Ballistics, Ammo Characteristics, Delivery Techniques FM 1-140

1. Neutralization knocks a target out of action temporarily. Neutralization of a target occurs when it suffers at least % percent or more casualties or damage. Reference FM 3-04.140, C1, par B-38, Pg B-7

2. is caused by the motion of the helicopter as the projectile leaves the weapon. (FM 3-04.140, pg 4-5)

3. The four types of ballistics are .(FM 3-04.140, pg 4-1).

4. Rockets are most accurate when fired IGE / OGE . (circle one).(FM 3-04.140, pg 4-5).. 5. Angular Rate Error is an example of what type of ballistic? (FM 3-04.140, pg 4-5).

6. Maximum effective range is defined as: . (FM 3-04.140, pg 7-2)

7. Is the Hellfire Missile is affected by Angular Rate Error? . (FM 3-04.140, pg 4-5)

8. The two types of fire are . FM 5-20(FM 101-5-1) • Direct fire is “fire directed at a target that is visible to the firer or firing unit.”• Indirect fire is “fire delivered on a target which cannot be seen by the firing unit.” (FM 3-04.140, pg 7-1)

9. The three modes of fires are . (FM 3-04.140, pg 7-1)

10. The 4 “T”s associated with aircraft control (firing techniques) during rocket engagements are? , , . (FM 3-04.140, pg 7-6)

11. Trajectory shift and Projectile drift combine to create the .(FM 3-04.140, p4-7)

12. Rockets will accelerate as they leave the launcher, the crosswind force acting upon the fins which causes the nose of the rocket to turn into the wind is known as (FM 3-04.140, pg 4-8)

13. Gravity, Yaw, and Wind Drift are what type of ballistics? (FM 3-04.140, pg 4-2)

14. What are three factors that effect dispersion? (FM 3-04.140, pg 4-12)

15. Angle of Impact is a characteristic of what type of ballistic? (FM 3-04.140, pg 4-11)

16. What is the cause of the greatest error for free flight rockets (besides poor pilot technique) and what is done to minimize that error? (FM 3-04.140, pg 4-1 & 4-2)

17. Firing rockets at maximum ranges Increases / Decreases (circle one) dispersion and Increases/ Decreases (circle one) accuracy. (FM 3-04.140, pg 4-12)

18. Yaw is the angle between the centerline of the projectile and its trajectory which results in the projectile’s trajectory changing which increases . Where would a projectile have its maximum Yaw? (FM 3-04.140, pg 4-2).

19. What two factors determine the amount of wind drift of a projectile. (FM 3-04.140, pg 4-3)

20. The exterior ballistic which causes a clockwise spinning projectile to move to the right is called? …………….. (FM 3-04.140, pg 4-2)

21. The MPSM submunition (M73) will land degrees off center percent of the time, resulting in a 90% probability of producing personnel injuries within a meter radius. (FM 3-04.140, pg 5-11)

22. Fragmentation effects can be expected from the M789 HEDP 30mm round within a meter radius.(FM 3-04.140, pg 5-6)

24. What is the approximate muzzle velocity of the 30mm round? fps (FM 3-04.140, pg 5-6)

25. What are the visual markings of the M789 30mm HEDP round? (FM 3-04.140, pg 5-7)

26. What are the visual markings of the M788 30mm TP round? (FM 3-04.140, pg 5-7)

27. When using ADEN (brass cartridge) 30mm ammo multiply the weight and moment by to compute the weight and balance. If using DEFA (steel cartridge) multiply by (-10-2, pg 6-15)

28. Arming of the Hellfire missile is based on a 10g acceleration and occurs between - meters after launch (FM 3-04.140, pg 5-22)

29. Maximum velocity of the Hellfire missile is meters per second, MACH , or MPH. (FM 3-04.140, pg 5-22).

30. The M261 MPSM has submunitions and provides range settings from meters to approximately meters. (FM 3-04.140, pg 5-10)

31. During running fire, align the helicopter into firing constraints with the while maintaining . . (ATM Page 4-199)

32. Running fire performed at airspeeds will offer a mix aircraft survivability and weapons accuracy. (TC 1-251 Task 1422 pg 4-171)

33. During running fire to avoid fratricide, do not engage when target area . ( TC 1-251 task 1422 pg 4-172, Note 3)

34. Fire delivered on a target, which cannot be seen by the firing unit, is known as . (FM 3-04.140, pg7-1)

35. The bursting radius of the M151 HE “10 Pounder” is and can produce a lethality radius in excess of . (FM 3-04.140, pg 5-10)

36. The M789 HEDP can penetrate in excess of of RHA at 2500 meters. (FM 3-04.140, pg 5-6)

37. You fire a burst of 30mm at a target, which misses to the left about 10 meters, you then adjust your line of sight to the right of the target and fire again hitting the target. What technique did you use? The . (FM 3-04.140, pg 7-7)

39. When planning a running fire engagement, when should the crew perform the “Bump” to unmask the active LOS? . (TC 1-251, task 1422 pg 4-172)

40. When conducting running fire engagements what airspeed does the ATM recommend and why? Suggested . (TC 1-251, task 1422 pg 4-172, Note 2)

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AWS

41. When conducting AWS Harmonization, the target should be located to (± ) meters in front of the aircraft. (TC 1-251, task 1469 pg 4-206)

42. When conducting AWS Harmonization, the CPG positions the GUN DH reticle over the actual impact point of the rounds. momentarily to store. (TC 1-251, task 1469 pg 4-207)

43. The AWS ammo handling system has a maximum capacity of . (-10-2. pg 4-89)

44. The 30mm Gun turret azimuth and elevation limits are? +/- AZ, + EL(+ within +/- deg. Of centerline, - Depression. (-10-2, pg 4-89)

45. The gun duty cycle is as follows: (-10-2, pg 4-90 and 4-91)

46. What is the “WARNING” associated with the 30mm? . (-10-2, pg 4-90 and 4-92)

47. The software range limit that the WP will provide fire control solutions for the 30mm is? . (-10, pg 4-89 and TC 1-251 pg 4-202)

48. In the event of a power loss the gun is spring driven to + degrees in elevation to prevent during landing (-10-2 pg. 4-89)

49. The warning regarding 30mm stoppage states: If or more rounds have been fired in the preceding 10 minutes, and a stoppage occurs, personnel must remain clear of the aircraft for m inutes. And the crew .(-10-2, pg 4-92)

50. The M789 HEDP 30mm round is an and round, and will penetrate of more than . (FM 3-04.140, pg 5-6)

51. The AWS WILL / WILL NOT (circle one) continue to follow the IHADSS LOS when operating in the NVS FIXED mode. (-10-2, pg 4-89, caution)

52. When the AWS is in the fixed gun Position, the WP will command the turret to + degrees in elevation, and +/- degrees in azimuth. (Boeing Software update for LOT 11 Slide 105 and 6.2) (-10-2, 140, and ATM is currently wrong)

53. In the event of an IHADSS failure with the gun selected and the HMD as the selected sight, the gun will remain in the last commanded position gun firing is . When the gun is de-actioned, it will . (–10-2, pg 4-22 Warning)

54. The 30mm AWS is limited to + - degrees with rockets actioned and degrees on the side of the next missile to be fired with missiles actioned when on the inboard pylon. (for ref only: TC 1-251 Feb 2000, task 1464 pg 4-288) & (student handout PFN 11-0921 AWS pg D-22 and D-23)

55. What is the elevation of the gun in the FIXED mode. + . . Boeing Software Update LOT 11

56. What is the Caution associated with the SQUAT ORIDE switch on the Load Maintenance Panel? . (-10-2 4-85)

57. The Sideloader/ Magazine Controller (S/MC) performs three distinct ammunition handling system functions? . (-10-2 pg 4-89)

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58. The 30mm can accommodate 3 different types of rounds? . (-10-2 pg 4-89) (ADEN Brass (British) DEFA Steel (French) cartridges)

59. The rate of fire for the 30 mm is? (-10 pg 4-89)

60. How many rounds will be displayed on the 30mm while in the training mode? (-10-2 pg.4-110)

Rockets

61. Wing Stores Pylons are commanded to the single fixed position of _____ degrees when the squat switch indicates airborne for more than ____ seconds. (–10-2, pg 4-93)

62. An MPSM shape-charge will penetrate in excess of inches of armor. (FM 3-04.140, pg 5-11)

63. The PEN button on the rocket control page may be used to defeat bunkers up to meters thick when the BNK is selected. SHO 11-0922 for ARS page D-18 or The bunker- or building-penetration mode provides up to 10 feet of penetration before detonation, referenced from the M433 fuze in FM 3-04.140 5-14,

64. With Hellfire Rails on pylons 2 and 3, and rocket launchers on pylons 1 and 4, what rocket zones and quantities of each are available? A- , B- , E- (-10-2, pg 4-94)

65. When rockets are in the cooperative mode the WP will use the and will disregard the . (TC 1-251, task 1462 pg 4-198)

66. Is the pilot permitted to make changes to the RKT page when in the cooperative mode. . … … )TC 1-251, task 1462 pg 4-198 NOTE)

67. Due to the possibility of surging the engines, do not fire rockets from inboard stations. Fire no more than with two launchers every seconds or fire with only outboard launcher installed without restrictions. (-10-2, pg 4-94)

68. The minimum range the MK66 rocket with M439 / M261 MPSM can be fired is M. (–10-2, pg 4-94)

69. Label the rocket steering cursors:

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T T

70. The target area coverage achieved by an M261 MPSM warhead as range increases. (FM 3-04.140, pg 5-11)

71. There are submunitions in each M261 MPSM warheads. (FM 3-04.140, pg 5-10)

72. In each M267 MPSM training warhead there are inert submunitions and smoke producing submunitions. (FM 3-04.140, pg 5-12)

73. Maximum range for MK66 rockets meters. TC 1-251 Task 1462 pg 4-196

74. What is a RAD and what does it do? . (FM 3-04.140, pg 5-10)

75. When forward airspeed exceeds KTAS, do not use M229/M423 (“17 pounder”) warhead/fuse combination for engagement of targets under ft distance, and ensure the line of fire is clear of obstruction (trees/buildings) for at least ft. (-10-2 pg.4-94)

76. Is the use of the MK66 MOD 2 rocket motor authorized? (-10-2, pg. 4-94)

77. Do not fire rockets with the M433 RC fuse in situations where they might fly closer than m from other airborne helicopters. (-10, pg.4-94)

78. The Aerial Rocket Subsystem can be employed independently by either crewmember or in the cooperative mode when the active sight is? . TC 1-251 pg 4-195 and pg 4-197)

79. What is the maximum airspeed for firing MPSM rockets? knots (-10-2 pg.4-94)

80. How can the crew check/verify the rocket type within each of the rocket zones and the amount of gun ammo loaded on preflight? Can these setting be change on the MPD load page? ,, ,,,,,,,, … . (-10-2, pg 4-85)

81. The pylons articulate independently and are controlled by the weapons processor through a range of + to – degrees. (-10-2, pg 4-93)

82. What does the inclusion of a HERO filter provide for a rocket? . (FM 3-04.140 Glossary, and pg 5-8)

PTWS

83. The minimum cloud ceiling to fire a “K” model missile in any mode (i.e. LOBL / LOAL) is? . (FM 3-04.140, pg 5-34)

84. What is the definition of Ripple fire? .(TC 1-251, task 1458 pg 4-177)

85. What symbol is displayed on the RF missile icon to indicate that the missile is ready to receive the target? “ ” (-10-2, pg 4-100)

86. When the RF missile-training mode is enabled, what symbol will be displayed on all tactical RF missile icons? “ ” (-10-2, pg 4-108 NOTE)

87. What does the TME emulate and replicate? . (–10-2, pg 4-108)

88. How long is the allowable training mode, missile elapsed ON time? minutes. (–10-2, pg 4-108)

89. What symbol will appear on the RF missile icon if the maximum allowable elapsed ON time is exceeded? “ ” (-10-2, pg 4-108)

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90. What is “transfer alignment”? . (–10-2, pg 4-100)

91. What are the three acquisition sources that may provide targeting information for an RF missile target handover? (–10-2, pg 4-100)

92. When will a centered “T” be displayed in the missile constraints box? . (-10-2, pg 4-100)

93. Why would the RF missile LOBL INHIBIT option be used? . (TC 1-251, task 1458 pg 4-188)

94. Which page has the command to “arm” the hellfire launchers without pressing the master “arm/safe” button? (–10-2, pg 4-88)

95. Can the BACKSCATTER inhibit be overridden by the trigger’s second detent? (TC 1-251 task 1458 pg 4-180)

96. At what time and for how long is the message “LASE NN TRGT” displayed in the High Action Display during LOAL SAL missile launches? (–10-2, pg 4-32 and 4-35)

97. What does the message “TARGET DATA?” mean in the HAD? (-10-2, pg 4-33)

98. The missile counter-counter measures (MSL CCM) button enables the counter-counter measure routine within the laser missile. This selection: (a) .(b) . (LBHMMS 11-0923 D-28)

99. The minimum altitude is meters to prevent the RF missile from impacting the ground during launch. (FM 3-04.140, pg 5-48)

100. To enable the missile to fly an arc outside the TADS target LOS and prevent degradation of TADS Video the aircraft should be rotated ____ to ____ degrees in the direction of the missile to be launched. . (FM 3-04.140, pg 5-37 and pg 5-38 fig 5-21).

101. An RF missile will arm only after launch when acceleration exceeds g's, approximately in front of the aircraft. (LBHMMS 11-0923 D-78)

102. During a remote designation, the designator should not be positioned within degree fan either side of the launching aircraft to target line or outside ±60 designator offset angle. (LBHMMS 11-0923 D-60)

103. Minimum SAL LOAL engagement ranges should be increased by meters if the target is 50 to 400 feet below the aircraft. (FM 3-04.140, pg 5-32)

104. Minimum SAL LOAL engagement ranges should be increased by meters if the target is 401 to 800 feet below the aircraft. (FM 3-04.140, pg 5-32)

105. Backscatter is generally caused by . (FM 3-04.140, pg 5-35)

106. List the seven laser related missile performance distracters. . (FM 3-04.140, pg 5-35 thru 5-40)

107. The 2ND target inhibit button is used to prevent secondary target information from being handed over from the FCR to the RF missile during a target engagement. Is this button common to both crewmembers? (-10-2, pg 4-104)

108. A RF missile uses a curved trajectory to induce relative motion between a stationary target and its background by flying an off-axis path to the target. This is called .

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( FM 3-04.140 pg 5-54 & 5-55)

109. What kind of DBS trajectory will a missile fly if the target is to the left of centerline? (FM 3-04-140 Pg 5-55)

110. Automatic RF missile power management. (Missiles Actioned) Complete the right column. (-10-2, pg 4-104)

Missiles available Missiles powered8

4-7 2-3 1 *

* Unless missiles are actioned, then 1 is powered.

111. The AUTO button will enable automatic missile power management. In the AUTO mode RF missiles will be powered up at minute intervals. This Does / Does not (circle one) occur when missiles are WAS ed. LBHMMS 11-0923 Pg D-65

112. The AUTO button will enable automatic missile power management, this prevents? . (-10-2 pg 4-104)

113. At a 20 degree offset launch angle an RF missile azimuth flight profile will use a maximum cross range of Meters at 8 km. FM 3-04.140, pg 5-51)

114. The LOAL LO/HI mode constraints box is always driven by what is displayed in the FCR/TSD page ACQ source window. True / False (TC 1-251 task 1458 pg 4-184(d)

115. What is the minimum engagement ranges for a LOAL DIR SAL “K” missile at zero degree offset? , . M At 7.5 degree offset? FM 3-04.140, pg 5-34)

116. What is the minimum effective range of a “K” LOBL engagement with a 0 degree offset angle from the aircraft datum line? m With a 20 degree offset? m. (FM 3-04.140, pg 5-34)

117. The LOBL missile constraint box is degrees. TC 1-251 pg 4-181

118. The LOAL missile constraint box is degrees. TC 1-251 pg 4-182

119. If the RF missile is tracking and the target range is greater than or equal to Km , the allowable constraints angle is degree. -10-2 Pg 4-30

120. If the RF missile is tracking and the target range is less than Km, the allowable constraints angle is degrees. -10-2 Pg 4-30

121. A flashing “R” in the Missile status and Inventory field indicates what? (-10-2, pg 4-99)

122. Define the following missile status messages: (-10-2, pg 4-99 and 4-100)

1. 2. 3. 1. .O M S 2. .T U F 3. .

123. What is the minimum effective range of a “K” LOAL-LO engagement with a 0 degree offset angle from the aircraft datum line? m. With a 7.5 Degree offset? m (FM 3-04-140 Pg 5-34)

124. What is the minimum effective range of a “K” LOAL-HI engagement with a 0 degree offset angle from the aircraft datum line? m. With a 7.5 Degree offset? m. (FM 3-04-140 Pg 5-34)

125. Where is the hazard area for a radiating RF missile located? . FM 3-04-140 Pg 5-42

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126. Training missile emulator (TME) can simulate up to RF missiles on the launcher for training. (-10-2 Pg 4-108)

127. What is the weight of an AGM-114L Longbow HELLFIRE missile? lbs (-10-2 pg 6-14)

128. What does the DEICE Button on the SAL missile page for? . (-10-2 pg 4-101)

129. What are the three modes the RF missile operates in? , FM 3-04-140 Pg 5-42

130. If the sight selected is FCR, what type of missile page will be displayed when the missile system is actioned or the missile button is selected? (LBHMMS 11-0923 D-24)

131. The maximum mask height and minimum standoff distance for a LOAL LO missile are? A LOAL HI? ‘ . (3-04.140 pgs 5-29 and 5-30 Fig 5-13 and 5-15)

FCR/RFI

132. The FCR has been selected as the active sight and the RF handover data recently received has been detected as outside the optimum navigational parameters for weapons engagement. ‘ . What HAD Sight Status Field message will be displayed? “ ” (-10-2, pg 4-33)

133. The FCR will provide reliable data while maneuvering up to degrees in roll and + degrees to - . degrees in pitch. (-10-2, pg 4-45 Note)

134.The GTM/RMAP FOV is: WFOV degrees, MFOV degrees, NFOV degrees and ZFOV . (-10-2, pg 4-55)

135. Which FCR priority scheme emphasizes only stationary ground targets? . (-10-2, pg 4-64)

136. Moving target symbols become stale after Seconds and stationary become stale after seconds. (-10-2, pg 4-52)

137. A single scan burst in GTM narrow FOV will give scans. (-10-2, pg 4-47)

138. When the FCR detects a moving targets at distances between K and K the RF missile will always default to . (TC 1-251 task 1458 pg 4-188 Note 2)

139. improves STI detection and classification and Moving Target Indicator (MTI) classification (-10-2 pg 4-48)

140. What does a flashing (3 second) ANTS symbol indicate? . (-10-2, pg 4-53)

141. switch is used to rapidly position the FCR centerline to the line of bearing of an emitting threat as detected by the RFI (-10-2, pg 4-66)

142. A cued search may be performed on a Fine Detect or Course Detect region of the RFI to? . .(-10-2, pg 4-66)

143. A maximum of RFI emitters can be displayed. (-10-2, pg 4-65)

144. RFI number one emitter will be displayed with a around the threat Symbol and target type. (-10-2 pg 4-65)

145. After RFI emitters have ceased radiating for seconds , the symbols will change to partial intensity TC 1-251, pg 4-108).

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146. The TSD page will display inside of the ASE footprint. (Boeing software V13 update) Slide 10 of ASE

147. The TSD page will display type targets outside of the ASE footprint. TC 1-251 pg 4-108)

148. The RFI can detect and radar signals. (-10-2, pg 4-113)

149. Label the following FCR targets: (-10-2, pg 4-52 Fig 4-47)

150. What does the message “RFI DATA ?” mean? . (-10-2, pg 4-33)

151. What is the caution associated with use of the FCR TEMP ORIDE button? . (-10-2, pg 4-63 CAUTION)

152. Which Priority scheme would you use if you expected to engage targets which on the move. . (-10-2 pg 4-64)

153. What will happen if you press the Display Zoom switch on the RH ORT Grip? . (-10-2, pg 4-12)

154. Label the following RFI. icons (-10-2 pg 4-65 Fig 4-70)

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1 31 31 3

X X

X X

ICON

ICON

ICON

(FLASHING)

ICON

155. A maximum of symbols may be displayed on the FCR page TPM format or IHADSS C-Scope formats at any one time. (-10-2 pg 4-62)

156. Terrain Sensitivity is for open fields and wooded areas with loose detection thresholds. (BOEING TRAINING MATERIAL V13 Sights SLIDE 18) Note: -10-2 is incorrect for sensitivity settings and will be corrected with -10 change???

157. selection in extreme cold weather (-10 deg C or colder) could result in damage to the FCR. (-10-2 pg. 4-63)

158. A shot-at symbol will be displayed beneath target symbols a scan burst and prior to a hellfire missile launch (-10-2 pg 4-53)

159. Terrain Profile Mode wide format displays a 180-degree scan sector when groundspeed decreases below knots and until increasing above knots. Narrow format displays a 90-degree scan sector when the ground speed increases above knots and until decreasing below knots. (-10-2 pg 4-65)

160. Selecting an RFI detected emitter using the cursor . (-10-2 pg 4-66)

161. Continuing to press the cued switch will . (-10-2 pg 4-66)

162. Friendly emitters are displayed in CYAN and enemy/gray emitters are displayed in . (-10-2 pg 4-118)

163. Selection of other than #1 emitter with the CAQ enabled places (selected emitter symbol) over that emitter. (-10-2 pg 4-66 and 4-67)

TADS

164. What does the LRFD in the “Last” position do? . (TC 1-251 task 1458 pg 4-178)

165. What is the maximum PRF laser frequency that may be entered? . (-10-2, pg 102 figure 4-101 and TC 1-251 pg 4-176)

166. Squeezing the laser trigger to the second detent provides: . (–10-2, pg 4-17)

167. After the initial internal boresight when will the INTERNAL B/S message will be displayed ? 1) Equal to or less than º F ( ºC), and the average optics temperature changes by greater than ºF ( ºC) (2) Equal to or less than º F ( ºC), and the average optics temperature changes by greater than ºF ( ºC)

168. When initiating internal boresight the sight is automatically set to and the sensor will be set to and the FOV to . (-10-2 pg 4-44)

169. During a TADS Drift Null, the aim point should remain within the . (-10-2, pg 4-43)

170. The initial automated internal boresight process takes approximately minutes due to the cue search process and subsequent boresights take approximately seconds as they use the AZ and EL cue data from the initial boresight. (Sights handout 11-0924 pg D-79)

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171. Following an internal boresight, which FOVs should be used in conjunction with laser operations? . (TC 1-251, task 1138 pg 4-100)

172. If the FLIR is not cooled when DTV is boresighted the FLIR boresight will . However, the DTV boresight is still valid. (Sights handout 11-0924 pg D-83)

173. During internal boresight the FLIR boresight will not start until the trigger is released. (Sights handout 11-0924 pg D-82)

174. Internal errors can develop in-flight due to temperature changes within the internal components of the TADS (thermal drift). When confidence in the boresight is suspect, an internal boresight should be accomplished. Recommended every ) (TC 1-251, task 1138 pg 4-100)

175. When the TADS is used as a sensor the range focus cannot be adjusted. T/F (Sights handout 11-0924 pg D-52)

176. The maximum allowable registration error allowed is ft at ft, which can be estimated by using the open area of the LOS reticle, which is equivalent to ft at ft. (-10-2, pg 4-81)

177. If the DTV internal boresight fails the FLIR boresight will not be performed. T/F (Sights handout pg D-77)

178. Internal boresight procedure can be completed in flight. T/F (Sights handout pg D-79)

179. To check the boresight correctors, the PLT/CPG must access the page initially, then select and the appropriate system. (-10-2, pg 2-132)

180. The MTT is capable of tracking primary target and up to secondary targets. (-10-2, pg 4-41)

181. If the pilot selects TADS, either by the NVS select switch or by linking the TADS to the FCR, while the CPG is sight select TADS, what will happen? . (-10-2, pg 4-7)

182. What three things will cause the LOS reticle on flight symbology to flash? 123. (-10-2, pg 4-25)

183. During single DP operations, both crew stations share common symbology and imagery on their HMDs. If both crewmembers have NVS mode switch to NORM or FIXED, which symbology and imagery will be presented on the HMDs? . (-10-2, pg 4-68)

184. Setting the IAT/OFS switch to IAT when the TADS LOS is within the primary tracking gates will adjust the symbol to the desired location on the target. (–10-2, pg 4-42)

185. Primary tracking gates will flash when approaching % of the FOV, limited at FOV edge, or when the gates are extremely . (–10-2 , pg 4-42)

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186. Label the High Action Display: (-10-2, Pg 4-43 Fig 4-36)

1___ ___ ____ 2___ _ _

3___ ___________

4___ _______

5___ _______

6___ ________

7___ ____________

8___ _________

187. The internal boresight aligns the TADS to the laser LOS and the to the LOS. (-10-2, pg 4-44)

188. The internal boresight shall be performed as part of preflight procedures prior, . when the TADS. (-10-2, pg 4-44)

189. Can the internal boresight be performed in flight? (–10-2, pg 4-44) 190. The boresight must be performed successfully before the FLIR boresight can be performed.

(-10-2 , pg 4-44)

191. A solid asterisk is displayed in front of the range indicates; . (-10-2, pg 4-34)

192. A flashing asterisk in the *XXXX message indicates . (–10-2, pg 4-34)

193. T/F There is no minimum distance for range focus for the MTADS. ( -10-2, pg 4-9)

194. How many bursts of laser energy are fired when pulling the RH ORT grip trigger to the first detent? , . (-10-2 pg 4-17)

195. field of view should be used for target acquisition and field of view or field of view should be used for target recognition and engagement (TC 1-251, task 1140 pg 4-104)

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1111 222223333333333333

44444 55556666666666666

77777777777778888888888888

196. The LMC requires a when the aircraft is rapidly moving laterally in reference to a target. (ATM Task 1422 pg 4-172 Note #5)

197. When storing a target with the TADS using the UPDT/ST switch on the ORT left handgrip, a TGT XX message will be displayed where for 4 seconds? (–10-2, pg 4-38)

198. With the 1000 point database, the shared points are stored in locations to . (-10-2, pg 3-87)

199. The TADS footprint symbol on the TSD changes from partial intensity green to when TADS is lasing. (-10-2 pg 3-89)

200. What do the TADS FOV Brackets surrounding the LOS reticle indicate? What if those brackets are not present? . (-10-2 pg 4-28)

Assorted Gunnery topics TSD, IDM, ASE, TESS ect.

201. When operating in the TESS / weapons TNG mode, what is displayed in the weapons inhibit section of the HAD when the system is “armed?” (-10-2, pg 4-37)

202. What must be entered on the Keyboard Unit to enable auto range? “ ”. (–10-2, pg 4-17)

203. The minimum altitude for auto ranging is approximately meters” with a 0. degree look down angle. (Sights handout 11-0924 D-42)

204. Can the flight crew override the “NAV DATA INVALID” message in the Sight Status field of the High Action Display? (-10-2, pg 4-33)

205. Can the flight crew override the “ACCEL LIMIT” message in the Weapon Inhibit Status field of the High Action Display? (-10-2, page 4-38)

206. A total of locations are available in the IDM shot-at file with an additional available for the ownship. (-10-2, pg 3-116 and pg 3-117)

207. CTRLM are numbered to with C through C being PPs for zone members. (-10-2, pg 3-88)

208 FCR target coordinate data is stored in when the CAQ button is used to select an FCR target. is used for an ATHS fire mission target. (-10-2, pg 3-88)

209. On the COORD page the L – L VAB’s are used to make a waypoint, control measure or target threat an acquisition source? (-10-2, pg 3-115 )

210. When you WAS any weapon system, that weapon system ICON (on the top-level weapons page) will turn . (-10-2, pg 4-87)

211. Describe the crewmember priority (WAS logic) for actioning any weapon system? What is the one exception to this rule? . (-10-2, pg 4-6)

212. When the Radar Jammer is transmitting a in the center of the Ownship Icon will be present. (-10-2, pg 4-118)

213. Where will an uncorrelated RWR Detect Icon be displayed? . (-10-2, pg 4-118)

214. How do you go to the WAR mode on the AN/ALQ 136? . (-10-2, pg 4-115)

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215. The configuration of the laser sensors of the Laser Detecting Set provides for degrees of coverage in azimuth and +- in elevation about the helicopter with substantial overlap. (-10-2, pg 4-113)

216. A maximum of PFZs and NFZs can be displayed on the TSD? (-10-2, pg 3-119)

217. When is the “PSN” button displayed? (-10-2, pg 3-84)

218. When in the TESS TNG mode, what does the MPD message “LIVE GUN AMMO” mean? ‘ ‘ (-10-2, pg 4-37)

219. What is the maximum range, which could be entered manually? k (-10-2 pg 4-17)

220. On what page would you change the ASE Voice threshold select from Search to ACQ? . (-10 4-118)

221. Label the switches on the handgrips: (-10-2, pg 4-10 & 4-11)

222. WARNING – The AN/ALQ-136(V)5 system poses a potential to personnel due to its operation frequency range and transmitter output power. When the system is powered up, personnel should remain clear of the transmit antennae by a minimum of 10 feet to prevent overexposure to high frequency RF radiation and its corresponding effects. (-10-2 Pg 4-115)

223. What is the purpose of the Cross-hatch symbol coding on the ARM/SAFE Status Window. ‘’’’ . (-10-2, 4-87)

224. True or False The COLOR button on the VIDEO Page serves the same function as the Day/Night/Mono knob on the MPD bezel. (-10-2, 4-74)

225. During single DP operations will the VCR still function? . (-10-2, pg 4-74)

226. What happens if you place the SYMB button (B2) to the BOOST position? . (-10-2, pg 4-74)

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227. Pressing the ZOOM VIEW on the Video page will result in? . (-10-2, pg 4-74)

228. The TSD FCR footprint will change from green when the FCR is scanning. (-10-2, pg 3-89)

229. The AMC wants yet another FARM report. What information will be included in the report? . (-10-2, pg 3-59)

230. You have IDMed the AMC a current FARM report. Assuming that you have not changed your callsign, what will happen to the FARM report that you sent to the AMC two minutes earlier? (-10-2, pg 3-117)

231. What are the available size selections for a TRP Priority Fire Zone? What is the default size? . . (-10-2, pg 3-120) & (for ref only: TC 1-251Feb 2000, task 1410 pg 4-187)

232. Label the following icons. -10-2 page 4-99 and 4-100

233. Can a target or a threat be added to a route on the TSD? (Boeing Training Material V13 NAV Slide 3)

234. When the pilot selects the PAN function, what will happen to the TSD map? -10-2 page 3-85

235. The Bob-up Box represents approximately a foot square area on the ground. Maximum displacement to the edge of the format is approximately Feet Lat and Long. (-10-2, Pg 4-26).

236. What message would the CPG expect to see in the HAD Sight Status field if the SAL priority missile channel does not match LRFD code? (LRFD not equal to missile seeker code) REMOTE (-10-2, pg 4-33)

237. Default range for the CPG is . For the pilot it is . (-10-2, pg 4-17)

238. Describe what will happen to the TADS if the Laser Spot Tracker is in Manual and the LST receives properly coded laser energy? . (-10-2, pg 4-43)

239. The is used for the transmission of the FCR NTS via the IDM to another Longbow. (-10-2, pg 4-51)

240. The FCR Scan Wiper Symbol will be when the FCR is conducting a single scan-burst. For a continuous scan it will be Green. (-10-2, pg 4-53)

241. The FCR page will display target symbols for any given scan. These targets represent the targets detected and classified during the scan. (-10-2, pg 4-52)

242. If the pilot’s selected sight is FCR and LINK is selected, the TADS FOV will automatically change to if DTV is the selected sensor, or if FLIR is the selected sensor. (-10-2, pg 4-131)

243. Is the Laser Spot Tracker capable of tracking PIM coded laser energy? (-10-2 , pg 4-103)

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ROT

CT

MF

244. Selecting the RJAM STBY button places the Radar Jammer in a standby mode for warm-up for minutes. (-10-2, pg 4-119)

245. On the ASE page up to RFI detected threats can be displayed on the outside of the ASE footprint and in the status window. Up to ASE detected threats can be displayed on the inside of the ASE footprint and in the status window. (-10-2, Boeing Training Material V13)

246. An RFI emitters will be displayed in full intensity during the period when the target is actively emitting for ____ seconds after the emitter becomes inactive, at which time the symbol will be displayed at partial intensity for ____ seconds. The symbol will blank ____ seconds after the emitter becomes inactive. (TC 1-251 Task 1144 Page 4-107)

247. Will FCR targets detected with the active NFZ be prioritized? ( , -10-2 pg 3-119)

248. The maximum airspeed for wing stores jettison is KTAS. from a hover to KTAS minimize sideslip if possible, from 45 KTAS to 130 KTAS ball centered (trim) if possible. (-10-2 pg 5-8)

249. True or False Only one Weapons Processor (WP) provides weapon system computations and control while the second remains in a ready state if needed? (-10-2 P 2-119)

250. The training mode is selected by pressing the TRAIN button (R4) on the WPN page. What two conditions must be met to enter and exit the training mode? (-10-2, pg 4-109)

251. The internal auxiliary fuel system (IAFS) incorporates a 100 gallon fuel tank and an ammunition storage magazine capable of holding approximately rounds and in the AHS allowing for approximately a 300 round capability. (-10-2 P 6-5 and AWS 11-0921 Student Handout D-7)

252. When ammunition is loaded using the side loader, there is approximately round space between the side loader and the gun. (AWS 11-0921 Student Handout D-10 NOTE)

253. What is the color of the M788 (TP) round? . ( AWS 11-0921 Student Handout D-15)

254. What is the depression limit of the gun turret assembly while on the ground with the GND ORIDE button selected ON? degrees ( AWS 11-0921 Student Handout D-20)

255. Aircraft ARM/SAFE power is controlled by the processor? ( AWS 11-0921 Student Handout D-34)

256. Weapon performance and safety inhibits are controlled the processor. ( AWS 11-0921 Student Handout D-35)

257. What crew station can conduct dynamic harmonization? ( AWS 11-0921 Student Handout D-53)

258. For dynamic harmonization the aircraft heading to the target will be º degrees (±5º). ( TC 1-251 pg 4-206)

259. What is turret bending and will the weapons processor compensate for this phenomenon? . (FM 3-04.140, pg 4-18)

260. The gunner must compensate for lead angle compensation when using which of the available sights; why? .

(FM 3-04.140, pg 4-17 and 4-20)

261. The target-state estimator will nominally take seconds for the algorithms to settle to provide a proper lead-angle. (FM 3-04.140, pg 4-19)

262. Trajectory shift and projectile drift combine to constitute the . (FM 3-04.140, pg 4- 7)

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263. The ground stow mode commands the pylons to the stow position of - º so that the wing stores are level with the terrain. (-10-2 P 4-93 and ARS 11-0922 Student Handout D-4)

264. During preflight and all live fires, when the AWS has been used, the will be inspected by the crew for cracks. (-10-2 pg 8-3)

265. Thrust misalignment is a characteristic of ballistics. (FM 3-04.140, pg 4-1 and 4-2)

265. The pilot may have to pitch the nose of the aircraft up when firing rockets beyond meters. The articulation pylons address angular rates in the pitch axis up to degrees per second. (FM 3-04.140 4-16 and ATM Task 1462 pg 4-196)

266. The motion of the aircraft as the projectile leaves the weapon causes . (FM 3-04.140 4-5)

267. Rockets are most accurate fired from a hover OGE or IGE. (FM 3-04.140, pg 4-15 and 4-16)

268. At about knots forward speed (indicated), the rotor disk is pitched forward so that the influence vector is just aft of the rocket launcher front bulkhead , thus reducing down wash to zero. (FM 3-04.140, pg 4-16)

269. What message will display when the actioning crewmember’s selected sight is Fire Control Radar (FCR), and there is no Next-To-Shoot (NTS) target? ( ARS 11-0922 Student

Handout D-44)

270. Live fire testing shows that most rockets achieve best effectiveness between to meters. (FM 3-04.140, pg 7-3)

271. The MK 66 motor spins clockwise up to revolutions per second to motor burnout caused by the flutes on the motor nozzle. (FM 3-04.140, pg 7-3)

272. The minimum range to target firing Flechette rocket is meters. The effective range with MK 66 rocket motors is to kilometers. (-10-2 P 4-94)

273. The weapons processor assigns a default of SAL missiles for both channels if sufficient missiles are available in the NORM mode with SAL SEL AUTO. (TC 1-251 pg 4-176)

274. is a mode of fire which involves firing multiple SAL missiles with the same laser code or multiple RF missiles. (TC 1-251 pg 4-177)

275. is a mode of fire that employs multiple missiles launched with two, or more, unique laser channel codes. (TC 1-251 pg 4-177)

276. In the ripple mode the weapons processor will divide the quantity of missiles with the odd missile being assigned to the priority channel. (TC 1-251 pg 4-177 and 4-176)

277. SAL LOBL missile constraints box is being driven by the . (TC 1-251 pg 4-178)

278. SAL LOAL DIR mode the missile constraints box is being driven by the . (TC 1-251 pg 4-178)

279. SAL LOAL LO/HI mode the missile constraints box is being driven by the , except when TRN is the ACQ selection and then it is being driven by the TRN point. ( LBHMMS 11-0923 Student Handout pg D-27)

280. For SAL WPN MSL Formant the ALT CHAN button is only selectable after a CHAN has been entered. ( LBHMMS 11-0923 Student Handout pg D-25)

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281. For a 4500 meter SAL hellfire engagement the last seconds needs to be steady-on-target time (terminal guidance). (FM 3-04.140, pg 5-24)

282. Your target is 6100 meters away and you need to clear a mask that is 670 feet above the aircraft, what trajectory (SAL K model) would you select to engage that target? (FM 3-04.140, pg 5-30)

283. What is the maximum laser delay time for an 8 kilometer SAL missile engagement? seconds (FM 3-04.140, pg 5-24)

284. During rapid fire engagement the maximum separation between targets should not exceed meters, with at least an second separation between missile launches. ( LBHMMS 11-0923 Student Handout pg D-61)

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