Limits Flashcards
1
Q
High RAWS warning
A
380 ft+-20 ft for 3 sec
2
Q
Low RAWS warning
A
170 ft+-10 ft continuous
3
Q
Min alt for using AFCS
A
200 ft
4
Q
Min recommended alt for bailout
A
3000 ft
5
Q
Min alt for 2 engine loiter
A
1000 ft
6
Q
APU automatic load monitoring alt
A
8000 ft
7
Q
CABIN PRESS light illuminates at
A
10000 ft +- 500ft
8
Q
Max alt for starting APU in flight
A
20000 ft
9
Q
Max alt for using APU for engine starts
A
6000 ft
10
Q
Max alt for flying with a cracked windscreen (middle layer)
A
10000 ft
11
Q
Max alt for turning off landing lights
A
10000 ft
12
Q
Alt for notifying crew to locate O2
A
25000 ft
13
Q
Max speed with flaps UP
A
VNE
14
Q
Max speed with flaps at MANEUVER
A
275 KTS
15
Q
Max speed with flaps at TAKEOFF/APPROACH
A
190 KTS
16
Q
Max speed with flaps at LAND
A
170 KTS
17
Q
Max speed with landing gear extended
A
300 KTS
18
Q
Max speed to extend landing gear 1.0 G or less
A
300 KTS
19
Q
Max speed to extend landing gear greater than 1.0 G
A
190 KTS
20
Q
Max speed to retract landing gear
A
190 KTS
21
Q
Max speed with landing lights extended
A
260 KTS
22
Q
Max speed with over wing hatch removed
A
170 KTS
23
Q
Max speed with main cabin door open
A
300 KTS
24
Q
Max speed with APU doors open
A
225 KTS
25
Max speed with IRDS turret extended
405 KTS
26
Max speed with AIMS turret extended
405 KTS
27
Max speed to extend or retract IRDS turret
375 KTS
28
Max speed to extend or retract AIMS turret
350 KTS
29
Speed range for dumping fuel
140 - 300 KTS
30
Speeds for in flight restart
Min 170 KTS
Max 345 KTS -6 per 1000 ft alt
210 KTS if range is critical
31
Max speed for retarding power levers into the ground range
w/ electrical pwr 135 KTS
| w/o electrical pwr 125 KTS
32
Max speed with bomb bay doors open
VNE
33
Max speed with windshield heat inop
240 KTS below 10000 ft
34
Normal speed for NTS check
180 +- 10 KTS
35
Max zero fuel weight P-3C
80400 lbs w/o foam
| 82400 lbs w/ foam
36
Max normal landing weight
103880 lbs
37
Max landing weight that does not require an immediate overweight inspection
114000 lbs
38
Max recommended takeoff weight
135000 lbs
39
Max tank imbalances for tanks 1 & 4 for takeoff
1400 lbs
40
Max tank imbalances for tanks 1 & 4 for in-flight and landing
4389 lbs
41
Max tank imbalances for tanks 2 & 3 for takeoff
5025 lbs
42
Max tank imbalances for tanks 2 & 3 for in-flight and landing
No limit
43
Min fuel to obtain dips in tanks 1 & 4
9500 lbs
44
Min fuel to obtain dips in tanks 2 & 3
5500 lbs
45
APU fuel burn rate w/ electrical pwr and ground air conditioning
300 pph
46
Max difference between flight station gauges and hydrostatic tester
1200 lbs
47
During in-flight restart, light off should occur within
10 sec
48
Max time from start of rotation to LOW rpm
60 sec
49
Flight station O2 bottles endurance
3.5 hrs at 25000 ft
50
O2 walk around bottle endurance
Little to no exertion 22 min
| Moderate exertion 5-10 min
51
Engine oil cooler augmentation occurs within (after all parameters are met)
8 sec
52
In-flight, max time allowed at zero or negative G's
10 sec
53
After returning from zero or negative G's, a shut down is required if oil press fluctuations last longer that
15 sec
54
Max time for landing lights on with no cooling air flow
30 sec
55
Test cycle time for EMP deice
44 sec
56
Normal cycle time for EMP deice
176 sec
57
Test cycle time for prop deice
160 sec
58
Normal cycle time for prop deice
160 sec
59
How long will the peanut gyro provide reliable information after a loss of power
9 min
60
Max time for OIL HOT light (alpha range)
5 min
61
Max time for OIL HOT light (beta range)
30 min
62
Victim Rescue Unit (VRU) endurance
5-60 min depending on size and exertion level
63
Stagnated start RPM reluctant to rise above
35-50%
64
Digital SHP gauge will indicate actual SHP at what RPM
43%
65
What RPM should fuel flow be indicated
16%
66
During start, EDC PRESS LOW light should go out at what RPM
16-65%
67
During start, light off should occur at what RPM
16-33%
68
During start, fuel manifold is energized closed at what RPM
16%
69
Fuel manifold drain valve is held closed by fuel pressure at what RPM
65%
70
Prop brake is held released by RGB oil pressure above what RPM
21%
71
During in-flight restart, PROP PUMP lights should be out by
55%
72
During a start, what RPM should the start button be pulled
57-64%
73
NORMAL RPM limits
96.3-99.1%
74
LOW RPM limits
71.0-73.8%
75
MAX REVERSE RPM limits
96.7-104.9%
76
FLIGHT IDLE RPM limits
94.5-98.4%
77
Fuel control maintains RPM above
97%
78
Pitchlock regulator dumps at what RPM
103.5%
79
Pitchlock reset , resets pitchlock RPM to
109%
80
Fuel topping governor limits
104.2-106.7%
81
APU RPM limits (on deck)
98-102%
82
APU RPM limits (in flight)
98-103%
83
APU overspeed
106%
84
LOW RPM TIT limit
410-730*C
85
NORMAL RPM TIT limit
445-645*C
86
FLIGHT IDLE TIT limit
430-705*C
87
MAX REVERSE TIT limit
580-790*C
88
Max TIT for 5 sec
1175*C
89
Max TIT for 5 min
1077 +6 -10*C
90
Max TIT for 30 min
1049*C
91
Max continuous TIT
1010*C
92
Recommended climb TIT
950*C
93
Recommended cruise TIT
925*C
94
Max residual TIT for and in-flight restart (prior to placing the fuel and ignition switch to on)
150*C
95
Max residual TIT for using Prime (prior to placing fuel and ignition switch to on)
100*C provided previous start didn't over temp
96
Max residual TIT for a ground start (prior to placing fuel and ignition switch to on)
200*C
97
Hot start TIT (record and continue)
830-850*C
98
Hot start TIT (discontinue)
850*C
99
Max TIT before an turbine inspection is required
965*C
100
TIT over temp light illuminates at
1080+-2*C
101
Max TIT allowed by the TD in temp controlling range
1077+6-10*C
102
Amount of TIT rise during engine anti ice check
Corresponding
103
Amount of TIT rise during wing deice check
10*C minimum
104
Fuel heater strainer heats fuel to
40-70*F
105
Zone 1 fire warning temp
600*F
106
Zone 2 fire warning temp
400*F
107
Zone 3 fire warning temp
400*F
108
Normal engine oil temp
60-90*c
109
Normal engine oil temp (extremely cold conditions)
50-60*C provided all pressure limits are maintained
110
OIL HOT light illuminates at
100*C
111
Transformer Rectifier overheat light illuminates at
150*C
112
When should engine anti ice be used for takeoff
below 8*C
113
Engine loiter is not recommended at what temp
below 10*C w/ visible moisture
| below 0*C w/o moisture
114
Min engine oil temp when using MIL-L-23699
-40*C
115
Min engine oil temp when using MIL-L-7808
-54*C
116
-2 APU EGT limits
688*C continuous
710*C peak for 10 sec
715*C max peak
117
-3 APU EGT limits
649*C continuous
| 704*C Peak
118
-10 APU EGT limits
649*C continuous
710*C peak for 10 sec
732*C max peak
119
Max Reverse coordinator position and blade angle
0* coord
| -13* blade angle
120
Ground Idle coordinator position and blade angle
9* coord
| -6* blade angle
121
Ground Start coordinator position and blade angle
15* coord
| 0* blade angle
122
NTS disabled below what coordinator position
24*
123
When is pitchlock reset energized
coord below 28*
| blade angle above 10*
124
Prop SYNC available above what coordinator position
32*
125
Flight Idle coordinator position and blade angle
34* coord
11* blade angle (beta range)
13* blade angle (alpha range)
126
Landing Gear Warning System Parameters
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
Max range airspeed
```
(config A,B,C)
205 + 1/2 Gross weight - Altitude
Adjust for wind
TAS + (HW x 0.3)
TAS - (TW x 0.25)
```
128
Flight Start coordinator position
48*
129
Auto Feather armed above what coordinator position
60*
130
Coordinator position TD switches to temp controlling
66*
131
Beta follow sets a min blade angle of 22.5 at what coordinator position
90*
132
E-handle positions the coordinator to what position when pulled
110*
133
At what blade angles is pitchlock cammed out
below 17* and above 57*
134
What blade angle is pitchlock available
17*-57*
135
Low pitch stops set min blade angle of
13*
136
Feather blade angle
86.65*
137
Minimum air at 16% RPM
25 psi
138
Oil pressure at 35% RPM
Rising
139
RGB oil pressure limits
50-250 psi (low)
| 150-250 psi (normal)
140
Engine oil pressure limits
50-60 psi
| max 100 psi (start and warm up)
141
Oil Pressure light illuminates
```
130 psi (RGB)
40 psi (engine)
```
142
Normal hydraulic pressure
2960-3200 psi
143
Minimum EBB pressure for flight
1900 psi
144
Fuel boost pump light illuminates at
2 psi
145
Fuel transfer pump light illuminates at
4 psi
146
Normal fuel boost pump pressure
15-30 psi
147
Minimum O2 pressure at 70*F
1500 psi
148
Fully discharged Brake Accumulator statically reads
800+-25 psi
149
Tank 5 pressure gauge range
green 0-7.0 psi
| red +7 psi
150
Main and standby regulator valve maintains what psi
150 psi above system demand
151
Max oil pressure fluctuation
+-20 psi (RGB)
| +-5 psi (engine)
152
Max Reverse SHP limits
1&4 1150+-150
| 2&3 1250+-150
153
Max SHP with oil temp below 0*C
Min SHP
154
Max SHP with oil temp 0-40*C
1000 SHP
155
Max SHP with oil temp above 40*C
Max SHP
156
Prop decouple range
-500 to -1700 SHP
157
NTS range
- 150 to -500 (1&4)
| - 100 to -500 (2&3)
158
Minimum SHP for opening a bleed air valve during an NTS check
800 SHP
159
Red over torque light illuminates at
4600 SHP
160
Flop over occurs at
5300 SHP
161
Fuel tank capacity 1&4
1606 gal
162
Fuel tank capacity 2&3
1671 gal
163
Fuel tank capacity 5A and 5
5A- 906 gal
| 5- 1740 gal
164
Prop deice current ranges (ground test)
front spinners 74-100 amps
cuffs 48-72 amps
aft spinner and islands 58-82 amps
165
Prop deice current ranges (flight)
front spinners 76-100 amps
cuffs 51-72 amps
aft spinners and islands 63-82 amps
166
Applications of a fully charged brake accumulator
8
167
Applications of a fully charged EBB
3 full, 6 partial
168
Hours a fully charged brake accumulator will hold the parking brakes
30
169
#1 Hydraulic system capacities
```
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
#2 Hydraulic system capacities
Total- 4.5 gal
Reservoir- 1 gal
Service- at 3/4 full
172
Capacity of bomb bay hyd reservoir
.75 gal (empties into #1 hyd system)
172
Max wind for opening the nose radome on deck
20 KTS
173
Output rating of AC generators
120 VAC, 3 Phase, 400 Hz
174
AC generator PMG rating
39 VAC, 1 Phase, 600 Hz
175
Amount of air used for cooling and flame control in the engine
75%
176
Amount of air used for combustion in the engine
25%
177
TD Start Limiting mode parameters
```
RPM - Below 94%
pwr lvr - any
Max take - 50%
Max put - 0%
TIT limit - 830*C
```
178
TD Temp limiting mode parameters
```
RPM - above 94%
Pwr lvr - below 66*
Max take - 20%
Max put - 0%
TIT limit - 1077*C
```
179
TD Temp controlling mode parameters
```
RPM - above 94%
Pwr lvr - above 66*
Max take - 20%
Max put 15%
TIT limit - 1077*C
```
180
Loiter airspeed
Gross weight + 90
181
Minimum altitude on station
```
-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
Bailout altitude
Recommended 3000 ft
| Should not be attempted at 1000 ft or less
183
Normal HRD bottle charge
10.5 lbs of Bromotrifloromethane with 600 psi of nitrogen.
184
Engine oil capacities
Total- 15.75 gal
Usable- 8.65 gal
Foaming space- 5.7 gal
Unusable oil - 1.4 gal
185
Minimum fuel in tanks 2&3
1000 lbs for hydraulic cooling
186
Water Breaker capacities
Head- 4.5 gal
| Emergency- 2.5 gal
187
EDC oil capacity
1 gal
188
APU oil capacity
1 gal
| service at 1/2 on lower gauge
189
Prop fluid capacity
6.2 gal
190
Refer turbine oil capacity
0.7 pints
| service at less than 3/4 full
191
Air multiplier oil capacity
8.45 oz
| service at less than 1/2 full
192
Hydraulic press low light illuminates at
1800 psi
193
Autopilot disconnect when #1 hyd system pressure drops to
1100 psi
194
1B Hyd pump turns off and on at what pressure
on at 2200 psi
| off at 2950+- 150 psi
195
In-flight brake pressure
90-105 psi
196
When does the fuel FILTERS light illuminate
7.5 psid across the low pressure filters
197
When does the fuel PRESS LOW light illuminate
19 psid across the engine driven centrifugal pump
198
When does prime terminate
when fuel manifold pressure reaches 50 psi
199
How much pressure is required to bring on the parallel light
150 psi
200
How much fuel pressure is required to hold the manifold drain closed
8-10 psi
201
Combustion can liner drain valves require how much air pressure to close
2-4 psi
202
The feather pump cuts out at what pressure
600-800 psi
203
What is the Isobaric range (w AFC-341)
0-13.3 in Hg
204
What is the Differential range (w AFC-341)
13.3-13.9 in Hg
205
What is Safety relief range (w AFC-341)
13.9-14.4 in Hg
206
EDC PRESS LOW light illuminates when
EDC oil pressure drops below 50 psi
207
What is the fuel boost pump case temp protection temperature
400*F
208
Hydraulic oil hot light comes on at
175*F
209
What is the hydraulic case temp protection temp
380+-20*F
210
What temp brings on the EDC temp high light
121*C
211
What temp brings on the L/E Hot light
110*C
212
What temp brings on the Bomb Bay Cold light
-3*C to 2*C
213
What temp brings on the Bomb Bay Hot light
54-60*C
214
What is the minimum temp rise when deicing the wing
10*C (20-30 sec)
215
What temp brings on the Wing Hot light
outboard -104*C (off at 96*C)
| center and inboard - 88*C ( off at 79*C)
216
What temp brings on a FUS DUCT hot light
88*C off at 79*C
217
What temp brings on the Rack Overheat light
135+-3*F off at 128*F
218
Minimum cooling duct temp
5*C
219
Max cooling duct temp
40*C
220
What is the speed bias motor's normal RPM range
96-106%
221
The transfer and boost pumps pump at a rate of
Transfer 5000 lbs/hr
| Scavenge 2000 lbs/hr
222
AC hydraulic pump output
8 gpm (2 used for cooling)
223
Fuel dump rate
1000 lbs/min
224
Refueling rate
1 hose - 300 gpm
| 2 hoses - 600 gpm
225
RGB reduction ratio
total-13.54:1
1st stage - 3.125:1
2nd stage - 4.333:1
226
How much SHP is lost when using engine anti ice
9% (5% increase in fuel flow to regain loss)
227
Max Heading Split
2* from INS-1 to INS-2
| 5* from INS to magnetic compass
228
Flaps : extension and deflection
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
Max time for flaps to move from Land to Up
20 sec
230
Max overweight takeoff
139760 lbs
231
Max time at full hot in auto mode
90 sec must stabilize within 30 min
232
Max time at full hot in manual mode
60 sec
233
how long does the MK-124 flare last
20 sec
234
What is the decent rate for the Thinpack parachute
less than 20 ft/sec
235
Prop pump output
PP1 20 qt/min
| PP2 40 qt/min
236
What are the indications of wind shear
airspeed +- 10 KTS
| VSI +- 500 ft/min
237
Emp deice overheat temp
104+-6*C out at 82*C
238
Engine starter duty cycle
1 min on, 1 min off
1 min on, 5 min off
1 min on, 30 min off
