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273 Cards in this Set
- Front
- Back
What is max take off weight?
|
13870 lbs
|
|
What are the engines on the cj3?
|
2x Williams FJ 44-3a
|
|
How much thrust does each engine produce?
|
2780 lbs
|
|
What anti-ice / De-ice systems does the airplane have on it?
|
* Engine, Windshield and Wing Bleed Air Anit-Ice
*Horizontal Stabil. Pneumatic Boot *Pitot-Static System & AOA Vane Electric Anti-Ice |
|
What does EGPWS stand for?
|
Enhanced
Ground Proximity Warning System |
|
What is described as an engine cycle?
|
Any operation involving;
Start Power to 80% N1 or above Shutdown |
|
Describe the Hydraulic System?
|
2 x Engine driven pumps supply hydraulic pressure.
Hydraulic Reservoir is located in fuselage, aft of right wing. Separate Electric pump for separate system with reservoir in right side nose compartment |
|
What components are operated by the Hydraulic System?
|
The Landing Gear
Flaps Speed Brakes Hydraulic from Electric Pump (separate sys.): Wheel Brakes |
|
When the amber DOOR SEAL light illuminates, what does this indicate?
|
The primary door seal failure and pressure falling below 5.5psi above cabin pressure.
|
|
Give a brief explanation of the Electrical System.
|
Main DC buses supplied from 2 x 28 Volt Starter/Generators, w/max output of 300 amps.
Engine start and secondary DC power available from a 44 amp/hr Battery or External. |
|
Where is Cabin Pressurization supplied from?
|
Bleed air from engines, conditioned by pre-coolers and heat exchangers. Maintains 8000ft cabin press. at FL450
|
|
What are the aircrafts basic dimensions?
|
Wingspan - 53 ft
Length - 51 ft Height - 15 ft Wheel Base - 16 ft |
|
What is the oil capacity for each engine/
|
4.37 Quarts
|
|
Total Usable Fuel?
|
4710 Lbs - 698 Gals
|
|
Hydraulic Fluid reservoir capacity?
|
2 Litres / 2.3 quarts
|
|
Oxygen System capacity?
|
50 Cubic Foot Bottle
1600 -1800 PSI Charge, regulated for 70 psi for usage. |
|
Max Ramp Weight?
|
14,070 lbs
|
|
Max Landing Weight?
|
12,750 lbs
|
|
Max Zero Fuel Weight?
|
10,510 lbs
|
|
What are the limits for Take Off Thrust setting?
|
5 Minutes for two operating engines
* for one engine inoperative may be used for 10 mins. |
|
Max ITT for engine starting?
|
0-15 secs - 1000 degC
15-30 sec - 900 deg C 30-40 sec - 840 deg C |
|
The engine should not be operated above 80% N2 until oil temp is above...?
|
10 degC / 50 deg F
|
|
Max ITT for the following settings?
1. Takeoff Thrust 2. Max Cont Thrust |
1. 877 max
2. 840 max |
|
What are the N2 RPM limits for;
1. Gnd Idle 2. Flt Idle 3. Take Off 4. Max Cont Thr. 5. Transient |
1. 53.4 min
2. 60.7 min 3. 100.0 max 4. 100.0 max 5. 100.7 max 20 secs |
|
N1 RPM limits for the following:
1. Take off 2. Max Continuous 3. Transient |
1. 102.8
2. 102.8 3. 103.9 max 20 secs |
|
What are the ITT limits (not incl. start/shutdown)?
|
0-10 secs - 891 degC
10s-5 mins - 877 degC 5-10mi - 840 cont |
|
Max tailwind component for engine start?
|
12 knots
|
|
Max cross wind component for engine start?
|
16 knots
|
|
Max time to light off (start)?
|
10 secs
|
|
Min Oil Temp for engine start?
|
-40 degC as indicated on the EIS
|
|
When is a battery pre-heat reqd?
|
If the battery is cold soaked in temps below 0 degF for 2 hours or longer.
|
|
Minimum Battery Voltage for start?
|
24 V dc
|
|
Max airport elevation for batt/gpu start?
|
14,000 for both
|
|
Min/Max GPU current capacity for start?
|
800/1100 amps
|
|
Normal starter current draw is?
|
approx 1000 amperes
|
|
What are the engine starter cycle limitations?
|
3 start within a 30 min period.
60 seconds between each cycle. **if using batt. to start then 3 starts per hour. |
|
Pitot/Static heat and AOA heat is limited on the ground to?
|
2 mins max
|
|
Max approved fuel imbalance?
|
200 lbs.
600 lbs demonstrated for emergency. |
|
What action is required if the FUEL LOW LEVEL L or R illuminates or observed fuel is less than 220 lbs?
|
Fuel Boost Pumps must be turned on.
|
|
Max Operating Speed limits..
1. Mmo above 29,300ft 2. Vmo btwn 8000 & 29,300ft 3. Vmo below 8000ft |
1. 0.737 Mach
2. 278 KIAS 3. 260 KIAS |
|
What is the aircrafts Va?
|
Maneuvering speed:
between 155 and 208 KIAS depending on conditions |
|
What is the Vfe?
|
T/O ad App - 200 KIAS
Land - 161 KIAS |
|
Max speed with the flaps failed to ground flaps (55deg)?
|
140 KIAS
|
|
What is the Vle?
|
Extended speed gear - 200KIAS
|
|
What is the Vlo?
|
200 KIAS up and down
|
|
What is Vsb?
|
Max Speed Brake limit
No Limit |
|
Max Altitude for TO and Land?
|
14,000 feet
|
|
Max Tailwind component for TO and Land?
|
10 Knots
|
|
Min ambient temp for TO and Land?
|
-53 degC / -65 degF
|
|
What is the max operating altitude?
|
45,000 feet
|
|
Max Take off / Landing altitude?
|
14,000 feet
|
|
Max Engine start altitude?
|
14,000 feet for both Battery and Gpu
|
|
Max (RAT) for Take off / Landing?
|
ISA + 39 deg c
|
|
Minimum ambient temp for start?
|
- 53 C
|
|
What is the minimum engine start temp for a cold soaked aircraft?
|
- 40C (soaked for 2 hours)
|
|
Max tail wind component for engine start?
|
12 knots
|
|
Max cross wind component for engine start?
|
16 knots
|
|
Max Engine ITT for start?
|
1000 C for 15 secs max
|
|
Max Engine ITT for Take off?
|
877 C
5 mins for 2 engines 10 mins for 1 engine |
|
Max Engine ITT for Flight?
|
840 C (MCT)
|
|
What is the max allowed time for engine light off - start sequence?
|
10 seconds
|
|
What is minimum N2 required for start?
|
8%
|
|
At what N2 does the start sequence end?
|
45%
|
|
What N2 will be observed at flight idle with the anti-ice on?
|
70%
|
|
What is normal N2 at flight idle?
|
60.7%
+/- 2.5% |
|
What is the max allowed N2 for Max continuous ops?
|
100%
|
|
What is the nose gear tire pressure?
|
125 psi
+/- 5 |
|
What is the main landing gear tire pressure?
|
137 psi
+/- 3 |
|
Is it acceptable to have two different brands of tire for the main landing gear?
|
No
|
|
How long after you turn on the battery master switch is acceptable before switching it off and why?
|
20 secs...
Not to interrupt FADEC self test |
|
What is the aircraft demonstrated cross wind component?
|
25 knots
|
|
After take off or a go around, what is the minimum altitude the auto pilot can be engaged?
|
350 feet agl
|
|
On an ILS approach, what minimum altitude can the auto pilot be operating until?
|
180 feet agl
|
|
On a non precision approach, at what altitude must the auto pilot be de-activated?
|
350 feet agl
|
|
At what minimum cruising altitude can the auto pilot be used?
|
1000 ft agl
|
|
What surfaces must the aircraft be operated on?
|
Paved surfaces only
|
|
Can the cabin be pressurized for Take off and Landing
|
No, must be de-pressurized
|
|
What position must the yaw damper and autopilot switchs be in for Take off and Landing?
|
Off position
|
|
Can the Engine Synchronizer be on for Take off and Landing
|
No
|
|
Are you allowed to depart with the Anti Skid inop?
|
No. Any Take off is PROHIBITED with it inop.
|
|
What is the minimum temperature that the tail de-ice boots can be operated?
|
-35c RAT
|
|
How long after landing before engine shut down?
|
2 mins with the ITT stabilized
|
|
How long prior to engine shut down does the engine anti-ice need to be off for?
|
2 minutes
|
|
Speed brakes must be retracted at what altitude prior to landing?
|
50 feet
|
|
What items are included on the Hot Battery Bus?
|
Lights (baggage and exit)
ELT Voltmeter Emergency Lighting Emergency Battery Pack |
|
How long will the Standby Flight Display run for on it's own internal battery?
|
88 mins
|
|
What items are on the Emergency Battery Bus?
|
L & R Standby N1
Comm 1 Nav and DME 1 FMS 2 (GPS 500) Tranx 1 Audio panels 1&2 AHRS 2 RTU 1&2 RIU L-B Flood Lights Stby ADC STBY Pitot Heat Co-pilot Pitot Static Heat ADC 2 Voltmeter Flap Control Gear and Hydraulic Control Gear lights/horn |
|
MEMORY ITEM
Engine Fail or Fire below V1 |
Brakes - As reqd
Throttles - Idle Spd Brakes - Extend |
|
MEMORY ITEM
Engine Fail or Fire above V1 |
Maint. Directional Control
Airspeed - Accel to Vr Rotate at - Vr, climb at V2 Landing Gear - Pos. rate/ gr up Wing Xflow switch - XFLOW Flaps - Retract at 1500ft min & accel to V2+10 |
|
MEMORY ITEM
Engine Fail during Final |
Thrust - INCREASE (as reqd)
Airspeed - VAPP Flaps - T/O APP |
|
MEMORY ITEM
Engine Fire LH or RH |
Throttle - IDLE (affected eng)
IF LIGHT REMAINS ILLUMINATE Engine Fire Button - LIFT AND PUSH Bottle Armed Button - PUSH |
|
MEMORY ITEM
Emergency Restart - Two Engines |
L/R Fuel Boost - BOTH ON
Throttles - OFF then IDLE (24% N2 max) If Altitude allows - INCREASE AIRSPEED TO 230 KTS |
|
MEMORY ITEM
Electrical Fire or Smoke or Environment System Smoke |
Oxygen Mask - DON and EMER
Mic Select - MIC OXY MASK |
|
MEMORY ITEM
Cabin Altitude / Cabin Decompress |
Oxygen Mask - DON & 100%
Mic Select - MIC OXY MASK Emergency Des - AS REQD Pass Oxygen - ENSURE RECEIVING |
|
MEMORY ITEM
Emergency Descent |
AP Trim Disc - PRESS/RELEASE
Throttles - IDLE Speed Brakes - EXTEND Pitch Attitude - INITIAL 7.5 deg THEN ADJUST |
|
MEMORY ITEM
Battery Overtemp |
Volt/Amp - NOTE
Battery Switch - EMER Volt/Amp - NOTE DECREASE |
|
MEMORY ITEM
Autopilot Malfunction |
AP Trim Disc - PRESS/RELEASE
|
|
MEMORY ITEM
Electric Elevator Trim Runaway |
AP Trim Disc - PRESS/RELEASE
Throttles - AS REQD Speed Brakes - AS RQD Manual Elev Trim - AS RQD Pitch Trim CB - PULL (left side) |
|
What is the Mmo (above 29,300ft)
|
0.737 m
|
|
What is the Vmo (8000 - 29300)
|
278 kias
|
|
What is the Vmo (below 8000)
|
260 kias
|
|
Max autopilot speed?
|
0.737m / 278 kias
|
|
What is Vfe?
15 deg 35 deg |
15 - 200 kias
35 - 161 kias |
|
Max Speed when flaps fail to ground?
|
140 kias
|
|
Max tire speed?
|
165 kts
|
|
Min speed in sustained icing and/or turbulent air penetration?
|
180 kias
|
|
What is Vmcg?
|
Minimum control ground - 89 kts
|
|
What is Vmca?
|
Min control airspeed -
88 @ flaps 0 81 @ flaps 15 |
|
Max landing weight?
|
12,750 lbs
|
|
Max zero fuel weight?
|
10,510 lbs
|
|
Max oil consumption per engine?
|
0.1 quart per hr or 1 quart every ten hours
|
|
Minimum Battery Voltage for start?
|
24 V
|
|
Max number of battery starts in a 60 min period?
|
3 battery starts an hour
|
|
A generator assisted start is equal to..?
|
1/3rd of a battery start
|
|
a GPU / EPU start is equal to...
|
0 Battery start
|
|
What are the starter limitations?
|
3 starts per 30 mins with 60 seconds rest in between
|
|
What is the max amperage on the ground?
|
200 amps
|
|
For flight below Fl 410 what is the max amperage continuous?
|
300 amps
|
|
For flight above Fl 410 what is the max continuous amperage?
|
250 amps
|
|
How long can you fly with T/O power set? What is max temp allowed for T/O power
|
877 deg
5 mins with 2 engines 10 minutes with 1 engine |
|
Min N2 for effective anti-ice?
|
75%
|
|
When you experience a dual generator failure, and the Battery switch is ON, how long will battery last for?
|
10 mins with everything powered.
|
|
When the Battery is selected to EMER - how long will Battery last for?
|
30 mins
|
|
What is the minimum temperature for operation of the tai de-ice boots?
|
-35 deg C indicated RAT
|
|
How long must engine ITT values stabilize for after landing prior to shut down?
|
2 mins
|
|
How long does the Engine Anti-ice need to be off for prior to shut down?
|
Min 2 mins to avoid FADEC fault due to PT2/TT2 tube not cooled.
|
|
Speed brakes must be retracted prior to what altitude before landing?
|
50 feet
|
|
If you experience a dual engine failure in flight, what minimum airspeed will you need to get to prior to starting?
|
230 KIAS
|
|
Is the AOA warning rotary test required prior to flight?
|
Yes - mandatory
|
|
When the Battery Over Temp Annunciator illuminates what is the temp?
|
> 145 deg
|
|
When both the BATT OTEMP and > 165 annunciator illuminates what is it indicating?
|
Battery temp has now reached > 160 deg
|
|
When the fuel low level light illuminates, what does it mean?
|
Fuel in the specific side is at 190 lbs +/- 20
|
|
If the primary door seal fails, what are the limitations?
|
Max 31,000 ft
|
|
What supplies pressure to the door seals for pressurization?
|
23 psi Service Bleed Air
|
|
What are the baggage compartment weight limits?
Nose Tail Aft Cabin |
Nose - 400 lb
Tail - 600 lb Aft Cabin - 100 lb |
|
Why is there no heating element for the fuel vents?
|
They are aerodynamically heated through design
|
|
What are the GCU's and what do they provide?
|
Generator Control Units
Provide: Start regulation Over Voltage protection Under Voltage protection |
|
With the loss of Normal DC electrical power, what valves fail to the close position?
|
Fuel Transfer Valve
Emergency Pressurization Valve Wing Ice X Flow valve |
|
With the loss of Normal DC power, what valves fail open?
|
Engine Anti Ice
Wing Anti Ice Windshield Bleed Air Air source fails to Both |
|
Is it acceptable to X-Gen start an engine on the ground?
|
Yes
|
|
Is it acceptable to X-Gen start an engine in the air?
|
It isn't possible, left squat switch
Concern of power spike from generator to avionics. |
|
How are the flight controls operated?
|
Through a series of:
Cables Pulleys Bell cranks etc |
|
What does the Rudder Bias do?
|
It assists the pilot with maintaining heading control when an engine failure occurs.
|
|
How does the Rudder Bias system work?
|
Engine bleed air is piped to provide equal pressure either side of rudder system in normal ops.
When an engine fails, that side blees air stops, allowing the operating engines B/A to provide pressure to the rudder system to aid directional control |
|
What holds the speed brakes up in the extended position?
|
Hydraulic pressure
|
|
If during flight with the speed brakes extended, you lose electrical, what happens to the speed brakes?
|
Speed Brake Hydraulic valve fails to open releasing the pressure, blowing the speed brakes to close
|
|
With the speed brakes extended, what power setting will automatically close them?
|
> 85% N2 setting
|
|
In order to fly single pilot in this aircraft, what is required?
|
Airspeed bugs set
Charts / Checklist Autopilot Storage (for charts) Headset with Mic |
|
If the BATT selector is moved to the EMER position, will there be a VOLTS read out?
|
Yes it's connected to the EMER Bus
|
|
Inside the engine, there is a Shaft Separation Detection Device, what does this do?
|
Detects the onset of failure of the N2 drive shaft and will shut down the engine by closing a plunger valve shutting off the fuel
|
|
Is the N2 high or low pressure?
|
High pressure Turbine, high compression centrifuge
|
|
Does the engine use fuel nozzles or a slinger to deliver fuel - why?
|
Slinger - more reliable
|
|
If the Fuel Low Press light illuminates on the annunciator panel, what is the fuel pressure?
|
< 5 psi
|
|
With the ignition in the NORM position, when do the ignitors turn on and what commands them?
|
FADEC will turn on the ignitors when necessary:
Start Engine Anti Ice on Take off Landing |
|
Service Air from the Hi Pressure Bleed Air system provides what psi and to what elements?
|
23 psi
Door seal Tail de-ice boots Hydraulic Pump Cabin air |
|
How do the FADECs continue to run in the event of complete electrical failure?
|
Permanent Magnet Alternators (PMA's) mounted on the fuel delivery units provide FADEC power in this event.
|
|
When the FADEC RESET is pressed, what is happening?
|
A full FADEC Reboot
|
|
When should an engine start be aborted?
|
False Start - No ITT/Fflow
Hot Start - ITT >1000 No N1 rotation by 12 % N2 Hung Start - Starter no disengage |
|
If during start, the engine ITT runs over 1000 deg, what should the pilot do in order to aid maintenance determine the appropriate action to take?
|
Note what VALUE did the temp get to and how LONG was it there for?
|
|
For engine failure in flight, what are the air start limitations?
|
with starter assist:
Descend to Max 25,000 ft If possible, increase speed to 200 kias. If Windmill Start only: Descend to Maximum 15,000 ft Increase speed to Min 230 kias |
|
What stall indications does the aircraft have?
|
AOA Indicator
Stick Shaker Stall Strips Airspeed Indicator Vortex Generators |
|
What is the aircraft Va?
|
Max maneuvering speed - 180 KIAS
|
|
What is the Max Altitude for the gear and flaps to lowered?
|
18,000 ft
|
|
With the Yaw Damper inoperative, what is the max operating altitude?
|
FL 300
Autopilot will not work with YD inop |
|
Describe the Hydraulic System
|
It's an Open Center System
Less Fluid Rqd produces less heat Less back up rqd runs at 60 psi unless a demand is placed then up to 1500 psi for short period |
|
How many Hydraulic pumps are there?
|
2 total, 1 each engine
|
|
There is 1 hydraulic fluid reservoir, how much fluid will it hold?
|
2.2 quarts
|
|
Describe how the Anti-Skid system works?
|
Transducer sends a frequency from each wheel hub
Control unit monitors both frequencies When it senses different freqs (different wheel rotation speed) then it adjusts brake pressure to avoid skid |
|
What will happen if a pilot lands the aircraft with their feet on the brakes?
|
There is touchdown protection built in.
keeps brakes off for 3 secs and upto 59kts of wheel rotation |
|
Can the anti skid be turned on while taxying out to the runway?
|
NO - must be stationary as brakes will not operate while anti-skid runs through self test
|
|
How much should you extend your required landing distance when you're forced to use the EMER BRAKE?
|
increase by 70%
|
|
With the Anti-skid inop, how much should you increase your landing distance?
|
Increase by 40%
|
|
What Anti-Ice / De-Ice systems does the airplane have?
|
De-ice boots on tail (23psi B/A)
Pitot/Static and AOA Vane Anti Ice Windshield B/A anrti-ice Backup windshield Alcohol (isopropyl for 10 mins) Wing and Pylon inlet B/A anti-ice Engine anti-ice and PT2/TT2 electric probe Engin |
|
When the windshield bleed air system is to be used, what limitations does it have?
|
Switch to LOW when >-18 deg C
Switch to HI when < -18 deg C |
|
When the tail de-ice boot cycle is on AUTO, what is the cycle times?
|
Left side 6 secs on, then 6 secs off, right side 6 secs on then 2:42 off.
3 min total cycle |
|
When the Tail de-ice boot switch is on MAN, what happens?
|
Boots inflate while switch held down and deflate when switch released
|
|
What is the ground limitation for the wing anti-ice use?
|
When the WING ICE light goes out, run for maximum of 1 minute so the wings don't get destroyed
|
|
When you lose normal DC power, what position do the windshield and wing anti ice valves fail in
|
They will fail to open
|
|
Icing conditions will occur when?
|
<10 deg C RAT and flight in visible moisture
and also when on ground less than 3/4 sm visibility. When on ground, slush, snow pick up is also a factor |
|
What is the minimum speed for flight in sustained icing?
|
180 KIAS unless on approach to land
|
|
What conditions will sound the Gear Horn?
|
< 130 KIAS
> 15 deg Flap - Can not silence |
|
What items are on the gear squat switches?
|
ADC's
Enviro System - compute climb Gear Handle Solenoid Anti-skid X gen start in flight Grnd Flaps Annunciator Stick shaker |
|
How do you lower the gear when the primary system fails?
|
Reduce airspeed < 200 kts
Pull T-handle to release up locks Rotate handle 45 degrees Pull collar to release nitrogen to blow gear down |
|
If you blow the gear down with the nitrogen, will there be enough pressure left in the tank if the EMER Brakes need to be used?
|
There should be enough
|
|
Which ELEC BUS is the Landing Gear Control on?
|
EMER BUS
|
|
During pre-flight and prior to turning on the battery power, where will the power brake accumulator charge be at?
|
In the light green pre-charge and then in the dark green charged section after battery power has been applied to charge the pressure
|
|
What will the brake fluid sight gauges show during the pre-flight before and after battery power?
|
Before battery power, both indicators show fluid.
After battery power, bottom full and top indicator almost empty as system is charged |
|
Nose tire pressure
Main tire pressure |
Nose - 125 psi +/-5
Main - 137 psi +/- 3 |
|
How many fuel drains are there?
|
10 total
3 each side of outer fuselage 2 each wing |
|
How many static wicks are required for flight?
|
Only 2 total can be missing, 1 per separate control surface
|
|
When fresh air is drawn in to the cabin is it pressurized?
|
No
|
|
When should the Fuel Boost Pumps come on, when in NORM position
|
During Engine Start
During Fuel Transfer When Low Level is detected |
|
Are you required to put prist in the aircraft when putting fuel on board?
|
No - The fuel / Oil heat exchangers sufficiently heat the fuel
|
|
When is the cabin temperature sensor?
|
Aft of the cabin by the floor on the aft bulkhead
|
|
Inside the cabin - where does the heat come from and where does the cool air come from?
|
Heat through the floor vents
Air conditioned cool air through flood vents and ceiling wemacs |
|
Is a first aid kit required on the aircraft
|
Yes
|
|
If the GPU is hooked up to the aircraft but the battery is physically disconnected, will you receive any power in the cockpit when the BATT is turned on
|
YES, the GPU will bypass.. MUST double check the BATT is connected, you can start engine and fly with BATT disconnected
|
|
What is the Max ambient temperature allowed for engine start?
|
ISA + 39 deg
|
|
What is the minimum allowable ambient temperature for T/O and Landing?
|
- 53 deg C
|
|
Name the 4 ways the Emergency Lighting can be turned on?
|
Switch by pilots knees
Auto after 5 g load Passenger Safety Switch Loss of DC power |
|
What lights make up the Emergency Lighting system?
|
2 x "Shark" lights on the right wing
2 x Emergency Exit lit signs by exits 1 x Ceiling light by main entrance to illuminate |
|
What items are secured when the Control Lock is engaged?
|
All flight controls to center/neutral
Throttles to cut-off |
|
What are the tow limits for the nose wheel when the control lock in the cockpit is ENGAGED?
|
60 degrees either side of center
|
|
What are the tow limits for the nose wheel when the control lock in the cockpit is NOT engaged?
|
95 degrees either side of center
|
|
Under what circumstances will the FLAP >35 deg annunciator illuminate?
|
On the Ground when flaps are down > than 35 deg and the power is set above 85%
In the Air with the flaps failed at more than 35 deg. for more than 8 seconds |
|
Under what circumstances will the stick shaker activate?
|
When on the ground in test mode
In the air, when airspeed is within 8-10% of stall speed |
|
Other than when it is in test mode, can the stick shaker activate when on the ground?
|
No, when not being tested, the gear squat switch de-activates, only activates when there is no w-o-w.
|
|
What items are part of the accessory gear box on each engine?
|
FDU
Hydraulic Pump Starter/Generator Fuel Pump Oil Pump |
|
At what pressure does the Low Oil Pressure warning come on?
|
When the oil pressure drops to 25 psi
|
|
MEMORY ITEM
Emergency Restart of Two Engines.. |
L/R Boost Pumps - BOTH ON
Throttles - OFF THEN BOTH IDLE (max N2 24%) If Alt Allows - INCREASE AIRSPEED TO 230 KIAS |
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What type of Engine Oil is usable?
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Mobil Jet II
Mobil Jet 254 |
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Why is ground idle system installed on the airplane?
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It recognizes when the aircraft is on the ground through the squat switch.
When power is at idle on gnd, it reduces idle thrust to a low setting, this helps to not need thrust attenuators like other cj models. |
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When on the ground and the throttles are in idle, the ground idle annunciator is on, showing it is working, what N2 value can be expected?
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around 57% N2
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Where is the Pitch Trim Circuit Breaker located?
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Left Circuit Breaker Panel
From the bottom row forward, go up one row and back three CB's |
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When the Battery is connected in the aft compartment, what, Bus is powered prior to the BATT switch being turned on?
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Hot Battery Bus
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What is the Ampere output of the generators?
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300 amperes
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What is a basic description of how the Williams FJ44-3a engine operates?
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Medium bypass, single stage fan design, single stage centrifugal hi pressure, driven by a single stage uncooled high pressure (HP) turbine. FADEC Controlled.
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When both Generators fail, does it trigger the Master Warning (RED) light?
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Yes
Only Master Caution for Single Gen Failure |
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If the GCU (Generator Control Unit) recognizes a fault or problem with the generator power/output, what does it do?
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The GCU will take its respective (l or r) generator offline.
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You have a dual generator in flight, what is the appropriate action prior to resetting one or both generators?
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Check the voltage of each Gen by switching VOL SEL switch to determine if one or both are faulting
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Can you depart with a Battery Over Temp?
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NO
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For Battery Limitations - How many Battery Starts are allowed in a 60 min (1 hr) period?
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3 max
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For Starter Limitations - How many starts in a 60 min (1hr) period?
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3 starts allowed in 30 mins with min. 1 min rest periods in between each start attempt
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For the Avionics - what does the term IAPS mean?
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Integrated
Avionics Processing System |
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What does the avionics IAPS do?
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Computes all of the data from the ADC, AHC, FADEC, ECU, FDU before translating and displaying
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Can a pilot depart under single pilot operations with the copilots PFD inop?
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No all three screens (PFD's and MFD) must be operating
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The autopilot is PROHIBITED for use with VOR approaches when what situation occurs?
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PROHIBITED when the VOR station is positioned 15 miles or more behind the airplane at any time during the approach
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if on an ADF approach, do you have to continuously monitor the ADF Morse Freq?
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No, if you are receiving a signal from the station, the ADF pointer will be displayed on the PFD, so you can continue the approach
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If on final approach to land, you realize that you have not set your V-speeds into your PFD, what is the best action?
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Continue the approach using the Green Donut as reference to your app speed
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After departing, at what speed will the departure V-speed be removed from the airspeed tape on the PFD?
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once the aircraft passes 200 KIAS, (careful if not exceeding 200 kts when single engine coming back around to land)
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If you want to set v-speeds for take off, what page would you go to using the DCP (display control panel)
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Refs page 1
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If you want to set v-speed for approach, what page would you go to?
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Refs page 2
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What page on the PFD would you go to if you want to set RA or BARO alt for approach?
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Refs page 3
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What page on the PFD would you access to change the HPA to Inches and the Transition Alt/Transition Lvl?
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Refs page 3
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Is your aircraft certified for Category II approaches?
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No
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Can the autopilot be used in severe icing conditions?
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No
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Minimum flight weight?
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8160 lbs
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What is the aircrafts demonstrated cross wind component?
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25 kts, not a limitation
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What is the maximum allowable contamination on the runway (slush/standing water)
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0.75 inches
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What is the maximum pressure differenatial?
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8.9 psid
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Continuous use of aircraft supplemental oxygen is not permitted about what altitude... with / without passengers?
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with - 25,000 ft
without - 40,000ft (w/eros) |
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When must the ground idle switch be turned on?
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When performing touch and go's
When operating on the ground with the engine anti-ice on |
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What portion of the engine is the fire detection system wrapped around?
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The N2 section
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How many engine fire extinguishing bottles are there and where are they located?
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2 located in the tail cone section
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How are you supposed to check the fire bottle charge pressure for flight?
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Check the placard in rear of aircraft with matching outside air temp.
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When you press the L or R fire light, what annunciator illuminations can you expect to see?
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Gen L or R
Hyd Press L or R Fuel Press L or R |
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Does a cross generator start count towards a battery start?
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yes 1/3 of a Batt Start
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What is the Voltage rating in the electrical system?
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29 volts
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What is the purpose of the battery disconnect switch?
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To electronically disconnect Battery.
In event of Battery Over temp In event of Stuck Starter |
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What items are on the Hot Battery Bus?
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Volt meter
Nose and Tail baggage lights Emergency Lights |
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What items are on the Emergency Battery Bus?
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Voltmeter
N1 indicator Comm 1 Nav 1 RTU 1 / Stdby HSI Floodlights Stdby flt. display Emergency Lighting Landing Gear Control Flaps Stdby pitot static heat Both audio panels Garmin 500 (FMS 2) |
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When do the fuel boost pumps come on when the switches are in normal?
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Start
X - feed Fuel Low pressure |
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If you get Type 4 anti-ice solution sprayed on the aircraft at an FBO, what is Cessna's recommendation regarding aircraft configuration on take off?
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Cessna recommends to take off with flaps 0
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What protects the fuel in the wings against the hot air passing through the leading edge for ice protection?
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Purge air from a small inlet hole by the wing root passes cool air between the hot bleed air and the fuel tank and gets expelled with the bleed air through a wing tip vent.
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Which aileron is the aileron trim tab on?
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Left Aileron
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Prior to Maneuvers Acronym
I C C E Y |
Ignitions ON
Computations VREF Clearing Turns COMPLETE Engine Sync OFF Yaw Damp OFF |
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What are the 5 items that limit Take off Weight?
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Max Gross Take Off Weight
Balanced Field Length 2nd Segment Climb Gradient Obstacle Clearance Req Vbke brake energy limit |
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What FAR's is the CE-525 certified under?
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Part 23 Commuter
Part 36 Noise Requirements |
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Can you fly the CJ and Cj-1 on the 525 type rating?
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Yes you can fly all of the 525 series
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Is the Pro Line 21 operators guide required on the aircraft for flight?
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Yes
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When is the most appropriate time to check the engine oil level to ensure correct reading?
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10 minutes after shut down
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With regard to circuit breakers, what is the definition for CHECK/RESET and just RESET
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CHECK/RESET - Check the CB, if it is in then leave it, if it is out then reset.
RESET - If it is in, then pull and reset, if it is out then reset. Both scenarios - 1 rest max |
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What indications in the cockpit display an Oil Filter Bypass?
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No cockpit Indication.
The oil filter bypass press indicator is checked on pre-flight |
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What does it mean when the annunciator panel Tail De-Ice Fail light illuminates?
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It means the Tail De-ice Timer has failed
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What is the cabin temperature limitations for the passenger oxygen masks?
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Must be at or above 0 deg C for 20 minutes after aircraft has been cold soaked for 2+hours
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When flying at night, how do you know when there is ice forming on the aircraft?
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By using the left wind inspection light and the windshield ice detector lights
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Will the passenger oxygen masks deploy automatically?
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Yes, if the Oxygen Control Valve is in Normal and cabin altitude exceeds 14,500ft. There must be DC power available.
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How does the emergency brake system work?
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It uses nitrogen from the emergency air bottle.
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What precautions should you take while using the emergency brakes?
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There's NO anti-skid protection.
There's limited use due to amount of air. Keep feet of pedals and don't taxi to the ramp |
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What are the three pressurization modes for the pressure controller?
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Auto - Digital controller schedule functioning, enter destination alt
Isobaric - Air Data sensor fail, Yellow light, pilot inputs Cruise and land data Manual - Total pressurization fail, manually control cabin alt |
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What switches turn on the AC compressor?
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AC to auto and Defog fan
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What is the temp range for the auto temperature control?
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65 - 85 deg F
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What do you do if the PILOTS PFD goes blank?
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Use the REV switch to move display to the MFD
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