Brainscape's Knowledge GenomeTM


Top Flashcards (Certified)
All Flashcards

C-130H > 1C-130H-1 Section 3 > Flashcards

1C-130H-1 Section 3 Flashcards

(81 cards)

Start Studying
1
Q

“land as soon as possible” expectations

A

Declare an emergency

Land at the nearest suitable airfield

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

“Land as soon as practical” expectations

A

Mission is to be terminated

An immediate landing at the nearest adequate airfield may not be necessary

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

Ground evacuation alarm bell signal

A

One long sustained ring

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

Bailout alarm bell signal

A

Prepare to bailout - three short rings

Bailout - one long sustained ring

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

Ditching or crashing landing alarm bell signal

A

Prepare to ditch/crash land - six short rings

Brace for impact - one long sustained ring

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

12 Engine shutdown conditions

A 
Certain propeller malfunctions
Uncontrollable rise in TIT
Uncontrollable rise in oil temperature 
Uncontrollable drop in oil pressure
Uncontrollable power
Unusual vibration or roughness
Nacelle overheat
Turbine overheat
Throttle control cable failure 
START VALVE OPEN light illuminates
Engine fire
Excessive visible fuel leak
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Engine shutdown procedure

A

CONDITION LEVER “FEATHER” (CP)

FIRE HANDLE “PULLED” (CP)

AGENT “DISCHARGED” (FOR FIRE OR NACELLE OVERHEAT)

  • land as soon as practical
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

If during the ESP, the fire or nacelle overheat condition persists after the first fire bottle is discharged, what should you do?

A

Isolate the wing by:

Placing engine bleed air switch to OFF

Closing the divider valve

If condition persists, discharge the remaining bottle on command of the pilot

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

APU EMERGENCY SHUTDOWN

A

FIRE HANDLE “PULLED” (E)

AGENT “DISCHARGED” (FOR FIRE) (E)

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

If during the APU EMERGENCY SHUTDOWN, the fire condition persists what should you do?

A

Isolate #1 and #2 by placing bleed air switches to OFF and closing the divider valve

If fire continues, discharge remaining bottle

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

Possible indicators of a bleed air leak:

A 
Fire warning lights
Low torque
Erratic engine instruments
Erratic electrical equipment
Wing overheat
Reduced bleed air manifold pressure

Note: bleed air failure is a land as soon as possible condition

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

Can you maintain aircraft pressurization with the bleed air switches turned OFF?

A

No, because airflow to both air conditioner units is lost

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

Should you open the APU bleed air valve after landing with an uncontrolled loss of bleed air that could not be isolated?

A

No, you could repressurize the leaking area

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

Steps for wing overtemp indication:

A

Wing anti-icing - OFF

If condition persists after 1 minute…

Affected wing bleed air switches - OFF

Bleed air divider valve - closed

APU/external air - OFF

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

Can a single air condition unit, augmented with under floor heat, maintain maximum cabin differential pressure?

A

Yes

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

Uncontrolled cabin pressure increase steps and cause:

A

Will only occur with a stuck outflow valve

  1. Turn off engine bleed air, one at a time
  2. Control px by turning bleed air on/off
  3. Shut down one air conditioning system if necessary to expedite depressurization
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

START VALVE OPEN LIGHT illuminated on the ground:

A

GROUND STOP and close the respective bleed air valve

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

ENGINE FIRE on the ground:

A

GROUND IDLE, ESP

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

Tailpipe fire/torching during start:

A

GROUND STOP, motor the engine

Note: if flames spread beyond the tailpipe, ESP

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

Tailpipe fire during flight:

A

Indicated by loss of oil quantity and/or heavy smoke

Monitor during flight and ESP prior to landing

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

Turbine overheat on the ground:

A

GROUND IDLE/GROUND STOP

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

Turbine overheat in the air:

A

Retard throttle toward FLIGHT IDLE

If condition persists, ESP

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

Nacelle overheat warning on the ground:

A

GROUND IDLE, ESP

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

High TIT on ground:

A

GROUND IDLE

TD switches NULL

if condition persists, GROUND STOP

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
High TIT in flight:
FLIGHT IDLE TD switches to NULL if condition persists, ESP
26
GROUND EGRESS
1. Set parking brake (P) 2. Notify tower (CP) 3. DC bus tie switch - TIED (E) 4. FEATHER (CP) 5. Evacuation command (P) 6. DC power switch - OFF (E) 7. SCNS power switch - OFF (N/E) 8. Chock airplane (LM)
27
During multiple engine power loss, why are the TD switches placed to NULL?
To remove the starting limiting fuel take that can occur in the AUTO position (at or below 94%, TIT limited to 830)
28
MULTIPLE ENGINE POWER LOSS/STALL/FLAMEOUT
TEMPERATURE DATUM CONTROL VALVE SWITCHES "NULL" (E) PROPELLER GOVERNOR CONTROL SWITCHES "MECH GOV" (CP/E) Note: land as soon as possible
29
With the loss of essential DC power, the engine bleed air regulator valves are fail safe: open or closed?
Closed
30
During multiple engine power loss/stall/flameout, why is the DC bus tied?
To power the essential DC bus, because the engine inlet air duct anti-icing valves will de-energize open, and may prevent engine recovery
31
For propeller malfunctions after takeoff, if no fire indications are present it is recommended to allow the engine to run until reaching what airspeed?
Vmca2
32
What is considered an uncontrolled propeller over speed?
Greater than 105%
33
Prop low oil light
Check for overspeed, underspeed, or fluctuation If RPM is within limits, continued operation is permissible If RPM is out of limits, place in MECH GOV If out of limits in MECH GOV, perform pitch lock check
34
Pitchlocked propeller
Operation in an underspeed condition is desirable (96-98%) Maintain a constant TAS to maintain constant RPM 150 KTAS if decoupled Do not allow RPM to decrease below 96%, ESP
35
Prop fails to feather
Reset fire handle if no fire indication exists Hold feather override button in for 30 seconds and then pull out 150 KTAS if possible
36
Decoupled propeller
Near zero torque, TIT, and fuel flow ESP
37
Prop brake failure
160 KIAS, not below Vmca2 If needed, accelerate in 10 knot increments to a maximum of 200 KIAS
38
Throttle control cable failure
Indicated by: - Throttle moves independently of pilot input - Throttle frozen or binding - Power unrelated to throttle position Shut down using fire handle
39
TD system malfunction
NULL LOCKED if fixed Pull fire handle to shut down if not fixed
40
SEC FUEL PUMP PRESS light above 65%
May be caused by failure of: - engine-driven fuel pump - pressure switch - paralleling valve stuck closed - failure of 65% switch in SSC Pull the ignition control CB
41
SSC failure (sheared shaft)
Indicated by: - SEC fuel pump press light - Electronic fuel correction light (>65% RPM) - TIT start limiting of 830 (>65% RPM) TD NULL Pull ignition control CB
42
Following a negative G condition, monitor GB and engine oil pressure for: If a loss of oil pressure occurs, ESP if oil pressure doesn't return to normal within:
2 minutes 10 seconds
43
Tach generator failure
Indicated by: - decrease or fluctuation of RPM and/or torque Synchrophaser OFF MECH GOVE
44
If cross feeding is being accomplished with the dump pumps, what should you be cognizant of?
Fuel transferring to uncommanded tanks. Anytime the dump manifold is pressurized, fuel can transfer into any tank if there is a failure of the check valve, refuel shutoff valve, or fuel line
45
An external fuel tank fuel level control valve failure may be indicated by:
Both boost pumps indicating less than 28 PSI
46
Fuel quantity indicator failure on 84-0206 and up will be indicated by:
Blank display, E6, E8, E9 codes, or totalizer going blank
47
Two things that you shouldn't do with a known or suspected fuel leak:
Use reverse thrust on landing Jettison or dispense flares
48
Prior to performing any procedure which removes all AC power, how should the fuel system be configured?
Tank to engine
49
Generator out light with normal frequency, voltage, and load:
Power indicator relay or TRU failure Leave the generator on and monitor freqs, volts, and load
50
Generator out light with freqs, volts, but no load:
Indicates a de-energized generator contact Place generator to OFF and monitor volts and freqs
51
Generator out light with no freqs, volt, or load:
Place generator to RESET then OFF If freqs and volts are normal on 3 phases, resume normal operation If no freqs or volts after RESET on 3 phases, the generator has failed (disconnect) If freqs and volts are indicated, but volts peak then drop to zero, an over voltage or feeder fault condition occurred (disconnect)
52
If phase voltage drops below __ volts for __ seconds or exceeds __ volts for __ seconds, the generator out light will illuminate
95 volts for 4 seconds 130 volts for 5 seconds
53
Generator failure on the ground
GROUND STOP
54
Hold the GEN DISC switch to DISC for approximately:
2 seconds
55
What should you do if a generator cannot be disconnected in flight?
ESP
56
LH DC BUS TRU FAULT INDICATOR
Deactivate LAIRCM by pulling the LH DC BUS TRU CB to prevent overheating or smoke and fumes
57
Indications of loss of essential AC bus:
Loss of autopilot (if in use) Heading indicator failure ESS AVI bus off light Loss of synchrophaser Malfunctioning nav equipment Illumination of th CPs AC instrument SEL PWR OUT light Loss of pilot's TCAS display
58
Illumination of the ISOL DC ON BAT/BAT DISCH light and/or battery voltage of 24 or less is an indication of:
RCR failure Note: illumination of the light, for a max of 25 seconds, is normal when high loads are placed on the essential AC or DC bus
59
Inflight door warning
Oxygen "ON, 100%" (on command of pilot) Depressurize Descend Aux Vent Check doors Master door warning light switch "OFF"
60
Cabin pressure for flight station windshield cracks or single pane in cargo compartment
10 in hg
61
Cabin pressure for both panes of cargo compartment window cracked
Zero in hg
62
If utility or booster hydraulic system pressure exceeds _____ PSI, do not turn off the hydraulic pump switches
3450
63
If hydraulic system pressure exceeds _____ PSI, follow the cruise engine shutdown procedure on an engine supplying the system
3900
64
Suction boost pump failure: if system pressure is less than _____ PSI, or hydraulic fluid level is decreasing, follow loss of system pressure procedure
2500
65
Failure of the utility hydraulic system will result in loss of:
Normal landing gear extension/retraction Normal brakes Nose wheel steering Half the flight controls
66
Loss of the aux hydraulic system will result in the loss of:
Cargo door and ramp Emergency brakes Emergency nose gear extension
67
Actions after a hard over maneuver in the flight controls:
Place the control boost switches to OFF Prepare to immediately adjust trim
68
Recommended control inputs and airspeed during an elevator control system failure:
Inboard engines for pitch Outboard engines for airspeed 170 KIAS
69
For aileron and rudder trip runaway:
Hold trim switch in the opposite direction Pull the CB
70
Elevator trim runaway
Hold the trim switch in the opposite direction Place the elevator trim switch to OFF Place the elevator trim switch in the EMER position and use the backup trim for operation of the trim tab
71
During an outboard flap failure that results in binding, do not attempt to move the flaps. If movement is necessary, move the flaps in ____ increments
10%
72
Two alternate methods for flap operation:
Overriding the flap selector valve on the utility hydraulic panel Mechanical operation of the flaps
73
Prior to landing with a known or suspected landing gear malfunction, if time permits, the engineer will visually inspect to confirm that:
The bottom of the ball nuts contact the bumper stops
74
If a hydraulic leak is the cause of the malfunction, or hydraulic pressure was lost after repositioning the landing gear lever, immediately place the landing gear lever in the ____ position and:
UP Pull the landing gear control CB
75
5 alternate landing gear operation methods:
Overriding the landing gear selector valve Manual gear extension (main gear) Emergency nose gear hydraulic extension Nose landing gear manual extension (free fall) Emergency manual main gear extension
76
If the electrical landing gear selector button required holding to lower the gear, hydraulic pressure will not be available for:
Nose wheel steering
77
Nose gear free fall flight parameters:
At or below 120 KIAS, but not below Vmca Pull the handle Accelerate quickly, but do not exceed 165 KIAS
78
How many chains and devices are required if the MLG tie down fixture is not available?
1X 25,000 lb. device and 3X 25,000 lb. chains per pair of struts OR 3X 10,000 lb. devices and 7X 10,000 lb. chains per pair of struts
79
Traffic pattern airspeeds when landing with two engines inoperative:
Downwind and base 160 KIAS Turn to final 150 KIAS or approach speed, whichever is higher
80
Recommended runway length and max weight for windmill taxi start
7000' 135,000 lbs
81
Airspeed and termination distance for windmill taxi start
100 KIAS until 4,000' remaining

C-130H (6 decks)

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