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CE560XLS > Systems And Limitations > Flashcards

Systems And Limitations Flashcards

1
Q

Max Ramp Weight

A

20,400

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2
Q

Max T/O Weight

A

20,200

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3
Q

Max Landing Weight

A

18,700

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4
Q

Zero Fuel Weight

A

15,100

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5
Q

Max Operating Altitude

A

45,000

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6
Q

Max T/O and Ldg Altitude

A

14,000

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7
Q

Turbulent Air Penetration Speed

A

180

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8
Q

Max Mach (MMo)

A

.75

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9
Q

Max Ldg Gear Extension Spd

A

250

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10
Q

Max Ldg Gear Retraction Spd

A

200

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11
Q

Max Tire GS

A

165

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12
Q

Flaps 7 Spd

A

200

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13
Q

Flaps 15 Spd

A

200

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14
Q

Flaps 35 Spd

A

175

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15
Q

Min Flight in Icing Spd

A

160

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16
Q

VMCA

A

Flaps 7,15. 90Kias

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17
Q

Pressure Differential

A

Max 9.7
Normal 0-9.6
Relief Valve 9.5

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18
Q

Maximum Pax load

A

7, plus 3 lap children due to O2 masks available.

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19
Q

IFR Fuel Reserve (lbs)

A

1037

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20
Q

Hot Spare Fuel

A

4500

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21
Q

Emergency Fuel

A

900

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22
Q

Minimum RWY Length

A

3800 x 60

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23
Q

Crosswind Limit (Dry or Wet)

A

24

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24
Q

Contaminated RWY Crosswind

A

> 150’: 15k
<150 : 10K

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25
Q

Max Tailwind for Ldg

A

10k

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26
Q

Equipment required for RVSM

A

-Autopilot
-Alt Alerting Device
-ALT reporting Transponder
-Static Port Heaters

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27
Q

APU Starts

A

3 attempts in 30 min, 90 second cooldown between

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28
Q

Max Alt for APU Start

A

20,000

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29
Q

Max APU Operating ALT

A

30,000

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30
Q

Min ALTs for Autopilot

A

-EnRoute 1000
-Appr without very guidance 300
-Appr with VG 180

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31
Q

Battery limits Engine Start

A

-3 attempts per hour
-Cross Gen 3:1
-APU Gen 3:1
-GPU (no penalty)

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32
Q

Min Batt V for engine start

A

24

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33
Q

Max GPU Rating

A

28V/1000A

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34
Q

Gen loads

A

-250A (4 min) on Ground, then 200A
-300A in flight

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35
Q

Max Fuel Load

A

6790 lbs
1006 Gals

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36
Q

Max Fuel Imbalance

A

-Normal Ops 400
-Emergency 800

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37
Q

Fuel Pressure Refueling Limit

A

10-55psi

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38
Q

Pitot/Static heat on Ground

A

2 minutes unless required in icing conditions

39
Q

Flaps setting after De-icing

A

Flaps 7 with Type 2,3,4

40
Q

Tail De-icing boot limit

A

-35C Airspeed 150 or greater
-40C less than 150k

41
Q

Approach Category

A

Cat B
Unless operational requirements above 120k, then use Cat C

42
Q

Takeoff Thrust Limits

A

ITT: 740
Time: 2 engines,5 min. 1 engine, 10 min.
N1 100.0
N2 102.8

43
Q

N2 Flight Idle Limits

A

49.3 min
53.2 Max

44
Q

Engine Start ITT Limit

A

740

45
Q

Transient ITT

A

780 (20 secs)

46
Q

Oil Pressure Limits

A

-Ground and Flight Idle 25-160
-T/O 45-160

47
Q

Oil Temp

A

Starting -40C
Ground Idle -40-121.1
T/O 10-121.1

48
Q

Starter Limits

A

3 attempts in 30 minutes, 90 second intervals
30 minute cooldown after 3 attempts

49
Q

Thrust Reverser Limits

A

-Idle below 60k
-3 minutes in 10 deployed
-30 seconds if APU is ON
-No TR during Touch and Go
-No TR to back up airplane

50
Q

Lav Door

A

Must be latched open for Takeoff and Landing

51
Q

XLS Wingspan

A

55.7’

52
Q

XLS Height

A

17.2’

53
Q

How many VGs per wing?

A

26

54
Q

How many Boundary Layer Energizers per wing?

A

11

55
Q

What engines in XLS?

A

PW545B w/4095lbs thrust

56
Q

What engines in XLS?

A

PW545B w/4095lbs thrust

57
Q

Engine driven Hydraulics power what systems?

A

Landing Gear
Speed brakes
Flaps
TRs
Horiz Stab

58
Q

Pressurization trivia

A

Sea-level cabin to 25,247’

App 6800’ pressure @FL450

59
Q

Doors with Caution Annunciation

A

Nose and Tailcone
Cabin Door
Emergency Exit
Battery
Baggage
Lav Door

60
Q

Engine Gen rating

A

30V
300A
Starter Generator

61
Q

Battery Rating

A

25V
44amp/hour

62
Q

What temp causes RED
BATT O’TEMP

A

> 160

63
Q

What items are AC powered

A

EL Panels by an AC Inverter

Windshield Heat by 2AC Engine driven Alternators

64
Q

How long will Secondary batts power the STBY Flight Display?

A

App 3.5 hrs

65
Q

Emergency Lighting consists of what items?

A

2 Emergency battery packs (5G inertia switch controlled)
5 Emergency Exit signs
4 Overhead Cabin lights in Exit areas
2 Strips of Aisle lighting
6 Cabin door step lights
3 Overwing Egress lights

66
Q

What causes EMER lights to illuminate?

A

Pass Safety switch in ON position
Normal aircraft power lost
5G impact

67
Q

Fuel Boost pumps operate automatically when?

A

Engine start
CROSSFEED
LO FUEL PRESS (approx 5.3-5.8 psi)
APU Operation (Right Boost Pump will operate, but no annunciation)

68
Q

Fuel CROSSFEED Valve is powered by what BUS?

A

Main DC

Fails in current position if Main DC power is lost

69
Q

How is fuel quantity measured?

A

7 fuel probes (capacitors) in each tank and a
FQSC (Fuel Quantity Signal Conditioner)

70
Q

Low Level Fuel Warning system
(LO FUEL LEVEL annunc)

A

Float switches in each tank
Approx 360#

71
Q

How long does the ELT record data?

A

30 minutes

72
Q

How does the fire detection system work?

A

Electrical resistance, detects temp, sets off Warning at 500F

73
Q

How many Fire Extinguisher bottles on board?

A

5 total
2 Engine
1 APU
2 Onboard handheld

74
Q

Arming [LH/RH] ENGINE FIRE button does what?

A

Arms both fire bottles
Trips respective GEN field
Locks out respective TR
Fuel SOV closes (respective)
HYD SOV closes (respective)

75
Q

What is the pressure of Hydraulic system during HYD PRESS indication?

A

Approx 1500 psi
(For up to 40 secs, if still illuminated, Master Caution will illuminate)

76
Q

IF Gear and Flaps are operated at the same time, what has priority?

A

Landing Gear

77
Q

How long can HYD PRESS stay illuminated with no problems?

A

40 seconds. After which, annunciator will flash and Master Caution will illuminate

78
Q

What causes Gear Horn to sound?

A

Gear not down and locked with:
-Throttles below 70% N2 and Flaps >15
-Throttles below 70% and Radar Alt <500’
-Throttles below 70%, non valid RA and airspeed <150k

79
Q

How do you activate Radar on the ground?

A

WX, then STAB 4X

80
Q

How long will the battery provide power to all critical systems?

A

10 minutes

When switched to EMER: approx 30 minutes

81
Q

What is the function of the BATTERY DISCONNECT switch on the L side panel?

A

Disconnects the battery electrically by opening the BATT DISC relay and removing the ground.

82
Q

What circuit breakers are on the Left CB panel?

A

Primary aircraft systems such as ENVIRONMENTAL, LIGHTS and ENGINE INSTRUMENTS, including some of the basic flight instruments.

83
Q

What circuit breakers are on the right CB panel?

A

Primarily the AVIONICS systems.

84
Q

Items on the engine Accessory Gearbox

A

Fuel control and fuel pump
Oil pumps
Hydraulic pump
Air/oil separator
Starter/generator
Alternator

85
Q

How many fuel nozzles in the engine combustion chamber

A

11

86
Q

EEC provides what functions?

A

Throttle detents
Engine governing for Ground and Flight Idle
Anti ice thrust setting compensation
Over speed protection
N1 and N2 speed limiting and/ or Syncing

87
Q

What items are anti-ice protected and how are they?

A

EEC (T0), Windshield, TAS probe(Rosemount), AOA, Pitot/Static are ELECTRICALLY protected.

Wings leading edges, Engine inlets, Engine fan nose cone and T1 (ITT) are BLEED AIR heated

Horizontal Stabilizer has inflatable pneumatic boots using Service Air

88
Q

What “TipToe”

A

T1 probe: Pneumatic heat

T0 probe: Electric heat

89
Q

How many PSI to inflate Horiz Stab boots?

A

23 psi

90
Q

What items are continuously heated?

A

T1 probe and engine nose cone
(Windshield heat switches are usually left in the On position so will usually be heated as well)

91
Q

What does selecting ENGINE ANTI ICE ON activate?

A

Engine inlets (P3 air)
Engine Stators (P3 air)
Engine ignitors activate
T0 probe is electrically heated

92
Q

What is the inflation time cycle for the Hor Stab boots?in AUTO mode?

A

18 sec inflate/deflate cycle
3 minutes OFF

Repeat

93
Q

Conditions for EDM (EMER desc) to occur?

A

Autopilot engaged
Aircraft alt above 30,000’
Cabin Alt 14,500 +/-500’

94
Q

Actions during EDM

A

90 degree Left turn
Alt select changes to 15,000’
Pitch to VMo-10

CE560XLS (2 decks)

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