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C130 > Ops Limits > Flashcards

Ops Limits Flashcards

1
Q

OIL QUANTITY

Engine Low Oil Light

A

4 Gallons

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2
Q

FUEL SYSTEMS

Imbalance Limits - Symmetrical’s

A

1000lbs

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3
Q

STARTING TIT

Temp Controlling Check (minimum temp range)

A

720’C - 750’C

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4
Q

APU LIMITS

Normal RPM

A

95 - 105%

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5
Q

ENGINE TIT

Reduced Power

A

900’C, 970’C, 1010’C

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6
Q

OXYGEN SYSTEM

Lox Quantity

A

25 liters

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7
Q

DUTY CYCLES

Propeller Auxiliary Pump

A

1 on 1 off; <2 min per 30 min

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8
Q

HYDRAULIC RUDDER BOOST PRESSURE LIMITS

Compensator Failure

A

3450PSI

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9
Q

PRESSURIZATION

Cracked Window - Cargo Compartment (1 Pane)

A

10inHg

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10
Q

APU LIMITS

Maximum RPM

A

106%

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11
Q

ENGINE RPM

Pitchlock Operations

A

96 - 98%

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12
Q 
ELECTRICAL SYSTEM (DC)
Minimum for Preflight
A

21V

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13
Q 
OIL PRESSURE (PSI)
Engine LSGI
A

<50PSI if normal at 100%

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14
Q

OIL TEMPERATURE

Minimum for Start

A

-40’C

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15
Q

HYDRAULIC SYSTEM PRESSURE LIMITS

Engine Low Pressure Light

A

1000PSI

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16
Q

PRESSURIZATION

Safety Valve

A

-0.76 to 15.9inHg

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17
Q

OIL TEMPERATURE

Flight (max temperature for how long?)

A

5 minutes

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18
Q

OIL TEMPERATURE

Normal

A

60 - 85’C

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19
Q

ENGINE RPM

Propeller Pitchlock at

A

103%

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20
Q

ENGINE TIT

Crossover

A

820’C +/- 20’C

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21
Q

APU LIMITS

Maximum EGT

A

650’C

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22
Q

OXYGEN SYSTEM

System Pressure - Continuous

A

270 - 340PSI

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23
Q 
OIL PRESSURE (PSI)
Gearbox Fluctuation
A

+/-20PSI

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24
Q

THROTTLE RANGE

Flight Idle

A

34’

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25
Q

ENGINE TIT

Normal Continuous

A

200 - 1010’C

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26
Q

OXYGEN SYSTEM

System Pressure - No Flow

A

270 - 455PSI

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27
Q 
ELECTRICAL SYSTEM (DC)
Load Range
A

1.03

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28
Q

FUEL SYSTEMS

Imbalance Limits - Outboard vs Inboard

A

500 - 1000lbs

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29
Q

HYDRAULIC SYSTEM PRESSURE LIMITS

Low Speed Ground Idle

A

2550PSI

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30
Q

HYDRAULIC SYSTEM PRESSURE LIMITS

Maximum

A

3500PSI

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31
Q

ENGINE RPM

Normal Ground Idle

A

94 - 102%

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32
Q

BLEED AIR SYSTEM

Minimum APU Output

A

35PSI

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33
Q

HYDRAULICS (AUX)

Maximum

A

3500PSI

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34
Q

ENGINE TORQUE

Decouple

A

-6,000inlbs

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35
Q

APU LIMITS

Starting Oil Pressure

A

10%

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36
Q

ENGINE TIT

Exceed 1083’C (for how long?)

A

5 seconds

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37
Q

ENGINE TIT

Max Continuous

A

1010’C

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38
Q

OIL QUANTITY

Maximum

A

12 Gallons

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39
Q

HYDRAULICS (Brakes)

Emergency Application

A

2900PSI

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40
Q

ANTI-ICING

Propeller / Spinner - Cycle

A

15sec on, 45sec off

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41
Q

ENGINE TIT

Military (30 Min)

A

1049’C

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42
Q

ENGINE RPM

Allowable Fluctuation

A

+/- 0.5%

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43
Q 
ELECTRICAL SYSTEM (DC)
Voltage
A

25 - 30V

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44
Q

HYDRAULIC RUDDER BOOST PRESSURE LIMITS

Relief Valve Fail

A

3900PSI

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45
Q

ANTI-ICING

Number of Ice Probes

A

2

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46
Q 
ENGINE TORQUE
Propeller Reversing (Max Diff)
A

1,000inlbs

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47
Q

HYDRAULICS (AUX)

Normal

A

2900 - 3300PSI

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48
Q

PRESSURIZATION

Cracked Window - Flight Station (1/2 Panes)

A

10inHg

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49
Q

ENGINE TORQUE

Oil Temp <0’C

A

Min Torque

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50
Q 
ELECTRICAL SYSTEM (AC)
Voltage
A

110 - 125V

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51
Q

ANTI-ICING

NESA - Cold Start

A

-43’C (-45’F)

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52
Q 
STARTING TIT
Stop Start (1 Restart) / 781 (temp range)
A

850’C - 965’C

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53
Q

BLEED AIR SYSTEM

Minimum Engine Output

A

70PSI

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54
Q

HYDRAULIC RUDDER BOOST PRESSURE LIMITS

Suction Boost Circuit

A

11 AMPS

55
Q

THROTTLE RANGE

Temperature Controlling

A

65 - 90’

56
Q

HYDRAULIC SYSTEM PRESSURE LIMITS

Normal

A

2900 - 3200PSI

57
Q

ENGINE TORQUE

NTS Action

A

-1,200 +/- 600inlbs

58
Q 
OIL PRESSURE (PSI)
Gearbox Mission Minimum
A

130PSI

59
Q

ANTI-ICING

Leading Edge - Overheat Light

A

200’F

60
Q

FUEL SYSTEMS

Fuel Tank Pressure - Auxiliary / External

A

23PSI

61
Q 
ELECTRICAL SYSTEM (AC)
Frequency
A

380 - 420HZ

62
Q

ANTI-ICING

NESA - Max OAT

A

27’C (81’F)

63
Q

PRESSURIZATION

Cracked Window - Cargo Compartment (2 Panes)

A

0inHg

64
Q

DUTY CYCLES

APU

A

1 on 4 off

65
Q 
OIL PRESSURE (PSI)
Gearbox Normal
A

150 - 250PSI

66
Q

HYDRAULIC SYSTEM PRESSURE LIMITS

Indication by

A

On Speed

67
Q

OIL QUANTITY

Propeller Oil Quantity

A

26 Quarts

68
Q 
OIL PRESSURE (PSI)
Engine Normal
A

50 - 60PSI

69
Q

HYDRAULIC SYSTEM PRESSURE LIMITS

Normal by

A

On Speed + 30sec

70
Q 
ELECTRICAL SYSTEM (DC)
Battery Voltage
A

24V

71
Q

ENGINE TIT

Takeoff Power

A

1077’C

72
Q

HYDRAULIC RUDDER BOOST PRESSURE LIMITS

Maximum (15 - 100% Flaps)

A

3500PSI

73
Q

HYDRAULIC SYSTEM PRESSURE LIMITS

Aileron Boost

A

2050

74
Q

FUEL SYSTEMS

Imbalance Limits - Wing to Wing

A

1500lbs

75
Q

APU LIMITS

Overspeed

A

110%

76
Q

FUEL SYSTEMS

Fuel Tank Pressure - Main Low Pressure Light

A

8.5PSI

77
Q

BLEED AIR SYSTEM

Bleed Air Checks - APU (30 - 15PSI)

A

16 seconds

78
Q 
ELECTRICAL SYSTEM (AC)
AC Generator Capacity
A

40KVA

79
Q

ENGINE RPM

Flight Idle on Ground

A

92.5 - 100.5%

80
Q 
OIL PRESSURE (PSI)
Engine Maximum Start
A

100PSI

81
Q

ENGINE RPM

Normal (Including Takeoff)

A

98 - 102% +/- 0.5%

82
Q

FUEL SYSTEMS

Fuel Tank Pressure - Aux/Ext

A

28 - 40PSI

83
Q

DUTY CYCLES

Engine

A

1 on 1 off; 1 on 5 off;

1 on 30 off (minutes)

84
Q

OXYGEN SYSTEM

Lox Low Light

A

2.5 liters

85
Q

BLEED AIR SYSTEM

14th Stage Pressure

A

125PSI

86
Q

PRESSURIZATION

Manual Control Hot to Cold (Time)

A

4 minutes

87
Q

STARTING TIT

Maintenance Action

A

<720’C

88
Q

ENGINE TORQUE

Max Allowable on Takeoff

A

19,600inlbs

89
Q

ANTI-ICING

Propeller / Spinner - Max Ground Cycles

A

2

90
Q

OIL QUANTITY

Expansion

A

7.5 Gallons

91
Q

STARTING TIT

Max Enrichment Start

A

100’C

92
Q

ANTI-ICING

Leading Edge - Normal Range

A

75 - 200’F

93
Q

HYDRAULIC RUDDER BOOST PRESSURE LIMITS

0 - 15% Flaps

A

1100 - 1400PSI

94
Q

ENGINE RPM

Fuel Control Limiting

A

103.5%

95
Q

ENGINE TORQUE

Oil Temp 0 - 40’C

A

4,500inlbs

96
Q

ENGINE RPM

Ignition by

A

35%

97
Q

ENGINE RPM

Max Reverse

A

96 - 106%

98
Q

OIL QUANTITY

Propeller Low Oil Light

A

2 Quarts low

99
Q

ENGINE TIT

Exceed 1175’C (for how long?)

A

Momentarily

100
Q

OIL TEMPERATURE

Maximum

A

85 - 100’C

101
Q

HYDRAULICS (Brakes)

Normal - 1 Application

A

2250PSI

102
Q

HYDRAULIC RUDDER BOOST PRESSURE LIMITS

Maximum (0 - 15% Flaps)

A

1600PSI

103
Q

ENGINE RPM

Low Speed Ground Idle

A

69 - 75.5%

104
Q

THROTTLE RANGE

Ground Idle

A

18’

105
Q 
OIL PRESSURE (PSI)
Gearbox LSGI
A

50PSI

106
Q

OIL TEMPERATURE

Ground (max temperature for how long?)

A

30 minutes

107
Q

STARTING TIT

Max Normal Start

A

200’C

108
Q 
ENGINE TIT
Takeoff Max (5 Min)
A

1067 - 1083’C

109
Q 
OIL PRESSURE (PSI)
Engine Flucturation
A

+/-10PSI

110
Q

APU LIMITS

Normal EGT

A

250 - 650’C

111
Q

ENGINE TORQUE

Low Pitch Stop Increasing

A

200inlbs

112
Q

FUEL SYSTEMS

Fuel Tank Pressure - Main

A

15 - 24PSI

113
Q

HYDRAULIC RUDDER BOOST PRESSURE LIMITS

15 - 100% Flaps

A

2900 - 3200PSI

114
Q

HYDRAULIC SYSTEM PRESSURE LIMITS

Suction Boost Light

A

20PSI

115
Q

ENGINE RPM

Igniters Energized

A

16%

116
Q

OIL QUANTITY

Minimum

A

4 Gallons

117
Q

PRESSURIZATION

Cabin Differential

A

15.16inHg

118
Q

HYDRAULICS (Brakes)

Normal - 2 Applications

A

2900 - 3200PSI

119
Q 
OIL PRESSURE (PSI)
Gearbox Maximum Start
A

250PSI

120
Q

THROTTLE RANGE

Low Speed Ground Idle

A

9 - 30’

121
Q

BLEED AIR SYSTEM

Bleed Air Checks - Engine (65 - 35PSI)

A

16 seconds

122
Q

THROTTLE RANGE

Temperature Limiting

A

0 - 65’

123
Q

PRESSURIZATION

Press Controller

A

-1.2 to 15.8inHg

124
Q

BLEED AIR SYSTEM

14th Stage Temperature

A

600’F

125
Q

STARTING TIT

781 Write Up (higher temp range)

A

830’C - 850’C

126
Q

OIL TEMPERATURE

Minimum Allowable

A

40’C

127
Q

ENGINE RPM

Oil Pressure Indication by

A

35%

128
Q

ANTI-ICING

Propeller / Spinner (Amps)

A

65 - 90 amps

129
Q 
ELECTRICAL SYSTEM (AC)
Load Range
A

1.05

130
Q

STARTING TIT

Overtemp Inspection / 781 (temp range)

A

Exceeds 965’C

131
Q

APU LIMITS

ON Speed Light On

A

95%

132
Q

ANTI-ICING

NESA - Operating Cycle

A

5sec on, 10sec off

133
Q

ANTI-ICING

Leading Edge - Maximum Ground Time

A

30seconds

C130 (8 decks)

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