NATOPS Closed Flashcards
1
Q
77. With a 100 percent fuel load, do not takeoff between \_\_\_\_ and \_\_\_\_ pounds (at 6.8 pounds per gallon) fuel quantity remaining. The aft CG limit could be exceeded when the aircraft enters climb mode. A. 8899, 11,560 B. 11,560, 13,090 C. 2500, 9000 D. 8799, 13,900
A
B. 11,560, 13,090
2
Q
99. What button commands immediate brake application? A. The "A" command B. 12 C. Brakes D. Override
A
D. Override
3
Q
67. Nose wheel steering starts at 60 knots navigation system groundspeed as ruddervators start to lose effectiveness slower than about \_\_\_\_ KCAS. A. 60 B. 80 C. 90 D. 100
A
B. 80
4
Q
64. CAUTION: Select 12 feet per second squared only when required for a(n) \_\_\_\_ condition and notify maintenance to complete main landing gear inspection. A. Short runway B. Tailwind C. Wet runway D. Emergency
A
D. Emergency
5
Q
70. The term "Land as Soon as Possible" means an emergency shall be declared. A landing should be accomplished at the nearest adequate \_\_\_\_, considering the severity of the emergency, weather conditions, field facilities, gross weight, and command guidance. A. Allied or Coalition airfield B. Mission Planned airfield C. Hard-surfaced runway D. U.S. controlled airfield
A
B. Mission Planned airfield
6
Q
65. Note: Between 3 and 7 minutes after each even hour UTC, if OmniSTAR is unavailable for landing the navigation quality might decrease below \_\_\_\_. A. 18 B. 17 C. 15 D. 5
A
A. 18
7
Q
41. CAUTION: During a contingency 3, using CGS commands to modify the aircraft route of flight is \_\_\_\_. A. Usually necessary B. Prohibited C. Not recommended D. Encouraged
A
C. Not recommended
8
Q
- WARNING: During a contingency 3, if an approach waypoint inside the ____ is selected as a go to waypoint, IMMC altitude management is not guaranteed to ensure recovery. If the engine is operating, the IMMC does not complete engine shutdown and the aircraft could remain well above the contingency 3 glideslope. The aircraft might not stop on the prepared surface or could land beyond the runway.
A. IAF
B. FAF
C. TD
D. Statement is false. Engine always shuts down prior to landing
A
A. IAF
9
Q
75. Ground station equipment failures could cause an apparent loss of communication with the aircraft. If aircraft command and control is lost without contigency 1 indications, how can a CGS force a contingency 1 timer? A. Cancel the mission plan B. Turn off the GCI C. Change Mode 3 code to 7600 D. Turn off the CAMA
A
B. Turn off the GCI
10
Q
51. Note: When using INMARSAT, configure \_\_\_\_ on LCP2. A. UHF SATCOM B. UHF LOS C. Ku-Band SATCOM D. CDL
A
A. UHF SATCOM
11
Q
63. When descending into hot and humid conditions (landing site dew point above \_\_\_\_ *F), open bleed air Shutoff Valve (SV8) to extend fuel heating to warm the avionics compartments. Adding heat to the compartments helps prevent excessive condensation in the compartments after landing. A. 75 B. 80 C. 85 D. 90
A
A. 75
12
Q
- What should the in-control data link setup for takeoff be?
A. A primary link from each available ground station
B. All available links
C. One wideband link
D. Two or three limks
A
A. A primary link from each available ground station
13
Q
90. Normally \_\_\_\_ mode provides the most stable flight conditions. A. Climb B. Cruise C. Descent D. Glideslope
A
A. Climb
14
Q
30. What happens if the ground safety pin is removed after engine start before the IMMC is ready? A. Aircraft shuts down B. Ready label appears C. VTC errors appear D. Nothing
A
A. Aircraft shuts down
15
Q
- WARNING: Ensure all personnel are clear of the aircraft before the ground safety pin is removed. Inadvertent operation could cause the aircraft to do what?
A. Aircraft to start taxi
B. Aircraft to start the flight termination test
C. Either A or B
D. Wideband link radiation
A
C. Either A or B
16
Q
29. If an aircraft system fault is set before a data link is first established or when a data link is reestablished after a contingency 1, will the subsystem status panel system button update to show the fault level? A. Yes B. No C. Only for a red fault D. Only if within 5 minutes
A
A. Yes
17
Q
86. Maximum crosswind for takeoff and landing is \_\_\_\_ knots. A. 10 B. 15 C. 25 D. 30
A
B. 15
18
Q
15. CAUTION: When the landing gear is extended with the total air temperature colder than \_\_\_\_ *F, the landing gear is cold soaked and the nitrogen in the strut can escape. A. -68 B. -40 C. -50 D. -65
A
D. -65 *F
19
Q
92. WARNING: Do not continue a landing below \_\_\_\_ feet AGL in moderate to severe turbulence. Moderate to severe turbulence could result in exceeding aircraft landing limitations. A. 4000 B. 2000 C. 500 D. 200
A
D. 200
20
Q
- The hydraulic system provides insufficient pressure to simultaneously do what?
A. Apply brakes and extend the landing gear
B. Extend the landing gear and power the AC generator motor
C. Power the AC generator and operate the ISS
D. Power the AC generator descending through FL600
A
B. Extend the landing gear and power the AC generator motor
21
Q
59. Note: For takeoff, both KN4072 navigation systems navigation quality must be \_\_\_\_ and both LN100 navigation systems navigation quality must be at least \_\_\_\_. A. 17, 17 B. 18, 18 C. 18, 16 D. 18, 17
A
C. 18, 16
22
Q
7. The wing tank fuel is coldest 6 to 12 hours after takeoff or when the fuel quantity remaining is about \_\_\_\_. A. 11,560 to 13,090 pounds B. 10,000 to 7500 pounds C. Less than 8799 pounds D. 9000 to 2500 pounds
A
B. 10000 to 7500 pounds
23
Q
- What does the IMMC do if, during a contingency 3, CGS commands are used to modify the aircraft route of flight and the aircraft enters a contingency 1?
A. The IMMC maintains the last valid override commands and does not transition back to the C3 route
B. The IMMC sets squawk to 7600 and transitions back to a contingency 3 route
C. The IMMC transitions to a contingency 2
D. The IMMC transitions to a contingency 1 route
A
A. The IMMC maintains the last valid override commands and does not transition back to the C3 route
24
Q
19. After takeoff, the landing gear retracts when passing \_\_\_\_ feet navigation system altitude AGL. A. 2000 B. 2500 C. 4000 D. 4500
A
C. 4000 feet
25
Q
80. Maximum continuous Interstage Turbine Temperature (ITT) is \_\_\_\_ *F. A. 1630 B. 1077 C. 1639 D. 1739
A
C. 1639
26
Q
54. If taxi is delayed and the ground crew must approach the aircraft, complete the \_\_\_\_ Checklist. A. Stop Taxi B. Operational Stop C. Common Ground Station Setup D. Hold Taxi
A
B. Operational Stop
27
Q
39. During ground operations, the contingency 1 timer is \_\_\_\_ seconds. During flight the contingency 1 timer default is \_\_\_\_ seconds and can be changed by the CGS. The contingency 2 timer is \_\_\_\_ minutes. A. 6, 30, 3 B. 30, 60, 3 C. 6, 60, 2 D. 10, 30, 2
A
A. 6, 30, 3
28
Q
- (T/F) Note: A data link not set as in control will not be available to establish an in-control link during a contingency 1.
A
False
29
Q
98. The brake controller can set different braking rates commanded through the IMMC. The rates are set automatically by the IMMC or commanded from the CGS flight control display at \_\_\_\_ feet per second squared. A. 4, 8, or 12 B. 4 or 8 C. 4, 8, or 14 D. 0, 4, or 8
A
A. 4, 8, or 12
30
Q
46. The \_\_\_\_ button border indicates the command was transmitted to the aircraft or is in the transmission process. The button border remains this color until the aircraft acknowledges receipt of the command in the CGS. A. Gold B. Gray C. Beige D. Purple
A
A. Gold
31
Q
60. CAUTION: Above \_\_\_\_ feet when the ISS AC power is on, turn off ISS AC power and ensure yellow caution SAR08 appears to indicate ISS shutdown is complete before starting a descent. If ISS AC electrical power is on when the PLA is reduced to flight idle, engine surge margin is reduced and engine flameout is possible. A. 70,000 B. 65,000 C. 57,000 D. 60,000
A
D. 60,000
32
Q
58. What does maintenance need to inspect if a stop taxi is required during a turn? A. All landing gear B. Brakes C. Tires D. Nose landing gear
A
D. Nose landing gear
33
Q
45. The Uninterruptible Power Supply (UPS) provides minimum electrical power for LRE operations if primary electrical power fails. If primary power is interrupted, the UPS can provide up to \_\_\_\_ minutes of alternate power to continue limited operations. A. 60 B. 30 C. 15 D. 5
A
C. 15 minutes
34
Q
95. A go to command to a Contingency 3 or Contingency 4A waypoint with altitude locked more than \_\_\_\_ feet above the IAF waypoint mission planned altitude can result in loss of aircraft. If a go to command with altitude unlocked is not used to return the aircraft to autonomous navigation prior to the \_\_\_\_ waypoint, the aircraft descends to the FAF waypoint mission planned altitude, holds the altitude, and continues on the last commanded course. A. 2000, FAF B. 1000, IAF C. 2000, IAF D. 1000, FAF
A
A. 2000, FAF
35
Q
- How will you know if the IFF mode 4 fails to reply to an interrogation?
A. The mode 4 reply caution appears on the ATC window in the CGS
B. There is no way to tell
C. A yellow IFF10 lfault appears
D. ATC will inform you
A
A. The mode 4 reply caution appears on the ATC window in the CGS
36
Q
- (T/F) The IMMCs send power control commands through the associated PDC to provide power on or off control to aircraft electrical equipment.
A
True
37
Q
87. Maximum tailwind component for takeoff and landing is \_\_\_\_ knots. A. 10 B. 15 C. 25 D. 30
A
C. 25
38
Q
55. Check aircraft gross weight is not between \_\_\_\_ for takeoff. A. 24,800 and 23,500 B. 13,090 and 11,560 C. 22,500 and 20,800 D. None of the above
A
A. 24,800 and 23,500
39
Q
21. If the ice detector senses ice, the text ICE appears in red right of the air temperature indication on the flight monitor and rescinds \_\_\_\_ after the last ice detection. A. 10 seconds B. 1 minute C. 45 seconds D. 2 minutes
A
B. 1 minute
40
Q
- (T/F) Note: If a red warning is set and the IMMC initiates stop taxi or if a red warning is set when the aircraft is stopped, the IMMC accepts subsequent CGS taxi and takeoff commands.
A
True