Sim Questions Flashcards

1
Q

Who monitors UHF guard emergency frequency?

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

What is the minimum taxiway width? Runway width?

A

30 feet; 80 feet (60 for max effort)

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

What are the taxi obstruction clearances?

A

Do not taxi an aircraft within 25 feet of obstructions without wing walkers. With wing walkers, avoid taxi obstructions by at least 10 feet

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

To minimize FOD potential while taxiing, use what engine setting?

A

low speed ground idle

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

How do you prevent skidding of the nose wheel?

A

By avoiding abrubt steering changes or by asymmetrical power and brake applications

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

What deviations are called out for heading, altitude, and airspeed?

A

heading: +/- 10 degrees
airspeed: +/- 10 knots
altitude: +/- 100 feet

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

Momentary minor corrections or deviations for stabilized approaches are acceptable and defined as: airspeed ______ from target; bank angle ______ from target; rate of descent _______ from target

A

airspeed: +10/-5 kts from target
bank angle: +/- 15 degrees from target
rate of descent: +/- 300 FPM from target

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

What UHF frequency is LRAFB ATIS broadcasted on?

A

251.1 (ch 16)

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

What call sign does 189 AW (AR ANG) use?

A

ROCK/PUMA/HIVE/CHEAT/PETRA/GOONY/HAWG/PROPS/SHAGGY/OUTLAW/HAWG

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

The radar altimeter is set to what altitude for departure/instrument approaches?

A

Set the radar altimeer to the HAT/Height above aerodrome (HAA) during instrument approaches [AFMAN11-2C-130HV3 5.12.4]

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

What instrument approach category is the C-130H? When will the next higher category be used?

A

Category “C” aircraft. If approach speeds exceed 140 knots, the minimums for category “D” will be used [AFMAN11-2C-140HV3 6.19]

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

For PAR approaches, Decision Altitude (DA) and visibility will be no lower than what values?

A

200 feet HAT and RVR 2400 (730 meters) or 1/2-mile visibility (800 meters) with no RVR readout available [AFMAN11-2C-130HV3 6.19.3.4)

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

Are you authorized to fly an RNAV (RNP) approach in a C-130H?

A

Not until aircraft navigation equipment is upgraded/certified, aircrews are rained, and MAJCOM/A3 has issued operational approval [AFMAN11-2C-130HV3 6.19.7]

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

“Established on track” for a VOR or TACAN procedure is defined as what? LOC? NDB?

A

VOR/TACAN: within half-full scale deflection
LOC: within full scale deflection
NDB: +/-5 degrees of required bearing of NDB

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

The stabilization points for instrument approaches is at _____ feet and ____ feet _____________.

A

500’ and 1000’ above touchdown

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

While on an ILS approach, do not descent below localizer minimums if the GSI indicates what?

A

if the aircraft is more than half-scale below or full scale above the glideslope [AFMAN11-202V3 16.8.9]

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

The ______ may never be used as the sole means of identifying the MAP

A

middle marker (MM) [AFMAN 11-202V3 16.8.10)

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

If being vectored for a PAR, what do you fly in case of lost communications?

A

Proceed with a published instrument approach procedure or previousy coordinated instructions. Change tansponder to appropriate codes.

Maintain last assigned altitude or the MSA/ESA, whichever is higher, until established on a segment of the published approach [FIH pg.13)

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

When performing an instrument takeoff, when do you raise the gear? Flaps?

A

When the airplane is in a definite climb as indicated by the altimeter and VVI, retract the gear.
Make an initial climb of at least 300 fpm, and retract flaps after airplane accelerates to a minimum of 20 knots above take-off speed. [TO 1C-130H-1 2-73]

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

When is radar service terminated when your aircraft is being vectored to a final approach course or when providing your own navigation on published routes to a final approach course?

A

landing is completed or when instructed to change advisory frequency at uncontrolled airports, whichever occurs first [AIM pg. 372]

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

Once an abort decision is made, what would you say is a key objective of any abort?

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

How do you call an abort?

A

On Takeoff: Any crewmember noting a safety of flight malfunction before hearing “go” or “rotate” (if refusal speed is greater than takeoff speed) will state “reject” and a brief description of the malfunction [AFMAN 11-2C-130H3 5.7.2]

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

If an engine failure occurs before reaching ______, the airplane must be stopped

A

refusal speed [TO 1C-130H-1 3A-14]

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

Define Vr

A

Based on the runway available - defined as the max speed to which the airplane can accelerate with engines at take-off power and then stop within the remainder of the runway available,

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Q

What is refusal speed based on?

A

with two engines (symmetrical power) in reverse, one engine in ground idle, one propeller windmilling and maximum anti-skid braking.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
26
Q

Balanced CFL is based on accelerating to? Unbalanced?

A

accelerate, lose an engine, and then either continue the takeoff with the remaining serviceable engines or stop in the remaining distance that makes up the balanced field length / Vmcg or Vrot, whichever is less, becomes the Vcef speed

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
27
Q

At what power setting is CFL based on?

A

Computed TO power, not exceeding 19,600 inch-pounds of torque

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
28
Q

Define Vmcg

A

the minimum airspeed at which the airplane may lose an outboard engine during the TO ground run and still maintain directional control

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
29
Q

When computing Vmcg for takeoff, when should the without-nosewheel steering option be used?

A

the lack of nosewheel steering is intended to represent reduced control on the ground due to wet, icy, or sand-covered runways [TO 1C-130H-1-1 3-24]

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
30
Q

What is the minimum a pilot must check when handed the mini TOLD chart?

A
  • verify GW independently from the TOLD card
  • Cross-check air minimum control Vmca (one engine INOP in ground effect), takeoff, and landing speeds
  • Review and compare the computed distances, ground roll, and climb gradient (if applicable) with the actual conditions, runway available, and departure procedures
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
31
Q

Define Vmca

A

Minimum speed at which a yawing tendency can be balanced with max rudder at a specified ban angle.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
32
Q

What is the airplane configuration for one engine inoperative Vmca?

A

a. No 1 engine windmilling on NTS
b. Zero bleed air
c. wings level
d. 180 pounds of rudder deflection or surface deflection
e. all other engines at max TO power
f. 50% flaps
g. 5 degrees bank
h. landing gear down

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
33
Q

A wings-level attitude requires an increase of approximately ____ (invariant with weight) above the charted one engine inoperative Vmca speeds. A 5-degree adverse bank angle (into the inoperative engine) requires a speed increase of ______ above the charted Vmca speeds at 80,000 pounds. This penalty increases significantly with increased gross weight (_______ at 140,000 pounds). Because of this effect, banked turns into the inoperative engine should _______.

A

11 KIAS ; 20 KIAS ; 37 KIAS ; be avoided

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
34
Q

Given the following, does Vmca increase or decrease?
a. Decrease in OAT:
b. Retracting the flaps:
c. Increase in PA:
d. Reduced power takeoff:
e. Feathered prop:

A
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
35
Q

If a nose wheel shimmy occurs on takeoff, the decision to continue or abort the takeoff will depend on the severity of the shimmy and ________ _______________. If the takeoff is continued, the nose wheel ____________ as soon as directional control permits to reduce the severity of the shimmy.

A

whether refusal speed has been reached. ; should be raised

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
36
Q

It is important to obtain two-engine minimum control speed as soon as possible after takeoff and prior to positioning the flap lever to less than _____. Why?

A

15%. Positioning is less or opeating the gear/flaps will increase the minimum control speed due to reduction in available hydraulic pressure

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
37
Q

During reduced power operations the throttles of operating engines may be advanced up to __________ as directional control permits.

A

maximum power

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
38
Q

If obstacle clearance is a consideration, pilots should be aware that obstacle clearance performance data is based on the assumption that gear retraction is initiated ________ after takeoff and propeller feathering initiated ________ after takeoff.

A

3 seconds ; 6 seconds

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
39
Q

In order to maintain directional control while stopping, the pilot must immediately make maximum use of _________________________.

A

nosewheel steering, flight controls, and differential braking

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
40
Q

Aircrew should minimize non-essential cockpit conversations and extraneous activities that could interfere with flight duties when operating below ______, during critical phases of flight, during periods of increased workload and during ___________.

A

18,000’ MSL ; periods of increased workload and during all taxi operations

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
41
Q

The minimum crew required to operate the H2 in flight is _______

A

pilot, copilot, engineer

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
42
Q

If taxi speed is 20 knots or higher, turn limit on the nose wheel steering is limited to _______

A

20 degrees

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
43
Q

The minimum amount of emergency brake pressure allowing one brake application is ____

A

2,900 PSI min

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
44
Q

What is the recommended airspeed for an air start? Max TIT?

A

TIT below 200 degrees C
airspeed: 180 KIAS or less

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
45
Q

During an air start, the flight engineer should call “NTS” by ______ and the copilot will release the condition lever to RUN at ______ which must occur by _______

A

10 percent RPM; until light-off

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
46
Q

A ground test valve is incorportated in the system so that pressure from the _______ hydraulic system may be used in ground maintenance operations

A

auxiliary hydraulic system

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
47
Q

MEL waiver authority for a training mission is ______

A

OG/CC

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
48
Q

Can a local training flight continue with an inoperative anti-skid system?

A

Yes - provided
1. flight manual performance limitations are applied
2. Is repaired at first capable repair facility
3. A local training flight may continue if the antiskid fails provided the system is turned off. Multiple landings are prohibited
4. Max effort or formation landing operations are prohibited

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
49
Q

If the suction boost pump fails, a ________ decrease in the static system pressure may also be indicated

A

100 to 200 PSI

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
50
Q

If using the manual landing gear selector valve button to lower the gear, the _________ will not be available if the button requires holding to lower the gear

A

hydraulic pressure

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
51
Q

When the name of the approach is followed by a single letter starting with the letter “A”, only ________ are provided on an instrument approach. The suffix letter is not used again for any procedures at that airfield.

A

circling minimums

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
52
Q

If a circling approach is to be flown at the destination, the weather must meet _______

A

both the ceiling and prevailing visibility minimums

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
53
Q

If a circling approach does not have a ceiling requirement published, how do you determine the required ceiling ?

A

the required ceiling is the HAA plus 100 feet and rounded up to the next one hundred foot value [afman11-202v3 18.14.7]

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
54
Q

If a circling approach is required, maintain ______. If approach speeds exceed ___ knots, the minimums for category “D” aircraft will be used

A

140 KIAS or approach speed, whichever is higher. ; 140 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
55
Q

The circling minima listed on instrument procedures apply to all approach types on the instrument procedure (e.g. ILS or LOC, VOR or TACAN, etc.). If planning to circle from an approach with vertical guidance, pilots must ensure the aircraft is within the _______ for the aircraft category and above the circling MDA before abandoning the ______

A

appropriate circling radius; precision glideslope

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
56
Q

What does the presence of the “negative (or inverse) C” symbol represent on the circling line of minima?

A

Circling approach protected areas used fixed-radius distances, depending on the a/c category

57
Q

For a straight-in or sidestep approach, the forecast weather for the destination must meet _______

A

required visibility minimums

58
Q

If full flight instrumentation is not available and operational, aircraft are limited to a DA/ Minimum Decest Altitude (MDA) based on a HAT of __________

A

300 feet and RVR 4000, or 3/4 mile visibility (1220 meters) with no RVR [afman11-2c-130hv3 6.19.4.1]

59
Q

When do you slow to approach speed on a circling maneuver?

A

When established on final

60
Q

If elevator control should fail (hydraulic assistance lost), achieve approximately level flight and _____ KIAS, using the ______ engines to assist in pitch control and the _____ engines to assist in airspeed

A

170 KIAS; inboard; outboard

61
Q

What are the 3 broad areas that most electrical malfunctions fall into?

A
  • Malfunctions of one or more of the primary power sources
  • Malfunctions on the distribution system
  • Malfunctions within equipment items
    [-1, 3A-32]
62
Q

Generator failure or generator system malfunction will be indicated by:
a. _________
b. __________
c. ___________
d. ___________

A

a. Illumination of a generator OUT light
b. Fluctuating/out of limits voltage and frequency
c. Illumination of a generator FAILED BRG light (some airplanes)
d. Illumination of a BUS OFF light

63
Q

What causes a Generator OUT Light to illuminate?

A

On airplanes with GCUs, if any phase voltage drops below 95 volts for more than 4 seconds, the gen out light will illuminate.
[-1, 3A-33]

64
Q

What cause an AC BUS OFF Light to illuminate?

A

If the average phase voltage of a generator is below approximately 90 volts, the BUS OFF light will illuminate.
[-1, 3A-33]

65
Q

If an engine bleed air regulator/valve cannot be closed (regulator/valve closure is determined by observing torque increase on the affected engine) and the bleed air system is leaking, it may be necessary to ______

A

shut down the engine

66
Q

When all bleed air switches are OFF, airflow to both air conditioner units is lose, thus ___________ the airplane

A

depressurizes

67
Q

In the event a fire is near an oxygen component or there is a possibility that the oxygen could increase the fire, consideration should be given to closing the ____________, provided portable oxygen bottles are adequate for the situation

A

oxygen manual shutoff valve

68
Q

For an APU emergency shutdown, how do you isolate the bleed air system if a fire persists after discharging the agent?

A

If condition persists, a break in the bleed air manifold may exist. Isolate by placing No 1 and No 2 bleed air switches to OFF and closing the divider valve. If the fire continues, discharge the remaining bottle.

69
Q

Normal airplane DC voltage: _____; Normal DC load: _______; Minimum battery voltage: _______

A

25-30V
1.03
24V

70
Q

Do all 4 Transformer Rectifiers (TRs) need to be operational for a local proficiency sortie?

A

yes

71
Q

Ensure the aircraft can meet or exceed the standard IFR departure climb gradient of 3.3% (____ feet power nautical mile) or the published climb gradient, whichever is higher, with _______ to the en route structure or an altitude at or above the minimum IFR altitude (MIA) within the en route structure

A
72
Q
A
73
Q

Obstacles that require a climb gradient greater than 200 feet per nautical mile for a very short distance only until the a/c is 200 above the DER are referred to as

A

low close in obstacles

74
Q

Name the different methods of IFR departure

A
75
Q

A ___________ may be reated to allow radar vectors to be sed in lieu of an ODP at some locations where an ODP has been established. _____ information states that headings are as assigned by ATC and climb gradients, when applicable, may be published immediately following the specified departure procedures

A
76
Q

What is the lowest weather minimums required for a takeoff from KLRF?

A
  • When less than 1600 but equal to or greater than 1000 RVR, crew may takeoff if mission priority dictates provided the runway has dual RVR readouts (touchdown and rollout) and displays (minimum RVR 1000 on both) and runway centerline lighting is operational
  • For runways with more than 1 operating RVR readout, it is mandatory the RVR reads a minimum of 1600 on all

If no RVR readout is available for the departure runway, visibility must be reported to be 1/2 mile (800 meters)

When wx is below approach and landing mins (ceiling or vis) a departure alternate is required

77
Q

When must you file a departure alternate?

A

if wx at airport is below the lowest landing minimums for suitable approach (ceiling or visibility or crosswinds)

78
Q

For a departure alternate within 30 minutes flying time, the existing weather must be equal to or better than the published approach minimums and forecast to remain so until 1 hour after _______, but in no case forecast to be lower than _______.

A

takeoff, 200-1/2 (RVR 2400)

79
Q

What are the 2 types of bleed air system failures?

A

Uncontrollable loss of bleed air and failure of an engine bleed air regulator

80
Q

The BUS OFF light will illuminate if the average phase voltage of a gen is below ____ volts; the GEN OUT light will illuminate any phase voltage drops below _____ volts for more than _____ seconds or exceed _____ volts for approx ____ seconds

A

90; 95; 4; 130; 5

81
Q

With a failed engine or engines, the yawing tendency caused by asymmetric thrust and windmilling propeller drag increases with increasing or decreasing speed and must be balanced by the aerodynamic controls, which become less effective with increasing or decreasing speed?

A

decreasing ; decreasing

82
Q

When landing with one or two engines inop, the air min control speed must be compared to the ______ and the higher of the two speeds used

A

recommended approach speed

83
Q

The approach for landing with 1 engine inop is made in the same manner as for a normal landing except flaps should not be extended more than 50% until _______

A

landing is assured

84
Q

Below _____ KIAS during flare, the combined flight idle thrust on the side with two engines operating will tend to turn the airplane into the side with only one operating engine

A

110

85
Q

Do not make ______ that result in large angles of yaw

A

hard rudder kicks

86
Q

Begin the 3 engine go around at or above ________

A

minimum control airspeed

87
Q

If a three engine go around must be attempted and speed is less than min control speed, it may be necessary to _________ to help maintain directional control until minimum control speed is attained

A

reduce power on the opposite engine

88
Q

It is important to obtain ________ as soon as possible after takeoff and prior to positioning the flaps lever to less than 15%

A

two engine min control speed

89
Q

What is the difference between Vmca1 and Vmca2?

A
90
Q

A wings level attitude requires an increase of approximately _____ KIAS above charted Vmca1 and _____ above charted Vmca2. For 5 degrees adverse bank: Vmca1 ______ KIAS, Vmca2 _______ KIAS

A

11 KIAS ; 14 ; 20 ; 30

91
Q

Banked turns into the inop engine should _______

A
92
Q

When using the c-130h2 autopilot, what are the implications of attempting to actuate manual elevator trim using the elevator trim switches on the control wheel?

A
93
Q

What are the steps to engage and command the autopilot to fly a specific heading?

A
94
Q

What are the steps to engage and command the autopilot to fly a coupled ILS approach?

A
95
Q

List 6 ways the autopilot may be disengaged. Which steps are considered the normal actions for discontinuing autopilot control?

A
  • positioning the elevator tab power selector switch out of the NORMAL position
  • actuating the elevator tab switch on the pilot’s or copilot’s control wheel
  • pulling AP circuit breaker
  • ## pressing the pilot’s or copilot’s go-around pushbutton
96
Q

The wx is 900 overcast with 2 miles vis and you are flying an autopilot coupled ILS approach. What are your responsibilities to ATC or the control tower?

A

Let tower know asap but no later then the FAF

97
Q

Once a holding pattern has been defined on the SCNS HOLD 1-2 and 2-2 pages, how do you command the SCNS to initially steer the airplane to the hold fix then around the outbound and inbound segments of the holding pattern?

A
98
Q

You are reviewing the ILS or LOC rwy 4R at KLIT and notice the IAP doesn’t have a published VDP. Why is this not published? If planning to fly the localizer only portion of the approach what special considerations should you consider if flying this procedure at night?

A
99
Q

What aircraft equipment (in addition to that required for normal operations) is required for NVG operations?

A
  • TCAS (Exeption: sytem must be operational, but OPSEC/EMCON guidance may require turning system off)
  • Pilot’s radar altimeter
  • SCNS with a min of one GPS or inertial navigation system (INS) must be operational for low-level flights flown using NVG enroute altitudes.
  • AN/APN-241. radar is required for single-ship, night, low-level flight.
  • VVI
100
Q

How should the crew utilize landing lights for NVG landings?

A

In landing areas with bright, incompatible lighting, overt aircraft lights may be necessary to achieve suitable landing references. or table 6.2 (ATTP 3-3)

101
Q

What should the pilot flying and pilot monitoring’s actions be if the pilot flying experiences spatial disorientation?

A

the PM will be ready to immediately assume aircraft control if the PF experiences spatial disorientation or an NVG malfunction (AFMAN11-2C-130HV3, 6.20)

102
Q

What are the weather minimums for NVG departures and approaches?

A

Departures: no different than normal takeoffs for qualified aircrew members (AFMAN11-2C-130H3, 6.16)
Approaches: VFR mins in accordance with AFMAN 11-202V3. qualified aircrews may fly IFR approaches with weather at approach mins. (6.20)

103
Q

When obstruction clearance is doubtful for taxiing, use one or more _____ ______. If _____ are unavailable, deplane one or more crewmembers to maintain obstruction clearance and provide marshalling using AFMAN 11-218 signals

A

wing walkers. If wing walkers (AFMAN11-2C-130HV3 5.9.2)

104
Q

How may the SCNS be utilized to aid in NVG ground operations?

A

taxiing

105
Q

What calls should the Navigator and PM make during NVG ground operations?

A

taxi GS.

106
Q

What are the required areas to be briefed for NVG operations?

A

review and coordinate NVG failure procedures for all phases of the mission, to include actions for smoke and fumes in the aircraft. Any crewmember who experiences NVG problems will inform the rest of the crew. If unable to regain the use of NVGs, the PIC should consider many factors for the mission. During cargo compartment emergencies, aircrews should return to normal lighting until the emergency is resolved. (AFMAN11-202V3, 4.21.14)

107
Q

What actions should a crew take if they experience an NVG failure after takeoff or after a go-around?

A

consider transitioning to overt lighting

108
Q

What actions should a crew take if they experience an NVG failure on landing?

A

consider transitioning to overt lighting or transferring the controls to the PM for the landing rollout, as the situation dictates (AFTTP 3-3, 6.8.5.6.3)

109
Q

You’re flying a SR in the CONUS using VFR procedures in VMC. What are your minimum altitudes according to AFMAN 11-202V3 and AFMAN 11-2C-130HV3?

A

At or below 1500 AGL (202V3 4.27.12.2)

110
Q

What are the minimum runway lengths for maximum effort takeoff and landings? What is the minimum runway lengths for maximum effort takeoff and landings? Whats the minimum runway width? Taxiway width?

A

minimum field length

  • when runwya widths less than 80 feet have lengths that fall within performance requirements for a normal landing, there is no requirement for max effort crews or procedures
  • runways less than 80 feet wide require max effort procedures if runway available is less than CFL
110
Q

When flying visual tactical approaches, how does stabilized approach criteria differ from normal approaches?

A
111
Q

When flying a VFR low-level route at 500 ft AGL, what is the minimum horizontal separation from the following?
a. A hospital
b. prohibited airspace
c. Nuclear power plants
d. magenta shaded areas on a TPC chart

A

a. 2,000’
b. 3 NM
c. 3 NM
d. 2,000’ radius (11-2C-130H3)

112
Q

At ____ KIAS, begin reducing reverse thrust if conditions permit to prevent debris from restricting visibility of damaging engines. Be at ground idle by _____KIAS. It’s also near this speed that the rudder becomes ineffective

A

60 KIAS; 40 KIAS (AFTTP 3-3)

113
Q

Name the components of the HOWDIE check

A

height of terrain, other side, wind, direction of turn, IAS, escape (AFTTP 3-3)

114
Q

You’re conducting a visual tactical approach. When may you descent from approach altitude?

A

until intercepting the planned glide slope and terrain clearance is assured (AFTTP 3-3, 6.3.5.1.2)

115
Q

How is the touchdown zone marked for a day VMC landing zone utilizing the AMP-1 marking pattern?

A

at a minimum, mark the touchdown zone and the end of the usable runway (not including the overrun) (DAFMAN13-217 4.4.3)

116
Q

For max effort landings, the max rate-of-decent (540 FPM) should be used for planning and wing fuel loads should be reduced accordingly. What are these fuel limitations?

A

-1

117
Q

In low level flight, pilots should be particularly alert for obstructions. Hills and mountains are easily avoided if the vis is good but radio and television towers, which may extend as much as 2,000 feet or more into the air, often from elevated ground, are less conspicuous. Even more dangerous, the guy-wires supporting such towers are virtually invisible. How far horizontally should you plan to avoid towers?

A

by a horizontal distance equal to at least the AGL height of the tower (11-202V3 12.13.3)

118
Q

When do most accidents occur in low level flight? Why?

A

turning and looking (11-202V3, 12.16)

119
Q

NVG enroute altitude is no lower than an indicated altitude of ___ feet above the highest ________, within the _________.

A

500 feet above the highest spot oterrain elevation within the tactical corridor (AFMAN11-2C-130H3, 13.5.1.4)

120
Q

If the aircrew does not visually identify the factor obstacles within the tactical corridor, the crew will climb to attain an altitude of ______ feet above the obstacle or avoid the obstacle laterally by _____ NM

A

500 feet above the obstacle or avoid the obstacle laterally by 2 NM (AFMAN11-2C-130HV3, 13.5.1.4)

121
Q

Warning: climb to MSA when the tactical situation allows to resolve any emergency procedures or if either the _____, ____, ______, ______, or _____ fail.

A

NVGs, SCNS, pressure altimeter, or radar altimeter ail (AFMAN11-2C-130H3, 13.5.1.4)

122
Q

For NVG tactical VFR approaches, bank angle will not exceed _____ degrees and the aircraft will not descent below ____ AGL until rolled out on final

A

45 degrees when any flaps are extended. 150 feet AGL until rolled out on final (AFMAN11-2c-130H3, 14.8)

123
Q

weather mins for NVG visual approaches, NVG visual pattern work, and crewmembers who are non-current and/or unqualified is _______

A

will adhere to VFR mins in accordance with AFMAN 11-202V3 (AFMAN11-2C-130HV3, 6.16)

124
Q

AFTTP 3-3C-130H suggests marking NVG controlling obstacle with what symbology?

A

red square

125
Q

Use an initial climb rate of _____ fpm at ____ knots GS (____ knots in mountainous terrain) to determine start-climb points

A

1,000 fpm at 220 KGS (240 knots in mountainous terrain) (AFTTP 3-3)

126
Q

Factor obstacles are those man made obstructions within the NVG corridor whose altitude plus ____ feet is greater than the NVG en route altitude Factor obstacles should be marked on charts with a _____. They should be annotated on a ______.

A

500 feet
black diamond
stick diagram
(AFTTP 3-3, 4.2.5.15)

127
Q

Beginning at _____ AGL, the PM should verbalize ______ and ______. The PM should also call out when passing ___ KIAS on landing roll

A

airspeed and rate of descent. 60 KIAS (AFMAN 11-2C-130HV3, 14.7.4.2)

128
Q

The reduction in field of view necessitates an active, aggressive scan on the part of the NVG wearer. A crewmember’s scan pattern may be disrupted _____ or _____. Under these conditions, an extra emphasis needs to be given to the ______, especially keeping the horizon in the field of regard.

A
129
Q

When approaching a ridge crossing, is it preferable to have a tailwind or a headwind?

A

tailwind (3-3,4.6.6.2.3)

130
Q

According to AFTTP 3-3.C-130H, what is the primary airdrop method?

A

MCAD (mission computer airdrop) - method of airdrop using the aircraft’s mission computer (SCNS) to navigate to the CARP. (7.3.1)

131
Q

According to AFTTP 3-3.C-130H, what are the typical personnel drop altitudes?

A

Between 800 and 1250 feet AGL (7.5.4)

132
Q

The HOWDIE check is a helpful acronym to use during ridge crossings. What do each of the letters stand for?

A

H - Height of terrain
O - Other side
W - Wind
D - Direction of travel
I - IAS at top
E - Escape path

133
Q

The 20, 10, 1 minute and 5 second advisories are required for all ______ airdrops?

A

personnel (AFMAN11-2C-130 16.11.2)

134
Q

When should a No Drop be called, who may call it, and who must acknowledge the call? (reference both AFMAN 11-2C130Hv3 and AFTTP 3-3.C-130H)

A

should the crew believe the drop will occur outside of safe parameters (11-2C-130H3 16.13)

If at 5 seconds, the slowdown checklist is not complete, any aircrew member believes the aircraft will not be inside the safety box at GL; or airspeed deviation is greater than 10 knots or altitude deviation is greater than 100 feet (AFTTP 3-3 7.4.8)

135
Q

For airdrops in visual conditions at or below 3,000’ AGL, the navigator develops and briefs a safety box using easily identifiable landmarks to identify the safety box boundaries. Navigators annotate these boundaries on a DZ mosaic. Select boundaries to ensure that if the airdrop is initiated anywhere inside of the safety box, the airdrop load or jumpers will land inside the surveyed DZ boundaries. For personnel airdrops, the navigator should also brief ____________ ___________ _____________.

A
136
Q

At 1 minute prior to release, the navigator will give the preparatory 1 minute advisory call. At 5 seconds prior to release, the navigator will give the preparatory 5 second advisory. At this time, the PM should _____________________________________.

A
137
Q

Loadmasters will acknowledge all time advisories except for ___________

A
138
Q

If the airdrop is aborted or a “no drop” situation occurs, the loadmaster will acknowledge “no drop?” and perform the completion of drop checklist. If the drop is to be reattempted, the airdrop checklist will be reinitiated beginning with ______________________.

A