XLS Initial Systems knowledge Flashcards
Dimensions of aircraft
Wing 56’, Length 52’, height 17’
Turning radius is
Wall to wall 70’, curb to curb 38’
Max ramp weight
20400
Max take off weight
20200
Max landing weight
18700
Max Fuel Weight (capacity)
6790
1006/503
Baggage weight limit
700
Max take off altitude
14,000’
Battery is what capacity and voltage
44amp and 25 volt
Components on the Hydraulic System
- Gear
- Flaps
- Thrust reversers
- Speed Brakes
- Stab Trim
Standby instrument good for how long
3.5 hours
Main ship battery is good for how long as long if it is put into Emer in how many minutes
30 minutes, if put in emer within 5 minutes
How long is the ship battery good for with no gens
10 Minutes
What items are on the battery buss
- Baggage light
- Tailcone Light
- Cabin Entrance Light
- Lav Level Light
- APU Oil Light
What lights are available on Emer power
Flood lights
Aux Panel Light
Fire Button Push will does what
- Closes Fuel
- Hydraulic
- Arms Bottle
- ELectric
Cabin Alt Master warning at what alt
10,000’
What altitude do the maskes drop
14,500 +- 500
Generator imbalance is a mx write up when it exceeds
10% of the total load
GCU regulates voltage to:
evens the load to what %
and
Volts to 28.5, parallels the load within 10% and protects
- Undervolt
- Reverse Current
- Overvolt
- Feeder Fault
- Fire Switch
Generator
Relay
————–
Field Relay
Generators max amps ground and air
200amp and 300 amp
Ground Generator max transient amps and time
250amps 4 minutes
GPU max volts and amps to prevent damage to shaft
>28 volts and or 1,000 amps
Max Engine ITT
740
Enroute Operational Limits
Max altitude for Flaps and Landing Gear Extended
18,000’
Fuel Limits
Minimum Fuel Temp
Maximum Fuel Temp
-40C
+57C
Take off - Max Ambient Temperature
ISA +39C
Maximum Tire Rotation speed
165 knots
Min airspeed in RVSM airspace
160KTS
Min weight in RVSMS airspace
14,000lbs
Powerplant Operating Limits (Time, Temp, N1, N2)
Takeoff
Time limit 5 minutes
ITT 740C
N1 100%
N2 102.8%
Powerplant Operating Limits (Temp, N1, N2)
Max Continuous
ITT 720C
N1 100%
N2 102.8%
Powerplant Operating Limits
Transient
Starting
780C 20 seconds
740C
Speed Limits
MMO above 26,515’
VMO 8,000 - 26,515
VMO Below 8,000
.75 mach
305KIAS
260KIAS
Load Factor
Flaps up
Flaps down
-1.2G - +3.0G at 20,200lbs
0. 00 - +2.0G at 20,200lbs down to 18,700lbs
Cabin Pressurization (Page 39 Cessna AFM)
Normal cabin pressure 0.00 to
Pressure Relief Valve
Pressure Gauge Red Line
- 6psi
- 5psi
- 7psi
Max allowable time thrust reverser deployed
3 minutes in any 10 minute period
APU Operating Limits (altitude)
Starting
Running
Starting 20,000’ Max EGT 690
Running 30,000’ 690 108%
Minimum Tail Deice (temps/speeds)
Min Temp for use below 150IAS -40C RAT
Min Temp for use above 150IAS -35C RAT
Battery service:
Don’t start Engine if battery is less than:
Use the APU if battery is less than:, but more than:
If battery is less than: needs service
24volts
24 volts 17 Volts
Below 17 volts, service
What pressure is service air
23psi
If there is a Master Caution and it goes away, what happens to the Light
If there is a Master Warning and it goes away, what happens to the light
Master Caution will go out.
Master Warning stays on
What white lights will give a Master Caution in air
White Ground Idle in air
Xflow Flashing
How do you check if an Engine Firebottle is low pressure
Absence light means ok
Primary Door seal will work from- to (psi)
At what PSI will the low light come on
6-23psi
light on a 5psi
Bad question - ignore
Pitot Static System
3 Pitot static probes
Static Ports
AOA
TAS probe Weight off wheels and avionics switch on
Air Duct overheat - how is this resolved? Auto or manual
No automatic changes Manual only
What happens to the system with
Wing Bleed Air Overheat
It will auto shutdown and wing anti-ice on the overheat side
Pressurization Controller:
High altitude Mode Starts at:
8,100’
If ADC1 Fails what happens to the pressurization controller
Failes to Isobaric mode and orange light
If Hydraulic systems stay pressurized, how long before what happens
After 40 seconds the warning will flash.
Stab gets its information from which static system
Standby
Air Bottle Both Gear and brakes use the same bottle. How many pulls before or after gear dropped
10 brake pulls with no gear
5 brake pulls with gear blow down
Gear Warning System When will you get gear warning
Gear not down
and power less than 70% N2
Flaps less than 15 degrees
Radar Alt less than 500’
Turbulent air penetration
180knots
Autopilot needs _ sources to work
2 valid AHRS
Ground idle light will come on _ seconds after landing
8
Low fuel limit light
360lbs +-20lbs
While taxiing in freezing conditions throttle up how often
15 seconds every 4 minutes
At what PSI does low brake pressure light come on
900
How is nosewheel centered on gear retraction
Mechanically
Speedbrakes retract with throttle at
80%
Engine Start Need fan rotation by
25% N2
Pitot tube off until _ minutes before take off, unless
2 minutes unless +-10C and visible moisture
Wind-shear are different. what are those warnings differences
Headwind is Amber Windshear
Tailwind is Red Windshear
EEC Controls 9 things.
N1 and N2 speed limiations
Acceleration and Decelartion limitations
Overpseed protection
Bleed valve conrtrol
Engine Diagnostics
N1 and N2 sync
Throttle detent positions
EEC Auto Modes
Climb
Cruise Decent
High Altitude
Ground
8,100’ high altitude mode
boundary layer Energizers How many each side and can any be missing
11 each side
none can be missing
Vortex Generators How many and can any be missing
26 per side and up to 3 missing
When does a fuel pump come on:
Low Fuel Pressure
Fuel Transfer
APU
Start
Service air is used for what:
Boots
Outflow Valves (pressurization components)
Door Seals
Throttle Detents
Main engine Bleed air comes from
P3
Fuel Capacity lbs and gallons
1006 gallons
6790
All but 3 gallons are usable
Single point fueling and de-fueling
55psi
-10ps
Fuel level sensors. How many
7 sensors in each wing
If fuel gets to ___Lbs, turn on fuel boost pumps
Low level Light comes on at ___lbs
400
360lbs +-20
Low fuel “PRESSURE” light comes on at ___lbs and turns off at ___lbs
<5psi
>7psi
Fuel Transfer rate in crossfee is ___lbs per hour
700lbs
max fuel imabalance is ____lbs
Max Emergency imbalance is ___lbs
400
800
Fuel transfer valve fails in what position (loss of power)
In the Last Position
What is in the Hydraulics systems
Gear
Speed Brakes
Flaps
Thrust Reversers
Stabilizer
Apu burns ___lbs per hour when loaded
110lbs
APU limitions on start and run in air (altitude)
start 20,000’
run 30,000’
Nose gear will turn up to x degrees with ruder and x degrees with differential power
20 degrees rudder
60 degrees diff power
Gear Warning horn will sound in what conditions
Gear not down and locked and
Throttles below 70%
Flaps no greater than 15
Or
Radio altimiter below 500’
or Non valid radio alt signal and below 150 knots
Pneumatics
Service air (Think Boots)
Boots Tails deice
Outflow Valves
Throttle detents
Seals - Accoustic and Door Seal
With pressure source knob selected off cabin pressure will rise at about ___FPM
500
If ADC1 fails what happens to pressure controller
Yellow light and it goes to ISOBARIC mode
If the primary seal fails what altitude are you limited to
25,000
PITOT Tube limitations
2 minutes on before take off unless less than +10C and visible moisture/reduced visibility <1 mile
Engine Anti Ice is always on what
Nose cone and T1 probe, always heated
Tiptoe
T1 probe is ____ heated
T0 probe is ____ heated
T1 is Bleed Air
T0 is electrically heated
Engine heat: Valve fail _____
Open
Wing Anti Ice
PurgePassage Overheat at ____
Wing Heat light goes out at at ____
160 degrees
230 Degrees
Airspeed
Green pointer is what speed
Max LOD, VSO 1.3
AOA Top of red is
1.1 VSO
Chapter 2 Section 22
REF speeds
Flaps 0 -
Flaps 15 -
Flaps 35 -
Ref +30
Ref +20
Ref +10
Half bank below this
Goodyear Standby is Driven by what?
It is self contained
HSI is driven by:
Standby ILS source is:
AHRS2
Nav1
How to turn on Wx radar on the ground:
Hit Stab 4xs
Turbulance penetration Speed
180kts
Hydraulics will flash after ___seconds meaning ____
40
Still pressurized
Stab gets it’s information from :
Standby Static System
Ground idle light comes on after __ seconds after touch down
8
In freezing conditions power should be brought up every ____ minutes for ____ seconds
4 minutes
15 seconds
Pressurization
To check Manual mode on the ground power must be at __%N2
This must be checked prior to dispatch in ISOBARIC mode
60
Low Brake Pressure comes on at what PSI
900
Speedbrakes retract with throttle at __ position
80%
Engine Start: must have N1 rotation by
25% N2
IF APU fail light is on, what is likely to have happened
Fire Bottle empy/low
ECU Fail
- QRC - EVACTUATION
“EVACTUATION QRC”
PARK BRAKE. LP. SET
Thrust Levers CUT OFF
LH & RH Engine Fire. Press
If fire present
BOTTLE 1&2 ARMED PUSH Press
APU MASTER Off
BATT. OFF
EVACTUATION. INITIATE