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Grafair Flashcards > Citation 560 > Flashcards

Citation 560 Flashcards

1
Q

DOUBLE ENGINE FAILURE memory items

A
  1. IGNITION 1 & 2 - BOTH ON
  2. BOOST PUMPS - BOTH ON
  3. THRUST LEVERS - IDLE
  4. SPEED (if altitude allows) - 200 KIAS
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2
Q

ENGINE FIRE BELOW V1 memory items

A
  1. THRUST LEVERS - IDLE
  2. BRAKES - APPLY
  3. SPEED BRAKES - EXTEND
  4. THRUST REVERSERS DEPLOY (on unaffected engine)
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3
Q

ENGINE FIRE ABOVE V1 memory items

A
  1. ROTATE - VR
  2. LANDING GEAR - UP
  3. SPEED - V2 UP TO 1500 AGL
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4
Q

ENGINE FIRE IN GENERAL memory items

A
  1. THROTTLE (affected engine) - IDLE

If fire warning light persists:
1. ENGINE FIRE SWITCH (affected engine)

  1. Either illuminated BOTTLE ARMED LIGHT - PUSH
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5
Q

ENGINE FAILURE DURING COUPLED APPROACH memory items

A
  1. POWER (operating engine) - INCREASE (as required)
  2. AUTOPILOT and YAW DAMPER - OFF
  3. AIRSPEED - Vapp
  4. RUDDER TRIM - TRIM (toward operating engine as desired)
  5. FLAPS - T.O AND APPR
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6
Q

EMERGENCY RESTART - TWO ENGINES memory items

A
  1. IGNITION - BOTH ON
  2. BOOST PUMPS - BOTH ON
  3. THROTTLES - IDLE
  4. IF ALTITUDE ALLOWS - INCREASE AIRSPEED TO 200 KIAS
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7
Q

CABIN DEPRESSURIZATION memory items

A
  1. CREW OXYGEN MASKS - DON MASKS
  2. MIC SELECTOR SWITCH - MIC OXYGEN MASK
  3. EMERGENCY DESCENT - AS REQUIRED
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8
Q

EMERGENCY DESCENT memory items (OM-B 3.10.1)

A
  1. PF: AIRPLANE BANK & PITCH - ROLL into moderate bank (if able) & PITCH 25 Degrees nose down
  2. THRUST LEVERS - IDLE
  3. SPEED - Mmo/Vmo (unless structural damage)
  4. SPEEDBRAKE - EXTEND
  5. MANUAL PAX MASKS - DROP (if needed)

PM: PASSENGER ADVISORY LIGHTS - PASS SAFETY
6. RECOGNITION LIGHTS - ON
7. ATC - CALL MAYDAY
8. TRANSPONDER - 7700
9. PASSENGERS - CHECK FOR OXYGEN (mask dropped)

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9
Q

ELECTRICAL FIRE OR SMOKE memory items

A
  1. OXYGEN MASKS - DON AND EMER
  2. MIC SELECTOR SWITCH - MIC OXYGEN MASK
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10
Q

THRUST REVER INADVERTENT DEPLOYMENT BELOW V1 memory items

A
  1. BRAKES - APPLY
  2. THROTTLES - IDLE
  3. SPEED BRAKES - EXTEND
  4. THRUST REVERSERS - BOTH DEPLOY (on unaffected engines)
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11
Q

THRUST REVERSER INADVERTENT DEPLPOYMENT ABOVE V1 memory items

A
  1. EMERGENCY STOW SWITCH - EMER (affected engine)

  1. POSITIVE RATE OF CLIMB - GEAR UP
  2. SPEED - Do not exceed 125 KIAS until thrust reversers stow
  3. AT 400’ AAL - FLAPS RETRACT at V2+10 and accelerate (do not exceed 200 KIAS after thrust reverser stows)
  4. THROTTLE (affected engine) - NORMAL OPERATION
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12
Q

THRUST REVERS INADVERTENT INFLIGHT DEPLOYMENT memory items

A
  1. CONTROL WHEEL / AUTOPILOT - GRIP/DISENGAGE
  2. EMERGENCY STOW SWITCH - EMER (affected engine)
  3. THROTTLE (affected engine) - CHECK IDLE
  4. AIRSPEED - REDUCE TO 125 KIAS OR BELOW (after thrust reverser stow, do not exceed 200 KIAS)
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13
Q

AUTOPILOT MALFUNCTION memory items

A
  1. AP TRIM DISC - PUSH
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14
Q

AUTOPILOT MALFUNCTION memory items

A

AP TRIM DISC - PUSH

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15
Q

ELECTRIC ELEVATOR RUNAWAY TRIM memory items

A

AP TRIM DISC - PUSH and HOLD

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16
Q

INADVERTENT STALL (STICK SHAKER, BUFFET AND/OR ROLL-OFF) memory items

A

AUTOPILOT - DISCONNECT
PITCH ATTITUDE - REDUCE
ROLL ATTITUDE - LEVEL
THROTTLES MAXIMUM THRUST

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17
Q

EMERGENCY EVACUATION memory items (OM-B 3.9.1)

A

LP:
L/R THROTTLES - CUT OFF
Both fire switch and fire bottle (if req) - PUSH
PA & ATC - EVACUATE
BATTERY SWITCH - OFF

RP:
L/R THROTTLES - CUT OFF (Check)
PASSENGERS - EVACUATE

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18
Q

CREW INCAPACITION memory items

A

If the other crew member does not respond on a challenge call out the 2:nd time or if incapacitation is suspected:
Put a hand on the other crew members shoulder and call “I HAVE CONTROLS”
If no response (pilot incapacitated):
Remove crew member from controls
give oxygen
call MAYDAY and land at nearest suitable airport

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19
Q

EGPWS (TERRAIN PULL UP audio alert) memory items

A

PF:
“TERRAIN - FULL THRUST”
Put hand on yoke and throttles
Disconnect A/P and climb to safe altitude with best angle of climb airspeed

PM:
Advice ATC of deviation
Monitor TAWS display, give guidance to PF
Advice the best escape route to PF (LEFT or RIGHT)

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20
Q

TCAS TA memory items

A

PF:
“TCAS, I HAVE CONTROL”
Be prepared to disconnect the A/P and put hands on the controls and thrust levers

PM:
Monitor TCAS display, zoom in if needed
Look out for traffic and advice PF

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21
Q

TCAS RA memory items

A

PF:
“AUTOPILOT OFF”
Disconnect A/P and follow TCAS green fly-to commands
Reduce or increase thrust accordingly
Ask PM to remove flight director (FD) if needed

PM:
Call ATC “TCAS RA”
Deselect lateral & vertical guidance (FD’s OFF)

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22
Q

WINDSHEAR memory items

A

PF:
“WINDSHEAR - FULL THRUST”
Apply full thrust
Pitch up 15 degrees initially, then up to stick shaker if required

PM:
Monitor flight instruments, and give guidance to PF until out of windshear

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23
Q

VOLCANIC ASH ENCOUNTER memory items

A

PF:
“VOLCANIC ASH”
REDUCE THRUST
180° TURN

PM:
CALL ATC
Monitor flight instruments, read checklist for volcanic ash

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24
Q

SEVERE ICING ENCOUNTER memory items

A

PF:
“SEVERE ICING”
DISCONNECT AUTOPILOT
LEAVE SEVERE ICING CONDITIONS
The quickest way of exit icing conditions is to climb or descent a few thousand feet.

PM:
CALL ATC and REQUEST CLEARANCE

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25
Q

PED SMOKE or FIRE RESPONSE Memory items

A

PF:
“I HAVE ATC”
CALL MAYDAY
LAND AS SOON AS POSSIBLE

PM:
FIRE GLOVES - ON
Put device in fire proof bag or metal waste bin, soak with large amount of water (no alcohol)

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26
Q

Aircraft state verification procedure

A

Both crew must verify all three ATTITUDE INDICATORS to confirm aircraft state.
If the aircraft state is uncertain, crew must fly pitch and thrust to recover a safe flight phase. Display GPS altitude on GPS/FMS to confirm a state of CLIMB, DESCENT OR CRUISE. Use the table attached as guidance.
Check probe, vane or pitot/static heat ON

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27
Q

What must both crew members verify to confirm the aircraft state?

A

All three ATTITUDE INDICATORS.

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28
Q

What should the crew do if the aircraft state is uncertain?

A

Fly pitch and thrust to recover a safe flight phase. Display GPS altitude on GPS/FMS to confirm a state of CLIMB, DESCENT OR CRUISE.

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29
Q

What should be checked regarding the probe, vane, or pitot/static heat?

A

Ensure it is ON.

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30
Q

What are the memory items for UNRELIABLE AIRSPEED, ALTITUDE OR PITCH?

A

PF:
- ‘STALL - FULL THRUST’
- A/P - OFF
- NOSE DOWN PITCH CONTROL - AS NEEDED
- BANK - WINGS LEVEL
- SPEED BRAKES - RETRACT
- WHEN OUT OF STALL - RETURN TO DESIRED FLIGHT PATH

PM:
- Monitor flight instruments, pitch, max thrust
- Guide if needed.
- Execute commands from PF.

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31
Q

What are the memory items for UNUSUAL ATTITUDES - NOSE HIGH?

A

PF:
- ‘NOSE HIGH - FULL THRUST’
- APPLY FULL THRUST
- REDUCE PITCH TO ZERO
- ROLL TO NEAREST HORIZON

PM:
- ‘NOSE HIGH’
- Monitor flight instruments
- Guide PF as needed.

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32
Q

What are the memory items for UNUSUAL ATTITUDES - NOSE LOW?

A

PF:
- ‘NOSE LOW - IDLE THRUST’
- REDUCE THRUST TO IDLE
- USE AIR BRAKES IF NEEDED
- ROLL TO NEAREST HORIZON (WINGS LEVEL)
- RAISE NOSE/PITCH TO ZERO

PM:
- ‘NOSE LOW’
- Monitor flight instruments
- Guide PF as needed.

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33
Q

What are the memory items for BRAKE FAILURE?

A

PF:
- REVERSE - APPLY
- BRAKE PEDALS - RELEASE, REMOVE FEET FROM BRAKE PEDALS
- EMERGENCY BRAKE HANDLE - PULL as required

PM:
- ADVISE PF IF FULL REVERSE IS NEEDED.

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34
Q

What is the Maximum Ramp Mass?

A

16500 lbs.

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35
Q

What is the Maximum Takeoff Mass (MTOM)?

A

16300 lbs.

36
Q

What is the Maximum Landing Mass (MLM)?

A

15200 lbs.

37
Q

What is the Maximum Zero Fuel Mass (MZFM)?

A

12200 lbs.

38
Q

What is the Mmo (above 28,000 feet)?

A

Mach 0.755.

39
Q

What are the Vmo values?

A

292 KIAS (8000 - 28,907 ft)
262 KIAS (<8000 ft).

40
Q

What is the Vfe for flaps 7°?

A

200 KIAS.

41
Q

What is the Vfe for flaps T/O & APPR 15°?

A

200 KIAS.

42
Q

What is the Vfe for flaps LAND 35°?

A

173 KIAS.

43
Q

What is the Vle (landing gear extended speed)?

A

292 KIAS.

44
Q

What are the Vlo values?

A

250 KIAS (extending)
200 KIAS (retracting).

45
Q

Vlo (landing gear operation speed)

A

250 KIAS (extending), 200 KIAS (retracting)

46
Q

Vsb (maximum speed brake operating speed)

A

No limit

47
Q

Vmca (minimum control speed air)

A

95 KIAS

48
Q

Vmcg (minimum control speed ground)

A

91 KIAS

49
Q

Maximum tire ground speed

A

165 KIAS

50
Q

Maximum speed autopilot operation

A

292 KIAS or mach 0.755

51
Q

Turbulent air penetration speed

A

180 KIAS

52
Q

Minimum Operating Limit Speeds for sustained flight in icing conditions (except takeoff, approach and landing)

A

160 KIAS

53
Q

Max operating altitude

A

45000 ft

54
Q

Maximum generator load

A

300 amps

55
Q

Maximum altitude for extension of flaps and landing gear

A

20000 ft

56
Q

Maximum tailwind component

A

10 kt

57
Q

Maximum demonstrated crosswind component

A

20 kt

58
Q

Takeoff and landing maximum air temperature operational limit

A

ISA + 39 ˚C

59
Q

Takeoff and landing minimum air temperature operational limit

A

-54 ˚C

60
Q

Maximum engine ITT (takeoff 5 minutes)

A

720 ˚C

61
Q

Maximum continuous engine ITT

A

700 ˚C

62
Q

Engine minimum oil pressure (idle)

A

40 psi

63
Q

Engine minimum oil pressure (takeoff)

A

60 psi

64
Q

What is the engine minimum oil pressure (above 60% turbine rpm)?

A

60 psi

65
Q

What is the engine maximum continuous oil pressure?

A

90 psi

66
Q

What is the engine maximum transient oil pressure?

A

100 psi (90 seconds)

67
Q

What is the maximum continuous N2?

A

97 %

68
Q

What is the maximum continuous N1?

A

100 %

69
Q

What is the maximum usable fuel (pressure refueling)?

A

5814 lbs

70
Q

What is the minimum fuel temperature for takeoff?

A

-40 ˚C (JET A-1)

71
Q

What is the maximum asymmetrical fuel differential?

A

Normal: 200 lbs
Emergency: 600 lbs (demonstrated)

72
Q

What is the normal maximum cabin pressure differential?

A

8.8 psi

73
Q

What is the autopilot minimum use height for non-precision approach?

A

300 ft AGL

74
Q

What is the autopilot minimum use height for CAT I ILS approach?

A

180 ft AGL

75
Q

At what KIAS must reverser thrust power be reduced to idle reverse detent position on landing roll?

A

60 KIAS

76
Q

What is the starter limitation with the battery as a power source?

A

Three engine starts per 30 minutes. Three cycles of operation with a 90-second rest period between cycles is permitted.

77
Q

What is the minimum starting engine oil temperature?

A

-40 ˚C

78
Q

What is the maximum and minimum in-flight maneuver load factor (flaps up)?

A

-1.52 to + 3.8 g at 16300 lbs

79
Q

What is the maximum and minimum in-flight maneuver load factor (flaps extended)?

A

0.0 to + 2.0 g at 16300 lbs

80
Q

What is the aircraft height?

A

15.00 ft (4.57 m)

81
Q

What is the aircraft length?

A

48.90 ft (14.90 m)

82
Q

What is the length of the Grafair Citation 560?

A

52.50 ft (16.00 m)

83
Q

What is the aircraft wheel track width?

A

17.60 ft (5.37 m)

84
Q

What is the engine model of the Grafair Citation 560?

A

Pratt & Whitney JT15D-5D

85
Q

What is the maximum thrust (T/O power) of the Grafair Citation 560?

A

3,045 lbs (static thrust)

Grafair Flashcards (4 decks)

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