Brainscape's Knowledge GenomeTM


Top Flashcards (Certified)
All Flashcards

KC-130J > Ch-4 > Flashcards

Ch-4 Flashcards

1
Q

Taxi and takeoff gross weight limitations:

A

Maximum normal: 164,000
Maximum alternate: 175,000

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Landing gross weight limitations

A

Recommended: 142,000
Maximum normal: 164,000
Maximum alternate 175,000

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Outboard tanks max

A

8310

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Inboard tanks max

A

7650

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Total main tanks

A

31,920

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Aux tanks

A

5810

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Total internal fuel weight max

A

43,540

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

External tanks

A

8,900

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Fuselage tank

A

24,390

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Total internal and external (fuel)

A

85,730

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Primary fuel management

A

-Outboards contain 500-1000 more fuel than inboards
-main tanks full except start/taxi/takeoff fuel
-no less than 7060 in 1 & 4 and no less than 6410 in tanks 2 & 3 when external tanks have fuel

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Alternate enroute fuel management

A

-May extend airframe service life
-when external and/or auxiliary tanks contain useable fuel 1&4 are maintained at max and 500-1000 more than 2&3
-w/ no fuel in aux & externals, 1&4 full, 2&3 used till 1520. 1&4 then used till 1520, tank-engine from there

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Secondary fuel management

A

Anything not primary or alternate

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Recommended loading limits

A

Area A: 3 g (symmetrical)
Area B & C: 2.5 g (symmetrical)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Alternate (cautionary) loading limits

A

Area D: 2.25 g (symmetrical)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Loading not recommended

A

Area E: 2 g (symmetrical)
Emergency situations

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Landing gear doors removed

A

200 gear up
168 gear down

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Flight is not permitted with forward nose gear door ______ and the aft door ______

A

Removed, installed

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

GS location - % Mac

A

15-30

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

External tank limits when fuselage tank is installed

A

If fuel is in the fuselage tank, external tanks should be empty when the fuselage tank contains less than 20,000 lbs. otherwise restricted to level flight

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

Taxing with inner brake locked, braking during revers taxiing

A

Prohibited

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

Taxi speeds & nose gear deflection
20 degrees
60 degrees

A

20 knots
5 knots

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

Taxiing w/ alternate gross weight

A

-Taxi & takeoff only on smooth surfaces free of dips depressions and holes
-max 10 knots
-taxi shortest distance possible
-minimum braking
-light braking in turns
-limit nose wheel to 5 degrees
-avoid abrupt or hard uneven brake applications

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

Max tire speeds
Nose-
Main-

A

139

174

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Three categories of airfields (strength)
High strength Marginal strength Substandard
26
High strength airfields: When Aircraft classification number (ACN) is greater than Pavement Classification Number (PCN)
Aircraft should normally NOT land on runway
27
Normal operation recommended tire deflection
35 %
28
Marginal strength airfields: California bearing ratio (CBR) min
3, Considerations should be given to operations having aircraft weights in excess of the weight limitation for 540 sink and on runways with CBR 6 or less
29
Predictions for number of passes on a marginal airfield are a function of _____ & _____ (figure 4.6-2)
Aircraft gross weight and CBR
30
Number of passes (for marginal field) based on recommendation of tire pressure corresponding to ____ tire deflection
39 % (To prevent excessive tire damage, do not exceed 39 %)
31
Applicable airfield strength recommendations for marginal and substandard fields (8 thing)
-inflate/deflate main gear tires to recommended psi -empty externals -do not exceed 10 knots during taxi -minimize breaking if porpoising -minimize nose gear loads using elevator on landing rollout and T/O, load with mid or aft CH -minimize reverse on unpaved -shut off flight station AC on unpaved (prevents clogging of heat exchanger) -limit gross weight to 164,000
32
Gross weight limits for substandard field
-Correspond to 540 sink rate -Decision to use substandard should be made by appropriate authority -Allow for increased maintenance and accelerated inspections
33
Maximum passenger load for extended over water operating more than 50 nautical miles from shore
-80 passengers including crew -with mixed cargo and passengers, 35 per overhead exit
34
With any flap extension, load factor is
2 g symmetrical 1.5 unsymmetrical
35
Load factor limits: Area A-
-1 - 3 symmetrical 0 - 2.33 rolling
36
Load factor limits: Area B
0 - 2.5 symmetrical 0 - 2 rolling
37
Load factor limits: Area C
0 - 2.5 symmetrical 0 - 2 rolling
38
Load factor limits: Area D
0 - 2.25 symmetrical 0 - 1.83 rolling
39
Load factor limits: Area E
Not recommended
40
High bank-angle limitations
-Apply to maneuvers beyond 60 degrees (flaps up) 45 degrees ( flaps extended) -large aileron inputs should be made between 0.5 and 1.5 g
41
Prohibited maneuvers
-Aerobatics and spins -practice stalls with power above 1000 HP -practice asymmetric power stalls -intentional zero or negative G maneuvers lasting longer than 7 seconds -sustained airspeed below stick pusher speed -intentionally maneuvering into a slide slip for a RUDDER alert -abrupt longitudinal control inputs at high speeds (faster than 1 g per second increase or decrease) -rapid toll reversals Moderate to large rudder inputs held until slideslip followed by opposite rudder
42
Because of propulsion system limitations, avoid intentional negative and zero g maneuvers lasting longer than ______
7 seconds
43
Air start can be conducted with or without use of starter below ______
25,000 ft
44
Max air start elevation for Jp-4
22,500 ft
45
With bleed air available, starter assisted air start can be accomplished at any speeds loss than ______
250 KIAS (NG below 29)
46
With bleed air not available, NG 15-29 If prop is windmilling at 100% NP, NG will stabilize at _________
15, at speeds as low as 110-130
47
If propeller is feathered, speed as high as ______ may be required to achieve 15 % NG
200-250
48
Static propeller feathering is limited to _____ cycles before propeller gearbox must be ______ or _____
2 Drained Engine started
49
Total auxiliary feather pump operation shall not exceed _____ seconds
80
50
Mgt start limits
807 for 2 seconds (max 175 to start)
51
Mgt ground
600
52
Mgt reverse
833
53
Mgt takeoff
852
54
Mgt max continuous
833
55
Min oil temp for start
-40
56
Engine power limited to idle when oil temp is less than _____ And to 1000 when oil temp is less than _____
0, 45
57
GPSI
15 seconds of rotation 110-210 LSGI 170-210 GI and above
58
EPSI
15 seconds of gas generator rotation 40-90
59
Oil temp
60-85
60
Shutdown engine if oil temp exceeds
93 86-93 for > 5 minutes
61
Starter duty cycle
70 sec on, 60 sec off for 5 cycles Then 20 min cooling
62
Takeoff crosswind restrictions Not pointed into wind +/- 45 degrees, with a component 15-35
2,500 HP max until greater than 35 KIAS
63
With WINDMILLING propeller (greater than one half revolutions per minute) and oil supplied (fire handle in), engine should be started within _____ and operated at Flt idle for at least ____
5 minutes 5 minutes
64
With FEATHERED propeller (less than than one half revolutions per minute) and oil supplied (fire handle in), engine should be started within _____ and operated at Flt idle for at least ____
6 hours 20 minutes
65
APU starter cycle
90 sec on 5 min off for three cycles, Min 60 minutes before subsequent start attempts (Different in 8.1 natops?)
66
Max APU RPM
110 Shuts down if exceeded
67
APU bleed air pressure
40-50 psi
68
APU EGT
Max continuous-680 710 for 3 seconds
69
APU generator voltage
108-117
70
Boost pump psi
15-24
71
Transfer pump psi
28-40
72
Fuselage transfer pump psi
28-46
73
Fuel unbalance
1000 lbs between symmetrical tanks 1500 lbs between wings One aux can be full with the other empty as long as all other tanks are symmetrically fueled or unbalanced towards the opposite side
74
Do not operate with autopilot when:
-Takeoff and landing -above Vh -ILS coupled below 200 feet HAT (cat 1) 100 feet HAT (cat 2) - below MDA on non precision -IPRA below 200 HAT -below 500 AGL for non approach operations -in RVSM unless able to hold +/- 65 feet -above 164,000 if below 1000 agl, during configuration or approach
75
Automatic flight Turn knob max bank angle
Approximately 35 degrees
76
Automatic flight Pilot/copilot engage bank angle
25 +/-3
77
Automatic flight Course intercept bank angle
25 +/- 3
78
Automatic flight On course bank angle
10
79
Automatic flight Localizer tracking
15 +/- 3
80
Vertical functions IAS hold
+/- 3
81
Vertical functions VS hold
+/- 70 fpm at 1000 fpm
82
Vertical functions ALT hold
+/- 40 feet of initial altitude
83
Vertical functions ALT SEL
+/- 40 feet with +/- 75 foot overshoot at 1000 fpm
84
Outflow valve differential control
14.3 +/- .2 in. Hg
85
Safety valve
15.0 +/- 0.3 in Hg (do not exceed 16)
86
Cabin differential pressure
Max 15.2 in. Hg
87
Flaps 10 percent
220
88
Flaps 20 percent
210
89
Flaps 30 percent
200
90
Flaps 40 percent
190
91
Flaps 50 percent
183
92
Flaps 60 percent
165
93
Flaps 70 percent
155
94
Flaps 80 percent
150
95
Flaps 90 percent
145
96
Flaps 100 percent
145
97
Landing gear extended
168
98
Landing lights extended
250
99
Cargo door open and locked, ramp up and locked
250
100
Paratroop air deflectors (opening)
150
101
Paratroop doors open and locked
250
102
High speed drogue
185-250
103
Low speed drogue (extending and retracting)
105-120
104
Low speed drogue (receiver engaged)
130
105
Severe turbulent air operations
180
106
Inoperative windshield ain’t-ice below 10k
187
107
Oxygen regulator pressure
270-340 (breathing) 270-455 (no flow)
108
Battery voltage
24 Vdc Min to charge 22
109
Loads (% of normal rated)
Ac generator 0-125 Ess and main DC busses 0-125
110
Propeller windmilling limitation for air start: NG < 7%, rotating <1/2 revolution/sec
3 min, or accelerate NG above 7% Or pull fire handle
111
Propeller windmilling limitations for air start: NG >/= 7%, rotating < 1/2 rev/sec
20 min or pull fire handle
112
Propeller windmilling limitation for air start Propeller windmilling > 1/2 rev/sec up to 100%
5 min or pull fire handle
113
Propeller windmilling limitation for air start: Fire handle pulled, propeller stopped or rotating <1/2 rev/sec
6 hours, run for 20 min to reset 6 hours

KC-130J (11 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2025 Bold Learning Solutions. Terms and Conditions