Boldface Flashcards
EMERGENCY ENGINE SHUTDOWN ON THE GROUND
PCL - OFF
FIREWALL SHUTOFF HANDLE - PULL
ABORT (BF)
PCL - IDLE
BRAKES - AS REQUIRED
ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF (SUFFICIENT RUNWAY REMAINING STRAIGHT AHEAD)
AIRSPEED - 110 KNOTS (MINIMUM)
PCL - AS REQUIRED
EMER LDG GR HANDLE - PULL (AS REQUIRED)
ENGINE FAILURE DURING FLIGHT
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
IMMEDIATE AIRSTART (PMU NORM)
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
UNCOMMANDED POWER CHANGES/LOSS OF POWER/UNCOMMANDED PROPELLER FEATHER
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
INADVERTENT DEPARTURE FROM CONTROLLED FIGHT
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
FIRE IN FLIGHT
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.
OBOGS FAILURE/OVERTEMP/PHYSIOLOGICAL SYMPTOMS
GREEN RING - PULL (AS REQUIRED)
DESCENT BELOW 10,000 FEET MSL - INITIATE
OBOGS SUPPLY LEVER - OFF (BOTH)
PHYSIOLOGICAL SYMPTOMS <32>
BOS PUSH MAN - PRESS ON
EJECTION boldface
EJECTION HANDLE - PULL
POST ejection checklist (steps 1-
- Canopy: Inspect the canopy/inspection lines
- Visor: Raise for better visibility
- Mask: Remove mask/CRU 60 (discard)
- Seat survival kit: Check that it deployed, hanging off LEFT (If not then pull kit release)
- LPU: Find reg toggles and pull downward to inflate
- Steer
BAT BUS
BATTERY BUS FAILURE
GEN BUS
GENERATOR BUS FAILURE
PMU FAIL
PMU FAILURE
GEN
GENERATOR FAILURE
CKPT PX
COCKPIT PX EXCEEDS 3.9 PSI
Red CANOPY
Canopy unlocked/unsafe
RED FUEL PX
FUEL PRESSURE BELOW 10 PSI MOTIVE LINE
RED OIL PX
OIL PX BELOW 40 PSI ABOVE IDLE, BELOW 15 AT IDLE
OBOGS FAIL
OBOGS has FAILED
CHIP light
CHIP - CHIP DETECTOR INDICATES OIL CONTAMINATION
CKPT ALT
COCKPIT ALT ABOVE 19,000 FEET
HYDR FL LO
HYD FLUID BELOW 1 QT
Amber OIL PX
OIL PX 15-40 PSI AT IDLE / 40-90 ABOVE IDLE 10 SECONDS
BUS TIE
BUS TIE SWITCH OPEN OR FAILED
FUEL BAL
IMBALANCE 30 POUNDS FOR 2 MINUTES, OR FUEL PROBE FAILURE
PMU STATUS
PMU FAULT OR WEIGHT ON WHEELS FAILURE
EHYD PX LO
EMERGENCY HYDRO PX 2400 +/- 150psi
TAD FAIL
RUDDER TAD FAILURE
OBOGS TEMP
OBOGS TEMP ABOVE 200F
L/R FUEL LO
L FUEL LO - LEFT TANK BELOW 110 POUNDS USABLE FUEL
R FUEL LO - RIGHT TANK BELOW 110 POUNDS USABLE FUEL
DUCT TEMP
ENVIRONMENTAL DUCT OR DEFOG DUCT ABOVE 300F
IGN SEL
IGNITION ON
M FUEL BAL
FUEL BALANCE SWITCH IN MANUAL
TRIM OFF
TRIM DISCONNECT SWITCH ACTIVATED
BOOST PUMP
BOOST PUMP ON FROM STARTER SWITCH/LOW PX/RELAY
ANTI-ICE
PROBES ANTI ICE SWITCH ON
TAD OFF
TAD IS SELECTED OFF
ST READY
PCL IS IN THE AUTO START POSITION
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
GEN BUS FAIL
What will you lose and what considerations?
EHSI, Altimiter, ASI/TAS/VSI, RMU, Air conditioning, NWS, speed brake, etc
