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Emergency Procedures

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Emergency Procedures Emergency Descent Why? Emergency Descent Uncontrollable Fire Sudden Loss of Cabin Pressurization Any other situation requiring immediate and ... – PowerPoint PPT presentation

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Title: Emergency Procedures


1
Emergency Procedures
2
Emergency Descent
  • Why?

3
Emergency Descent
  • Uncontrollable Fire
  • Sudden Loss of Cabin Pressurization
  • Any other situation requiring immediate and rapid
    loss of altitude

4
Emergency Descent
  • How?

5
Emergency Descent
  • Reduce the throttle to idle
  • Roll into a bank angle of approximately 30-45
    degrees
  • Set propeller to low pitch ( High RPM)

6
Emergency Descent
  • Extend landing gear and Flaps as recommended by
    the manufacturer
  • Do not exceed VNE, VLE, VFE, or VA if turbulent

7
Emergency Approach Landing
  • Maintain your composure
  • Fly the airplane
  • Maintain your glide speed
  • Adhere to the checklist
  • Manage resources

8
Emergency Approach Landing
  • Factors to consider
  • Wind
  • Surface conditions
  • Gear Position

9
Emergency Approach Landing
  • Size of landing area
  • Obstructions
  • Key Position

10
How to Crash
  • Very Carefully
  • Ground Speed
  • Stopping Distance
  • Deceleration Forces 9G
  • 50 mph 9.4 feet
  • 100 mph 37.6 feet

11
Best Glide Speed
  • Gear and Flaps retracted
  • Propeller to low RPM (High Pitch)
  • Pitch
  • Trim

12
Best Glide Speed
  • Checklist
  • Any deviation from the best glide speed will
    reduce the distance you can glide

13
180o Turn After Takeoff
  • Standard rate turn takes 1 minute
  • At 65 knots, radius of turn is 2100 feet.
  • Upon completion of the turn you are 4,200 feet to
    one side of the runway

14
180o Turn After Takeoff
  • An additional turn of 45o takes 15 seconds
  • If you descend at 1,000 fpm total altitude loss
    will be 1.316 feet.

15
In-Flight Fire
  • Follow the POH
  • Types

16
In-Flight Fire
  • Follow the POH
  • Types
  • Cabin, Wing, Electrical, Engine
  • Emergency Descent
  • Slip away from the fire

17
Partial Power Loss
  • Best Performance Airspeed Best Glide Speed
  • Causes

18
Partial Power Loss
  • Air
  • Carburetor Ice
  • Induction Icing
  • Fuel
  • Water
  • Contamination affecting flow

19
Partial Power Loss
  • Spark
  • Plugs fowled, wire disconnected
  • Magneto
  • Mechanical

20
Door Opening in Flight
  • Fly the airplane
  • Noise does not hurt
  • Land the airplane
  • Secure the door

21
Asymmetrical Flap Extension
  • One flap works the other does not
  • Rolling motion
  • Hazardous if in the traffic pattern at low
    altitude

22
Asymmetrical Flap Extension
  • Return the flaps to the up or previous position
  • Go around if necessary

23
Emergencies
  • ELT
  • Diversion
  • High Oil Temperature
  • Exhaust Leak

24
Emergencies
  • Engine Failure on Takeoff
  • Severe Turbulence
  • Spatial Disorientation
  • Survival Equipment

25
The maximum cumulative time that an emergency
locator transmitter may be operated before the
rechargeable battery must be recharged is A. 30
minutes. B. 45 minutes. C. 60 minutes.
26
The maximum cumulative time that an emergency
locator transmitter may be operated before the
rechargeable battery must be recharged is A. 30
minutes. B. 45 minutes. C. 60 minutes.
27
In small airplanes, normal recovery from spins
may become difficult if the A. CG is too far
rearward, and rotation is around the CG. B.
spin is entered before the stall is fully
developed. C. CG is too far rearward, and
rotation is around the longitudinal axis.
28
In small airplanes, normal recovery from spins
may become difficult if the A. CG is too far
rearward, and rotation is around the CG. B.
spin is entered before the stall is fully
developed. C. CG is too far rearward, and
rotation is around the longitudinal axis.
29
When diverting to an alternate airport because of
an emergency, pilots should
30
A. apply rule-of-thumb computations, estimates,
and other appropriate shortcuts to divert to the
new course as soon as possible. B. rely upon
radio as the primary method of navigation. C.
climb to a higher altitude because it will be
easier to identify checkpoints.
31
A. apply rule-of-thumb computations, estimates,
and other appropriate shortcuts to divert to the
new course as soon as possible. B. rely upon
radio as the primary method of navigation. C.
climb to a higher altitude because it will be
easier to identify checkpoints.
32
An abnormally high engine oil temperature
indication may be caused by A. a defective
bearing. B. the oil level being too low. C.
operating with an excessively rich mixture.
33
An abnormally high engine oil temperature
indication may be caused by A. a defective
bearing. B. the oil level being too low. C.
operating with an excessively rich mixture.
34
Frequent inspections should be made of aircraft
exhaust manifold-type heating systems to minimize
the possibility of
35
A. a cold-running engine due to the heat
withdrawn by the heater. B. exhaust gases
leaking into the cockpit. C. a power loss due
to back pressure in the exhaust system.
36
A. a cold-running engine due to the heat
withdrawn by the heater. B. exhaust gases
leaking into the cockpit. C. a power loss due
to back pressure in the exhaust system.
37
A pilot's most immediate and vital concern in
the event of complete engine failure after
becoming airborne on takeoff is
38
A. maintaining a safe airspeed. B. landing
directly into the wind. C. turning back to the
takeoff field.
39
A. maintaining a safe airspeed. B. landing
directly into the wind. C. turning back to the
takeoff field.
40
If severe turbulence is encountered during
flight, the pilot should reduce the airspeed
to A. minimum control speed. B. maximum
structural cruising speed. C.
design-maneuvering speed.
41
If severe turbulence is encountered during
flight, the pilot should reduce the airspeed
to A. minimum control speed. B. maximum
structural cruising speed. C.
design-maneuvering speed.
42
To best overcome the effects of spatial
disorientation, a pilot should A. increase the
breathing rate. B. rely on body sensations. C.
rely on aircraft instrument indications.
43
To best overcome the effects of spatial
disorientation, a pilot should A. increase the
breathing rate. B. rely on body sensations. C.
rely on aircraft instrument indications.
44
Bonanza F33A
  • Emergency Airspeeds (3400 lbs)
  • Emergency Descent
  • Maximum Glide Range
  • Emergency Landing Approach

45
Bonanza F33A
  • Emergency Airspeeds (3400 lbs)
  • Emergency Descent 154
  • Maximum Glide Range 105
  • Emergency Landing Approach
  • 83

46
Emergency Descent
  • Power
  • Propeller
  • Landing Gear
  • Airspeed

47
Emergency Descent
  • Power Idle
  • Propeller High RPM
  • Landing Gear Down
  • Airspeed Establish 154 KTS

48
Engine Failure-Take Off Ground Roll
  • Throttle
  • Braking
  • Fuel Selector
  • Battery and Alternator Switches

49
Engine Failure-Take Off Ground Roll
  • Throttle Closed
  • Braking Maximum
  • Fuel Selector Off
  • Battery and Off Alternator Switches

50
Engine Failure - In Flight
  • Fuel Selector Valve
  • Auxiliary Fuel Pump
  • Mixture
  • Magnetos

51
Engine Failure - In Flight
  • Fuel Selector Valve Select Other Tank
  • Auxiliary Fuel Pump ON
  • Mixture Full Rich, then Lean as Required
  • Magnetos Check Left, Right, then Both ON

52
Maximum Glide Configuration
  • Landing Gear
  • Flaps
  • Cowl Flaps
  • Propeller
  • Airspeed

53
Maximum Glide Configuration
  • Landing Gear UP
  • Flaps UP
  • Cowl Flaps Closed
  • Propeller Pull for Low RPM
  • Airspeed 105 KTS

54
Landing Without Power
  • Airspeed
  • Fuel Selector Valve
  • Mixture
  • Magneto/Start Switch

55
Landing Without Power
  • Flaps
  • Landing Gear
  • Battery and Alternator Switches

56
Landing Without Power
  • Airspeed 78 to 83 KTS
  • Fuel Selector Valve OFF
  • Mixture Idle Cut-off
  • Magneto/Start Switch Off

57
Landing Without Power
  • Flaps As Required
  • Landing Gear Down or UP(terrain)
  • Battery and OFF Alternator Switches

58
Landing Gear Retracted w/Power
  • Throttle
  • Mixture
  • Battery, Alternator, and Magneto/Start Switches

59
Landing Gear Retracted w/Power
  • Keep wings level during touchdown
  • Get Clear of Airplane as soon as possible after
    it stops

60
Landing Gear Retracted w/Power
  • Throttle Closed
  • Mixture Idle Cut- off
  • Battery, Alternator, OFF and Magneto/
    Start Switches

61
Landing Gear Retracted w/Power
  • Keep wings level during touchdown
  • Get Clear of Airplane as soon as possible after
    it stops

62
Propeller Overspeed
  • Throttle
  • Airspeed
  • Oil Pressure
  • Land

63
Propeller Overspeed
  • Throttle Retard to Red Line
  • Airspeed Reduce
  • Oil Pressure Check
  • Land Select Nearest Suitable Site and follow
    Landing Emergency procedures

64
Landing Gear Manual Extension
  • LDG GR Motor Circuit Breaker
  • Landing Gear Switch Handle
  • Handcrank Handle Cover
  • Handcrank

65
Landing Gear Manual Extension
  • If electrical system is inoperative, check
    landing gear position lights and warning horn
  • Handcrank

66
Landing Gear Manual Extension
  • LDG GR Motor Circuit Breaker Off (out)
  • Landing Gear Switch Handle Down
  • Handcrank Handle Cover Remove
  • Handcrank Engage and turn counterclockwise as Far
    as Possible (50 turns)
  • If electrical system is operative, check landing
    gear position lights and warning horn
  • Handcrank Disengage

67
Spins
68
Spins
  • Prohibited
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