Citation 560 Flashcards

(85 cards)

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
PED SMOKE or FIRE RESPONSE Memory items
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)
26
Aircraft state verification procedure
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
27
What must both crew members verify to confirm the aircraft state?
All three ATTITUDE INDICATORS.
28
What should the crew do if the aircraft state is uncertain?
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.
29
What should be checked regarding the probe, vane, or pitot/static heat?
Ensure it is ON.
30
What are the memory items for UNRELIABLE AIRSPEED, ALTITUDE OR PITCH?
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.
31
What are the memory items for UNUSUAL ATTITUDES - NOSE HIGH?
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.
32
What are the memory items for UNUSUAL ATTITUDES - NOSE LOW?
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.
33
What are the memory items for BRAKE FAILURE?
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.
34
What is the Maximum Ramp Mass?
16500 lbs.
35
What is the Maximum Takeoff Mass (MTOM)?
16300 lbs.
36
What is the Maximum Landing Mass (MLM)?
15200 lbs.
37
What is the Maximum Zero Fuel Mass (MZFM)?
12200 lbs.
38
What is the Mmo (above 28,000 feet)?
Mach 0.755.
39
What are the Vmo values?
292 KIAS (8000 - 28,907 ft) 262 KIAS (<8000 ft).
40
What is the Vfe for flaps 7°?
200 KIAS.
41
What is the Vfe for flaps T/O & APPR 15°?
200 KIAS.
42
What is the Vfe for flaps LAND 35°?
173 KIAS.
43
What is the Vle (landing gear extended speed)?
292 KIAS.
44
What are the Vlo values?
250 KIAS (extending) 200 KIAS (retracting).
45
Vlo (landing gear operation speed)
250 KIAS (extending), 200 KIAS (retracting)
46
Vsb (maximum speed brake operating speed)
No limit
47
Vmca (minimum control speed air)
95 KIAS
48
Vmcg (minimum control speed ground)
91 KIAS
49
Maximum tire ground speed
165 KIAS
50
Maximum speed autopilot operation
292 KIAS or mach 0.755
51
Turbulent air penetration speed
180 KIAS
52
Minimum Operating Limit Speeds for sustained flight in icing conditions (except takeoff, approach and landing)
160 KIAS
53
Max operating altitude
45000 ft
54
Maximum generator load
300 amps
55
Maximum altitude for extension of flaps and landing gear
20000 ft
56
Maximum tailwind component
10 kt
57
Maximum demonstrated crosswind component
20 kt
58
Takeoff and landing maximum air temperature operational limit
ISA + 39 ˚C
59
Takeoff and landing minimum air temperature operational limit
-54 ˚C
60
Maximum engine ITT (takeoff 5 minutes)
720 ˚C
61
Maximum continuous engine ITT
700 ˚C
62
Engine minimum oil pressure (idle)
40 psi
63
Engine minimum oil pressure (takeoff)
60 psi
64
What is the engine minimum oil pressure (above 60% turbine rpm)?
60 psi
65
What is the engine maximum continuous oil pressure?
90 psi
66
What is the engine maximum transient oil pressure?
100 psi (90 seconds)
67
What is the maximum continuous N2?
97 %
68
What is the maximum continuous N1?
100 %
69
What is the maximum usable fuel (pressure refueling)?
5814 lbs
70
What is the minimum fuel temperature for takeoff?
-40 ˚C (JET A-1)
71
What is the maximum asymmetrical fuel differential?
Normal: 200 lbs Emergency: 600 lbs (demonstrated)
72
What is the normal maximum cabin pressure differential?
8.8 psi
73
What is the autopilot minimum use height for non-precision approach?
300 ft AGL
74
What is the autopilot minimum use height for CAT I ILS approach?
180 ft AGL
75
At what KIAS must reverser thrust power be reduced to idle reverse detent position on landing roll?
60 KIAS
76
What is the starter limitation with the battery as a power source?
Three engine starts per 30 minutes. Three cycles of operation with a 90-second rest period between cycles is permitted.
77
What is the minimum starting engine oil temperature?
-40 ˚C
78
What is the maximum and minimum in-flight maneuver load factor (flaps up)?
-1.52 to + 3.8 g at 16300 lbs
79
What is the maximum and minimum in-flight maneuver load factor (flaps extended)?
0.0 to + 2.0 g at 16300 lbs
80
What is the aircraft height?
15.00 ft (4.57 m)
81
What is the aircraft length?
48.90 ft (14.90 m)
82
What is the length of the Grafair Citation 560?
52.50 ft (16.00 m)
83
What is the aircraft wheel track width?
17.60 ft (5.37 m)
84
What is the engine model of the Grafair Citation 560?
Pratt & Whitney JT15D-5D
85
What is the maximum thrust (T/O power) of the Grafair Citation 560?
3,045 lbs (static thrust)