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Bold Face Memory Items > IN-FLIGHT EMERGENCIES > Flashcards

IN-FLIGHT EMERGENCIES Flashcards

0
Q

ENGINE FAILURE DURING FLIGHT

A
    1. ZOOM/GLIDE - 125 KNOTS (MINIMUM)
    1. PCL - OFF
    1. INTERCEPT ELP
    1. Airstart - ATTEMPT IF WARRANTED

if conditions do not warrant an airstart:

    1. FIREWALL SHUTOFF handle - PULL
    1. Execute Forced Landing or Eject
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1
Q

ENGINE FAILURE DURING FLIGHT

*memory item

A
    1. ZOOM/GLIDE - 125 KNOTS (MINIMUM)
    1. PCL - OFF
    1. INTERCEPT ELP
    1. Airstart - Attempt if warranted
    1. FIREWALL SHUTOFF handle - Pull
    1. Execute Forced Landing or Eject
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2
Q

PMU NORM AIRSTART

A
  1. PCL - OFF
  2. Confirm the position of the following
    a. START, IGN, BOOST PUMP, and PMU circuit breakers (left front console) - In
    b. FIREWALL SHUTOFF handle - Down
  3. BLEED AIR INFLOW switch - OFF
  4. BOOST PUMP switch - ON
  5. IGNITION switch - ON
  6. STARTER switch - AUTO/RESET
  7. PCL - IDLE, above 13% N(sub 1)
  8. Engine instruments - Monitor ITT, N(sub 1), and oil pressure
    If unsuccessful:
  9. PCL - OFF
  10. FIREWALL SHUTOFF handle- Pull
  11. Execute Forced Landing or Eject
    If successful:
  12. PCL As required after N(sub 1) reaches IDLE RPM (approx. 67% N(sub 1)
  13. STARTER switch - NORM
  14. GEN switch - Verify ON, reset if necessary
  15. BLEED AIR INFLOW switch - NORM
  16. OBOGS - As required
  17. PEL - Execute
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3
Q

PMU OFF AIRSTART

A
  1. PCL - OFF
  2. PMU switch - OFF
  3. Confirm the position of the following
    a. START, IGN, BOOST PUMP, and PMU circuit breakers (left front console) - IN
    b. FIREWALL SHUTOFF handle - Down
  4. BLEED AIR INFLOW switch - OFF
  5. BOOST PUMP switch - ON
  6. IGNITION switch - ON
  7. STARTER switch - MANUAL
  8. PCL - at 13% N(1), MINIMUM, ADVANCE TO OBTAIN INITIAL FUEL FLOW, THEN SLOWLY TO IDLE
  9. Engine instruments - Monitor ITT, N(1), and oil pressure
    If unsuccessful:
  10. PCL - OFF
  11. FIREWALL SHUTOFF handle- Pull
  12. Execute Forced Landing or Eject
    If successful:
  13. PCL As required after N(1) reaches IDLE RPM (approx. 67% N(1)
  14. STARTER switch - NORM
  15. GEN switch - Verify ON, reset if necessary
  16. BLEED AIR INFLOW switch - NORM
  17. OBOGS - As required
  18. PEL - Execute
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4
Q 
IMMEDIATE AIRSTART (PMU NORM)
(memory item)
A

*1. PCL - OFF
*2. STARTER switch - AUTO/RESET
*3. PCL - IDLE, ABOVE 13% N(1)
*4. Engine instruments - Monitor ITT, N(sub 1), and oil pressure
IF AIRSTART IS UNSUCCESSFUL:
*5. PCL - OFF
*6. FIREWALL SHUTOFF handle- Pull
*7. Execute Forced Landing or Eject
If successful:
*8. PCL As required after N(1) reaches IDLE RPM (approx. 67% N(1))
*9. PEL - Execute
10, Confirm the position of the following:
a. BOOST PUMP switch - ON
b. IGNITION switch - ON
11. STARTER switch - NORM
12. BLEED AIR INFLOW switch - NORM
13. GEN switch - Verify ON, reset if necessary
14. OBOGS - As required

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5
Q

UNCOMMANDED POWER CHANGE/LOSS OF POWER/UNCOMMANDED PROPELLER FEATHER

A
    1. PCL - MID RANGE
    1. PMU SWITCH - OFF
    1. PROP SYS CIRCUIT BREAKER (left front console) PULL, IF N(p) STABLE BELOW 40%
    1. PCL- AS REQUIRED

if power is sufficient for continued flight:
*5. PEL - EXECUTE

if power is insufficient to complete PEL:

    1. PROP SYS circuit breaker- RESET; AS REQUIRED
    1. PCL - OFF
    1. FIREWALL SHUTOFF handle - PULL
    1. Execute Forced Landing or Eject
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6
Q

COMPRESSOR STALLS

A

*1. PCL - SLOWLY RETARD BELOW STALL THRESHOLD
*2. DEFOG switch - ON
*3. PCL - SLOWLY ADVANCED (AS REQUIRED)
if power is sufficient for continued flight:
*4. PEL - EXECUTE
if power is insufficient to complete PEL:
*5. PCL - OFF
*6. FIREWALL SHUTOFF handle - PULL
*7. Execute forced landing or eject

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7
Q

INADVERTENT DEPARTURE FROM CONTROLLED FLIGHT

A
    1. PCL - IDLE
    1. CONTROLS - NEUTRAL
    1. ALTITUDE - CHECK
    1. Recover from unusual attitude
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8
Q

FIRE IN FLIGHT

A 
if fire is confirmed
*1. PCL - OFF
*2. FIREWALL SHUTOFF HANDLE - PULL
if fire is extinguished:
*3. Forced landing - EXECUTE
if fire does not extinguish or forced landing is impractical:
*4. Eject (BOTH)
if fire is not confirmed
*5. PEL - EXECUTE
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9
Q

SMOKE AND FUME ELIMINATION/

ELECTRICAL FIRE

A
  1. Descent below 10,000 ft MSL - Initiate (AsReq)
  2. PRESSURIZATION switch - RAM/DUMP
    Note
  3. BLEED AIR INFLOW switch - OFF
IF SMOKE/FIRE PERSISTS:
4. BAT and GEN switches - OFF
WARNING
5. AUX BAT switch - OFF (AsReq)
6. CFS - Rotate 90 counterclockwise and pull (if necessary)
WARNING
7. Restore electrical power - AsReq
Note
8. Land ASAP
Note
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10
Q

PMU FAILURE

A

if the PMU FAIL warning illuminates, accomplish the following:
1. PCL - MINIMUM PRACTICAL FOR FLIGHT
2. PMU switch - OFF
to reset PMU:
3 IGN, START, and PMU circuit breakers (left front console - CHECK AND RESET IF NECESSARY
4. PMU switch - NORM (ATTEMPT SECOND RESET IF NECESSARY)
if PMU reset is unsuccessful:
5. PMU switch - OFF
6. Land as soon as practical

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10
Q

PMU FAULT

IN FLIGHT

A

the PMU has detected a discrepancy in the weight on wheels switch. A reset is not possible

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11
Q

CHIP DETECTOR WARNING

A
    1. PCL - MINIMUM NECESSARY TO INTERCEPT ELP; AVOID UNNECESSARY PCL MOVEMENTS
    1. PEL - EXECUTE
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12
Q

OIL SYSTEM MALFUNCTION OR LOW OIL PRESSIRE

A

if only amber OIL PX caution illuminates:

    1. Terminate maneuver
    1. Check oil pressure; if pressure is normal, continue operations

if red OIL PX warning illuminates and/or amber OIL PX caution remains illuminated for 5 seconds:

    1. PCL - MINIMUM NECESSARY TO INTERCEPT ELP; AVOID UNNECESSARY PCL MOVEMENTS
    1. PEL - EXECUTE
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13
Q

Generator Inoperative

A
  1. STARTER switch - NORM (BOTH)
    Note
  2. GEN switch - ON (front or back)
  3. GEN REST switch - Depress and hold for a minimum of 1 second

IF GEN REMAINS INOP (DC VOLT BELOW 25V AND AMMETER DISCHARGING)
4. Descent below 10,000 ft MSL - INITIATE (AsReq)
5. GEN switch - OFF (BOTH)
6. BUS TIE switch - OPEN (BUS TIE caution and GEN BUS warning illuminate)
Note:
7. Land ASAPractical
WARNING

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14
Q

Gen Bus Inop

A
  1. BUS TIE switch - NORM
    Note:
  2. Land ASAPractical
15
Q

Battery Bus Inop

A 
Note
1. Descent below 10,000 ft MSL - Initiate (AsReq)
WARNING
2. BUS TIE switch - OPEN
Note:
3. AUX BAT switch - ON
Note:
4. Standby VHF - ON
5. Land ASAPractical
16
Q

PRECAUTIONARY EMERGENCY LANDING

PEL

A
    1. Turn to nearest suitable field
    1. Climb or accelerate to intercept ELP
    1. Gear, flaps speed brake - UP
      1. Conduct a systematic check of the aircraft and instruments for additional signs of impending engine failure
      2. BOOST PUMP switch - AS REQUIRED
      3. IGNITION switch - AS REQUIRED
      4. Plan to intercept the emergency landing pattern at or below high key in the appropriate configuration and a minimum airspeed of 120 KIAS
17
Q

FORCED LANDING

A
    1. Airspeed - 125 KIAS PRIOR TO EXTENDING LANDING GEAR
    1. EMER LDG GR handle - PULL (A/R)
    1. Airspeed - 120 KIAS MIN UNTIL INTERCEPTING FINAL; 110 KIAS MIN ON FINAL
    1. Flaps- A/R

accomplish the following as conditions permit:

  1. Distress call- TRANSMIT
  2. ELT switch - A/R
  3. Transponder - 7700 (A/R)
  4. Harness - LOCKED (BOTH)
  5. Emergency Ground Egress procedure - EXECUTE (A/R)
18
Q

ABORT

A
    1. PCL - IDLE

* 2. BRAKES - A/R

19
Q

TIRE FAILURE DURING TAKEOFF

A

if the decision is made to stop:
1. Abort

if takefoff is continued:

  1. Gear and flaps position - DO NOT CHANGE
  2. Straight- in approach - EXECUTE
20
Q

ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF

SUFFICIENT RUNWAY REMAINING STRAIGHT AHEAD

A
    1. AIRSPEED - 110 KNOTS (MIN)
    1. PCL - AS REQUIRED
    1. EMER LDG GR HANDLE - PULL (A/R)
    1. Flaps - A/R
21
Q

FLIGHT WITH SHATTERED/DAMAGED CANOPY

A
  1. OBOGS - MAX (A/R) (BOTH)
  2. Airspeed - 150 KIAS MAX
  3. Descend - BELOW 18,000 FT MSL
  4. PRESSURIZATION switch- DUMP BELOW 18,000 FT MSL IF CANOPY DAMAGED BUT INTACT
  5. Controllability Check - A/R
  6. Land as soon as possible
22
Q

CANOPY UNLOCKED

A
  1. Airspeed - 150 KIAS MAX; AVOID ABRUPT MANEUVERING
  2. Descend below 18,000 ft MSL
  3. PRESSURIZATION switch - DUMP BELOW 18,000 FT MSL
  4. Land ASAP
23
Q

RUNAWAY TRIM

A
  1. Trim interrupt button (control stick) - DEPRESS AND HOLD
  2. Airspeed - A/R TO REDUCE CONTROL FORCES
  3. TRIM DISCONNECT switch (left console) - TRIM DISCONNECT
  4. Trim interrupt button (control stick) - RELEASE
  5. AIL/EL TRIM or RUD TRIM circuit breaker(s) (left front console) - PULL A/R
  6. TRIM DISCONNECT switch (left console) - NORM
  7. Controllability Check - A/R
24
Q

STUCK/FAILED TRIM

A
  1. TRIM DISCONNECT switch (left console) - NORM

2. AIL/EL TRIM or RUD TRIM circuit breaker(s) (LF console) - CHECK, RESET IF OPEN

25
Q

TRIM AID DEVICE FAILURE (TAD)

A
  1. TAD circuit breaker (RF console) - CHECK IN OR PULL AND RESET
  2. TRIM AID switch - ENGAGE AFTER TAD FAIL CAUTION EXTINGUISHES
26
Q

ASYMMETRIC FLAPS

SPLIT-FLAP CONDITION

A
  1. Airspeed - A/R TO MAINTAIN CONTROL AND MIN CONTROL EFFORT
  2. Flap control handle - ACTUATE TO MIN OR ELIMINATE FLAP ASYMMETRY
  3. Controllability Check - A/R
  4. Land via straight-in approach
27
Q

CONTROLLABILITY CHECK

STRUCTURAL DAMAGE/FLIGHT CONTROL MALFUNCTION

A
  1. Climb to min 6000 feet AGL, if practical

on aircraft with a suspected rudder trim push rod failure, perform steps 2 thru 7; otherwise, proceed to step 8

  1. TAD switch - OFF
  2. Check rudder trim indicator position
  3. TRIM DISCONNECT switch - NORM
  4. RUD TRIM circuit breaker (LF console) - CHECK, RESET IF OPEN
  5. Rudder trim - MOVE LEFT AND/OR RIGHT
  6. Rudder pedals - MOVE LEFT AND/OR RIGHT
  7. Check flight characteristics, gradually slowing aircraft to landing configuration and airspeed
  8. Fly no slower than min controllable airspeed plus 20 KIAS until on final approach
  9. Fly a power-on, straight-in approach requiring min flare and plan to touchdown at no less than previously determined min controllable airspeed
28
Q

CONTROLLED EJECTION

A

Perform as time and conditions permit

  1. Notify crewmember of decision to eject (BOTH)
  2. Altitude - 2000 FEET AGL MIN (RECOMMENDED)
  3. Airspeed - 125-180 KIAS (RECOMMENDED)
  4. Distress call - TRANSMIT
  5. Transponder - 7700
  6. Loose equipment - STOW (BOTH)
  7. Visor - DOWN (BOTH)
  8. Oxygen mask and helmet - FASTENED AND TIGHT, CHIN STRAP FASTENED (BOTH)
  9. Leg restraint garters - CHECK (BOTH)
  10. Harness - LOCKED (BOTH)
  11. SSK deployment knob - A/R (BOTH)
  12. Turn aircraft toward uninhabited area
  13. PCL - OFF
  14. Assume proper position:
    a. Head back firmly against headpad
    b. Shoulders and back against seat back
    c. Elbows close to body
    d. Legs flat on seat pad
    e. Legs extended, but not rigid
29
Q

EJECT

A

*1. EJECTION HANDLE - PULL (BOTH)

30
Q

POST EJECTION PROCEDURES

A
  1. Inspect canopy - CAREFULLY INSPECT CANOPY AND SUSPENSION LINES FOR DAMAGE AND/OR MALFUNCTIONS
  2. (I) INFLATE LPU - LOCATE TOGGLES AND PULL DOWN TO WAIST
  3. (R) RAFT release raft by pulling the SSK manual release handle -A/R
  4. (O) Options - A/R
    a. LeMoinge slots - Locate toggles on front riser. Pull down on
    toggles to turn chute into wind prior to landing (egL toggle = L turn)
    b. Visor - If descending over water, raise visor for increase visibility.
    If descending over land, leave visor down for increase face and eye
    protection
    c. Oxygen mask - If descending over water, remove ox mask from
    face and discard. If descending over land, loosen bayonet fittings
    and retain mask for increased face protection
    d. Gloves - over water, may be removed for dexterity, stow
    over land, keep on for proection
    e. Survival Seat Kit (SSK) over water, do not discard, (release both
    leg straps). over land discard only during daylight and over open
    terrain; do not pull SSK manual release handle
  5. (K) KOCH FITTINGS - LOCATE CANOPY RELEASE UPPER (KOCH) FITTINGS
  6. Preparing to land procedures (approx 200’ AGL)
    a. If over land - discard SSK
    b. Locate clear landing area and steer into wind
    c. Grab risers at retainer loops with elbows pointed forward, toggles
    at eye level, with head erect, and eyes on the horizon
    d. Ensure feet and knees are together, knees are slightly bend, balls
    of feet are lower than heels
  7. Landing/post-landing procedures - OVER LAND
    a. Perform Parachute Landing Fall (PLF) - FIVE POINST OF
    CONTACT:
    1. Balls of feet
    2. Side of calf
    3. Side of thigh
    4. Side of buttocks
    5. Shoulder blade
      b. release upper KOCH fittings after completion of PLF
  8. Landing/post-landing OVER WATER
    a. Release upper KOCH fittings as soon as feet touch the water
    and perform ADR (post-water entry)
    1. (A) Avoid the chute
    2. (D) Disentangle the chute
    3. (R) Release the SSK and retrieve survival items
31
Q

LIFT RAFT OPERATION

A
  1. When clear of parachute canopy, retrieve the life raft by locating the drop line and pulling the raft to you
  2. Position raft to board near CO2 bottle
  3. Grasp raft and forcibly push down below waist
  4. Use boarding handles, pull into raft and turn towards seated position
  5. Locate sea anchor and deploy
  6. Retrieve ruck sack
  7. Pull canopy over shoulders
  8. Use integral bailer to remove water from inside life raft as follows:
    a. Use bailer intuitively
    b. Use bailing sponge to dry floor drain into bailer
    c. when finished tie to floor with bowline knot
  9. Feed antenna of emer. transmitter through sleeve in canopy
  10. Close canopy and attach edges with the strips along the edge
  11. Pull raft hood canopy over face and attach
32
Q

RESCUE

A

if picked up by rescue helicopter with no rescue swimmer deployed, the following should be followed

  1. Stow or discard loose gear and roll out toward CO2 bottle
  2. Ensure helmet visor has been lowered and swim away from raft
  3. disconnect lower KOCH fittings after rescue strop has been lowered
use the following procedures with rescue strop
(allow strop or other equipment to GND to water before touching)
1. Grasp free end of rescue strop
2. Encircle body
3. Attach to rescue hook
4. Grab strop
5. head down thumb up
6. Cross feet clear of water

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