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CE560XLS > Systems And Limitations > Flashcards

Systems And Limitations Flashcards

(94 cards)

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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
Max Tailwind for Ldg
10k
26
Equipment required for RVSM
-Autopilot -Alt Alerting Device -ALT reporting Transponder -Static Port Heaters
27
APU Starts
3 attempts in 30 min, 90 second cooldown between
28
Max Alt for APU Start
20,000
29
Max APU Operating ALT
30,000
30
Min ALTs for Autopilot
-EnRoute 1000 -Appr without very guidance 300 -Appr with VG 180
31
Battery limits Engine Start
-3 attempts per hour -Cross Gen 3:1 -APU Gen 3:1 -GPU (no penalty)
32
Min Batt V for engine start
24
33
Max GPU Rating
28V/1000A
34
Gen loads
-250A (4 min) on Ground, then 200A -300A in flight
35
Max Fuel Load
6790 lbs 1006 Gals
36
Max Fuel Imbalance
-Normal Ops 400 -Emergency 800
37
Fuel Pressure Refueling Limit
10-55psi
38
Pitot/Static heat on Ground
2 minutes unless required in icing conditions
39
Flaps setting after De-icing
Flaps 7 with Type 2,3,4
40
Tail De-icing boot limit
-35C Airspeed 150 or greater -40C less than 150k
41
Approach Category
Cat B Unless operational requirements above 120k, then use Cat C
42
Takeoff Thrust Limits
ITT: 740 Time: 2 engines,5 min. 1 engine, 10 min. N1 100.0 N2 102.8
43
N2 Flight Idle Limits
49.3 min 53.2 Max
44
Engine Start ITT Limit
740
45
Transient ITT
780 (20 secs)
46
Oil Pressure Limits
-Ground and Flight Idle 25-160 -T/O 45-160
47
Oil Temp
Starting -40C Ground Idle -40-121.1 T/O 10-121.1
48
Starter Limits
3 attempts in 30 minutes, 90 second intervals 30 minute cooldown after 3 attempts
49
Thrust Reverser Limits
-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
Lav Door
Must be latched open for Takeoff and Landing
51
XLS Wingspan
55.7’
52
XLS Height
17.2’
53
How many VGs per wing?
26
54
How many Boundary Layer Energizers per wing?
11
55
What engines in XLS?
PW545B w/4095lbs thrust
56
What engines in XLS?
PW545B w/4095lbs thrust
57
Engine driven Hydraulics power what systems?
Landing Gear Speed brakes Flaps TRs Horiz Stab
58
Pressurization trivia
Sea-level cabin to 25,247’ App 6800’ pressure @FL450
59
Doors with Caution Annunciation
Nose and Tailcone Cabin Door Emergency Exit Battery Baggage Lav Door
60
Engine Gen rating
30V 300A Starter Generator
61
Battery Rating
25V 44amp/hour
62
What temp causes RED BATT O’TEMP
>160
63
What items are AC powered
EL Panels by an AC Inverter Windshield Heat by 2AC Engine driven Alternators
64
How long will Secondary batts power the STBY Flight Display?
App 3.5 hrs
65
Emergency Lighting consists of what items?
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
What causes EMER lights to illuminate?
Pass Safety switch in ON position Normal aircraft power lost 5G impact
67
Fuel Boost pumps operate automatically when?
Engine start CROSSFEED LO FUEL PRESS (approx 5.3-5.8 psi) APU Operation (Right Boost Pump will operate, but no annunciation)
68
Fuel CROSSFEED Valve is powered by what BUS?
Main DC Fails in current position if Main DC power is lost
69
How is fuel quantity measured?
7 fuel probes (capacitors) in each tank and a FQSC (Fuel Quantity Signal Conditioner)
70
Low Level Fuel Warning system (LO FUEL LEVEL annunc)
Float switches in each tank Approx 360#
71
How long does the ELT record data?
30 minutes
72
How does the fire detection system work?
Electrical resistance, detects temp, sets off Warning at 500F
73
How many Fire Extinguisher bottles on board?
5 total 2 Engine 1 APU 2 Onboard handheld
74
Arming [LH/RH] ENGINE FIRE button does what?
Arms both fire bottles Trips respective GEN field Locks out respective TR Fuel SOV closes (respective) HYD SOV closes (respective)
75
What is the pressure of Hydraulic system during HYD PRESS indication?
Approx 1500 psi (For up to 40 secs, if still illuminated, Master Caution will illuminate)
76
IF Gear and Flaps are operated at the same time, what has priority?
Landing Gear
77
How long can HYD PRESS stay illuminated with no problems?
40 seconds. After which, annunciator will flash and Master Caution will illuminate
78
What causes Gear Horn to sound?
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
How do you activate Radar on the ground?
WX, then STAB 4X
80
How long will the battery provide power to all critical systems?
10 minutes When switched to EMER: approx 30 minutes
81
What is the function of the BATTERY DISCONNECT switch on the L side panel?
Disconnects the battery electrically by opening the BATT DISC relay and removing the ground.
82
What circuit breakers are on the Left CB panel?
Primary aircraft systems such as ENVIRONMENTAL, LIGHTS and ENGINE INSTRUMENTS, including some of the basic flight instruments.
83
What circuit breakers are on the right CB panel?
Primarily the AVIONICS systems.
84
Items on the engine Accessory Gearbox
Fuel control and fuel pump Oil pumps Hydraulic pump Air/oil separator Starter/generator Alternator
85
How many fuel nozzles in the engine combustion chamber
11
86
EEC provides what functions?
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
What items are anti-ice protected and how are they?
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
What "TipToe"
T1 probe: Pneumatic heat T0 probe: Electric heat
89
How many PSI to inflate Horiz Stab boots?
23 psi
90
What items are continuously heated?
T1 probe and engine nose cone (Windshield heat switches are usually left in the On position so will usually be heated as well)
91
What does selecting ENGINE ANTI ICE ON activate?
Engine inlets (P3 air) Engine Stators (P3 air) Engine ignitors activate T0 probe is electrically heated
92
What is the inflation time cycle for the Hor Stab boots?in AUTO mode?
18 sec inflate/deflate cycle 3 minutes OFF Repeat
93
Conditions for EDM (EMER desc) to occur?
Autopilot engaged Aircraft alt above 30,000’ Cabin Alt 14,500 +/-500’
94
Actions during EDM
90 degree Left turn Alt select changes to 15,000’ Pitch to VMo-10

CE560XLS (2 decks)

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