Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
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) |