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

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

112. Air alignment may be performed if _______.

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

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

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

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

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

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

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)

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

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

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

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

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

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

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

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

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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

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

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

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.

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.

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.

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.

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.

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.

 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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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

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.

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.

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.

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.

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.

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.

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.

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.

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.

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

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

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

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