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KC130J > Ch 4 & 7 > Flashcards

Ch 4 & 7 Flashcards

1
Q

Flap Airspeeds

A 
10%-220KIAS
20-210
30-200
40-190
50-183
60-165
70-155
80-150
90-145
100-145
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2
Q

Pre engine Start MGT and NG limit

A

175*C; 0 for 30 secs

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3
Q

Engine Anti ice Requirement

A

For Takeoff and Taxi, less than 10*C with visible moisture

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4
Q

Climb speed schedule

A

180KIAS to 10k
170 to 15k
160 to 25k
4 eng climb speed above 25k

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5
Q

✔️D✔️STAR-GO

A 
Emergency checklist complete
Dump fuel, declare an emergency
Normal checklist complete
Systems affected-(eng #? Gen? Load picked up? Hydraulics?)
Trim plan/TCAS to TA
Airspeed -Ldg, VMCA1/2, 145/139TAS, 70kts if inboard
Reverse plan- gnd Idle, reverse
Go around plan- which wing which rudder
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6
Q

Clean G limit

A

Area A -1 to 3g sym and 0 to 2.33 g asym

Area B,C 0 to 2.5 sym, and 0 to 2.0 asym

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7
Q

Recommended Oil

A

Mil-PRF-23699F

Mil-L-7808

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8
Q

Airspeed: High Speed Drogue Operation

A

185-250 kts

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9
Q

Airspeed: Ldg gear -ext, landing light ext

A

168; 250

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10
Q

Gnd Idle limits:

MGT & NG

A

Mgt less than 600

NG less than 72%

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11
Q

NP limits
Feathered lgsi
Unfeathered lgsi
Gnd idle/flight

A
  1. 20-30%
  2. 71-75%
  3. 99-101%
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12
Q

Gearbox oil pressure limits
Feathered lsgi
Unfeathered lsgi
Gnd idle/flight

A

> 15
110-210
170-210

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13
Q

Apu limits

  1. Max cont EGT
  2. Max RPM
  3. Bleed Air Pressure
A
  1. 680*C,710 max
  2. 110% -begins auto shutdown
  3. 40-50 psi
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14
Q

Engine start timing limits

A

NG w/in 10 sec
E Psi w/in 15 sec of NG
G Psi w/in 15 sec of NP

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15
Q

Eng starter limit cycle

A

70 on 60 off for 5 cycles then 20 min cooling

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16
Q

APU starter duty cycle

A

1min on 4 min off with no limit on number of duty cycles

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17
Q

Flight limits

  1. MGT
  2. NG
  3. NP
  4. G Psi
  5. E Psi
  6. Temp
  7. Qty
A
  1. Mgt 833*C
  2. NG 102%
  3. NP 99-101%
  4. G Psi 170-210
  5. E Psi 40-90
  6. Temp 60-85
  7. Qty 4-14.1
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18
Q

Wing/Emp Anti ice Test Limit

A

If the test needs to be repeated and OAT is over 70*F, wait at least 10min to prevent overheating, test requires at least 3 eng hi speed to supply bleed air, if test passes with only 1 or more engine low speed, it’s safe for icing

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19
Q

Crosswind takeoff procedures

A

15-25-35-45
Wind is not within 45* and is 15kts or greater,
Hold brakes and set power to 2500hp, release brakes and when IAS reaches 35 kts advance power to T.O.

20
Q

Primary fuels

A

Jp-5
Jp-8
F-24
Jet-A1

21
Q

5 conditions for Special High Speed Landing Procedure

A
  1. 100% flap at weights above 155,000lbs
  2. 50% flap at weights above 130,000lbs
  3. All 0% flap landings
  4. All landings at field elevation above 4000MSL
  5. All landings at field elevation above 2000MSL when temp is ISA+15
22
Q

Airspeed: cargo door and ramp

A

250

23
Q

Airspeed: paratroop doors open and locked

A

250

24
Q

Airspeed: paratroop doors opening and closing, paratroop air deflectors open

A

150

25
Q

Airspeed: low speed drogue extension, retraction; max speed

A

105-120; 130

26
Q

Airspeed: Severe Turbulent Air operation

A

65KIAS above power off stall speed not to exceed 180kts

27
Q

Airspeed: INOP windshield anti ice below 10k

A

187

28
Q

Airspeed: Ldg gear door removed, Max Speed

  1. Gear down
  2. Gear up
A

Down- 168

Up- 200

29
Q

Weight: Taxi, TO Max normal

A

164,000lbs

30
Q

Weight: Taxi, TO max alternate

A

175,000lbs

31
Q

Weight: Landing Max Normal

A

164,000lbs

32
Q

Weight: Landing Max alternate

A

175,000lbs

33
Q

Weight Landing Recommended

A

142,000lbs

34
Q

Nose gear deflection

20* and 60*

A 
20* = 20kts
60* = 5kts
35
Q

Max Tire speeds

A

Nose 139

Main 174

36
Q

TCAS limits

A 
45 tspdr equipped targets
40nm forward 15left/right 12 nm rear
Abv 12700 above 2700 below
Normal 2700 above/below
Below 2700 above 12700 below
37
Q

Blade angle: Green B

A

Blade angle is between 28 and 10.5, FADEC has detected no failures preventing ground range and speed is below 145kts

38
Q

Blade angle white Beta

A

Propeller is in beta range and blade angle is less than 10.5

39
Q

Benefits of Blade Angle Scheduling

A

Makes engine out stops easier to control, are not available if power levers are brought below flt idle above 115kias

40
Q

LOX requirements

A
  1. overwater 18 L

2. over land 10L

41
Q

Min bleed air for start

A

22psi

42
Q

Before attempting ground restart, how long do you wait NG reaches 0?

A

30 secs

43
Q

Wind shear indications

A
  1. +-20kias
  2. +-500fpm
  3. +- 6* pitch attitude changes
  4. +- 1.5 dots on glide slope deviation
44
Q

Max taxi speed above 164k

A

10kts

45
Q

Fuel tank limits

A 
1&4 -8310
2&3 -7650
Aux -5810
Ext -8900
Fus tank-24390
46
Q

Avionics temp limit

A

Operations of electronic equipment for more than 30 min at temp above 95*F will reduce life expectancy

47
Q

Autopilot limits (7)

A

Do not operate:

  1. Takeoff and landing
  2. Above Vh
  3. ILS below 200 above HAT or below MDA on non Prec
  4. IPRA below 200 above HAT
  5. At or below 500A for non coupled approaches
  6. In RVSM unless able to maintain +-65ft
  7. Above 164k lbs for config changes, approaches, below 1kft

KC130J (1 decks)

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