Boldface Flashcards

1
Q

EMERGENCY ENGINE SHUTDOWN ON THE GROUND

A

PCL - OFF
FIREWALL SHUTOFF HANDLE - PULL

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2
Q

ABORT (BF)

A

PCL - IDLE
BRAKES - AS REQUIRED

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3
Q

ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF (SUFFICIENT RUNWAY REMAINING STRAIGHT AHEAD)

A

AIRSPEED - 110 KNOTS (MINIMUM)
PCL - AS REQUIRED
EMER LDG GR HANDLE - PULL (AS REQUIRED)

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4
Q

ENGINE FAILURE DURING FLIGHT

A

ZOOM/GLIDE - 125 KNOTS (MINIMUM)
PCL - OFF
INTERCEPT ELP

2G pullup at 20 degrees if above 150 knots
0.5G bunt over to capture 125 knots

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5
Q

IMMEDIATE AIRSTART (PMU NORM)

A

PCL - OFF
STARTER SWITCH - AUTO/RESET
PCL - IDLE, ABOVE 13% N1

125-200 knots sea level - 15,000 feet
135-200 knots 15,001 - 20,000 feet
Excess of 1,200 feet lost during restart
PCL movement before 67% N1 may cause engine failure

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6
Q

UNCOMMANDED POWER CHANGES/LOSS OF POWER/UNCOMMANDED PROPELLER FEATHER

A

PCL - MID RANGE
PMU SWITCH - OFF
PROP SYS CIRCUIT BREAKER (left front console) - PULL, IF Np STABLE BELOW 40%

  • Incorrect signal to feather dump solenoid may cause feather, pulling PROP SYS CB removes power from solenoid and prop unfeathers
  • 15-20 seconds to fully unfeather
  • PCL above idle is best for engine recovery
  • Ground idle not available during landing
  • If rate of descent at 125 knots is greater than 1500 ft/min, use power up to 131% torque to achieve 1350-1500 ft/min descent. If unable, set PCL off
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7
Q

INADVERTENT DEPARTURE FROM CONTROLLED FIGHT

A

PCL - IDLE
CONTROLS - NEUTRAL
ALTITUDE - CHECK

Power on/advertent departure inverted or power-on results in high stresses on the engine. Suspect possible engine damage, chip light

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8
Q

FIRE IN FLIGHT

A

PCL - OFF
FIREWALL SHUTOFF HANDLE - PULL

Do not shut down for unconfirmed fire:
Fluctuating fuel flow
Excessive ITT
Visual
Erratic operation
Roughness
- May be from high engine compartment temps due to bleed air leak. Retard PCL and see if light goes out.

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9
Q

OBOGS FAILURE/OVERTEMP/PHYSIOLOGICAL SYMPTOMS

A

GREEN RING - PULL (AS REQUIRED)
DESCENT BELOW 10,000 FEET MSL - INITIATE
OBOGS SUPPLY LEVER - OFF (BOTH)

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10
Q

PHYSIOLOGICAL SYMPTOMS <32>

A

BOS PUSH MAN - PRESS ON

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11
Q

EJECTION boldface

A

EJECTION HANDLE - PULL

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12
Q

POST ejection checklist (steps 1-

A
  1. Canopy: Inspect the canopy/inspection lines
  2. Visor: Raise for better visibility
  3. Mask: Remove mask/CRU 60 (discard)
  4. Seat survival kit: Check that it deployed, hanging off LEFT (If not then pull kit release)
  5. LPU: Find reg toggles and pull downward to inflate
  6. Steer
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13
Q

BAT BUS

A

BATTERY BUS FAILURE

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14
Q

GEN BUS

A

GENERATOR BUS FAILURE

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15
Q

PMU FAIL

A

PMU FAILURE

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16
Q

GEN

A

GENERATOR FAILURE

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17
Q

CKPT PX

A

COCKPIT PX EXCEEDS 3.9 PSI

18
Q

Red CANOPY

A

Canopy unlocked/unsafe

19
Q

RED FUEL PX

A

FUEL PRESSURE BELOW 10 PSI MOTIVE LINE

20
Q

RED OIL PX

A

OIL PX BELOW 40 PSI ABOVE IDLE, BELOW 15 AT IDLE

21
Q

OBOGS FAIL

A

OBOGS has FAILED

22
Q

CHIP light

A

CHIP - CHIP DETECTOR INDICATES OIL CONTAMINATION

23
Q

CKPT ALT

A

COCKPIT ALT ABOVE 19,000 FEET

24
Q

HYDR FL LO

A

HYD FLUID BELOW 1 QT

25
Amber OIL PX
OIL PX 15-40 PSI AT IDLE / 40-90 ABOVE IDLE 10 SECONDS
26
BUS TIE
BUS TIE SWITCH OPEN OR FAILED
27
FUEL BAL
IMBALANCE 30 POUNDS FOR 2 MINUTES, OR FUEL PROBE FAILURE
28
PMU STATUS
PMU FAULT OR WEIGHT ON WHEELS FAILURE
29
EHYD PX LO
EMERGENCY HYDRO PX 2400 +/- 150psi
30
TAD FAIL
RUDDER TAD FAILURE
31
OBOGS TEMP
OBOGS TEMP ABOVE 200F
32
L/R FUEL LO
L FUEL LO - LEFT TANK BELOW 110 POUNDS USABLE FUEL R FUEL LO - RIGHT TANK BELOW 110 POUNDS USABLE FUEL
33
DUCT TEMP
ENVIRONMENTAL DUCT OR DEFOG DUCT ABOVE 300F
34
IGN SEL
IGNITION ON
35
M FUEL BAL
FUEL BALANCE SWITCH IN MANUAL
36
TRIM OFF
TRIM DISCONNECT SWITCH ACTIVATED
37
BOOST PUMP
BOOST PUMP ON FROM STARTER SWITCH/LOW PX/RELAY
38
ANTI-ICE
PROBES ANTI ICE SWITCH ON
39
TAD OFF
TAD IS SELECTED OFF
40
ST READY
PCL IS IN THE AUTO START POSITION
41
BAT BUS FAIL What will you lose, what considerations must you account for?
- Plan to use landing gear emergency extension system (LDG GR control/indications inop) Most notable failures will be EADI, GPS, AEDD, PRESSURIZATION OIL PX, HYD FL LO annunciators
42
GEN BUS FAIL What will you lose and what considerations?
EHSI, Altimiter, ASI/TAS/VSI, RMU, Air conditioning, NWS, speed brake, etc