Quiz
T-6 Electrical System
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Questions in this quiz (42)
1The T-6A electrical system includes a [blank_start]28[blank_end] VDC, [blank_start]300[blank_end] ampere (amp) starter/generator, a [blank_start]24[blank_end] VDC lead acid battery, a [blank_start]24[blank_end] VDC auxiliary battery, and a [blank_start]28[blank_end] VDC external power receptacle.
- A28
- B300
- C24
- D24
- E28
2A [blank_start]bus tie[blank_end] switch allows isolation of the battery and generator buses, if required.
- Abus tie
3Each electrical distribution circuit is protected by a [blank_start]circuit breaker[blank_end].
- Acircuit breaker
4Primary aircraft electrical power is provided by the [blank_start]generator[blank_end] function of the [blank_start]starter/generator[blank_end], located on the engine [blank_start]accessory gearbox[blank_end] at the rear of the engine.
- Agenerator
- Bstarter/generator
- Caccessory gearbox
5The starter/generator is regulated and monitored by a [blank_start]generator control unit[blank_end] located under a panel in the aft cockpit.
- Agenerator control unit
6Power from the generator is controlled by a generator control switch, placarded [blank_start]GEN[blank_end], located in the right front portion of each cockpit on the [blank_start]right forward[blank_end] switch panel.
- AGEN
- Bright forward
7Power for the generator control switches is provided by a circuit breaker labeled [blank_start]GEN SW[blank_end] on the [blank_start]front[blank_end] cockpit [blank_start]generator bus[blank_end] circuit breaker panel.
- AGEN SW
- Bfront
- Cgenerator bus
8The generator bus is divided into a [blank_start]front[blank_end] and [blank_start]rear[blank_end] bus for the respective cockpits.
- Afront
- Brear
9The front cockpit generator bus powers the [blank_start]rear generator bus[blank_end] and the front [blank_start]cockpit avionics[blank_end] bus.
- Arear generator bus
- Bcockpit avionics
10The rear cockpit avionics bus is powered by the [blank_start]forward generator bus[blank_end] through the front [blank_start]cockpit avionics[blank_end] bus.
- Aforward generator bus
- Bcockpit avionics
11The rear cockpit generator bus is controlled by a circuit breaker labeled [blank_start]AFT GEN[blank_end] on the [blank_start]front[blank_end] cockpit [blank_start]generator bus[blank_end] circuit breaker panel.
- AAFT GEN
- Bfront
- Cgenerator bus
12Both front and rear cockpit [blank_start]avionics buses[blank_end] are controlled by circuit breakers, labeled [blank_start]FWD AVI[blank_end] and [blank_start]AFT AVI[blank_end], on the [blank_start]front[blank_end] cockpit [blank_start]generator bus[blank_end] circuit breaker panel.
- Aavionics buses
- BFWD AVI
- CAFT AVI
- Dfront
- Egenerator bus
13The rear cockpit avionics bus receives power through the
- Afront cockpit battery bus.
- Brear cockpit battery bus.
- Crear cockpit generator bus.
- Dfront cockpit avionics bus.
14The rear cockpit battery bus receives power from the [blank_start]front[blank_end] cockpit [blank_start]battery bus[blank_end].
- Afront
- Bbattery bus
15The rear cockpit avionics bus receives power from the [blank_start]front[blank_end] cockpit [blank_start]battery bus[blank_end] through the [blank_start]front[blank_end] cockpit [blank_start]avionics bus[blank_end].
- Afront
- Bbattery bus
- Cfront
- Davionics bus
16The rear cockpit battery bus is controlled by a circuit breaker labeled [blank_start]AFT BAT[blank_end] on the [blank_start]front[blank_end] cockpit [blank_start]battery bus[blank_end] circuit breaker panel.
- AAFT BAT
- Bfront
- Cbattery bus
17Both front and rear cockpit [blank_start]avionics battery buses[blank_end] are controlled by circuit breakers, labeled [blank_start]FWD AVI[blank_end] and [blank_start]AFT AVI[blank_end], on the [blank_start]front[blank_end] cockpit [blank_start]battery bus[blank_end] circuit breaker panel.
- Aavionics battery buses
- BFWD AVI
- CAFT AVI
- Dfront
- Ebattery bus
18Circuit breakers labeled FWD AVI and AFT AVI control front and rear cockpit avionics buses and are located on the front cockpit
- Aright forward switch panel.
- Bbattery bus circuit breaker panel only.
- Cgenerator bus circuit breaker panel only.
- Dbattery bus and generator bus circuit breaker panels.
19A circuit breaker labeled [blank_start]AVI MSTR[blank_end] on the front cockpit battery bus circuit breaker panel allows the avionics master switch to be activated.
- AAVI MSTR
20Except for the back-up UHF control head and UHF transceiver, power for all avionics and radio systems in both cockpits is furnished through _____ on the right forward switch panel in the front cockpit.
- Aa bus tie switch
- Ban avionics master switch
- Ca master battery switch
- Dan auxiliary battery switch
21When the bus tie switch is engaged ([blank_start]NORM[blank_end]), the generator feeds both generator bus powered items and battery bus powered items.
- ANORM
22T-6A secondary power components consist of a [blank_start]24[blank_end] VDC, [blank_start]42[blank_end] amp-hour battery, a [blank_start]24[blank_end] VDC, [blank_start]5[blank_end] amp-hour auxiliary battery, and an [blank_start]external power[blank_end] receptacle.
- A24
- B42
- C24
- D5
- Eexternal power
23The primary battery provides power for engine starts and is capable of powering all electrical systems (except [blank_start]air conditioning[blank_end], which is automatically shed) in the event of generator failure with the bus tie closed.
- Aair conditioning
24Battery power is controlled through ______ on the right forward switch panel in either cockpit.
- Aan auxiliary battery switch.
- Ba battery switch.
- Ca bus tie switch.
- Dan avionics master switch.
25The auxiliary battery is controlled by the auxiliary battery switch, placarded [blank_start]AUX BAT[blank_end], on the right forward switch panel in the front cockpit.
- AAUX BAT
26A switch labeled AUX BAT on the front cockpit left console test panel is positioned forward to test the _____ during preflight checks.
- Astandby battery
- Bbattery charge circuits
- Cauxiliary battery
- Dstarter/generator
27External power is controlled by the _____ and distributed on the _____.
- Aexternal power switch; external power bus
- Bavionics master switch; avionics bus
- Cgenerator control switch; generator bus
- Dbattery switch; battery bus
28Lighting for EFIS displays, the RMU, the AOA indexer, and the GPS control panel is adjusted using the knob labeled INSTR PANEL on the trim control panel.
- ATrue
- BFalse
29_____ lights can be detached and relocated to the right canopy rail for use as an area or map light.
- AConsole
- BKnee board
- CInstrument
- DUtility
30The [blank_start]landing light[blank_end] is located aft and inboard of the left main landing gear strut, and is exposed as the landing gear is [blank_start]extended[blank_end].
- Alanding light
- Bextended
31Power to the landing light is controlled by a switch placarded [blank_start]LDG[blank_end], located on the trim control panel in the front cockpit.
- ALDG
32After the LDG switch has been turned on, the light only comes on when the gear is [blank_start]down and locked[blank_end].
- Adown and locked
33The [blank_start]taxi light[blank_end] is located aft and inboard of the right main landing gear strut, and is exposed as the gear is [blank_start]extended[blank_end].
- Ataxi light
- Bextended
34Power to the taxi light is controlled by a switch located on the trim control panel in the front cockpit and labeled [blank_start]TAXI[blank_end].
- ATAXI
35The taxi light only illuminates when the switch is on and the gear is [blank_start]down and locked[blank_end].
- Adown and locked
36The T-6A is equipped with [blank_start]navigation lights[blank_end] at the leading and trailing edges of each wingtip, as well as [blank_start]anti-collision strobe lights[blank_end] at each wingtip near the leading edge.
- Anavigation lights
- Banti-collision strobe lights
37When switched on, both the [blank_start]red[blank_end] navigation light at the left wingtip and the [blank_start]green[blank_end] navigation light at the right wingtip are [blank_start]constantly illuminated.[blank_end]
- Ared
- Bgreen
- Cconstantly illuminated.
38The [blank_start]white[blank_end] position lights at the trailing edge of each wingtip are [blank_start]constantly illuminated[blank_end].
- Awhite
- Bconstantly illuminated
39The anti-collision strobe lights at each wingtip flash synchronously at a rate of about [blank_start]30[blank_end] times per [blank_start]minute[blank_end].
- A30
- Bminute
40The anti-collision strobe lights are controlled with a switch placarded [blank_start]ANTI-COLL[blank_end] on the front cockpit trim control panel.
- AANTI-COLL
41Navigation lights are controlled by a switch labeled [blank_start]NAV[blank_end], also on the trim control panel in the front cockpit.
- ANAV
42Light output from the instruments, control panels, and displays can be adjusted by using dimming controls located on the _____ in each cockpit.
- Aright forward switch panel
- Bannunciator panel
- Ctrim control panel
- Dgenerator control panel
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- T-6/A Texan II Quiz on T-6 Electrical System, created by Ryan Curtis on 06/12/2018.
- Author
- Ryan Curtis
- Language
- English
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