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 |
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Definition
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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 |
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Definition
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Term
112. Air alignment may be performed if _______.
Ref: TO 1C-130-1-4 p 7-15 |
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Definition
B. valid GPS or DVS data is available |
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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 |
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Definition
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Term
114. Up to _____ DZ waypoints may be defined at a time.
Ref: TO 1C-130-1-4 p 7-35 |
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Definition
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Term
115. Up to _____ LZ waypoints may be defined at a time.
Ref: TO 1C-130-1-4 p 7-42 |
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Definition
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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) |
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Definition
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Term
117. Up to _______ reference points may be defined in the SCNS library.
Ref: TO 1C-130-1-4 p 7-26 |
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Definition
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Term
118. A flight plan may comprise up to _____________ waypoints.
Ref: TO 1C-130-1-4 p 7-27 |
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Definition
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Term
119. During sensitive steering operations, cross track error (XTK) is displayed in ____.
Ref: TO 1C-130-1-4 p 7-46
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Definition
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Term
120. The INS battery bus supplies DC power to the ___ and the _____ IDCU.
Ref: T.O. 1C-130-1-4 p 1-24 |
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Definition
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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. |
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Definition
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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. |
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Definition
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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. |
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Definition
C. the AERP system will protect the user against rapid decompression on the aircraft |
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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. |
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Definition
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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. |
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Definition
D. all three answers are correct |
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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. |
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Definition
C. 3 feet to the left of the center line of the airplane and slightly aft of the pilot's side |
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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. |
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Definition
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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. |
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Definition
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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. |
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Definition
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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. |
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Definition
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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. |
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Definition
C. stand clear of area under rope latter when the ladder is released |
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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 |
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Definition
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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 |
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Definition
C. one long, sustained ring |
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Term
134. When time and circumstances do not permit issuance of verbal emergency instructions, the signal for ditching or crash landing imminent is ___________________________________. |
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Definition
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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. |
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Definition
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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. |
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Definition
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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. |
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Definition
D. above and forward of the paratroop doors |
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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. |
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Definition
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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. |
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Definition
B. during emergencies or maintenance |
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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. |
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Definition
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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. |
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Definition
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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. |
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Definition
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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. |
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Definition
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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. |
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Definition
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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. |
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Definition
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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. |
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Definition
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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. |
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Definition
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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.
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Definition
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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. |
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Definition
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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. |
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Definition
B. cargo ramp and door, paratroop doors, and forward crew door |
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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. |
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Definition
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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 |
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Definition
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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. |
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Definition
A. the emergency escape hatches and paratroop doors |
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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. |
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Definition
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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.
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Definition
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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. |
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Definition
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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. |
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Definition
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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. |
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Definition
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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. |
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Definition
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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. |
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Definition
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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. |
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Definition
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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
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Definition
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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 |
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Definition
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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 |
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Definition
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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 |
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Definition
C. Earth rate / coriolis errors |
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