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P-3C Flight Engineer > Limits > Flashcards

Limits Flashcards

1
Q

High RAWS warning

A

380 ft+-20 ft for 3 sec

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2
Q

Low RAWS warning

A

170 ft+-10 ft continuous

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3
Q

Min alt for using AFCS

A

200 ft

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4
Q

Min recommended alt for bailout

A

3000 ft

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5
Q

Min alt for 2 engine loiter

A

1000 ft

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6
Q

APU automatic load monitoring alt

A

8000 ft

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7
Q

CABIN PRESS light illuminates at

A

10000 ft +- 500ft

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8
Q

Max alt for starting APU in flight

A

20000 ft

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9
Q

Max alt for using APU for engine starts

A

6000 ft

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10
Q

Max alt for flying with a cracked windscreen (middle layer)

A

10000 ft

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11
Q

Max alt for turning off landing lights

A

10000 ft

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12
Q

Alt for notifying crew to locate O2

A

25000 ft

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13
Q

Max speed with flaps UP

A

VNE

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14
Q

Max speed with flaps at MANEUVER

A

275 KTS

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15
Q

Max speed with flaps at TAKEOFF/APPROACH

A

190 KTS

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16
Q

Max speed with flaps at LAND

A

170 KTS

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17
Q

Max speed with landing gear extended

A

300 KTS

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18
Q

Max speed to extend landing gear 1.0 G or less

A

300 KTS

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19
Q

Max speed to extend landing gear greater than 1.0 G

A

190 KTS

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20
Q

Max speed to retract landing gear

A

190 KTS

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21
Q

Max speed with landing lights extended

A

260 KTS

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22
Q

Max speed with over wing hatch removed

A

170 KTS

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23
Q

Max speed with main cabin door open

A

300 KTS

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24
Q

Max speed with APU doors open

A

225 KTS

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25
Q

Max speed with IRDS turret extended

A

405 KTS

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26
Q

Max speed with AIMS turret extended

A

405 KTS

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27
Q

Max speed to extend or retract IRDS turret

A

375 KTS

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28
Q

Max speed to extend or retract AIMS turret

A

350 KTS

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29
Q

Speed range for dumping fuel

A

140 - 300 KTS

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30
Q

Speeds for in flight restart

A

Min 170 KTS
Max 345 KTS -6 per 1000 ft alt
210 KTS if range is critical

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31
Q

Max speed for retarding power levers into the ground range

A

w/ electrical pwr 135 KTS

w/o electrical pwr 125 KTS

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32
Q

Max speed with bomb bay doors open

A

VNE

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33
Q

Max speed with windshield heat inop

A

240 KTS below 10000 ft

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34
Q

Normal speed for NTS check

A

180 +- 10 KTS

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35
Q

Max zero fuel weight P-3C

A

80400 lbs w/o foam

82400 lbs w/ foam

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36
Q

Max normal landing weight

A

103880 lbs

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37
Q

Max landing weight that does not require an immediate overweight inspection

A

114000 lbs

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38
Q

Max recommended takeoff weight

A

135000 lbs

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39
Q

Max tank imbalances for tanks 1 & 4 for takeoff

A

1400 lbs

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40
Q

Max tank imbalances for tanks 1 & 4 for in-flight and landing

A

4389 lbs

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41
Q

Max tank imbalances for tanks 2 & 3 for takeoff

A

5025 lbs

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42
Q

Max tank imbalances for tanks 2 & 3 for in-flight and landing

A

No limit

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43
Q

Min fuel to obtain dips in tanks 1 & 4

A

9500 lbs

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44
Q

Min fuel to obtain dips in tanks 2 & 3

A

5500 lbs

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45
Q

APU fuel burn rate w/ electrical pwr and ground air conditioning

A

300 pph

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46
Q

Max difference between flight station gauges and hydrostatic tester

A

1200 lbs

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47
Q

During in-flight restart, light off should occur within

A

10 sec

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48
Q

Max time from start of rotation to LOW rpm

A

60 sec

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49
Q

Flight station O2 bottles endurance

A

3.5 hrs at 25000 ft

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50
Q

O2 walk around bottle endurance

A

Little to no exertion 22 min

Moderate exertion 5-10 min

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51
Q

Engine oil cooler augmentation occurs within (after all parameters are met)

A

8 sec

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52
Q

In-flight, max time allowed at zero or negative G’s

A

10 sec

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53
Q

After returning from zero or negative G’s, a shut down is required if oil press fluctuations last longer that

A

15 sec

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54
Q

Max time for landing lights on with no cooling air flow

A

30 sec

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55
Q

Test cycle time for EMP deice

A

44 sec

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56
Q

Normal cycle time for EMP deice

A

176 sec

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57
Q

Test cycle time for prop deice

A

160 sec

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58
Q

Normal cycle time for prop deice

A

160 sec

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59
Q

How long will the peanut gyro provide reliable information after a loss of power

A

9 min

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60
Q

Max time for OIL HOT light (alpha range)

A

5 min

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61
Q

Max time for OIL HOT light (beta range)

A

30 min

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62
Q

Victim Rescue Unit (VRU) endurance

A

5-60 min depending on size and exertion level

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63
Q

Stagnated start RPM reluctant to rise above

A

35-50%

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64
Q

Digital SHP gauge will indicate actual SHP at what RPM

A

43%

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65
Q

What RPM should fuel flow be indicated

A

16%

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66
Q

During start, EDC PRESS LOW light should go out at what RPM

A

16-65%

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67
Q

During start, light off should occur at what RPM

A

16-33%

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68
Q

During start, fuel manifold is energized closed at what RPM

A

16%

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69
Q

Fuel manifold drain valve is held closed by fuel pressure at what RPM

A

65%

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70
Q

Prop brake is held released by RGB oil pressure above what RPM

A

21%

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71
Q

During in-flight restart, PROP PUMP lights should be out by

A

55%

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72
Q

During a start, what RPM should the start button be pulled

A

57-64%

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73
Q

NORMAL RPM limits

A

96.3-99.1%

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74
Q

LOW RPM limits

A

71.0-73.8%

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75
Q

MAX REVERSE RPM limits

A

96.7-104.9%

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76
Q

FLIGHT IDLE RPM limits

A

94.5-98.4%

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77
Q

Fuel control maintains RPM above

A

97%

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78
Q

Pitchlock regulator dumps at what RPM

A

103.5%

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79
Q

Pitchlock reset , resets pitchlock RPM to

A

109%

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80
Q

Fuel topping governor limits

A

104.2-106.7%

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81
Q

APU RPM limits (on deck)

A

98-102%

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82
Q

APU RPM limits (in flight)

A

98-103%

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83
Q

APU overspeed

A

106%

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84
Q

LOW RPM TIT limit

A

410-730*C

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85
Q

NORMAL RPM TIT limit

A

445-645*C

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86
Q

FLIGHT IDLE TIT limit

A

430-705*C

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87
Q

MAX REVERSE TIT limit

A

580-790*C

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88
Q

Max TIT for 5 sec

A

1175*C

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89
Q

Max TIT for 5 min

A

1077 +6 -10*C

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90
Q

Max TIT for 30 min

A

1049*C

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91
Q

Max continuous TIT

A

1010*C

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92
Q

Recommended climb TIT

A

950*C

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93
Q

Recommended cruise TIT

A

925*C

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94
Q

Max residual TIT for and in-flight restart (prior to placing the fuel and ignition switch to on)

A

150*C

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95
Q

Max residual TIT for using Prime (prior to placing fuel and ignition switch to on)

A

100*C provided previous start didn’t over temp

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96
Q

Max residual TIT for a ground start (prior to placing fuel and ignition switch to on)

A

200*C

97
Q

Hot start TIT (record and continue)

A

830-850*C

98
Q

Hot start TIT (discontinue)

A

850*C

99
Q

Max TIT before an turbine inspection is required

A

965*C

100
Q

TIT over temp light illuminates at

A

1080+-2*C

101
Q

Max TIT allowed by the TD in temp controlling range

A

1077+6-10*C

102
Q

Amount of TIT rise during engine anti ice check

A

Corresponding

103
Q

Amount of TIT rise during wing deice check

A

10*C minimum

104
Q

Fuel heater strainer heats fuel to

A

40-70*F

105
Q

Zone 1 fire warning temp

A

600*F

106
Q

Zone 2 fire warning temp

A

400*F

107
Q

Zone 3 fire warning temp

A

400*F

108
Q

Normal engine oil temp

A

60-90*c

109
Q

Normal engine oil temp (extremely cold conditions)

A

50-60*C provided all pressure limits are maintained

110
Q

OIL HOT light illuminates at

A

100*C

111
Q

Transformer Rectifier overheat light illuminates at

A

150*C

112
Q

When should engine anti ice be used for takeoff

A

below 8*C

113
Q

Engine loiter is not recommended at what temp

A

below 10*C w/ visible moisture

below 0*C w/o moisture

114
Q

Min engine oil temp when using MIL-L-23699

A

-40*C

115
Q

Min engine oil temp when using MIL-L-7808

A

-54*C

116
Q

-2 APU EGT limits

A

688C continuous
710C peak for 10 sec
715*C max peak

117
Q

-3 APU EGT limits

A

649*C continuous

704*C Peak

118
Q

-10 APU EGT limits

A

649C continuous
710C peak for 10 sec
732*C max peak

119
Q

Max Reverse coordinator position and blade angle

A

0* coord

-13* blade angle

120
Q

Ground Idle coordinator position and blade angle

A

9* coord

-6* blade angle

121
Q

Ground Start coordinator position and blade angle

A

15* coord

0* blade angle

122
Q

NTS disabled below what coordinator position

A

24*

123
Q

When is pitchlock reset energized

A

coord below 28*

blade angle above 10*

124
Q

Prop SYNC available above what coordinator position

A

32*

125
Q

Flight Idle coordinator position and blade angle

A

34* coord
11* blade angle (beta range)
13* blade angle (alpha range)

126
Q

Landing Gear Warning System Parameters

A

Any landing gear not down and locked and:

  1. below 153+-3 KIAS and any Pwr lever below 48*(can be canceled).
  2. below 142+-3 KIAS and any Pwr lever below 60*(can’t be canceled).
  3. the flap handle is moved to the Landing position.
127
Q

Max range airspeed

A 
(config A,B,C)
205 + 1/2 Gross weight - Altitude
Adjust for wind
TAS + (HW x 0.3)
TAS - (TW x 0.25)
128
Q

Flight Start coordinator position

A

48*

129
Q

Auto Feather armed above what coordinator position

A

60*

130
Q

Coordinator position TD switches to temp controlling

A

66*

131
Q

Beta follow sets a min blade angle of 22.5 at what coordinator position

A

90*

132
Q

E-handle positions the coordinator to what position when pulled

A

110*

133
Q

At what blade angles is pitchlock cammed out

A

below 17* and above 57*

134
Q

What blade angle is pitchlock available

A

17-57

135
Q

Low pitch stops set min blade angle of

A

13*

136
Q

Feather blade angle

A

86.65*

137
Q

Minimum air at 16% RPM

A

25 psi

138
Q

Oil pressure at 35% RPM

A

Rising

139
Q

RGB oil pressure limits

A

50-250 psi (low)

150-250 psi (normal)

140
Q

Engine oil pressure limits

A

50-60 psi

max 100 psi (start and warm up)

141
Q

Oil Pressure light illuminates

A 
130 psi (RGB)
40 psi (engine)
142
Q

Normal hydraulic pressure

A

2960-3200 psi

143
Q

Minimum EBB pressure for flight

A

1900 psi

144
Q

Fuel boost pump light illuminates at

A

2 psi

145
Q

Fuel transfer pump light illuminates at

A

4 psi

146
Q

Normal fuel boost pump pressure

A

15-30 psi

147
Q

Minimum O2 pressure at 70*F

A

1500 psi

148
Q

Fully discharged Brake Accumulator statically reads

A

800+-25 psi

149
Q

Tank 5 pressure gauge range

A

green 0-7.0 psi

red +7 psi

150
Q

Main and standby regulator valve maintains what psi

A

150 psi above system demand

151
Q

Max oil pressure fluctuation

A

+-20 psi (RGB)

+-5 psi (engine)

152
Q

Max Reverse SHP limits

A

1&4 1150+-150

2&3 1250+-150

153
Q

Max SHP with oil temp below 0*C

A

Min SHP

154
Q

Max SHP with oil temp 0-40*C

A

1000 SHP

155
Q

Max SHP with oil temp above 40*C

A

Max SHP

156
Q

Prop decouple range

A

-500 to -1700 SHP

157
Q

NTS range

A
  • 150 to -500 (1&4)

- 100 to -500 (2&3)

158
Q

Minimum SHP for opening a bleed air valve during an NTS check

A

800 SHP

159
Q

Red over torque light illuminates at

A

4600 SHP

160
Q

Flop over occurs at

A

5300 SHP

161
Q

Fuel tank capacity 1&4

A

1606 gal

162
Q

Fuel tank capacity 2&3

A

1671 gal

163
Q

Fuel tank capacity 5A and 5

A

5A- 906 gal

5- 1740 gal

164
Q

Prop deice current ranges (ground test)

A

front spinners 74-100 amps
cuffs 48-72 amps
aft spinner and islands 58-82 amps

165
Q

Prop deice current ranges (flight)

A

front spinners 76-100 amps
cuffs 51-72 amps
aft spinners and islands 63-82 amps

166
Q

Applications of a fully charged brake accumulator

A

8

167
Q

Applications of a fully charged EBB

A

3 full, 6 partial

168
Q

Hours a fully charged brake accumulator will hold the parking brakes

A

30

169
Q

1 Hydraulic system capacities

A 
Total- 16.2 gal
Reservoir- 5.6 gal
w/ accum charged, gear down 5.0
w/ accum charged, gear up 4.0 gal
Service- 0.8 gal below any configuration
170
Q

2 Hydraulic system capacities

A

Total- 4.5 gal
Reservoir- 1 gal
Service- at 3/4 full

172
Q

Capacity of bomb bay hyd reservoir

A

.75 gal (empties into #1 hyd system)

172
Q

Max wind for opening the nose radome on deck

A

20 KTS

173
Q

Output rating of AC generators

A

120 VAC, 3 Phase, 400 Hz

174
Q

AC generator PMG rating

A

39 VAC, 1 Phase, 600 Hz

175
Q

Amount of air used for cooling and flame control in the engine

A

75%

176
Q

Amount of air used for combustion in the engine

A

25%

177
Q

TD Start Limiting mode parameters

A 
RPM - Below 94%
pwr lvr - any
Max take - 50%
Max put - 0%
TIT limit - 830*C
178
Q

TD Temp limiting mode parameters

A 
RPM - above 94%
Pwr lvr - below 66*
Max take - 20%
Max put - 0%
TIT limit - 1077*C
179
Q

TD Temp controlling mode parameters

A 
RPM - above 94%
Pwr lvr - above 66*
Max take - 20%
Max put 15%
TIT limit - 1077*C
180
Q

Loiter airspeed

A

Gross weight + 90

181
Q

Minimum altitude on station

A 
-W/ rad alt and RAWS:
 200 ft (day/VMC) 300 ft(night/IMC)
-W/o rad alt or RAWS, w/ updated baro alt:
300 ft (day/VMC) 500 ft (night/IMC)
-W/o rad alt or updated baro alt:
500 ft (day/VMC) 1000 ft (night/IMC)
182
Q

Bailout altitude

A

Recommended 3000 ft

Should not be attempted at 1000 ft or less

183
Q

Normal HRD bottle charge

A

10.5 lbs of Bromotrifloromethane with 600 psi of nitrogen.

184
Q

Engine oil capacities

A

Total- 15.75 gal
Usable- 8.65 gal
Foaming space- 5.7 gal
Unusable oil - 1.4 gal

185
Q

Minimum fuel in tanks 2&3

A

1000 lbs for hydraulic cooling

186
Q

Water Breaker capacities

A

Head- 4.5 gal

Emergency- 2.5 gal

187
Q

EDC oil capacity

A

1 gal

188
Q

APU oil capacity

A

1 gal

service at 1/2 on lower gauge

189
Q

Prop fluid capacity

A

6.2 gal

190
Q

Refer turbine oil capacity

A

0.7 pints

service at less than 3/4 full

191
Q

Air multiplier oil capacity

A

8.45 oz

service at less than 1/2 full

192
Q

Hydraulic press low light illuminates at

A

1800 psi

193
Q

Autopilot disconnect when #1 hyd system pressure drops to

A

1100 psi

194
Q

1B Hyd pump turns off and on at what pressure

A

on at 2200 psi

off at 2950+- 150 psi

195
Q

In-flight brake pressure

A

90-105 psi

196
Q

When does the fuel FILTERS light illuminate

A

7.5 psid across the low pressure filters

197
Q

When does the fuel PRESS LOW light illuminate

A

19 psid across the engine driven centrifugal pump

198
Q

When does prime terminate

A

when fuel manifold pressure reaches 50 psi

199
Q

How much pressure is required to bring on the parallel light

A

150 psi

200
Q

How much fuel pressure is required to hold the manifold drain closed

A

8-10 psi

201
Q

Combustion can liner drain valves require how much air pressure to close

A

2-4 psi

202
Q

The feather pump cuts out at what pressure

A

600-800 psi

203
Q

What is the Isobaric range (w AFC-341)

A

0-13.3 in Hg

204
Q

What is the Differential range (w AFC-341)

A

13.3-13.9 in Hg

205
Q

What is Safety relief range (w AFC-341)

A

13.9-14.4 in Hg

206
Q

EDC PRESS LOW light illuminates when

A

EDC oil pressure drops below 50 psi

207
Q

What is the fuel boost pump case temp protection temperature

A

400*F

208
Q

Hydraulic oil hot light comes on at

A

175*F

209
Q

What is the hydraulic case temp protection temp

A

380+-20*F

210
Q

What temp brings on the EDC temp high light

A

121*C

211
Q

What temp brings on the L/E Hot light

A

110*C

212
Q

What temp brings on the Bomb Bay Cold light

A

-3C to 2C

213
Q

What temp brings on the Bomb Bay Hot light

A

54-60*C

214
Q

What is the minimum temp rise when deicing the wing

A

10*C (20-30 sec)

215
Q

What temp brings on the Wing Hot light

A

outboard -104C (off at 96C)

center and inboard - 88C ( off at 79C)

216
Q

What temp brings on a FUS DUCT hot light

A

88C off at 79C

217
Q

What temp brings on the Rack Overheat light

A

135+-3F off at 128F

218
Q

Minimum cooling duct temp

A

5*C

219
Q

Max cooling duct temp

A

40*C

220
Q

What is the speed bias motor’s normal RPM range

A

96-106%

221
Q

The transfer and boost pumps pump at a rate of

A

Transfer 5000 lbs/hr

Scavenge 2000 lbs/hr

222
Q

AC hydraulic pump output

A

8 gpm (2 used for cooling)

223
Q

Fuel dump rate

A

1000 lbs/min

224
Q

Refueling rate

A

1 hose - 300 gpm

2 hoses - 600 gpm

225
Q

RGB reduction ratio

A

total-13.54:1
1st stage - 3.125:1
2nd stage - 4.333:1

226
Q

How much SHP is lost when using engine anti ice

A

9% (5% increase in fuel flow to regain loss)

227
Q

Max Heading Split

A

2* from INS-1 to INS-2

5* from INS to magnetic compass

228
Q

Flaps : extension and deflection

A

UP- 0% ext and 0* defl
Maneuver - 40% ext and 10* defl
Takeoff/Approach 77% ext and 18* defl
Down - 100% ext and 40* defl

229
Q

Max time for flaps to move from Land to Up

A

20 sec

230
Q

Max overweight takeoff

A

139760 lbs

231
Q

Max time at full hot in auto mode

A

90 sec must stabilize within 30 min

232
Q

Max time at full hot in manual mode

A

60 sec

233
Q

how long does the MK-124 flare last

A

20 sec

234
Q

What is the decent rate for the Thinpack parachute

A

less than 20 ft/sec

235
Q

Prop pump output

A

PP1 20 qt/min

PP2 40 qt/min

236
Q

What are the indications of wind shear

A

airspeed +- 10 KTS

VSI +- 500 ft/min

237
Q

Emp deice overheat temp

A

104+-6C out at 82C

238
Q

Engine starter duty cycle

A

1 min on, 1 min off
1 min on, 5 min off
1 min on, 30 min off

P-3C Flight Engineer (1 decks)

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