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Aviation > Little Wings > Flashcards

Little Wings Flashcards

1
Q

In reference to aircraft altitude, what do the colours green, yellow and red represent in the KMD 550/850 EGPWS?

A

Green - terrain/obstacles are below aircraft altitude
Yellow - terrain/obstacles are at or above aircraft altitude
Red -terrain/obstacles are at least 2000’ above aircraft altitude

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2
Q

How is do you test the KMD 550/850 EGPWS?

A

It will self test on startup. For a manual test, select the outer rotary knob to “TST”

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3
Q

What does the tiny “F” represent in between the range keys?

What actions should be taken?

A

A system hardware fault exists. Recycle unit power; if fault re-occurs the unit must be serviced.

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4
Q

How do you display the colour key in the TOPO ON mode of the KMD 850?

A

Move the joystick pointer to any area and select “MORE INFO”

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5
Q

What message indicates invalid GPS position data?

A

NO EXTERNAL POSITION DATA

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6
Q

How do you enable and disable Autozoom on the KMD 850?

A

RNG UP on 2000nm, or hold either range key for 2s+. Pressing either range key or having an invalid flight plan will cancel Autozoom.

Active Autozoom is indicated by small black text next to the range setting.

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7
Q

How can you manually test the Stormscope?

A

On the KMD, AUX - WX SETUP - SOTRM SCOPE - NOISE/STRIKE/SELF TEST

The Sotrmscope will self test several times a minute

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8
Q

Is normal to receive a NO DATA RECEIVED FROM STORMSCOPE message during the Stormscope self test?

A

Yes

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9
Q

What will inhibit Stormscope stikes from being overlaid on the KMD Map display?

A

Invalid heading information

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10
Q

How do you clear discharge points on the KMD 850?

A

Move the joystick

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11
Q

Regarding discharge points, what is indicative of a thunderstorm building and dissipating?

A

Building - discharge points reappear faster and in larger numbers
Dissipating - discharge points reappear slower and in smaller numbers

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12
Q

What is the primary difference between Strike Mode and Cell Mode on the Stormscope?

A

Strike Mode displays all lightning strikes with an “x” within the selected view. It is most useful during light electrical activity to potentially identify a building thunderstorm faster than Cell Mode.

Cell Mode will only plot strikes with a “+” and which are associated with a cluster of other strikes as well as strikes within 25nm of the aircraft. It is most useful during periods of heavy electrical activity and will indicate the areas in which cells are present.

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13
Q

How can the flight plan be overlaid on the KMD WX page?

A

OVLY - FLIGHT PLAN

Vice versa for Map Mode

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14
Q

What action should be taken using the Stormscope after receiving erroneous indications during taxi?

A

Clear the screen

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15
Q

Does the Traffic Alerting System provide TA and RA information?

A

No, it only provides TA

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16
Q

What does the arrow represent on the TAS display?

A

The intruder is climbing or descending at 500+fpm

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17
Q

How is a TA displayed in Map Mode?

A

A yellow TRFC is displayed and if auto pop-up is enabled the traffic display will be presented

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18
Q

What is “No Bearing Traffic”?

A

traffic recorded by the TAS of which the bearing cannot be detected. Traffic information is displayed in the top right corner of the MFD. Up to two intruders can be displayed.

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19
Q

What view options are available in the TAS display of the KMD 850?

A

Normal, Above, Below and Unrestricted

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20
Q

How is the KMD 850 TAS tested?

A

A test is performed by using the outer knob to TST. A successful test will indicate one of each symbol. A failed test is indicated by a yellow “TAS FAIL” and the associated system fault.

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21
Q

What is the difference between Wx and WxA on the RDR2000?

A

Wx displays the static colours (green -weak, yellow-moderate, red-heavy, magenta-intense)
WxA displays the intense returns as flashing black and magenta

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22
Q

What colours are displayed in GND MAP mode on the RDR2000?

A

Green, Yellow and Magenta

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23
Q

Do radar transmissions occur when the RDR2000 is tested?

A

No

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24
Q

What is the STBY function on the RDR2000?

A

It fully energizes the radar but does not emit radar transmissions. The antenna is parked at 0 degrees.

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25
Q

How is a successful test of the RDR2000 displayed?

A

To test, select TST and tilt up 7 degrees. The test pattern displays all colours along the arc as the small ripple moves along the outer edge in the 80nm range.
Returns should be evident if the radar is selected ON and aimed at obstacles…

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26
Q

Is the RDR2000 active in ON and LOG modes?

A

It is always active in ON unless a strut switch is fitted. It will be active in LOG mode if it is not interfaced with a graphics unit.

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27
Q

What does RADAR stand for?

A

RAdio Detecting And Ranging

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28
Q

In the RDR2000 how is a target alert indicated?

A

Two red arcs at the top of the screen. It only functions in Wx/WxA from 80nm-240nm.

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29
Q

What can cause altitude rings on the RDR 2000?

A

The shape and physical condition of the nose cone can reflect side lobes down to the ground which are then received by the radar. These will occur at approximately Inm per 6000’ of altitude.

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30
Q

What are the four radar returns indicative of hail?

A

Hooks, fingers, scalloped edges and U-shaped edges.

They appear suddenly, along any edge of the storm and change in intensity in a matter of seconds.

Weak or fuzzy projections are not normally associated with hail.

Any ragged edges, steep gradients or rapid changes in shape or intensity will contain severe turbulence.

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31
Q

How should the RDR 200 tilt be managed to optimise weather targets?

A

In the 40/80nm range, adjust the tilt to fill the display with ground return.
tilt up until the outer third of the display is ground return.
If a return continues strong into the lower thirds of the display it is a hazardous storm/s.
If shadows are detected behind strong returns then there is hazardous weather there too.

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32
Q

How is the Vertical Path mode operated on the RDR 2000?

A

Set the azimuth use the TRK buttons then select VP.

All symmetrical images represent ground return. Any asymmetrical images are weather returns.

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33
Q

How many degrees of tilt inaccuracy is satisfactory before the RDR 2000 should be serviced?

A

2 degrees from one side to the other. This can be checked scanning the ground return or via the STAB test.

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34
Q

When will the “STAB LMT” warning enunciate on the RDR 2000?

A

when the combined pitch and roll exceed 30 degrees. It will remain on until the attitude is restored to within limits.

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35
Q

How can the RDR 2000 Stabilisation be checked?

A

Select MAP - STAB OFF
Set 20NM
GAIN MAX
Fly straight and level
Tilt down to show ground return to the third range mark. If the inner ring is not parallel then the antenna bracket is not mounted correctly.
Turn STAB on. If the figure is lopsided then adjust with the ROLL TRIM using a screwdriver until it appears parallel.
Roll the aircraft and check again.

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36
Q

How is the KFC 225 AFCS tested?

A

A self test on startup is indicated by PFT on the display. A red “P” may be indicated momentarily on the face of the autopilot indicating pitch is not available during the test.

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37
Q

What happens when the AP button of the KFC 225 AFCS is pressed?

A

The flight director, autopilot and yaw damper are engaged.

If the flight director is not already engaged it will adopt wings level at the current attitude.

When AP is pressed again the autopilot will disengage.

38
Q

Which buttons engage the flight director on the KFC 225 AFCS?

A

AP, FD, HDG, NAV, APR, REV, ALT, ARM, GA

39
Q

How can the KFC 225 AFCS autopilot be disengaged?

A

Illumination of the pitch or roll annunciators

Pressing the AP, GA, AP DISC or ELEC TRIM

40
Q

When will the KFC 225 AFCS NAV and APR modes automatically capture?

A

When within half scale deflection. If either mode is pressed again it will disengage.

41
Q

How can Pitch mode (PIT) be entered on the KFC 225 AFCS?

A

By pressing ALT with ALT mode engaged; or

by engaging the flight director or AP for the first time

42
Q

By how much is the flight path angle changed when pressing the vertical trim buttons on the KFC 225 AFCS?

A

0.5 degrees per depression or 0.8 degrees/sec if held.
If in VS mode the rate of change will be 100ft/min or 300ft/min per sec if held.
If ALT mode is active it will adjust the Altitude reference by 20ft/press or 500ft/min if held, synchronising the altitude reference to when the button is released.

43
Q

How is an altitude armed in the KFC 225 AFCS altitude selector?

A

By rotating the rotary knobs with the flight director engaged; or
by selecting ARM

44
Q

How is the KFC 225 AFCS Vertical Speed displayed?

A

It is displayed in the ALT ARM window when the CWS or the VS UP/DN buttons are pressed.

45
Q

When will the KFC 225 AFCS Altitude Alert chime and flash?

A

Chime - 1000’ before approaching a preselected altitude and 200’ after leaving it.

ALERT illuminates as:
a solid alert in the region from 1000’-200’ from the selected altitude.

a two second flash when crossing the selected altitude; and

flashes continuously in the 200’-1000’ range beyond the preselected altitude.

46
Q

How is the yaw damper engaged?

A

By engaging the autopilot or by pressing the YD button. It may be disengaged by pressing the YD button.

47
Q

How is the electric trim used?

How is a trim failure detected and displayed?

A

Both buttons must be pressed in order for the trim to operate.

If a switch fails or is held down for 3 seconds then the PT annunciator will illuminate and disable the electric trim system.

48
Q

When CWS is pressed on the KFC 225 AFCS, will it resume the original modes once released?

A

It will only resume wings level in ROL mode if the angle of bank is less than 6 degrees when released.
PIT, ROL, ALT and VS commands will be synced with the release of CWS.

49
Q

What does the TRIM FAIL annunciator represent?

A

A system test has detected a pitch trim fault in the start up or continuous monitoring in flight. Emergency procedures apply.

50
Q

Will the KFC 225 AFCS capture an altitude on an ILS glidepath?

A

No, but it will with glideslope ARM.

51
Q

What do these voice messages from the KFC 225 AFCS indicate?

TRIM IN MOTION, TRIM IN MOTION
CHECK PITCH TRIM

A

TRIM IN MOTION, TRIM IN MOTION - pitch trim running for more than 5 seconds

CHECK PITCH TRIM - an out of trim condition has existed for more than 16 seconds

Hold the control wheel firmly and press CWS to check for an out of trim condition.
Manually retrim as required and release CWS.
Discontinue use of the autopilot if the out of trim condition is not fixed or returns.

52
Q

If the HDG warning flag appears during operation, the compass card indications will be in error. What actions should be taken?

A

Disconnect the AP

Pull the KG 102A Directional Gyro circuit breaker.

53
Q

Engine Fire in flight recall

A
  1. Fuel Selector Valve…………………………………OFF
  2. Mixture Control……………………………………….Idle Cut Off
  3. Propeller………………………………………………..Feathered
  4. Aux Fuel Pump……………………………………….OFF
  5. Magneto/Start Switch………………………………OFF
  6. Alternator Switch ……………………………………OFF

If Fire Persists-

  1. Land at Nearest Suitable Airport
  2. Land as soon as possible
54
Q

Engine Failure after takeoff (above decision speed)

A

Autopilot - Disengage (may be engaged once AFM OEI procedures are complete)
1. Mixture…………………………………………………..Full Rich
2. Pitch ……………………………………………………..Full Forward
3. Throttles……………………………………………… ..Full Forward
4. Gear………………………………………………………UP
5. Flaps……………………………………………………..UP
6. Maintain directional control………………..5°into Operating Engine
Pitch to maintain 100KIAS
7. Dead Leg/Dead Engine…………………………….Confirm with Throttle
8. Dead Engine ………………………………………….Feather and Secure

Considerations and additional checklists

Cross-feed Fuel - Emergency Checklist / AFM 3-12
OEI Landing - AFM 3-11

55
Q

ENGINE FAILURE DURING GROUND ROLL

A
  1. Throttles……………………………………………………..Closed
  2. Braking……………………………………………………….Maximum

Checklist

  1. Fuel selectors………………………………………………………………OFF
  2. Magnetos…………………………………………………………………….OFF
  3. Alternators………………………………………………………………….OFF
  4. Battery……………………………………………………………………… OFF
56
Q

ENGINE FIRE ON GROUND

A
  1. Mixture Controls……………………………………..Idle Cut Off
  2. Continue to crank affected engine
  3. Fuel Selector Valves……………………………….OFF
  4. Battery and Alternator Switches………………..OFF
  5. Extinguish with fire extinguisher
57
Q

ELECTRICAL SMOKE OR FIRE

A
  1. Battery and Alternator Switches……………………OFF

WARNING
Electrically operated flight instruments and navaids will become inoperative

  1. All Electrical Switches……………………………………OFF
  2. Battery and Alternator Switches………………………ON
  3. Essential Electrical Switches…………………………..ON
    ……………………………………………………Isolate Defective Equipment
  • Ensure fire is out and will not be aggravated by draft
  • Turn off CABIN HEAT and push in the CABIN AIR control
  • Open pilot’s storm window if required
58
Q

EMERGENCY DESCENT

A
  1. Propeller…………………………………………Full Fine- 2700RPM
  2. Throttles………………………………………………………..Closed
  3. Airspeed………………………………………………………..152kts
  4. Landing Gear ………………………………………………..Down
  5. Flaps…………………………………………………………….15 degrees
59
Q

ALL EMERGENCY CHECKLIST ITEMS (14)

A
  1. ENGINE FAILURE DURING GROUND ROLL
  2. ENGINE FAILURE AFTER TAKEOFF (AFTER DECISION POINT)
  3. ENGINE SECURING PROCEDURE
  4. ENGINE FIRE ON GROUND
  5. ENGINE FIRE IN FLIGHT
  6. ELECTRICAL SMOKE OR FIRE
  7. EMERGENCY GEAR EXTENSION
  8. GEAR UP LANDING
  9. CROSSFEED
  10. ENGINE AIR START
  11. EMERGENCY DESCENT
  12. ILLUMINATION OF ALTERNATOR LIGHTS
  13. EMERGENCY STATIC AIR SOURCE SYSTEM
  14. GLIDE
  15. UNLATCHED DOOR IN FLIGHT
60
Q

GLIDE

A
  1. Propellers………………………………………………………Feather
  2. Flaps…………………………………………………………….UP
  3. Landing Gear…………………………………………………UP
  4. Cowl Flaps ……………………………………………………Closed
  5. Airspeed……………………………………………………….120kts

The glide ratio in this configuration approximately 2nm per 1000ft of altitude above the terrain

61
Q

What are the power settings and fuel flow for holding?

A

18”/2300rpm/80L/Hr

62
Q

What are the KFC 225 Autopilot limitations?

A
  1. Preflight test completed successfully prior to each flight
  2. during autopilot operation a pilot must have their seatbelt fastened in the left seat
  3. autopilot and YD must be off for takeoff and landing
  4. CAT 1 approaches only
  5. Speed range 90-210 KIAS
  6. Alt captures below 800’ are prohibited
  7. Must be disengaged below 200’ for landing otherwise below 800’
  8. overriding the autopilot to change pitch and roll is prohibited
  9. the SERVO POWER CB must be pulled following any in-flight illumination of the red TRIM warning light
  10. Pitch mode is permissible in severe turbulence
  11. Not to be used with inoperative AH
  12. Do not operate in severe icing
63
Q

AUTOPILOT, AUTOPILOT TRIM or MANUAL ELECTRIC TRIM MALFUNCTION

A
  1. Airplane Control Wheel - GRASP FIRMLY
  2. AP DISC/TRIM INTER Switch - PRESS &
    HOLDTHROUGHOUT RECOVERY
  3. Aircraft - RETRIM manually
  4. AFCS CMPTR & SERVO POWER Circuit Breakers - PULL (right hand CB Panel)

DO NOT ATTEMPT TO ENGAGE AUTOPILOT AGAIN

The avionics master switch may be selected off whilst the AFCS CMPTR & SERVO POWER Circuit Breakers are found and pulled

If the fault is identified as a TRIM FAIL then the AFCS CMPTR may be reset allowing the use of the FD only.

64
Q

STALL

A
  1. “Stall”
  2. Autopilot - Disengage
  3. Control Column - Relax pressure
  4. Power Max
    5.
65
Q

On the Remote Mode Annunciator what do the colours Green, White, Red and flashing green represent

A

Green - Mode active
White - Mode armed
Red - Autopilot Disconnect
Flashing Green - automatic disconnect

66
Q

What are VH-VLW ice protection limitations:

  1. When is sustained flight in icing conditions prohibited?
  2. What is the max time the windshield heat can be used on ground?
  3. What is the minimum airspeed during icing conditions?
  4. Minimum ambient operating temperature of deicing boots?
  5. When can’t the propeller deice system be operated?
A
  1. With flap extended, except for approach and landing
  2. 10 min
  3. 130 KIAS
  4. -40 deg C
  5. With the propellers stationary (OEI?)
67
Q

What is the definition of Severe Icing?

A

unusually extensive ice accumulation on the airframe and windscreen in areas not normally observed to collect ice, and/or

ice on the upper surface of the wing aft of the protected area, and/or

ice on the engine nacelles and propeller sinners father aft then normally observed

68
Q

SEVERE ICING

A 
Autopilot - Disengage
Min Speed - 130 KIAS
Avoid excessive manoeuvering
Exit icing conditions
Do not move flap until airframe is clear of ice
69
Q

When must the wing icing inspection lights be selected on?

A

Before flight into known/forecast icing conditions at night

70
Q

OEI MISSED APPROACH

A 
Go Around Button - Press
Power - Set Max available
Pitch - To GA bars
(Positive rate) Gear - Up
Flaps - Up
Airspeed - 100 KIAS
71
Q

AFM Emergency Checklists not in Little Wings Emergency Checklist

A
  1. START Annunciator Illuminated (Starter Engaged) 3-14
  2. LEFT and/or RIGHT ALTR Annunciator Illuminated (Alternator Failure) 3-15
  3. Landing Gear Manual Extension 3-16
  4. ICE PROTECTION
    a) FAILURE OF AUTO MODE 3-17
    b) FAILURE OF BOOTS TO INFLATE 3-18
    c) FAILURE OF AUTO & MANUAL MODE 3-18
    d) PROP DE-ICE ABNORMAL AMPS
    i) 0 AMPS 3-18
    ii) 0-14 AMPS 3-18
    iii) 18-23 AMPS 3-19
    iv) >23 AMPS 3-19
    e) FAILURE OF WINDSHEILD HEAT 3-20
  5. LOSS OF ONE ALTERNATOR
72
Q

MISSED APPROACH

A 
GA Button - PRESS
Propellers - MAX
Power - MAX 
Pitch - up to GA Bars
Airspeed - 95 KIAS
Flap - UP
Gear - UP
Cowl Flaps - OPEN
73
Q

Normal Checklists Not Included in Little Wings Checklist

A

HEATER OPERATION 4-33
WINDSHEILD DEFOGGING 4-34
BEFORE TAKEOFF ICE PROTECTION SYSTEM CHECKS 4-35

74
Q

What should happen to the windshield heat if the DG needs to be reset?

A

switched OFF for 15 seconds to allow a stable reading of the standby compass

75
Q

How much are stall speeds increased by with de-ice boots inflated?

A

4 knots in all configurations

76
Q

which surfaces must be clear of frost prior to takeoff?

A

wings, stabilizers and all control surfaces

77
Q

What is the two engine climb speed reduced to in icing conditions?

A

130 KIAS

78
Q

What is the min speed for holding in icing conditions?

A

140 KIAS

79
Q 
What does each annunciator represent when illuminated?
LEFT ALTR
RIGHT ALTR
START
AFT DOOR 
GEAR UP
A

LEFT ALTR -Left alternator off the line
RIGHT ALTR - right alternator off the line
START - starter energised
AFT DOOR - aft utility door is unlatched
GEAR UP - landing gear is up with full flaps; or
landing gear is up and manifold pressure is below approximately 13”Hg on both engines

80
Q

What system design will stop the landing gear from retracting?

A

Both throttles are below 15”/Hg

Only one needs to be at or above 15”/Hg to retract

81
Q

Is it permissible to taxi with a flat strut?

A

No

82
Q

Can the direction of the landing gear switch be changed mid cycle?

A

No

83
Q

When will the landing gear warning horn alarm?

A

If either or both throttles are retarded below a throttle position associated with an engine setting sufficient to sustain two engine flight with the gear retracted.

The horn can be silenced by advancing the throttles above this point…

84
Q

What is the propeller synchronisation split limit?

A

25rpm

85
Q

What are the limitations of the stall warning system?

A

It only functions with the battery and alternator switches on and is only indicative of a stall when the tone is steady.

86
Q

How long does the Ice AUTO setting inflate the boots for?

A

12s

87
Q

What is the standard amperes for the propeller de-ice operating?

A

14-18amp

88
Q

What is the standard amperes for the propeller de-ice operating?

A

14-18amp

89
Q

What are the Air Conditioning limitations?

A 
Must be off for: 
takeoff
engine fire on ground
engine fire in flight
engine failure after takeoff and in flight
air start procedure
air conditioning system malfunction
before engine shutdown
90
Q

When can the air conditioning system be switched on?

A

After engine start; and

after gear is retracted and clear of all obstacles

91
Q

How much will the range and airspeed be reduced by in cruise with the air-conditioning on?

A

~3%

Aviation (11 decks)

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