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HC-130P NAV MQF 110 - 165 RITTER
Part 3 of 4
56
Aviation
Professional
04/12/2012

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Cards

Term


110. Accuracy of the DOP and TAS submode solutions are maximized by entering a current ________ on the
FLT PRMTR 2-3 display page.

Ref: TO 1C-130-1-4 p 7-5

Definition
 A. compass deviation
Term


111. If critical memory information is not available due to battery failure or receiver replacement, or if the last
known position is invalid, the GPS will perform a cold initialization to collect the almanac information. A cold
initialization may take up to ____ hour(s) as opposed to the normally quick startup.

Ref: TO 1C-130-1-4 p 7-12

Definition
B. 2
Term

 

112. Air alignment may be performed if _______.

Ref: TO 1C-130-1-4 p 7-15

Definition
B. valid GPS or DVS data is available
Term


113. When the compass system is in DG mode, heading inputs [to the SCNS] are assumed to be grid format.

Ref: TO 1C-130-1-4 p 7-34

Definition
A. True
Term

114. Up to _____ DZ waypoints may be defined at a time.

Ref: TO 1C-130-1-4 p 7-35

Definition
 D. 8
Term


115. Up to _____ LZ waypoints may be defined at a time.

Ref: TO 1C-130-1-4 p 7-42

Definition
 C. 6
Term


116. If the order of the flight plan sequence is reversed, waypoint information that will be deleted includes:

Ref: TO 1C-130-1-4 p 7-30.1 (Fig 7-18)

Definition
 D. all the above
Term


117. Up to _______ reference points may be defined in the SCNS library.

Ref: TO 1C-130-1-4 p 7-26

Definition
 D. 450
Term

 

118. A flight plan may comprise up to _____________ waypoints.

Ref: TO 1C-130-1-4 p 7-27

Definition
 B. 68
Term


119. During sensitive steering operations, cross track error (XTK) is displayed in ____.


Ref: TO 1C-130-1-4 p 7-46

Definition

 C. yards
Term


120. The INS battery bus supplies DC power to the ___ and the _____ IDCU.

Ref: T.O. 1C-130-1-4 p 1-24

Definition
B. INU, navigator's
Term

121. How many oxygen recharger outlets are located on the HC-130P?

Ref: TO 1C-130(H)H-1 p 1T-2; TO IC-130(H)N-1, p.1-268.

Definition
 C. 9
Term


122. There are ___ portable oxygen bottles located on the HC-130P aircraft.

Ref: TO 1C-130(H)H-1 p 1T-2; TO IC-130(H)N-1, p.1-273.

Definition
 C. 10
Term


123. Which statement is not a WARNING associated with the AERP system?

Ref: TO 1C-130(H)H-1 p 1T-5 ; TO IC-130(H)N-1, p. 1-278.

Definition
 C. the AERP system will protect the user against rapid decompression on the aircraft
Term


124. There are _____ hand-operated fire extinguishers, _____ in the flight station and _____ in the cargo
compartment.

Ref: TO 1C-130(H)H-1 p 1V-3; TO IC-130(H)N-1, p.3-2.

Definition

 B. 4, 1, 3
Term


125. Emergency exit lights on the HC-130 may be actuated by _________.

Ref: TO 1C-130(H)H-1 p 1V-3; TO IC-130(H)N-1, p.1-310.

Definition
 D. all three answers are correct
Term


126. The crew entrance door jettison handle is a yellow handle located _______.

Ref: TO 1C-130(H)H-1 p 1U-6; TO IC-130(H)N-1, p.1-311.

Definition
 C. 3 feet to the left of the center line of the airplane and slightly aft of the pilot's side
Term

127. The navigator's shoulder harness reel lock will function automatically and provide proper restraint
regardless of which way the seat faces.

Ref: TO 1C-130(H)H-1 p 1U-7; TO IC-130(H)N-1, p.1-314.

Definition
 B. False
Term

128. The shoulder harness inertial reel LOCKED position is used only when a crash landing is anticipated.

Ref: TO 1C-130(H)H-1 p 1U-7; TO IC-130(H)N-1, p.1-314.

Definition

 A. True
Term


129. Life raft release handles are located in the following areas:

Ref: TO 1C-130(H)H-1 p 1V-3; TO IC-130(H)N-1, p.1-310.

Definition

 D. All of the above
Term


130. An emergency escape rope is installed ________ of each overhead escape hatch.

Ref: TO 1C-130(H)H-1 p 1V-2 ; TO IC-130(H)N-1, p.1-311.

Definition
 C. aft
Term

131. The WARNING associated with the center overhead escape rope ladder is ___________.

Ref: TO 1C-130(H)H-1 p 1V-2; TO IC-130(H)N-1, p.1-311.

Definition
 C. stand clear of area under rope latter when the ladder is released
Term

132. When more than one crewmember has the same checklist response to the same item, all subsequent to the
initial crewmember responding need respond only with crew position. (Exception: Altimeters)

Ref: TO 1C-130(H)H-1 p 2-3

Definition
 A. True
Term


 

133. On the ground, the signal to abandon the aircraft, if time and circumstances do not permit issuance of
verbal emergency instructions, is ___________________________________.

Ref: TO 1C-130(H)H-1 p 3A-4

Definition
 C. one long, sustained ring
Term

 

 134. When time and circumstances do not permit issuance of verbal emergency instructions, the signal for
ditching or crash landing imminent is ___________________________________.

Definition
 C. six short rings
Term

 

135. If a main wheel well fire exists, the area on both sides of the wheel will be cleared of personnel and
equipment for at least _____________ (or IAW AF directives if ammunition is aboard).

Ref: TO 1C-130(H)H-1 p 3A-9; TO IC-130(H)N-1, p.3-9.

Definition
B. 300 feet
Term


136. If a main wheel well fire exists, or if hot brakes are suspected, chock nose wheel only.

Ref: TO 1C-130(H)H-1 p 3A-10; TO IC-130(H)N-1, p.3-9.

Definition
 A. True
Term

137. Chopping locations are painted on each side of the fuselage _______________ . The locations are marked
in yellow on the inside and black on the outside of the fuselage.

Ref: TO 1C-130(H)H-1 p 3-9; TO IC-130(H)N-1, p.3-31.

Definition

 D. above and forward of the paratroop doors
Term


138. Do not dump fuel under _____ feet above the terrain. This will prevent the possibility of a ground source
igniting the fuel vapors.

Ref: TO 1C-130(H)H-1 p 3A-29; TO IC-130(H)N-1, p.3-31.

Definition
 B. 5000 ft AGL
Term


139. Circuit breakers should be pulled only ________________________.

Ref: TO 1C-130(H)H-1 p 3A-31; TO IC-130(H)N-1, p.3-31.

Definition

 B. during emergencies or maintenance
Term


140. If fire, smoke, or overheat of electrical equipment occurs, every attempt should be made to locate the
malfunctioning unit(s)/bus. If able to locate the source, isolate it by turning off/pulling circuit
breakers/removing the electrical plug(s).

Ref: TO 1C-130(H)H-1 p 3A-36; TO IC-130(H)N-1, p.3-40.

Definition
 A. True
Term

 141. Smoke developed in the cargo compartment will move forward into the flight deck. The forward escape
hatch must be opened to effectively eliminate smoke and fumes during all elimination emergencies.

Ref: TO 1C-130(H)H-1 p 3A-46; TO IC-130(H)N-1, p.3-51.

Definition
 A. True
Term


142. If flammable fumes are present, electrical equipment should not be turned on or off until the fumes are
eliminated

Ref: TO 1C-130(H)H-1 p 3A-44; TO IC-130(H)N-1, p.3-50.

Definition
 A. True
Term


143. If the door warning light illuminates in-flight, the airplane does not have to be completely depressurized
before making a door check.

Ref: TO 1C-130(H)H-1 p 3A-48; TO IC-130(H)N-1, p.3-53.

Definition
 B. False
Term


144. Do not attempt a takeoff with a known or suspected landing gear malfunction.

Ref: TO 1C-130(H)H-1 p 3A-57; TO IC-130(H)N-1, p.3-63.

Definition
 A. True
Term


145. If a malfunction is encountered in lowering the landing gear, once the landing gear is down and locked, it
will not be moved from this position.

Ref: TO 1C-130(H)H-1 p 3A-57; TO IC-130(H)N-1, p.3-63.

Definition
 A. True
Term


146. Ditching must be considered as a last resort and attempted only when conditions are ideal or there is no
other alternative.

Ref: TO 1C-130(H)H-1 p 3A-84; TO IC-130(H)N-1, p.3-88.

Definition

 A. True
Term


147. Overwater bailout avoids the numerous risks associated with ditching.

Ref: TO 1C-130(H)H-1 p 3A-76; TO IC-130(H)N-1, p.3-80.

Definition
 A. True
Term


148. Do not attempt to inflate the life jacket/LPU prior to bailing out as it may be damaged in egress from the
airplane as well as hinder the wearers in their exit.


Ref: TO 1C-130(H)H-1 p 3A-76; TO IC-130(H)N-1, p.3-80.

Definition
 A. True
Term


149. Bailout from the crew entrance door from a _________ position from the rear edge of the door.

Ref: TO 1C-130(H)H-1 p 3A-77; TO IC-130(H)N-1, p.3-82.

Definition
 C. squatting
Term


150. If the airplane is under control and time permits, the order of preference for bailout exits is
______________________________________.

Ref: TO 1C-130(H)H-1 p 3A-76; TO IC-130(H)N-1, p.3-80.

Definition
B. cargo ramp and door, paratroop doors, and forward crew door
Term

151. During a bailout, lowering the ramp above _____ knots may cause severe buffeting. If airspeed cannot be
reduced to _____ knots, open only the cargo door.

Ref: TO 1C-130(H)H-1 p 3A-77; TO IC-130(H)N-1, p.3-82.

Definition
 A. 150, 150
Term


152. The primary ground exit for flight deck members is __________.

Ref: TO 1C-130(H)H-1 p 3-78 (Fig 3A-16 Evacuation Routes); TO IC-130(H)N-1, p.3-14, 3-16

Definition
C. Crew Entrance Door
Term


153. Before making a gear-up landing, open all of the following:

Ref: TO 1C-130(H)H-1 p 3A-83; TO IC-130(H)N-1, p.3-87.

Definition
 A. the emergency escape hatches and paratroop doors
Term


154. To obtain direct contact with all intercom stations, regardless of their settings, use the ________.

Ref: TO 1C-130(H)H-1 p 1R-3; TO IC-130(H)N-1, p.4-13.

Definition

 B. call button
Term

 

155. To use the TACAN in the air to air mode, the receiving airplane/helicopter must select a channel _____
channels above or below the cooperating channel.


Ref: TO 1C-130(H)H-1 p 1Q-4; TO IC-130(H)N-1, p.4-76.

Definition
 A. 63
Term


156. To test the CARA for correct operation, set altitude reference to ________ feet using the SET control
knob.

Ref: TO 1C-130(H)H-1 p 1M-51; TO IC-130(H)N-1, p.4-78.

Definition

 C. 400
Term


157. [AN/APN-241] Real Beam Ground Map (RBGM) is the map mode provided during degraded radar
operations when incomplete stabilization data is being received in the radar from the INU (STAB LOST
condition).

Ref: TO 1C-130(H)H-1 p 1Q-19; TO IC-130(H)N-1, p.4-113.

Definition
 A. True
Term


158. [AN/APN-241] For range scales greater than ______NM, turbulence information data is not available.

Ref: TO 1C-130(H)H-1 p 1Q-22; TO IC-130(H)N-1, p.4-117.

Definition
D. 80
Term

159. [AN/APN-241] In skin paint mode the clutter notch selections are ______________ knots.

Ref: TO 1C-130(H)H-1 p 1Q-23; TO IC-130(H)N-1, p.4-118.

Definition
A. 55, 70, and 110
Term

160. [AN/APN-241] In the Skin Paint mode, the maximum range scale available is ______ NM.

Ref: TO 1C-130(H)H-1 p 1Q-23; TO IC-130(H)N-1, p.4-118.

Definition
 C. 20
Term


161. [AN/APN-241] When an overtemperature condition is detected, a flashing OVTEMP message is
displayed. To prevent damage to the system, the radar will automatically shut down if the temperature
continues to increase.

Ref: TO 1C-130(H)H-1 p 1Q-21; TO IC-130(H)N-1, p.4-119.

Definition
 A. True
Term


162. The C-12 compass systems begin to operate when power is supplied to the airplane electrical AC buses.
However, a ____ minute warmup is required for gyro stabilization.


Ref: TO 1C-130(H)H-1 Para: 1Q-9

Definition
 C. 5
Term


163. C-12 compass system. During directional gyro operations, the precession rate should not exceed _____
degrees per hour.

Ref: TO 1C-130(H)H-1 1Q-9

Definition
 A. 2
Term


164. Each C-12 compass system should be within _____ of actual airplane heading based on a ground or
airborne heading check.

Ref: TO 1C-130(H)H-1 p 1Q-9

Definition

 A. 1 degree
Term


165. The Latitude Knob is rotated to set the correct latitude location in degrees, of the airplane position. This
setting allows the compass system to automatically correct the __________ and __________ at the set latitude.

Ref: TO 1C-130(H)H-1 p 1Q-8

Definition
 C. Earth rate / coriolis errors
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