In 101

Front 1

Of the two 5 inch displays in the EFIS, which one is capable of showing the both displays information (composite)

Back 1

BOTH of them are capable of being in Composite mode

Front 2

The EFIS system consists of what components?

Back 2

Two 5 inch (I have a good reference of the combined length of these displays) displays and a Control panel

Front 3

Are the EFIS Systems in the front cockpit intergrated with the rear cockpit?

Back 3

Yes

Front 4

What is the information that the two primary displays of the EFIS system provide?

Back 4

Attitude and Heading

Front 5

What are the 4 EADI display modes?

Back 5

Enroute, Approach, Composite, and Unusual Attitude

Front 6

What are the three EHSI display modes?

Back 6

Enroute, Approach, and Composite

Front 7

The EHSI enroute and approach modes each offer _ different display formats?

Back 7

5

Front 8

How many separate display modes are available between the total EFIS system?

Back 8

15

Front 9

General Purpose of EFIS system (and or any cockpit display) (Generic answer)

Back 9

Optimize in-flight information.

Front 10

Displays must be managed correctly to optimize in flight information as well as too. . .

Back 10

minimize unecessary and distracting information

Front 11

EADI is primary inflight source providing infromation about ____ and ____

Back 11

Pitch and Roll

Front 12

In an EADI failure, what items will be taken off of the screen?

Back 12

Blue Sky, horizon line, sky pointer, and roll/pitch scale

Front 13

In an EADI failure, what items will show up on the screen?

Back 13

Red Box with Red Letters saying "ALTITUDE FAIL". Red elongated X at bottom.

Front 14

EHSI provides ______ information?

Back 14

Heading

Front 15

If heading becomes unavailable or unreliable what indication is seen by you the pilot?

Back 15

Red boxed HDG in the top right of center. (This happens on the "appropriate" EFIS display?)

Front 16

General Guidelines for EFIS (PROCEED TO NEXT SLIDE)

Front 17

Match the display with the current ______

Back 17

Task. Display enroute when you're enroute, approach when you're approaching.

Front 18

Display only what you _____ and can acurately _____.

Back 18

Need; interpret

Front 19

Avoid displaying any information that……

Back 19

you cannot easily discern or that distracts you from flying the aircraft

Front 20

What is the process to changing the EFIS displays?

Back 20

Aviate, Navigate, Communicate.

Front 21

Aviate (relate to changing EFIS)

Back 21

The display should readily support controlled flight

Front 22

Navigate (relate to changing EFIS)

Back 22

The display should provide discernable and usable navigation information

Front 23

Communicate (relate to changing EFIS)

Back 23

Don't sacrifice control to communicate with controllers

Front 24

What are the 4 Standby instruments below the EFIS, and the 1 on the top right of the glare shield?

Back 24

STBY: Airspeed Ind., Attitude Ind., Altimeter, Turn and Bank Ind., and the Magnetic Compass

Front 25

Standby instruments operate ____________ of the primary instruments?

Back 25

Independently

Front 26

If you're flying and you have a EFIS failure, Generator Failure, ADC Failure, or primary pitot/static failure, what do you cross check?

Back 26

Standby instruments

Front 27

Through which bus are the Standby's powered?

Back 27

Battery Bus (normally)

Front 28

If the battery bus fails, how are the standby's powered?

Back 28

Aux Bat

Front 29

The Aux Bat switch is located in which cockpit?

Back 29

Front

Front 30

Which dimmer switch controls lighting to the STBY instruments?

Back 30

Instrument dimmer switch

Front 31

What affect will the insturment dimmer switch have on the STBY's when they are operating on AUX BAT power and why?

Back 31

None. Their lighting is fixed off the Aux Bat

Front 32

STBY Airspeed gets it's information from what sources?

Back 32

Secondary Pitot and Static system

Front 33

The STBY Airspeed Ind. Is graduated from _ to __ knots (x__)

Back 33

6 to 35; 10 (60 to 350)

Front 34

From __ to ___ knots, airspeed is in __ knot increments and labled every __ knots up too ___

Back 34

60 to 250; 5; 20; 200

Front 35

From ___ to ___ knots, airspeed is in __ knot increments and labeled every __ knots?

Back 35

250 to 350; 10; 50

Front 36

What does the Mach limiting pointer look like?

Back 36

Barber Pole

Front 37

Using the Standby's has two challenges to a pilots routine. (tap to see what they are)

Back 37

They are smaller and with different markings so it may be harder to detect smalller changes, AND you're cross check will be different.

Front 38

Which STBY's require power? (other than for lighting)

Back 38

Attidude and the Needle in the turn and bank

Front 39

What is the criteria for a red flag to be visable on the left side of the stby attitude indicator?

Back 39

Caged and/or with power off. (So, if the batter bus fails, what do you expect to see?) A Red Flag

Front 40

After all electronic power is cut from the STBY attiude ind., how long will it operate and with what attitude deviation?

Back 40

plus or minus 6° for 9 minutes

Front 41

Prior to applying power to the attidue indicator, you need to have it in what position?

Back 41

Pulled and caged.

Front 42

When setting the STBY attitude indicator, you want to align what two parts or it?

Back 42

Little mini airplane onto the balls artificial horizon based on your sitting height parallax

Front 43

When do you want to cage the STBY Attitude indicator?

Back 43

Prior to adding or removing power

Front 44

What bank angle do you want to have when adjusting your STBY attitude indicator?

Back 44

0° Adjust in wings level flight

Front 45

What system attains static pressure to operate the STBY altimeter?

Back 45

Secondary Pitot and Static system

Front 46

The guage has a single point needle that reads what increments?

Back 46

20 foot increments

Front 47

What does it mean when you see a diagonal hatch pattern in the 10,000 foot counter on the STBY altimeter?

Back 47

You're below 10,000 feet.

Front 48

In the event of an electrical failure, what powers the STBY Altimeter?

Back 48

the Aux Battery

Front 49

What two STBY instruments are not functional when the secondary pitot and static system fails?

Back 49

STBY Altimeter and STBY Airspeed Indicator

Front 50

How does the needle on the STBY Turn and Bank Indicator give you turn rate information?

Back 50

By how much it's deflected

Front 51

How much needle deflection on the Turn and Bank Indicator is indicative of a standard rate turn?

Back 51

One needle width

Front 52

Which part of the stby turn and bank indicator will work in the event of power failure?

Back 52

the slip/skid information.

Front 53

What is the source of the Magnetic Compass's power?

Back 53

It doesn't use power

Front 54

What does a compass correction card show you?

Back 54

Deviation caused by avionics and radios operating. It's located on the right canopy rail

Front 55

What should your bank and airspeed be when taking readings from Mag Compass?

Back 55

Level and Unaccelerated

Front 56

Turning North

Back 56

Compass Lags 30°

Front 57

Turning South

Back 57

Compass Leads turn 30°

Front 58

When accelerating or descending on an East/West heading, the compass will turn towards the _____.

Back 58

North

Front 59

What will you do on an East or West heading to make the compass turn South?

Back 59

Climb or decelerate

Front 60

A.N.D.S

Back 60

Accelerate North, Decelerate South

Front 61

Which STBY instruments have partial or limited operation without electrical power?

Back 61

Standby Attitude: 9 minutes, 6° deviation. Turn and Bank Indicator: Slip information only

Front 62

Which STBY instruments function without power?

Back 62

Airspeed, Altimeter (although smooth indications are lost), Magnetic Compass

Front 63

Why are smooth indications lost to standby Altimeter?

Back 63

The stand by altimeter has a powered vibrator (sexy) to allow smooth indication. Without power, the vibrator doesn't work

Front 64

What is "Control Performance Concept" of attitude flying?

Back 64

An aircraft is controlled in flight by adjusting attitude and power to produce desired results

Front 65

What are the three categories of Instrument

Back 65

Control Instruments, Performance Instruments, and Navigation Instruments

Front 66

What are the control instruments?

Back 66

EADI and PEDD

Front 67

Why are the control instuments labeled is such?

Back 67

They display immediate attitude and power allowing pilot to be precise adjustments

Front 68

What are the main performance instruments?

Back 68

Altimeter, Airspeed, VSI

Front 69

What are the "other" performance instruments?

Back 69

EHSI, AOA Indicator, and Turn and Bank Indicator

Front 70

What are the procedures for "control and performance" concept of instrument flight?

Back 70

AETC! Establish attitude and power; Trim pressures, Cross Check performance instruments to asses results, Adjust power and/or attitude

Front 71

The relationship between attitude and power in instrument flight should result in. . . .

Back 71

the desired aircraft performance

Front 72

What will changing the pitch attitude without compensating with power do?

Back 72

Cause a change on your performance instruments(VSI, Altimeter, and Airspeed, AOA, EHSI, and Turn and Bank)

Front 73

What is the primary reference during a level turn?

Back 73

EADI

Front 74

Talk through what happens if you increase bank without increasing power?

Back 74

ASI Decrease, AOA Increase, VSI eventually shows descent, ALT will decrease, EHSI turn rate will increase, and Turn and Bank indications will increase

Front 75

What instrument is your primary power reference?

Back 75

PEDD

Front 76

How do you climb for airspeed?

Back 76

Full power, adjust attitude for airspeed

Front 77

In both climbs and descents, level turns require power increases (T/F)

Back 77

TRUE (maybe. . . Now I'm confused)

Front 78

When you adjust power, you need to cross check. . .?

Back 78

ASI, VSI, Altimeter, EADI and Turn and Bank

Front 79

Why do you not make adjustments based on performance instruments without referencing control instruments?

Back 79

Performance instruments lag behind control instruments.

Front 80

"Chasing" the performance indications is defined as. . .?

Back 80

focusing too much attention on a performance instrument (such as VSI) and trying to stabilize it without cross referencing control instruments

Front 81

Where does the cross check originate?

Back 81

EADI

Front 82

What is the cross check for a Turn

Back 82

Start at EADI to set bank, then EHSI to set leadpoint and rollout HDG, and scan you're other performance instruments with slightly less priority

Front 83

Descent Cross Check procedures are:

Back 83

EADI For pitch; PEDD for power; and cross check VSI and Altimeter.

Front 84

Power and Attitude are adjusted in a descent to control what?

Back 84

Descent Rate and airspeed

Front 85

Climb Cross Check procedures:

Back 85

PEDD to ADD power; EADI for pitch; EHSI, airspeed, vsi, and altimeter

Front 86

What do you reference if you have an electrical failure in flight?

Back 86

Standby instruments

Front 87

What are some things to consider when shifting your instrument flight cross check to STBY instruments only

Back 87

Remain on STBY's unless situation demands other wise, Small changes are harder to detect, Be Aware of Parallax, Increase your scan speed

Front 88

Define: Instrument Flight:

Back 88

flying the aircraft solely on aircraft instruments without external references due to any environmental condition that denies a discernable horizon.

Front 89

What is your primary reference for flying at night? Horizon or instruments?

Back 89

your flight instruments as horizon at night is unreliable

Front 90

During your attitude instrument checks, what are you checking for?

Back 90

Ensure attitude indicators are erect and angle of bank pointers are aligned vertically with zero bank index

Front 91

What is your altimeter tolerance that you are checking in preflight?

Back 91

The altimeter should be set to local barometric setting and be within 75 feet of field elevation

Front 92

What is the heading tolerance you check in preflight?

Back 92

EHSI and Mag compass should be within 5° of of known heading (like RWY heading when aligned).

Front 93

What are the navigation tolerances you check in preflight?

Back 93

after you tune and identify, ensure bearing pointers point to the station and check that the CDI error is not greater than plus or minus 4°. Distance should be within 1/2 mile or 3% of distance to facility. (1234: 1/2 mile, 3%, 4°)

Front 94

Spatial Disorientation is what?

Back 94

Example: You may believe that the clouds are level with horizon and attempt to "level the wings" based on your sight. Cross check would show bank.

Front 95

When can Spatial D occur?

Back 95

any flight condition but mostly when you're without a definable horizon

Front 96

How do you minimize effects of Spatial D?

Back 96

good instrument scan and trusting your instruments

Front 97

If you increase airspeed, what trim inputs do you put in for elevator and rudder?

Back 97

down elevator trim and left rudder trim

Front 98

so if you decrease airspeed, what are your trim inputs?

Back 98

Up elevator, right rudder trim

Front 99

If you maintain airpseed and increase power, what trim inputs do you need?

Back 99

right rudder, down elevator trim

Front 100

If you decrease power with constant airspeed, what are you trim inputs?

Back 100

left rudder, up elevator trim

Front 101

What is the primary purpose of the EADI?

Back 101

act as source for primary attitude information

Front 102

Why is it important to manage the EFIS display?

Back 102

to optimize flight information

Front 103

the standby airspeed indicator is operated by the?

Back 103

Secondary Pitot and Static system

Front 104

T/F: Once all electrical power to standby attitude indicator is lost, it will continue to operate indefinitely?

Back 104

FALSE: (9minutes, 6° deviation)

Front 105

T/F: If the standby turn and bank indicator loses electrical power, the turn needle will contine to operate.

Back 105

FALSE: Just the skid/slip indicator

Front 106

How long does standby attitude indicator provide reliable information after loss of power?

Back 106

9 minutes

Front 107

The standby instruments operate independently of the primary flight instruments (T/F)

Back 107

TRUE

Front 108

The relationship between attitude and pwer in instrument flying should result in _______.

Back 108

Desired aircraft performance

Front 109

Which performance instruments lag?

Back 109

VSI and Altimeter

Front 110

Which instrument is the origin of the cross check?

Back 110

EADI

Front 111

The hub and spoke method is the only cross-check method used and is not modified for any maneuever (T/F)

Back 111

FALSE

Front 112

The recommended way to achieve smooth and precise aircraft control in flight is to trim in this order ___, ____, ____.

Back 112

Rudder, Elevator, Aileron

Front 113

What is the approximate pwer setting in level flight at 150 KIAS at 15,000 feet with a clean configuration?

Back 113

35%

Front 114

To maintain level flight on final approach at 110 knots with gear down and flaps set at TO, what is the approximate power required?

Back 114

35%

Front 115

What is the EFIS system composed of?

Back 115

Two displays (EADI, EHSI) AND the control panel

Front 116

Without power, the standby attitude indicator will provide up to 9 minutes of attitue information and may have as much as ____° error

Back 116

6°

Front 117

The standby altimeter operates off the ____.

Back 117

Secondary Pitot and Static system

Front 118

Primary and Standby instruments operate off of ________ pitot/static systems

Back 118

Different

Front 119

The concept of flying an aircraft in instrument conditions centers on controlling ________.

Back 119

Attitude and Power

Front 120

The two control instruments are?

Back 120

EADI and PEDD

Front 121

What are the performance instruments?

Back 121

Altimeter, Airspeed, VSI, AOA, and Turn and Bank Indicator

Front 122

What cross-check method is the base for all cross checks?

Back 122

Hub and Spoke

Front 123

When setting the local altimeter, it should be within how many feet of airfield elevation?

Back 123

75 feet

Front 124

The approximate power setting at 110KIAS for a non-precision final approach with gear and flaps set to TO and 1000fpm descent is ____% torque?

Back 124

16%