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Fragen in diesem Quiz (75)
1Once “KNOCK IT OFF” is called, all participating aircraft will
- AAcknowledge with call sign in roll call fashion
- BCease tactical maneuvering and end the scenario
- CDeconflict flight paths
- DAll of the above
2Normal recovery fuel is the fuel on initial or at the FAF at the base of intended landing or alternate. Establish fuel quantity locally or ________ pounds, whichever is higher
- A300
- B350
- C400
- D450
3Pilots will declare emergency fuel to the controlling agency as soon as it becomes apparent that an aircraft will enter or start an instrument final approach at the of intended landing, or alternate if required, with_____ pounds of fuel or less
- A250
- B300
- C350
- D500
4Pilots will declare minimum fuel to the controlling agency as soon as it becomes apparent that an aircraft will enter initial or start an instrument approach at the base of intended landing, or alternate if required with ______ pounds of fuel or less
- A250
- B300
- C350
- D500
5While airborne, if revised forecast winds for ETA (+-1 hour) exceed limits specified in the flight manual, the pilot will terminate the mission in time to return to the operating base _____ unless a suitable alternate is available
- ABefore the forecast time of increased winds
- BWith sufficient fuel to fly low approaches for a minimum of one hour (or as directed by local operating procedures)
- CWith sufficient fuel to fly low approaches for a minimum of two hours (or as directed by local operating procedures)
- DA or B
- EA or C
6Precipitation adversely affects aircraft performance and reduces visibility. If conditions permit, pilot should maximize climb or descent rate to exit potential or actual icing conditions
- ATrue
- BFalse
7For air-to-air operations, a coordination brief between all involved players shall include the following
- AAFI 11-214 Air-to-air Training Rules, altitude deconfliction, and FAA Special Request Aproval
- BEmergency mission/lost link explanation, FAA special request approval, and altitude deconfliction
- CAltitude deconfliction, emergency mission/lost link explanation and deconfliction, and AFI 11-214 Air-to-Air Training Rules
- DNone of the above
8Aircrews will not takeoff if forecast or reported _____ turbulence for Light/Category I aircraft is present along the route of flight
- ALight
- BSevere
- CModerate
- DNone of the above
9Abort the mission, regardless of apparent damage or subsequent normal operation, if any of the following occur
- ABird strike
- BOver-G
- CFlight control system anormalies (including uncommanded flight flight control points)
- DEngine failure
- EAll of the above
10The PIC is the final authority on the number of people allowed in the GCS (to include visitors) during operations
- ATrue
- BFalse
11Aircrew will perform operations check at least _____. These checks will include fuel level, oil level, electrical, datalink, engine parameters and emergency mission status at a minimum
- AOnce every 30 minutes
- BOnce per hour
- COnce every two hours
- DOnce per shift
12Change out one crewmember at a time to ensure continuous monitoring of the aircraft. The ______ is the final authority in determining if circumstances are safe to replace crews.
- Aincoming PIC
- Boutgoing PIC
- Cboth A and B
- DNone of the above
13Aircrew will not place items (checklists, charts, etc.) behind the ______ at any time.
- Aflap lever, condition lever, throttle, or speed lever
- Bcontrol stick
- CKVM switch
- DPSO
14The DTV video will be degraded until approximately 1 hour after sunrise and approximately 1 hour prior to sunset due to the lack of visible light
- ATrue
- BFalse
15The fuel heater will automatically shed when aircraft voltage drops below ______ V
- A23
- B24
- C25
- D26
16If DEEC fails, the backup mode torque schedule limits engine power as a function of OAT and density altitude, and will not allow a command greater than ______% torque.
- A28
- B70
- C78
- D84
- E96
17Use Terminate procedures when safety of flight is not a factor, and in the following cases:
- AReaching BINGO fuel
- BDLOs are met or are unattainable
- CTraining Rules/other limits met
- DExceeding area boundaries
- EAll of the above
18Decreasing oil level may be an indication of an oil leak (external or internal), excessive oil consumption, or oil foaming. What are some important points to remember?
- AMinimize aircraft maneuvering and avoid excessive throttle movements.
- BFluctuating oil pressure combined with fluctuating oil level may be an indication of a clogged oil vent line.
- COil leaking inside the engine compartment can ignite and burn out of control resulting in the loss of the aircraft.
- DAll of the above
19The Aircraft Component Currents Requirements chart shows typical continuous amperage for each device. However, momentary in-rush current can be up to ______ times as much when a unit is first turned on.
- A1 or 2
- B1 or 3
- C2 or 3
- D2 or 4
20During a forced landing (and operating on battery power), once the landing gear is lowered, battery life may preclude another full landing gear cycle prior to a successful touchdown.
- ATrue
- BFalse
21Which of the following aircraft components draws the highest maximum amps?
- AMTS
- BLynx SAR
- CPitot heat
- DKu-band datalink
- EFuel heater
22What is the maximum allowable EGT in flight?
- A660
- B675
- C695
- D776
23Briefings and debriefings should take place in the following order of priority: Face to face, Telephonic/electronic, Airborne.
- ATrue
- BFalse
24______ or lower should be used when penetrating areas of turbulence.
- AVA (maneuvering airspeed)
- BVT (threshold speed)
- CVNE (never exceed speed)
- DVS (stall speed)
25Which item has the greatest drag index?
- ATAMLG landing gear extended
- BPropeller unfeathered (not rotating, worst case)
- CEmpty M-299 half rack (2 rails)
- DGBU-12
- EGBU-38
26In altitude preference mode, the aircraft attempts to maintain airspeed for the commanded altitude by adjusting the throttle setting calculated by the closed loop power function.
- ATrue
- BFalse
27In speed preference mode, the aircraft attempts to maintain airspeed for the commanded altitude by adjusting pitch, maintaining the commanded throttle setting.
- ATrue
- BFalse
28A ______ indicates operating procedures, techniques, etc., which could result in injury to personnel and/or loss of life if not carefully followed.
- AWarning
- BCaution
- CAdvisory
29______ expresses a provision that is binding.
- AShall
- BShould and May
- CWill
30The EPO switch disconnects ______ from the GCS.
- Aall AC power
- Ball AC power and UPS output
- CUPS output
- DNone of the above
31What does setting GCS Ignition to “Hot” do?
- AEnables the Engine Start Module (ESM)
- BActivates the EFIU
- CActivates the electric fuel pumps
- DA & C
- EAll of the above
32The EFIU monitors engine RPM received from the tach generator. If RPM drops below ______% it automatically performs an in- flight restart
- A28
- B60
- C78
- D89.5
- E92.5
33RPA crew will notify the controlling agency that they are “LOST LINK.”
- ATrue
- BFalse
34If both electric fuel pumps fail, ______.
- Athe engine will only continue to run until the fuel in the header tank is depleted
- Bit is not possible to jettison fuel
- Cthe engine will immediately stop
- DA and B
- EAll of the above
35[Block 1] Batteries cannot be charged in flight. [Block 5] Supplied by either engine power or ground power, the aircraft electrical system has an on-board charging system for five batteries.
- ATrue
- BFalse
36The flaps are set automatically when airspeed exceeds ______ KIAS or landing gear is up and ______.
- A134; airspeed hold is on
- B110; cruise mode is on
- C121; altitude hold is on
- D100; the speed lever is full forward
37Pilots must be alert to the possible consequences of deactivating SAS during flight. When SAS is deactivated, all ______ safety limitations are immediately turned off.
- Astall protect
- Bcruise mode
- Cautopilot
- Dengine over speed protection
38With Cruise Mode ON, control sensitivity is reduced. Roll, pitch, and yaw gains are scaled with airspeed. Scaling limits roll to ______ up to ______ depending on airspeed.
- A±5°; ±40°
- B±10°; ±40°
- C±10°; ±60°
- D±15°; ±60°
39Cruise mode is on when any hold mode is engaged, when stall protect is enabled, or anytime airspeed is over ______.
- A.7 coefficient of lift
- B.8 coefficient of lift
- C100 KIAS
- D110 KIAS
- E120 KIAS
40Do not zero trims in flight. Doing so will result in a 50-knot airspeed hold command if airspeed hold is engaged.
- ATrue
- BFalse
41The ______ feature is the first level of stall protection provided by the autopilot. It automatically decambers the ailerons when AOA increases above +5º to prevent the wing tips from stalling.
- Aairspeed limit override
- Baileron tip stall override
- Cstall protect
- Dcruise mode
42Upon lost link while jettisoning fuel, both jettison valves will remain open.
- ATrue
- BFalse
43Stall protect is turned on and off by the pilot, but only takes effect at speeds below ______.
- A.7 coefficient of lift
- B.8 coefficient of lift
- C100 KIAS
- D110 KIAS
- E120 KIAS
44Stall protect prevents stall by deflecting the ruddervators down when AOA exceeds a threshold value of 7 degrees. Stall protect disengages when the AOA is less than 3 degrees.
- ATrue
- BFalse
45Mission programming employs “fly-to” logic. For each mission leg during autonomous flight, the aircraft will use the programmed settings for the upcoming waypoint. Once the waypoint is passed, the settings for the next waypoint go into effect.
- ATrue
- BFalse
46Lost link programming and the emergency mission will not activate if “Lost Link – OK” is set ON during an operational mission.
- ATrue
- BFalse
47During a loss of command link, how much time passes until the RCM sends a reset command to the airborne modem?
- AArming time + 180 seconds
- BArming time + 100 seconds
- CArming time + 60 seconds
- DArming time + 30 seconds
- EArming time + 10 seconds
48If EGI ______ fails, the Ku SATCOM will not be able to aim properly, which may cause the aircraft to lose Ku-band link and go lost link
- A1
- B2
- C3
- D4
49The transmission of the C-Band LOS datalink is referred to as the ______ and ______, while the Ku-Band SATCOM
transmissions are called ______ and ______.- Auplink; downlink; command link; return link
- Bcommand link; return link; uplink; downlink
- Ctransmit; receive; command link; return link
- Dcommand link; return link; transmit; receive
50The IR nose camera has its own heater and fan to prevent fogging.
- ATrue
- BFalse
51The ice detector signal stays on for ______ seconds after the ice has cleared.
- A30
- B60
- C45
- D90
52The ______ mode (of the ARC-210) provides continuous scanning of four preset channels.
- Amanual
- Bscan
- Cpreset
- Danti-jam
53A ______ background (on a VIT data element) indicates an abnormal condition. This generally indicates that the value is out of the normal operating parameters and should be monitored.
- Awhite
- Bred
- Cyellow
- Dgreen
54A ______ background (on the VIT data element) indicates a warning condition. This generally indicates the value is in a critical condition and will require corrective action
- Agreen
- Byellow
- Cred
- Dboth B and C
55The deice system’s automatic mode is intended to be used when the aircraft is operating autonomously. If outside air temperature is less than ______, pitot heat is automatically turned on.
- A0 °C
- B15 °C
- C10 °C
- D21 °C
56For an operational or emergency mission, when LOS TX #1 Inhibit is selected On, TX1 will be prevented from operating during that mission leg. What else is true about LOS TX Inhibit On?
- AThis inhibit overrides any other programming and positively prevents the transmitter from operating under any circumstances
- BTransmitters will power up whenever triggered by later autonomous programming
- CTransmitters will power up whenever triggered by later autonomous programming inside of lights-on range
- DTransmitter frequencies will change to en route cruise settings
57Data from the Preset Configuration window cannot be applied/uploaded if the aircraft airspeed is above ______ KIAS.
- A40
- B50
- C60
- D70
58In cruise mode, avoid flying the aircraft at AOA greater than ______ degrees. A high AOA can result in divergent roll oscillations.
- A+2.5
- B+5
- C+7.5
- DNone of the above
59The engine may exceed maximum allowable EGT when disengaging Altitude Hold with the throttle in the ______ position.
- AFull aft
- BMidrange
- CFull forward
- DFull reverse
60During an MCE gaining handover, the SATCOM command link is established when:
- AI say it is
- BThe “Ku SATCOM Command Link – lost” warning message disappears
- CSystem amps increase by approximately 10 amps
- DUplink signal strength increases
61What is the maximum bank angle if heading hold, Nav mode, Direct-to, or lost LOS link mode is engaged?
- A30°
- B5°
- C0°
- D40°
62Upon successful hand-off it is necessary to update the datalink preset values found in Section 9; otherwise, the aircraft will retain the preset values for the losing GCS. Changing any of the preset values in the HDD will result in all presets values being resent to the aircraft; however, entering an identical value in the HDD for a preset will not update any values.
- ATrue
- BFalse
63It is possible for the actual nose camera lens inside the fuselage to fog during descent. Fogging of the actual nose camera lens cannot be prevented with the use of nose lens heat. The Nose IR lens heater may be used to clear the nose EO camera.
- ATrue
- BFalse
64If external power source is shut off due to a GCS fire, the UPS batteries will still provide power if they were not turned off prior to evacuation
- ATrue
- BFalse
65With a left PSO rack (Pilot Station) failure or rack lock-up, the pilot has the option of sending the aircraft lost link prior to executing the PSO-1 Rack Lock-Up checklist.
- ATrue
- BFalse
66If no emergency mission is loaded on PSO-2, then as soon as the rack switch button is pressed, the emergency mission start point will immediately change to ______ regardless of what the PSO-1 tracker display shows.
- Athere is no change
- Bthe last waypoint
- Cwaypoint 1
- Dthe sixth-to-last waypoint
67Loss of control may be indicated by complete failure of the aircraft to respond to pilot control command. This may be caused by ______.
- Aairspeed or pitot–static failure
- Bcatastrophic AOA failure below 120 KIAS with stall protect on, SAS failure
- Cautopilot sensor failure, structural failure, or airframe icing
- DAll of the above
68A stall condition may be indicated by ______.
- Awarnings on the pilot HUD
- Bexcessively high AOA
- Cunexpected loss of altitude
- DAll of the above
69Pitot heat does not guarantee absence of ice from the pitot-static system. Moisture can freeze in the unheated areas of the system. This malfunction may be indicated by an FCA PPT sensor warning message, abnormal attitude, abnormal airspeed indications, or a combination of any of these. These conditions may result in ______.
- Aaircraft pitch down or oscillation
- Bloss of datalink
- Closs of aircraft control
- DAll of the above
70Roll shaping limits the roll rate for pilot roll command inputs and autopilot turns (Direct-to, heading hold, NAV, or PCL mode)
to reduce the possibility of lost link when rapid roll movements are used.- ATrue
- BFalse
71Attempting to lower the gear with less than ______ volts may cause a complete loss of battery power, leading to a possible loss of aircraft.
- A21
- B24
- C22
- D28
72Do not allow the engine to windmill between ______ and ______ percent RPM. Operation within this range may cause engine damage
- A18; 28
- B10; 28
- C60; 65
- D50; 68
73The air start airspeed envelope is between ______ KIAS.
- A100 and 160
- B100 and 180
- C150 and 200
- DNone of the above
74_____ of the external fuel tank fuel is unusable.
- A1%
- B2%
- C3%
- D4%
75Maximum bank angle in emergency missions is limited to __________.
- A20°
- B14°
- C30°
- D15°
Informationen
- Beschreibung
- Quiz am QUAL, erstellt von 72 promocion am 25/01/2022.
- Autor
- 72 promocion
- Sprache
- Español
- Aufrufe
- 2
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