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KC-130J NATOPS > Ch 4 - OPS Limits > Flashcards

Ch 4 - OPS Limits Flashcards

1
Q

APU Limits: Max Continuous EGT °C

A

680°C

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2
Q

Ground Engine Prop Limits: MGT °C

A

<600°C

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3
Q

Low-speed drogue while ext/ret/eng airspeed

A

105-120 kts

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4
Q

Flap Airspeed 70%

A

155 kts

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5
Q

Takeoff Normal: Oil Temp °C

A

60-85°C

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6
Q

Ground Engine Prop Limits: Prop Gear Box: Unfeathered LSGI

A

110-210

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7
Q

Four Engine Flameout

A

*A. Aircraft attitude . . . . . . . . . . . Adjust to maintain 15-28% NG (PF)
*B. Power levers (all) . . . . . . . . . . . . . . . . . FLT IDLE (PF)
*C. CROSS FEED switches . . . . . . . CLSD (PM/CM)
*D. No. 2 and No. 3
ENGINE START switches . . .. . . STOP, START, Release (PM)
*E. No. 1 and No. 4 ENGINE START switches . . . . . . . . . STOP, START, Release (PM)

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8
Q

Landing Gear Extended airspeed

A

168 kts

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9
Q

Nose gear deflection speed: 60 degrees

A

5°

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10
Q

Takeoff Normal: MGT °C

A

≤852°C

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11
Q

Cargo Door (all positions) airspeed

A

250 kts

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12
Q

Flight Limits: MGT °C

A

<833°C

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13
Q

Flight Limits: NP% RPM

A

99-101%

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14
Q

APU Limits: On/Off and #cycles

A

1 min on, 4 min off. No limit for cycles

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15
Q

Flap Airspeed 20%

A

210 kts

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16
Q

Max tire speed: Main wheels

A

174 kts

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17
Q

Engine Fail Below Refusal Speed

A

*A. Aborted Takeoff procedure. . . . Accomplish (PF/PM)

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18
Q

Max Reverse: Eng Oil Pressure

A

40-90 psi

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19
Q

Engine Fire Shutdown

A

This procedure also applies if visible smoke or flames occur without an ACAWS message.

  • A. FIRE handle . . . . . . . . . . . . . . . . . . . Pull (PM)
  • B. Agent . . . . . . . . .. . . . . . . . Discharge (if required) (PM)
  • If the condition persists, wait a minimum of 15 seconds after the first bottle is discharged and then discharge the remaining bottle. The agent should be discharged when an indication continues after the FIRE handle has been pulled, or if any other indication or malfunction is suspected that requires fire extinguisher agent.
  • C. ENGINE START switch . . . . . . . . . . . . . . . STOP (PM)
  • Do not attempt a restart.
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20
Q

Taxi T/O Max alternate gross weight limit

A

175,000 lbs

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21
Q

High-speed drogue operations airspeed

A

185-250 kts

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22
Q

Nose gear deflection speed: 20 degrees

A

20°

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23
Q

Landing recommended gross weight limit

A

142,000 lbs

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24
Q

Fire/Smoke/Fumes Elimination

A

*A. Crew/Passengers . . . . . . . . . . . . . Notify (PF/PM)
Utilize ICS/PA/Caution Lights/Alarm Bells.
*B. Oxygen . . . . . . . . . . EMERGENCY, 100%, ON (ALL)
Note
-If crewmembers leave their crew positions to assist in the emergency, ensure that the oxygen regulator is switched OFF. When the checklist is complete, re-pressurize the aircraft as required and ensure all oxygen regulators are OFF.
-Consideration should be given to one of the pilots
remaining on oxygen until after landing.

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25
Q

Ground Engine Prop Limits: Prop Gear Box: Feathered LSGI

A

> 15

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26
Q

Eng Start Limits: On/Off and #cycles/cooling time

A

70 sec on, 60 sec off for 5 cycles then 20 min cooling time is required.

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27
Q

Landing gear door removed max speed, gear up airspeed

A

200 kts

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28
Q

Max Reverse: Oil Temp °C

A

60-85°C

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29
Q

Hydraulic Low/Loss/Leak

A

*A. ENGINE PUMPS switches (affected sys) . . . . . OFF (PM)
*B. SUCTION BOOST PUMPS
switch (affected sys) . . . . . . . . . . . . . . OFF (PM)

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30
Q

Sink rate limit: With AR PODS: Main Tanks (6.5 software)

A

28,000 lbs

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31
Q

Ground Engine Prop Limits: NP% RPM: Unfeathered LSGI

A

71-75%

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32
Q

Ground Engine Prop Limits: NP% RPM: Feathered LSGI

A

20-30%

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33
Q

Ground Engine Prop Limits: Prop Gear Box: Unfeathered GI

A

170-210

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34
Q

Flap Airspeed 90%

A

145 kts

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35
Q

Flight Limits: NG%

36
Q

Ground Engine Prop Limits: Oil Temp Feathered LSGI °C

37
Q

Start Eng and Prop Limits: Oil Temp Min °C

38
Q

Start Eng and Prop Limits: Engine Oil Pressure: increase pressure _____ seconds of NG

39
Q

Rapid Decompression

A

*A. OXYGEN . . . . . . . . . . NORMAL, 100%, ON (ALL)

40
Q

Aborted Takeoff

A

*A. Abort . . . . . . . . . . . . . . . . . . . . . Announce (PF)
Caution: Do not move the power levers below FLT IDLE above 139 KTAS due to the possibility of an over frequency condition caused by excessively high propeller RPM transients leading to all engine-driven generators tripping off-line. Anti-skid protection will be lost resulting in increased stopping distance, possible loss of directional control and damage to the gear doors if hard braking is applied causing the main tires to fail.
-With an inboard engine shut down, moving the power levers below FLT IDLE above 70 KTAS may cause a loss of directional control resulting in damage to the aircraft.
*B. Power levers . . . . .. . . . . . . . . GND IDLE (PF)
Warning: The pilot monitoring must check for BETA indications. Selection of asymmetric reverse will likely cause directional control difficulties.
Note: Pause for approximately 1 second with the power levers at GND IDLE for the pilot monitoring to check for BETA indications then state “INBOARDS ONLY,” or “OUTBOARDS ONLY,” or “ALL FOUR” to identify which engines should be used for reverse.
*C. Brakes and nose wheel steering . . . . As required (PF)

41
Q

Ramp (all positions) airspeed

42
Q

Flap Airspeed 10%

43
Q

Flight Limits: Oil Temp °C

44
Q

Takeoff Normal: Eng Oil Pressure

45
Q

Inoperative windshield anti-icing below 10,000 ft airspeed

46
Q

APU Limits: Maximum continuous EGT is ____°C. If EGT exceeds ____°C for longer than ____ seconds, the ACAWS alerts the crew to reduce APU loading. If RPM exceeds ____ percent, the APU automatically shuts down and the ACAWS alerts the crew that an APU overspeed has occurred.

A

Maximum continuous EGT is 680 °C. If EGT exceeds 710 °C for longer than 3 seconds, the ACAWS alerts the crew to reduce APU loading. If RPM exceeds 110 percent, the APU automatically shuts down and the ACAWS alerts the crew that an APU overspeed has occurred.

47
Q

Flap Airspeed 100%

48
Q

Flap Airspeed 40%

49
Q

Flight Limits: Are Max Continuous and Idle the same?

50
Q

Sink rate limit: With AR PODS: Tank 1 and 4 (6.5 software)

51
Q

Start Eng and Prop Limits: Prop Gear Box: Increase pressure ____ seconds of NP

52
Q

Landing max normal gross weight limit

A

164,000 lbs

53
Q

Flight Limits: Prop Gear Box

54
Q

Takeoff Normal: NG%

55
Q

Ground Engine Prop Limits: NG%

56
Q

Takeoff Normal: NP% RPM

57
Q

APU Fire (Ground/Inflight)

A
  • A. APU Fire handle . . . .. . . . . . . . Pull (P/CP/CM)

* B. Agent . . . . . . . Discharge (if required) (P/CP/CM)

58
Q

Max Reverse: NP% and RPM

59
Q

Flight Limits: Eng Oil Pressure

60
Q

Max tire speed: Nose wheel

61
Q

Start Eng and Prop Limits: MGT °C

62
Q

Hose Rapid Trail

A

*A. Call . . . . . . . . . . . . . . .. . . . . “RAPID TRAIL” (CM)
Note
“RAPID TRAIL” is subsequent white hose marking bands
appearing from pod tunnel every 1 second or less.
*B. RWND/TRAIL LSK and verify LSK . . . . . Select (CM/PM)
*C. Report status . . . . . . . . . . . . . . . . . . . . . . . (CM)

63
Q

Broken Hose

A
  • A. Broken Hose. . . . . . . . . . . . Announce (CM)
  • B. CNI-MU POD CTRL page 1/2 HYDRAULIC POWER LSK . .. . . . . (confirm) OFF (CM)
  • C. CNI-MU POD CTRL page 1/2 MASTER POWER LSK . . . . . . . . . . . . . . . . . . . OFF (CM)
64
Q

Sink rate limit: Auxiliary tanks

A

No restriction

65
Q

Ground Engine Prop Limits: Engine Oil Pressure feathered LSGI

A

40-<90 psi

66
Q

Paratroops doors opening/closing airspeed

67
Q

Ground Engine Prop Limits: NP% RPM: Unfeathered GI

68
Q

Taxi T/O Max normal gross weight limit

A

164,000 lbs

69
Q

Severe turbulent air operation airspeed

70
Q

Start Eng and Prop Limits: NG%

71
Q

Paratroop air deflectors open airspeed

72
Q

Max Reverse: NG%

73
Q

Landing gear door removed max speed, gear down airspeed

74
Q

Max Reverse: Prop Gear Box

75
Q

Landing max alternate gross weight limit

A

175,000 lbs

76
Q

Landing Light Extended airspeed

77
Q

Flap Airspeed 50%

78
Q

Flap Airspeed 30%

79
Q

Flap Airspeed 80%

80
Q

Low-speed drogue receive engage max speed airspeed

81
Q

Flap Airspeed 60%

82
Q

Takeoff Normal: Prop Gear Box

83
Q

Sink rate limit: External tanks

A

≤ 500 lbs

84
Q

Ground Evacuation

A

*A. Parking brake . . . . . . . . . . . . . . . . . . . . . . Set (P)
If a hot brake is suspected or main wheel well fire exists, set opposite brake only.
*B. Tower . . . . . . . . . . . . . . . . . . . Notify (CP)
*C. Pressurization . . . . . . . . . . . . . EMER DEPRESS (CP)
*D. Exits . . . . . . . . . Open (as required) (CM)
*E. FIRE handles for all engines and APU . . .. . Pull (CP)
*F. Crew/passengers . . . . Notify to evac the aircraft (CP)
G. External Power/APU Switch . . .. . . . . . . . . . . OFF (CP)
H. Battery switch . . . . . . . . . . . . . . . . . . . . . . . OFF (CP)
I. Manual oxygen shutoff valve . . . . . . . . . . CLOSE (if practical) (CMBR)
J. Aircraft . . . . . . .. . . . . . . Chock (if practical) (CMBR)
If hot brakes are suspected or main wheel fire exists, chock nose gear only.

85
Q

Sink rate limit: Without AR PODS: Main Tanks (6.5 software)

A

29,500 lbs

86
Q

Engine Fail After Refusal Speed

A

*A. Takeoff . . . . . . . . . . . . . . . . . . . Continue (PF)
*B. Directional control . . . . . . . . . . . . Maintain (PF)
Maintain directional control and wings level with rudder and ailerons.
At rotation speed:
*C. Aircraft attitude . . . . . . Rotate to target pitch (PF)

87
Q

Max Reverse: MGT °C

KC-130J NATOPS (4 decks)

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