Multi Engine Procedures & Normal Operations

Question 1

What does I.M.S.A.F.E. Stand for?

Answer 1

• Illness
• Medication
• Stress
• Alcohol
• Fatigue
• Emotions

Question 2

What does CRM stand for?

Answer 2

Crew Resource Management: the effective use of all available resources for flight crew personal to assure a safe and efficient operation, reducing error, avoiding stress, and increasing efficiency.

Question 3

What does SRM stand for?

Answer 3

Single-Pilot Crew Resource Management: the art of managing all onboard and outside resources available to a pilot before and during flight to help ensure a safe and successful outcome.

Question 4

What is an M.E.L.?

Answer 4

Minimum Equipment List: inoperable equipment operations, specific to each aircraft, must have an LOA (Letter of Authorization)

Question 5

If you have an M.E.L. And L.O.A., what will the FAA issue for the aircraft?

Answer 5

Supplemental Type Certificate

Question 6

How much fuel does the gas collator in the right engine consume if installed?

Answer 6

5 GPH

Question 7

What issue may occur if the electric fuel pump is left on after start?

Answer 7

Flooding of the engine

Question 8

When should takeoffs not be attempted?

Answer 8

When weather is below landing minimums

Question 9

What should be checked during takeoff roll?

Answer 9

• RPM
• Manifold Pressure
• Oil Temperatures
• Oil Pressure
• Fuel Flow Indicator
• Air Speed Indicator

Question 10

When should the first power reduction be made?

Answer 10

When at a safe maneuvering speed and altitude. After gear and flaps retraction, accelerate to Vy

Question 11

Go around procedure

Answer 11

• Mixture, props, and throttle full forward
• Pitch up to positive rate of climb
• Flaps 25°
• Gear up
• Flaps 0° after obstruction clearance
  (Full power, flaps to takeoff, retract gear)

Question 12

How long does the gear take to retract?

Answer 12

6 seconds

Question 13

Vso

Answer 13

69 (Stall speed in landing configuration)

Question 14

Vs1

Answer 14

76 (Stall speed in specific configuration)

Question 15

Vmc

Answer 15

80 (Minimum control speed)

Question 16

Vsse

Answer 16

84 (Safe single-engine speed)

Question 17

Vx

Answer 17

90 (Best angle of climb speed)

Question 18

Vy

Answer 18

105 (Best rate of climb speed)

Question 19

Vxse

Answer 19

93 (Best single-engine angle of climb speed)

Question 20

Vyse

Answer 20

105 (Best single-engine rate of climb speed)

Question 21

VLo

Answer 21

125 (Maximum landing gear up operating speed)

150 (Maximum Landing gear down operating speed)

Question 22

Vle

Answer 22

150 (Maximum landing gear extended speed)

Question 23

Vfe

Answer 23

10° - 160
25° - 140
40° - 125

Question 24

Va

Answer 24

146 (at max weight of 4,200 lbs)

133 (at 2743 lbs)

Question 25

Vno

Answer 25

190 (Maximum structural cruise speed)

Question 26

Vne

Answer 26

217 (Never exceed speed)

Question 27

V

Answer 27

150 (storm window open speed)

Question 28

Vr

Answer 28

85 (Rotation speed)

Question 29

Vcc

Answer 29

120 (Cruise climb speed)

Question 30

Outboard Stall Warning

Answer 30

When flaps are at 0° and 10°

Question 31

Inboard Stall Warning

Answer 31

When flaps are at 25° and 40°

Question 32

How many static systems does the aircraft have?

Answer 32

One static system comprised of two static ports

Question 33

How is the Hartzell prop operated?

Answer 33

By oil and nitrogen

Question 34

How does the prop governor work?

Answer 34

Governor supplies oil to the propellor to maintain constant speed More oil=more rpm Less oil=less rpm

Question 35

How long does it take to feather the prop?

Answer 35

6 seconds

Question 36

When does the anti feathering lock engage?

Answer 36

Below 800rpm

Question 37

How does the gear avoid retracting on the ground?

Answer 37

A squat switch that is located on the left gear

Question 38

When will the landing gear pressure system shut off?

Answer 38

1,800 psi

Question 39

Nose gear is steerable up to what degree?

Answer 39

42° ( 21° left and 21° right)

Question 40

How many quarts of oil are needed?

Answer 40

6-8 quarts per engine

Question 41

What type of fuel can be used?

Answer 41

100LL and 100

Question 42

How many fuel tanks and how much do they hold?

Answer 42

4 fuel tanks that each hold 24.5 gallons (98 total gallons)

Question 43

How much usable fuel?

Answer 43

93 gallons (5 gallons unusable)

Question 44

What kind of flaps are used?

Answer 44

Spring loaded and single slotted

Question 45

What does it mean by the ailerons are differential?

Answer 45

They will go higher up than down

Question 46

The landing gear is….

Answer 46

Hydraulically operated electrically powered

Question 47

How does the emergency gear extension work?

Answer 47

Gravity powered but wont lock

Question 48

When will the gear horn go off?

Answer 48

When power is back below 14” without gear down

Question 49

How is the manifold pressure indicated?

Answer 49

Through a connection on cylinder 3

Question 50

What should the manifold pressure equal before start?

Answer 50

Pressure altitude

Question 51

What is considered a light twin?

Answer 51

Less than 6,000 pounds

Question 52

Max weight

Answer 52

4,200 lbs

Question 53

Max landing weight

Answer 53

4,000 lbs

Question 54

Fuel burn rate

Answer 54

30 gal per hour

Question 55

Explain the alternator(s)

Answer 55

Two alternators that each produce 60 amps and 14 volts

Question 56

Explain the batteries

Answer 56

35 amps and 12 volts

Question 57

Explain the break system

Answer 57

Hydraulically powered but completely separate from the landing gear system

Question 58

What kind of fuel system is used?

Answer 58

Fuel injected using fuel servos

Question 59

Explain the engine

Answer 59

``` L: Lycoming I: Injected Engine H: Horizontally Opposed A: Air cooled N: Normally aspirated D: Direct Driven 360: 360 cubic inch 200:Horse power at 2700 rpm ```

Question 60

Max CHT (cylinder head temperature)

Answer 60

475°

Question 61

Max oil temperature

Answer 61

245°

Question 62

Tire pressure

Answer 62

Front: 31psi Mains: 50-53psi

Question 63

Max crosswind

Answer 63

15mph (12kts)

Question 64

Max baggage

Answer 64

100 lbs

Question 65

Gyro suction limitations

Answer 65

4.5 - 5.2” hg

Question 66

Absolute ceiling

Answer 66

19,400’

Question 67

Service ceiling

Answer 67

17,900

Question 68

SE absolute ceiling

Answer 68

5,000’

Question 69

SE service ceiling

Answer 69

3,650’

Question 70

Definition of absolute ceiling

Answer 70

The altitude at which the maximum rate of climb goes to zero

Question 71

Definition of service ceiling

Answer 71

The altitude at which the maximum rate of climb is 100 ft/min