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P3C > Acronyms > Flashcards

Acronyms Flashcards

1
Q

FFFFBOGE

A

F-CLOSES FUEL SHUTOFF VALVE E&M
F-CLOSES FUEL TANK EMERGENCY SHUTOFF VALVE M
F-ACTUATES FEATHER SYSTEM BY SUCKING FEATHER BUTTON IN E
F-POSITIONS FEATHER VALVE TO FEATHER POSITION M
B-CLOSES BLEED AIR VALVE E
O-CLOSES OIL TANK SHUTOFF VALVE E
G-CLOSES GENERATOR COOLING AIR DOOR M
E-DUMPS EDC & CLOSES FIREWALL SHUTOFF VALVE E

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2
Q

SAM

A

3 CIRCUIT BREAKERS BEHIND COPILOT
S-START DC
A-ARMAMENT
M-MON DC

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3
Q

HUAMARI

A 
LOST TO PARTIAL LOAD MONITORING BELOW 8,000
H-HF2
U-UHF2
A-ADF
M-MARKER BEACON
A-AUTOPILOT
R-RADAR
I-INS 2
ABOVE 8000
1A HYDRAULIC PUMP
DE-ENERGIZES ANTI-ICE SYSTEM
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4
Q

BUPER

A 
NO EXTERNAL POWER
B-BATTERY
U-UPLOCK SWITCH
P-PHASE WRONG
E-EXTERNAL POWER CIRCUIT BREAKER
R-RUNAROUND FEEDER 4
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5
Q

32MM

A 
PARTIAL POWER SUPPLIED TO AIRCRAFT
3-TRANSFORMER RECTIFIER 3
2-ESS DC BUS FEEDER 2
M-ESS BUS MONITORING SWITCH
M-MON ESS AC BUS
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6
Q

BUGGPIIT IP CAG

A 
POWERED BY FLIGHT DC
B-BELL
U-UTILITY LIGHTS
G-GOB RELAY
G-GEN 4 AUX CONTROL
P-PITCHLOCK RESET
I-INVERTER RELAY
I-IFF
T-TURN NEEDLE (MON AC PRIMARY)
I-INS 1&2
P-PEANUT GYRO (MON DC PRIMARY)
C-COPILOT CDU
A-ADDU (MON AC PRIMARY)
G-GPS AMPLIFIER
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7
Q

BIG 4

A

BUS A CONTROL (MON DC)
BUS B CONTROL (MON DC)
GEN 4 TRANSFER CONTROL (MON DC)
GEN 4 AUX CONTROL (FLT DC)

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8
Q

GFASG

A 
APU START IN FLIGHT
G-GEN OFF
F-FUEL
A-ARM 1. GOB 2.CLOSES LCV 3. BYPASS SCISSOR SWITCH
S-START
G-GEN ON
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9
Q

POSSFIRE

A 
POWERED BY FLIGHT AC
P-PILOT PITOT HEAT
O-OUTFLOW VALVE
S-STANDBY ATTITUDE (MON AC)
S-STANDBY VERT GYRON (MON AC)
F-FDI (MON AC)
I-IFF TRANSPONDER
R-RADALT
E-ESSENTIAL LIGHTING (MON AC)
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10
Q

WEEBOC

A 
USES OF 14TH STAGE BLEED AIR
W-WING DEICE
E-ENGINE ANTI-ICE
E-ENGINE START
B-BOMB BAY HEATING
O-OIL COOLER AUGMENTATION
C-CLOSES 5TH AND 10TH STAGE BLEED AIR
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11
Q

FESSMOS

A 
POWER ACCESSORY SECTION
F-FUEL CONTROL UNIT
E-ENGINE DRIVEN FUEL PUMP (3)
   PRIMARY AND SECONDARY, ENGINE-DRIVEN FUEL          PUMP
S-SPEED SENSE CONTROL
S-SPEED SENSE VALVE
M-MAIN OIL PUMP
O-OIL FILTER
S-SCAVENGE OIL PUMP
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12
Q

STOGE

A 
RGB ACCESSORY SECTION
S-STARTER
T-TACH GENERATOR
O-OIL PUMP/FILTER ASSEMBLY
G-GENERATOR (2,3,4)
E-ENGINE DRIVEN COMPRESSOR (2&3)
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13
Q

CONDITIONS TO SHIFT TO LOW RPM

A
  1. NO POWER LEVER MOVEMENT
  2. MIN TORQUE USED, 0 DEGREES BLADE ANGLE
  3. NO USE OF BLEED AIR
  4. LESS THAN 50 KNOTS
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14
Q

FEAR THE BOMB BAY

A 
CONTROLLED BY 1 AND 2 HYD SYSTEM
F-FLAPS
E-ELEVATOR
A-AILERON
R-RUDDER
BOMB BAY
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15
Q

BETTER U FLY BACK VFR

A 
SINGLE GEN BRIEF FLYING (IF GEN FAILS)
B-BOOST HANDLES UNCOVERED
U-UTILITY LIGHTS
F-FLASHLIGHTS
B-BRIEF COPILOT TO TURN OF ESS BUS MONITORING SWITCH FOR BATTERY BACK UP
VFR FLIGHT BACK
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16
Q

CONDITIONS TO GO ON INDUCING

A

OIL COOLER DOOR FULLY OPEN
POWER LEVER BELOW 32 DEGREES COORDINATOR (BETA)
START SELECTOR OFF

17
Q

WHY SHIFT TO LOW RPM

A

FOD PREVENTION
NOISE ABATEMENT
FUEL CONSERVATION

18
Q

TROUBLESHOOTING TECHNIQUE

A

LIGHT SWITCH CIRCUIT BREAKER BUS COMPONENT

19
Q

GOOFBUTS

A 
PROBABLE CAUSES FOR GEN OFF LIGHT
G-GENERATOR FAILURE
O-OVERVOLTAGE
O-OFF FREQUENCY
F-FEEDER FAULT
B-BUS MONITORING SWITCH OFF
U-UNDERVOLTAGE
T-TRANSFER RELAY 2 OR 3 FAILURE
S-SUP PANEL FAILURE
20
Q

DAVI

A 
PRESURRIZATION LOSS
D-DON OXYGEN MASKS
A-ALERT CREW
V-VERIFY OBSTACLE CLEARANCE
I-INVESTIGATE PRESSURIZATION LOSS
21
Q

VPFOOTC

A 
REASONS TO SHUTDOWN AN ENGINE
V-VIBRATION
P-POWER LOSS
F-FIRE
O-OIL HOT
O-OIL PRESSURE LOW
T-TIT UNCONTROLLABLE
C-CHIPS LIGHT W/ SECONDARIES
22
Q

TAB FREEPLAY

A 
REASON TO NOT GO BOOST OUT
T-TRIM TAB MALFUNCTION
A-AUTOPILOT MALFUNCTION
B-BINDING OF FLIGHT CONTROLS
FREE PLAY OF CONTROLS
23
Q

ABCDEF WIND UP THE TAILPIPE

A 
REASONS FOR HOT START
A-AIR SUPPLY POOR
B-BLADE ANGLE INCORRECT
C-COMPRESSOR STALLED
D- MALFUNCTIONING TD
E- ELECTRICAL FAULT
F- FAULTY FUEL CONTROL
WIND UP THE TAILPIPE
24
Q

DITCHES

A 
IF IMMEDIATE DITCH, WHAT TO TRY AND GET DONE BEFORE IMPACT
D-DESCEND/DEPRESSURIZE
I-IFF
T-TECHNIQUE/TIME
C-CONFIGURATION
H-HEADING
E-EMERGENCY MESSAGE
S-SPEEDS
25
Q

2B A 2P and LAND

A 
PROP PROTECTIVE MEASURES
B-BETA FOLLOWUP
B-BRAKE
A-AUTOFEATHER
P-PITCHLOCK
P-PITCHLOCK RESET
L-LOW PITCH STOPS
A-AIRSTART (45 DEGREES)
N-NTS
D-DECOUPLE
26
Q 
International
Space 
Station
Pilots
F
Double
Ds
A 
EDC PROTECTIVE MEASURES
I-ICE LIMITER
S-SURGE CONTROL
S- SHEAR (257 HP)
P- PRESSURE RATIO LIMITING
F-FLOW CONTROL
D-DISCONNECT
D-DUMP
27
Q

HEATER, FEEDERS, AND EATERS

A

WHAT IS LOST WHEN ON 1 GENERATOR AND TURN ON EMP AND/OR PROP DEICE
HEATER-SIDE WINDSHIELD HEAT
FEEDERS-MON DC ON ELECTRONIC POWER FEEDERS (MON DC) AND MON AC ON ELECTRONIC POWER FEEDERS (BUS A)
EATERS-GALLEY POWER

28
Q

Super Fly Feeds the Bear

A 
Unresettable Generator Malfunctions
Super-Supervisory panel failure
Fly-Flyweight Diode busted
Feeds-Feeder Fault
Bear-Bearing Failure

P3C (10 decks)

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