EPs (Escalated Panics) Flashcards
INDICATIONS:
- AIRCRAFT SPINNING
- NF/NR INCREASE
- AIRCRAFT DEBRIS POSSIBLY SEEN FLYING
COMPLETE LOSS OF TAIL ROTOR COMPONENTS [B]
INDICATIONS:
- RGT/LFT (OR BOTH) FUEL BOOST PUMP - light illuminates
- FUEL PSI DROPS TO ZERO IF BOTH
LAND AS SOON AS PRACTICAL FOR ONE
LAND AS SOON AS POSSIBLE FOR BOTH (WARNING ASSOCIATED)
FUEL BOOST PUMP FAILURE
INDICATIONS: *ON GROUND*
- EGT RISES
- FUEL PSI DROPS
- ENG FIRE / FIRE - light illuminates
FIRE - GROUND
INDICATIONS: *AT ENGINE START-UP*
- VDC - DROPS BELOW 23.5V
- EGT SPIKES
ENGINE HOT START [B]
INDICATIONS:
- MISCMPR - light illuminates
- Mis-compared gauge lettering becomes yellow and a yellow double sided arrow appears above the gauge label
MISCMPR
INDICATIONS:
- AIRCRAFT IN COMPLETE SPIN
- AIRCRAFT AIRSPEED <60 KTS
COMPLETE LOSS OF TAIL ROTOR THRUST (UNCONTROLLABLE) [B]
INDICATIONS:
- AIRCRAFT OUT OF TRIM
- NOSE SWINGS RIGHT
- AIRCRAFT ROLLS LEFT
- ANTI-TORQUE PEDALS HAVE NO EFFECT
- AIRSPEED >60 KTS
COMPLETE LOST OF TAIL ROTOR THRUST (CONTROLLABLE)
INDICATIONS:
- CHIP DET - light illuminates
(TRANSMISSION/TAIL ROTOR) CHIP DETECTION
INDICATIONS:
- 20 MIN FUEL - light illuminates
- FUEL GAUGE BETWEEN 130 - 240 LBS
20 MIN FUEL
INDICATIONS:
- MAIN AMP - INCREASES
- AIRCRAFT CABIN IS FILLED WITH SULFUR (ROTTEN EGG) SMELL
OVERHEATED BATTERY
INDICATIONS:
- CENTER/DUAL/TRIPLE MFD DISPLAY BLACKS OUT
MFD FAILURE (SINGLE/DUAL/TRIPLE)
INDICATIONS:
- ABRUPT, EVASIVE MANEUVER
- INADVERTENTLY LOWER COLLECTIVE
- MOMENTARY SPIKE IN NF/NR
- BUMP FELT AND/OR HEARD
- ENTIRE AIRCRAFT MAY SHAKE
MAST BUMPING
INDICATIONS:
- XMSN OIL -
- PSI DROPS *or*
- C° INCREASES
TRANSMISSION OIL - HOT/LOW PRESSURE
INDICATIONS:
- RED “X” OVER ATTITUDE INDICATOR
- “IN ALIGN” NEXT TO HEADING INDICATOR
AHRS IN ALIGN
INDICATIONS:
- DC GEN - light illuminates
- VDC GAUGE DROPS
MAIN GENERATOR FAILURE
INDICATIONS:
- CYCLIC STIFFNESS IN 2 OF 4 QUADRANTS
ISOLATED CONTROL STIFFNESS (CYCLIC)
INDICATIONS:
- RPM WARN - light illuminated
- NF, NR, NG, EGT, ENG OIL PSI, XMSN OIL PSI, TQ% - ALL DROP
ENGINE FAILURE [B]
INDICATIONS: *AFTER ENTERING AUTO-ROTATION*
- NF/NR - DOES NOT SPLIT
- RPM WARN - light illuminates
CLUTCH FAILS TO DISENGAGE
INDICATIONS: *F.A.F.D.&.H*
- ACIDIC SMELL
- SMOKE COMING FROM OVERHEAD PANEL
- MAIN AMP - OVER AMPERAGE
ELECTRICAL FIRE - IN FLIGHT
INDICATIONS: *F.A.F.D.&.H*
- RPM WARN - light illuminates
- NF - INCREASES
- NR - DECREASES
- TQ% - DROPS
- LEFT YAW
MAIN DRIVESHAFT FAILURE [B]
INDICATIONS:
- ENG FUEL PUMP - light illuminates
ENGINE FUEL PUMP MALFUNCTION
INDICATIONS:
- RIGHT YAW
- RPM WARN - light illuminates
- NF/NR INCREASES
ENGINE OVER-SPEED [B]
INDICATIONS:
- AIRCRAFT NOSE BEGINS TO SLOWLY TURN RIGHT
- DOES NOT RESOLVE WITH FULL LEFT PEDAL
LOSS OF TAIL ROTOR EFFECTIVENESS
INDICATIONS:
- COLLECTIVE FORCED DOWN
- AIRCRAFT STARTS TO DESCEND
FLIGHT CONTROL SERVO HARD-OVER (COLLECTIVE) [B]
INDICATIONS:
- AIRCRAFT BEGINS TO DESCEND
- NF/NR GAUGES SLIGHTLY DROPS
ENGINE UNDER-SPEED [B]
INDICATIONS: *IN AUTO-ROTATION* ATTEMPTING POWER RECOVERY*
- NF/NR DOES NOT MARRY BACK UP
CLUTCH FAILS TO RE-ENGAGE [B]
INDICATIONS:
*WITH INCREASED COLLECTIVE*
- NF/NR DECREASES
- EGT & NG SLIGHTLY INCREASES
- TQ% INCREASES
*WITH DECREASED COLLECTIVE*
- NF/NR INCREASES
- EGT & NG DECREASES
- TQ% DECREASES
DROOP CAM COMPENSATOR FAILURE
INDICATIONS:
FUEL FILTER - light illuminates
FUEL FILTER CONTAMINATION
INDICATIONS: *F.A.F.D.&.H*
- ENG FIRE - light illuminates
- EGT - RISES
- SMOKE & FUMES NOTICED
FIRE - IN FLIGHT
INDICATIONS:
- CYCLIC IS FORCED TO THE FRONT-RIGHT QUADRANT
- AIRCRAFT BEGINS TO ROLL OVER
FLIGHT CONTROL SERVO HARD-OVER (CYCLIC) [B]
INDICATIONS:
- RED “X” ON TOP LEFT GAUGE (AIRSPEED) & RIGHT TWO GAUGES (ALTIMETER & VERTICAL SPEED)
- RED “X” REMAINS WHEN “ADC” IS PRESSED ON MFD
ADC FAILURE (DUAL)
INDICATIONS:
- RISING EGT & NG
- TQ% STUCK AT 40%
VARIABLE INLET GUIDE VAIN (VIGV) ACTUATOR FAILURE (CLOSED)
INDICATIONS:
- PEDALS FEEL STIFF
- AIRCRAFT GOES OUT OF TRIM (L/R)
FIXED PITCH FAILURE
INDICATIONS:
- FLUCTUATING: NF, NG, EGT, & TQ%
- LOUD BANGING HEARD IN AIRCRAFT
ENGINE COMPRESSOR STALL
INDICATIONS:
- HYD PRESS LO - light illuminated
- ALL CONTROLS ARE MOVABLE WITH MODERATE BINDING
HYDRAULIC POWER FAILURE
