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SR 22 Emergency Procedures > Tom McGovern > Flashcards

Tom McGovern Flashcards

SR22 EPs

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1
Q

Airspeeds for Emergency Operations

A

Maneuvering Speed:
3400 lb …………………………………………………………………..133 KIAS

Best Glide:
3400 lb …………………………………………………………………….88 KIAS
2900 lb …………………………………………………………………….87 KIAS

Emergency Landing (Engine-out):
Flaps Up…………………………………………………………………..90 KIAS
Flaps 50%………………………………………………………………..85 KIAS
Flaps 100%………………………………………………………………80 KIAS

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2
Q

Engine Fire During Start

A
  1. Mixture ……………………………………………………………………CUTOFF
  2. Fuel Pump …………………………………………………………………….OFF
  3. Fuel Selector………………………………………………………………….OFF
  4. Power Lever …………………………………………………………FORWARD
  5. Starter …………………………………………………………………….. CRANK
  6. If flames persist, perform Emergency Engine Shutdown on
    Ground and Emergency Ground Egress checklists
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3
Q

Emergency Engine Shutdown On Ground

A
  1. Power Lever …………………………………………………………………. IDLE
  2. Fuel Pump (if used) ………………………………………………………..OFF
  3. Mixture ……………………………………………………………………CUTOFF
  4. Fuel Selector………………………………………………………………….OFF
  5. Ignition Switch………………………………………………………………..OFF
  6. Bat-Alt Master Switches…………………………………………………..OFF
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4
Q

Engine Failure On Takeoff (Low Altitude)

A
  1. Best Glide or Landing Speed (as appropriate) ……….. ESTABLISH
  2. Mixture ……………………………………………………………………CUTOFF
  3. Fuel Selector………………………………………………………………….OFF
  4. Ignition Switch………………………………………………………………..OFF
  5. Flaps ……………………………………………………………. AS REQUIRED
    If time permits:
  6. Power Lever …………………………………………………………………. IDLE
  7. Fuel Pump …………………………………………………………………….OFF
  8. Bat-Alt Master Switches…………………………………………………..OFF
  9. Seat Belts …………………………………………….. ENSURE SECURED
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5
Q

Engine Failure In Flight

A
  1. Best Glide Speed…………………………………………….. ESTABLISH
  2. Mixture …………………………………………………………AS REQUIRED
  3. Fuel Selector………………………………………………SWITCH TANKS
  4. Fuel Pump …………………………………………………………….. BOOST
  5. Alternate Induction Air …………………………………………………..ON
  6. Ignition Switch……………………………………………..CHECK, BOTH
  7. If engine does not start, proceed to Engine Airstart or Forced Landing checklist, as required.
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6
Q

Engine Airstart

A
  1. Bat Master Switches ……………………………………………………….ON
  2. Power Lever …………………………………………………………½” OPEN
  3. Mixture ………………………………………………………RICH, AS REQ’D
  4. Fuel Selector………………………………………………SWITCH TANKS
  5. Ignition Switch …………………………………………………………..BOTH
  6. Fuel Pump………………………………………………………………..BOOST
  7. Alternate Induction Air……………………………………………………..ON
  8. Alt Master Switches ……………………………………………………….OFF
  9. Starter (Propeller not Windmilling) ………………………..ENGAGE
  10. Power Lever ……………………………………………..slowly INCREASE
  11. Alt Master Switches ………………………………………………………… ON
  12. If engine will not start, perform Forced Landing checklist.
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7
Q

Rough Running Engine or Partial Power Loss

A
  1. Fuel Pump……………………………………………………………….. BOOST
  2. Fuel Selector …………………………………………….SWITCH TANKS
  3. Mixture ……………….CHECK appropriate for flight conditions
  4. Power Lever ……………………………………………………………SWEEP
  5. Alternate Induction Air…………………………………………………..ON
  6. Ignition Switch ………………………………………….BOTH, L, then R
  7. Land as soon as practical.
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8
Q

Low Oil Pressure

A

• WARNING •
Prolonged use of high power settings after loss of oil pressure will lead to engine mechanical damage and total engine failure, which could be catastrophic.

• Note •
Full power should only be used following a loss of oil pressure when operating close to the ground and only for the time necessary to climb to an altitude permitting a safe landing or analysis of the low oil pressure indication to confirm oil pressure has actually been lost.

If low oil pressure is accompanied by normal oil temperature, it is possible that the oil pressure sensor, gage, or relief valve is malfunctioning. In any case, land as soon as practical and determine cause.

  1. Power Lever ………………………………….MINIMUM REQUIRED
  2. Land as soon as possible.
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9
Q

Propeller Governor Failure

A

Propeller RPM will not increase:

  1. Oil Pressure …………………………………………………………….. CHECK
  2. Land as soon as practical.

Propeller overspeeds or will not decrease:

  1. Power Lever ……………………………ADJUST (to keep RPM in limits)
  2. Airspeed…………………………………………………REDUCE to 90 KIAS
  3. Land as soon as practical.
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10
Q

Smoke and Fume Elimination

A
  1. Heater …………………………………………………………………………..OFF
  2. Air Vents………………………………………………..OPEN, FULL COLD
  3. Prepare to land as soon as possible.
    If airflow is not sufficient to clear smoke or fumes from cabin:
  4. Cabin Doors …………………………………………….PARTIALLY OPEN
    Airspeed may need to be reduced to partially open door in flight.
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11
Q

Engine Fire In Flight

A
  1. Mixture ………………………………………………………………….. CUTOFF
  2. Fuel Pump……………………………………………………………………..OFF
  3. Fuel Selector………………………………………………………………….OFF
  4. Airflow Selector ………………………………………………………………OFF
  5. Power Lever …………………………………………………………………IDLE
  6. Ignition Switch ………………………………………………………………..OFF
  7. Cabin Doors ……………………………………………..PARTIALLY OPEN
    Airspeed may need to be reduced to partially open door in flight.
  8. Land as soon as possible.
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12
Q

Wing Fire In Flight

A
  1. Pitot Heat Switch …………………………………………………………..OFF
  2. Navigation Light Switch………………………………………………..OFF
  3. Strobe Light Switch………………………………………………………OFF
  4. If possible, side slip to keep flames away from fuel tank and cabin.
    • Note •
    Putting the airplane into a dive may blow out the fire. Do notexceed VNE during the dive.
  5. Land as soon as possible
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13
Q

Cabin Fire In Flight

A

• WARNING •
If the airplane is in IMC conditions, turn ALT 1, ALT 2, and BAT 1 switches OFF. Power from battery 2 will keep the Primary Flight Display operational for approximately 30 minutes.
1. Bat-Alt Master Switches……………………………….OFF, AS REQ’D
• Note •
With Bat-Alt Master Switches OFF, engine will continue to run. However, no electrical power will be available.
2. Heater …………………………………………………………………………..OFF
3. Air Vents………………………………………………………………… CLOSED
4. Fire Extinguisher……………………………………………………ACTIVATE
• WARNING •
Halon gas used in the fire extinguisher can be toxic, especially in a closed area. After extinguishing fire, ventilate cabin by opening air vents and unlatching door (if required).

If airflow is not sufficient to clear smoke or fumes from cabin:
5. Cabin Doors ……………………………………………..PARTIALLY OPEN
Airspeed may need to be reduced to partially open door in flight.

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14
Q

Cabin Fire In Flight ( Part 2)

A
  1. When fire extinguished, Air Vents …….OPEN, FULL COLD
  2. Avionics Power Switch ………………………………………………..OFF
  3. All other switches ………………………………………………………..OFF
  4. Land as soon as possible.
    If setting master switches off eliminated source of fire or fumes and airplane is in night, weather, or IFR conditions:
    • WARNING •
    If airplane is in day VFR conditions and turning off the master switches eliminated the fire situation, leave the master switches OFF. Do not attempt to isolate the source of the fire by checking each individual electrical component.
  5. Bat-Alt Master Switches………………………………………………..ON
  6. Avionics Power Switch ………………………………………………….ON
  7. Activate required systems one at a time. Pause several seconds between activating each system to isolate malfunctioning system. Continue flight to earliest possible landing with malfunctioning system off. Activate only the minimum amount of equipment necessary to complete a safe landing.
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15
Q

Emergency Descent

A
  1. Power Lever ………………………………………………………………….IDLE
  2. Mixture …………………………………………………………AS REQUIRED
    • Caution •
    If significant turbulence is expected do not descend at
    indicated airspeeds greater than VNO (178 KIAS)
  3. Airspeed……………………………………………………….VNE (201 KIAS)
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16
Q

Inadvertent Spiral Dive During IMC Flight

A
  1. Power Lever ………………………………………………………………….IDLE
  2. Stop the spiral dive by using coordinated aileron and rudder control while referring to the attitude indicator and turn coordinator to level the wings.
  3. Cautiously apply elevator back pressure to bring airplane to level flight attitude.
  4. Trim for level flight.
  5. Set power as required.
  6. Use autopilot if functional otherwise keep hands off control yoke, use rudder to hold constant heading.
  7. Exit IMC conditions as soon as possible.
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17
Q

CAPS Deployment

A
  1. Airspeed……………………………………………MINIMUM POSSIBLE
    Maximum demonstrated deployment speed is 133 KIAS.
  2. Mixture (If time and altitude permit) …………………….CUTOFF
  3. Activation Handle Cover………………………………………REMOVE
  4. Activation Handle (Both Hands) ..PULL STRAIGHT DOWN
    Pull the activation T-handle from its holder. Clasp both hands around the handle and pull straight down in a strong, steady, and continuous motion. Maintain maximum pull force until the rocket activates. Pull forces up to, or exceeding, 45 pounds may be required. Bending of the handle-housing mount is to be expected.

• WARNING •
Jerking or rapidly pulling the activation T-handle will greatly
increase the pull forces required to activate the rocket. Use a firm and steady pulling motion – a “chin-up” type pull
enhances successful activation

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18
Q

CAPS Post Deployment

A
  1. Mixture ………………………………………………………CHECK, CUTOFF
  2. Fuel Selector ………………………………………………………………….OFF
  3. Bat-Alt Master Switches………………………………………………….OFF
  4. Ignition Switch ………………………………………………………………..OFF
  5. Fuel Pump……………………………………………………………………..OFF
  6. ELT………………………………………………………………………………..ON
    11.Seat Belts and Harnesses ………………………………………TIGHTEN
    All occupants must have seat belts and shoulder harness securely fastened.
    12.Loose Items ……………………………………………………………SECURE
    If time permits, all loose items should be secured to prevent injury from flying objects in the cabin at touchdown.
    13.Assume emergency landing body position.
    The emergency landing body position is assumed by placing both hands on the lap, clasping one wrist with the opposite hand, and holding the upper torso erect and against the seat backs.
    14.After the airplane comes to a complete stop, evacuate quickly and move upwind.
19
Q

Emergency Landing Without Engine Power

A
  1. Best Glide Speed ………………………………………………..ESTABLISH
  2. Radio……………………………………..Transmit (121.5 MHz) MAYDAY
  3. Transponder …………………………………………………SQUAWK 7700
  4. If off airport, ELT …………………………………………………..ACTIVATE
  5. Power Lever ………………………………………………………………….IDLE
  6. Mixture ………………………………………………………………….. CUTOFF
  7. Fuel Selector………………………………………………………………….OFF
  8. Ignition Switch ………………………………………………………………..OFF
  9. Fuel Pump……………………………………………………………………..OFF
  10. Flaps (when landing is assured) ………………………………….100%
  11. Master Switches……………………………………………………………..OFF
  12. Seat Belt(s) …………………………………………………………. SECURED
20
Q

Ditching

A
  1. Radio …………………………………..Transmit (121.5 MHz) MAYDAY
  2. Transponder …………………………………………………..SQUAWK 7700
  3. CAPS………………………………………………………………….. ACTIVATE
    If available, life preservers should be donned and life raft shouldbe prepared for immediate evacuation upon touchdown.

Consider unlatching a door prior to assuming the emergency
landing body position in order to provide a ready escape path.

  1. Airplane……………………………………………………………….EVACUATE
    It may be necessary to allow some cabin flooding to equalize
    pressure on the doors. If the doors cannot be opened, break out the windows with the egress hammer and crawl through the opening.
  2. Flotation Devices …….INFLATE WHEN CLEAR OF AIRPLANE
21
Q

Landing Without Elevator Control

A
  1. Flaps ……………………………………………………………………..SET 50%
  2. Trim ………………………………………………………………….SET 80 KIAS
  3. Power ………………………….AS REQUIRED FOR GLIDE ANGLE
22
Q

Power Lever Linkage Failure

A

If the power lever is stuck at or near the full power position, proceed to a suitable airfield. Fly a forced landing pattern. With landing assured, shut down engine by moving mixture control full aft to CUTOFF. If power is needed again, return mixture control to full RICH and regain safe pattern parameters or go-around. If airspeed cannot be controlled, shut engine down and perform the Forced Landing
checklist. After landing, bring the airplane to a stop and complete the Emergency Engine Shutdown on Ground checklist.

If the power lever is stuck at or near the idle position and straight and level flight cannot be maintained, establish glide to a suitable landing surface. Fly a forced landing pattern.

  1. Power Lever Movement……………………………………………VERIFY
  2. Power ………………………………………………………………..SET if able
  3. Flaps ……………………………………………………………..SET if needed
  4. Mixture ………………………….AS REQUIRED (full rich to cut-off)
  5. Land as soon as possible.
23
Q

Brake Failure During Taxi

A
  1. Engine Power………………………………………………… AS REQUIRED
    • To stop airplane - REDUCE
    • If necessary for steering – INCREASE
  2. Directional Control ……………………MAINTAIN WITH RUDDER
  3. Brake Pedal(s) …………………………………………………………….PUMP
    If directional control can not be maintained:
  4. Mixture ……………………………………………………………………CUTOFF
24
Q

Aborted Takeoff

A
  1. Power Lever ………………………………………………………………….IDLE
  2. Brakes…………………………………………………………..AS REQUIRED

• Caution •
For maximum brake effectiveness, retract flaps, hold control
yoke full back, and bring the airplane to a stop by smooth,
even application of the brakes to avoid loss of control and/or a blown tire.

25
Q

Inadvertent Icing Encounter

A
  1. Pitot Heat ………………………………………………………………………. ON
  2. Exit icing conditions. Turn back or change altitude.
  3. Cabin Heat ………………………………………………………..MAXIMUM
  4. Windshield Defrost …………………………………………FULL OPEN
  5. Alternate Induction Air…………………………………………………..ON
26
Q

Inadvertent IMC Encounter

A
  1. Airplane Control ………..Establish Straight and Level Flight
  2. Autopilot ……………..Engage to hold Heading and Altitude
  3. Heading…………………………………….Reset to initiate 180° turn
27
Q

Door Open In Flight

A

The doors on the SR22 will remain 1-3 inches open in flight if not latched. If this is discovered on takeoff roll, abort takeoff if practical.

If already airborne:

  1. Airspeed…………………………………..REDUCE TO 80 – 90 KIAS
  2. Land as soon as practical.
28
Q

Landing With Failed Brakes

A

One brake inoperative

  1. Land on the side of runway corresponding to the inoperative brake.
  2. Maintain directional control using rudder and working brake.

Both brakes inoperative
1. Divert to the longest, widest runway with the most direct headwind.
2. Land on downwind side of the runway.
3. Use the rudder for obstacle avoidance.
• Note •
Rudder effectiveness will decrease with decreasing airspeed.

  1. Perform Emergency Engine Shutdown on Ground checklist.
29
Q

Landing With Flat Tire

A

Main Gear

  1. Land on the side of the runway corresponding to the good tire.
  2. Maintain directional control with the brakes and rudder.
  3. Do not taxi. Stop the airplane and perform a normal engine shutdown.

Nose Gear

  1. Land in the center of the runway.
  2. Hold the nosewheel off the ground as long as possible.
  3. Do not taxi. Stop the airplane and perform a normal engine shutdown.
30
Q

Alternator Failure (cause) – ALT caution light

A

The most likely the cause of the alternator failure is a wiring fault, a malfunctioning alternator, or a malfunctioning control unit. Usually, electrical power
malfunctions are accompanied by an excessive rate of charge or a discharge rate shown on the ammeter.

31
Q

Alternator (CAUTION)

A

Alternators in this airplane are self-exciting. These alternators require battery power for alternator starting; however, once started, the alternators will provide self-generated field power to continue operation in case of a battery failure. To assure alternator restart power is available if the alternators fail, the batteries should not be turned off during flight.

32
Q

Alternator (reduce electrical load)

A

If it is necessary to reduce electrical loads due to an alternator malfunction, switch off electrical components and/or systems that are not essential for the current flight conditions rather than pulling circuit breakers. Load shedding in this manner will prevent accidental circuit breaker disconnection and loss of power to flight-critical systems.

See Figure Electrical Power Distribution, for details on electrical busses and what components/systems they power.

33
Q

ALT 1 Light Steady

A
  1. ALT 1 Master Switch …………………………………………………….OFF
  2. Alternator 1 Circuit Breaker………………..CHECK and RESET
  3. ALT 1 Master Switch …………………………………………………….ON
    If alternator does not reset:
  4. Switch off unnecessary equipment on Main Bus 1, Main Bus 2, and the Non-Essential Buses to reduce loads. Monitor voltage.
  5. ALT 1 Master Switch ……………………………………………………OFF
  6. Land as soon as practical.
34
Q

ALT 1 Light Flashing
The most likely cause is a severely discharged battery along with heavy equipment loads. In this
event, reduce loads on Main and Non-Essential buses and monitor amperage until charging rate is within normal limits. Then loads can be added as required.

A
  1. Ammeter Switch……………………………………………………………BATT
  2. If charging rate is greater than 30 amps, reduce load on Main Bus 1, Main Bus 2, and Non-Essential buses.
  3. Monitor ammeter until battery charge rate is less than 15 amps.
  4. When battery charge rate is within limits, add loads as necessary for flight conditions.
35
Q

ALT 2 Light Steady
Except during low RPM operations, steady illumination indicates a failure of ALT 2. If alternator cannot be brought back, Essential bus loads will be powered from ALT 1, BAT 1, and BAT 2.

• Note •
ALT 2 light will illuminate steady and ALT 2 will not come on line until 1700 - 2200 RPM.

A
  1. ALT 2 Master Switch …………………………………………………..OFF
  2. Alternator 2 Circuit Breaker ……………CHECK and RESET
  3. ALT 2 Master Switch ……………………………………………………ON

If alternator does not reset:

  1. Switch off unnecessary equipment on Main Bus 1, Main Bus 2,and Non-Essential Buses to reduce loads.
  2. ALT 2 Master Switch ………………………………………………….OFF
  3. Land as soon as practical.
36
Q

LOW VOLTS Warning Light Illuminated

Illumination of the LOW VOLTS light indicates that the voltage measured at the Essential Bus is 24.5 volts or less.

Typically, this indicates that the airplane is operating on battery power only and both alternators have failed or are off.

A
  1. Land as soon as practical.
37
Q

Communications Failure

A
  1. Switches, Controls …………………………………………………..CHECK
  2. Frequency …………………………………………………………….CHANGE
  3. Circuit Breakers………………………………………………………..CHECK
  4. Headset………………………………………………………………… CHANGE
  5. Hand Held Microphone ……………………………………..CONNECT
38
Q

If erroneous readings of the static source instruments (airspeed,altimeter and vertical speed) are suspected - Static Source Blocked

A

The alternate static source valve, on side of console near pilot’s right ankle, should be opened to
supply static pressure from the cabin to these instruments.

39
Q

Static Source Blocked (notes)

A

If selecting the alternate static source does not work, in an emergency, cabin pressure can be supplied to the static pressure instruments by breaking the glass in the face of the vertical speed indicator.

When static pressure is supplied through the vertical speed indicator, the vertical speed UPDOWN indications will be reversed (i.e., the needle will indicate UP for descent and DOWN for climb).

With the alternate static source on, adjust indicated airspeed slightly during climb or approach according to the Airspeed Calibration (Alternate Static Source) table in Section 5 as appropriate for vent/ heater configuration.

40
Q

Static Source Blocked

A
  1. Pitot Heat ………………………………………………………………………..ON
  2. Alternate Static Source ……………………………………………..OPEN
41
Q

Pitot Tube Blocked

A

If only the airspeed indicator is providing erroneous information, and in icing conditions, the most probable cause is pitot ice.

If setting Pitot Heat ON does not correct the problem, descend to warmer air.

If an approach must be made with a blocked Pitot tube, use known pitch and power settings and the GPS groundspeed indicator, taking surface winds into account

42
Q

Electric Trim/Autopilot Failure

A

Any failure or malfunction of the electric trim or autopilot can be overridden by use of the control yoke.

If runaway trim is the problem, deenergize the circuit by pulling the circuit breaker (PITCH TRIM, ROLL TRIM, or AUTOPILOT) and land as soon as conditions permit.

43
Q

Electric Trim/Autopilot Failure (procedures)

A
  1. Airplane Control …………………………..MAINTAIN MANUALLY
  2. Autopilot (if engaged) …………………………………….Disengage
    If Problem Is Not Corrected:
  3. Circuit Breakers…………………………………..PULL AS Required
    • PITCH TRIM
    • ROLL TRIM
    • AUTOPILOT
  4. Power Lever ………………………………………………AS REQUIRED
  5. Control Yoke…………………….MANUALLY HOLD PRESSURE
  6. Land as soon as practical.
44
Q

Airspeeds for Normal Operation

Takeoff Rotation
Enroute Climb
Landing Approach
Go-Around

A

Takeoff Rotation:
• Normal, Flaps 50%………………………………………………..70 KIAS
• Obstacle Clearance, Flaps 50%………………………………78 KIAS
Enroute Climb, Flaps Up:
• Normal ……………………………………………………….. 110-120 KIAS
• Best Rate of Climb, SL …………………………………………101 KIAS
• Best Rate of Climb, 10,000……………………………………..95 KIAS
• Best Angle of Climb, SL………………………………………….78 KIAS
• Best Angle of Climb, 10,000 ……………………………………82 KIAS
Landing Approach:
• Normal Approach, Flaps Up …………………………….90-95 KIAS
• Normal Approach, Flaps 50% …………………………..85-90 KIAS
• Normal Approach, Flaps 100% ………………………….80-85 KIAS
• Short Field, Flaps 100% (VREF) ………………………………77 KIAS
Go-Around, Flaps 50%:
• Full Power…………………………………………………………….80 KIAS
Maximum Recommended Turbulent Air Penetration:
• 3400 lb……………………………………………………………….133 KIAS
• 2900 lb……………………………………………………………….123 KIAS
Maximum Demonstrated Crosswind Velocity:
• Takeoff or Landing ………………………………………………..20 Knots

SR 22 Emergency Procedures (1 decks)

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