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72 Cards in this Set

  • Front
  • Back

IFF transponder power source and location

FEAC / MEDC
FEDC backup when switch is held in backup position

H rack
purpose of IFF BAT PWR switch
hold it on to provide FEDC power instead of MEDC to the IFF (FEAC must be powered)
rate of turn control power source and location
MEAC

C rack
standby gyro power source and location
MEAC / FEAC

C rack
FDI power source
MEAC / FEAC
when is backup power provided to FDIs
when ESS IND AND LTG CONT CB on MEAC is deenergized (bus loss or CB pulled)
power for ___ is swapped from ___ to ___ when the ESS IND & LTG CB on ___ stops receiving power
- both FDIs
- standby gyro
- red instrument lights

MEAC to FEAC
ESS IND & LTG on MEAC
explain all the FDI and standby gyro CBs
Primary:
P FDI - ATT IND PILOT (D1) on MEAC
CP FDI / standby gyro (shared) - ATT IND COPLT / V GYRO (D2) on MEAC

Backup: activated by lack of power to ESS IND & LTG CONT (C5) on MEAC
all three - ATT IND / V GYRO on FEAC

Both FDIs and the standby gyro then have a final CB on the no-name bus that secures all power to that component:
- PILOT ATTITUDE IND
- COPILOT ATTITUDE IND
- VERT GYRO
peanut gyro power source
non-EFDS:
FEAC

EFDS (same as non-EFDS pilot turn needle)
Pri: MEDC
Alt: FEDC with ESS BUS MON switch OFF
where do the attitutde indicators get their signals from (FDIs, peanut gyro)
FDI - INS 1, INS 2, or standby gyro
peanut gyro - its own internal gyro
HSI power source
MEAC
HSI mode lights power source
MEAC
altimeter power source
mode C - MEAC (pilot side only)
vibrator - MEDC
which altimeter provides mode C
pilot
turn needed power source and location
PILOT - non-EFDS
Pri: MEDC
Alt: FEDC with ESS BUS MON switch OFF

COPILOT - non-EFDS
MEDC

EFDS
part of the EFDI (MEAC / FEAC)

Location (turn rate gyro):
under the CP seat
turn needles get their inputs from
turn rate gyros under the copilot seat
radar altimeter power source and location
FEAC

doppler well
autopilot power source and location
Bus A / MDC

C rack
OAT indicator power source
EMDC
AOA power source and location
MEDC

transmitter at NAV/COMM station
trim indicator power source
autopilot trim servo-motor
RAWS power source and location
MEAC / MEDC

B rack
landing gear handle lights power source
EMDC
VOR-1 power source and location (and name the two types)
MEAC / MEDC

VOR nav converter in B rack
Receiver in J rack

ARN-87 old ones
MLR-2020A-1 new ones with protected ILS
VOR-2 power source and location (and name the two types)
MEAC / MEDC (same as VOR-1)

VOR nav converter in B rack
Receiver in J rack
TACAN power source and location
MEAC / MEDC

C rack
UHF-1 power source and location
MEAC / MEDC

F rack
UHF-2 power source and location
Bus A / MDC

F rack
VHF radio power source (and describe the three different kinds)
Old non-digital - ARC-197 (VHF only)
Red digital radio - ARC-182 (UHF/VHF)
Back digital radio - ARC-210 (UHF/VHF)

All MEDC
HF-1 power source and location
MEAC / MEDC

B rack (HF-2 in F rack)
HF-2 power source and location
Bus A / MDC

F rack (HF-1 in B rack)
ADF power source and location
MDC

ADF filter - B rack
ADF receiver - F rack
INS-1 power source and location
MEAC / MEDC
Synchro-excitation voltage - MEAC
Battery backup - FEAC

H rack
INS-2 power source and location
Bus A / MDC
Synchro-excitation voltage - MEAC
Battery backup - FEAC

H rack
marker beacon power source and location
MDC

F rack
CDNU power source
MEDC
glideslope receiver power source and location
MEDC

B rack
GPS receiver power source and location
MEAC

C rack
ICS power source; how to secure power
MEDC
MEAC needed to select radios

COMMUNICATION INTERPHONE DC CB on the FECB panel
ICS interconnect box power source and location
MEDC

B rack
Nav J box power source and location
MEAC / MEDC

B rack
purpose of Nav J box
signals routed to flight instruments through this box
TAS computer power source and location
MEAC / MEDC

C rack
electronic control amplifier purpose, power source, and location
boosts navaid output to a usable level for display on instruments

MEAC / MEDC

B rack
RAWS power source and location
MEAC / MEDC (both RAWS 1 and RAWS 2)

B rack
strobe light power source and location
Bus B / EMDC

flasher relay: main load center
upper strobe power supply: overhead near main cabin door
lower strobe power supply: HSC
SDRS power source and location
MDC

MLC
what do the left and right pitot tubes connect to
left
- pilot airspeed

right
- copilot airspeed
- autopilot air data sensor
- true airspeed transducer
- landing gear warning system
RAWS warnings come on when ___ and are inhibited when ___
- high: 3 seconds at 380 +/- 20 ft
- low: continuous at 170 +/- 10 ft
- RADALT is unreliable
- loss of power to the RADALT

Inhibited when:
- nose gear is down
- aircraft is on the ground
- flaps below maneuver
- aircraft is 500-1000 ft above reference altitude
what items are in the B rack
- RAWS 1 & 2
- VOR 1 & 2 nav converters
- glideslope receiver
- ADF filter
- Nav J box
- ECA 1 & 2
- flight director
what items are in the C rack
C1/C2:
- autopilot
- TACAN
- GPS
- TAS computer
- standby gyro
- rate of turn control

C3:
- sync box
- side windshield heat
what items are in the F rack
- marker beacon receiver
- ADF receiver
- UHF 1 & 2
- HF-2
what items are in the H rack
- INS 1 & 2
- MHRS compass couplers 1 & 2
- APX-72 IFF transponder
- ladder power
what items are in the J rack
- VOR 1 & 2 receivers
- VHF radio
what items are in the main load center
- runaround relays 1 & 2
- transformer rectifiers 1 & 2
- transfer relays
- sup panels for gens 2, 3, 4, and APU
- fuel flow power supply
- strobe light flasher relay
- prop deice timer
- external power monitor
- SDRS
explain TR load meters on MLC CB panel
- shows the percentage of load on the TR
- scale of 0.0 to 1.0
- TRs 1 & 2 should be approx equal
list items in the HSC
- 4 hydraulic pumps
- 2 hydraulic reservoirs
- air brake bottle
- brake accumulator
- aileron boost package
- flap motor
- landing gear control valve
- bottom strobe light power supply
list items in the doppler well
- cabin exhaust fan
- outflow valve
- radar altimeter
which aircraft has single vs. dual RAWS
PB-20N autopilots have only one RAWS
explain the selection of top vs. bottom antennas with the ___ radio
ARC-182 (red digital U/VHF)

- top is VHF only, bottom is U/VHF
- Caution: selection of the top antenna while using a UHF freq could cause radio damage
- if only the top antenna works, CASS is selected on the bottom antenna at the acoustic operator station
quickest way to tell if you have a CIP aircraft
U/VHF POWER button above copilot CDNU
if the UHF 1 & 2 lights aren't working on the ICS panel, but radios actually work
communication selector panel power at the NAV/COMM station needs to be turned on
how do you know if anyone has ICS DISC selected
your ICS OVERRIDE button illuminates green
what does ICS DISC do
incoming ICS is disconnected from your headset and goes to the other pilot, who cannot select ICS DISC at the same time
can you take the aircraft if the INS won't align
- don't have to align to get into ATT REF mode
- only time you need them in NAV mode is outside NAVAID coverage
max altimeter split
+/-75 ft from field elevation
at 10,000 ft: 200 ft
at 20,000 ft: 300 ft
max airspeed split
5 kts at 140 kts
RAWS can be tested by
pressing the TEST buttons on MEDC
use of TAS heater
- should be off except in icing
- Warning: use only during flight
weather radar operation with people or when flying
not on within
- 15 ft of people
- 75 ft of fueling
major effects of MEDC loss
- Ess Bus Mon switch needs to be turned off for P turn needle or peanut gyro
- wedge
- no fire protection (tell observers)
- ground air sensing (flight idle stops, REFR OVHT on landing)
- probably fails to feather on #1 or #4
- no bus priorities / transfer relays
major effects of MEAC loss
- red instrument lights, FDIs, and standby gyro auto swap to FEAC via Ess Int and Ltg CB
- lost INS 1
- lost sychro-excitation voltage to display INS 2 (CP select stby gyro)