flown to an altitude where temperatures are higher.

24
Q

When should you not use the autopilot?

A

a. During takeoff and landing.
b. At airspeeds above maximum recommended airspeed V
H.
c. During ILS coupled approach below 200 feet (CAT 1), 100 feet (CAT 2) AGL or when flying over the localizer transmitter.

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.

d. not req.
e. At or below 500 feet AGL for non-approach operations.
f. In RVSM airspace unless the autopilot, in altitude 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.

25
Q

What are the altimeter differential limits?

A

ALTIMETERS (DIFFERENTIAL)
Static reading ±40 feet of field elevation

NOTE
When comparing the indicated altitude to the elevation of
a known check point, the maximum allowable error is ±40
feet for the pilot, copilot, and standby altimeters. Since
the standby altimeter does not compensate for temperature,
these tolerances only apply to the standby altimeter if the
flight station temperature is between 55 °F/13 C° and 95
°F/35 °C.

1,000 feet MSL 60 feet
10,000 feet MSL 200 feet
20,000 feet MSL 280 feet
30,000 feet MSL 350 feet

26
Q

What is the maximum and minimum cabin differential pressure?

A

CABIN DIFFERENTIAL PRESSURE
Maximum 15.3 in. Hg
CAUTION
Do not exceed 16.0 in. Hg of cabin differential pressure to
avoid the possibility of structural damage to the aircraft.

Minimum −1.6 in. Hg

27
Q

What are the engine start-up limits?

A
  • prior to start MGT of 175
  • max transient MGT of 807 for 2 seconds
  • increasing engine oil pressure within 15 seconds of gas generator rotation
  • increasing propeller oil pressure within 15 seconds of prop rotation
28
Q

What are the engine starter duty cycle limits?

A

70 seconds on, 60 seconds off for 5 cycles. Then a 20 minute cooling period is required.

CC130J (7 decks)

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