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41 Cards in this Set
- Front
- Back
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Trim Interrupts - where it is, difference between that and the disconnect. |
-On the control stick, right hand side. -Push and hold trim interrupt to disconnect the trim systems. -Pressing this also disconnects TAD, which stays off when released. |
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Speed Brake Operation |
-Retracts with PCL max, or if flaps set to TO or LDG -Wont extend if flaps down -Controlled by PCL Thumb rocker, 3 position spring centred -Electrically activated, Hydraulically powered, mechanically operated. |
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TAD - how it operates, and what inputs it uses |
-Trim Aid Device -Pitch rate, torque, airspeed, altitude all inputs -Affects rudder ONLY -Only an assistant/aid, A/C will still require pilot input |
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Ground trim tabs |
-Located just inboard of ailerons -Adjusted by maintenance pers. on the ground -Assist in straight and level flight |
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Fuel Autobalancing System and related CAS messages |
-Autobalances normally to within 20lbs in each wing. -If imbalance more than 20lbs for 30 secs stops flow from light tank. -If imbalance is more than 30lbs for more than 120 secs, then FUEL BAL CAS caution, autobalance system shuts off, MASTER CAUT, aural tone. -Autobalance system can be reset by toggling auto/manual/auto to reset to try for another 120 seconds to correct imbalance. Can be reset multiple times. |
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Fuel Boost Pump operation and CAS Message |
Operates if: -Less than 10psi in motive fuel flow line -On startup -Manually toggling the system on CAS message: Green BOOST PUMP advisory |
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Fuel Quantity Indications |
-Bars go yellow at 150lbs per tank -Bars beneath 110lbs per talk trigger FUEL LO L, FUEL LO R in amber, MASTER CAUT, aural tone -Collector tank volume split between wing tanks. |
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Generator, how it's controlled, indications of failure and CAS messages |
-Controlled by GCU in rear cockpit -Switches to turn on/off electrically interlocked and magnetically held. Turning one on turns the other off, but not vice versa. Control held by the ON switch. -Gen failure indicated by red GEN on CAS, MASTER WARN, aural warning, voltage drop, negative ampage. |
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Gen Bus failure indications |
-MASTER WARN, MASTER CAUTION plus aural tone -CAS Warnings: GEN BUS, EDM Fail, ADC Fail, IRS Fail, FUEL fail, TAD Fail, TAD OFF, ANTI ICE -Loss of left MFD |
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What runs off HOT BATT BUS |
-Ram Air Valve -Clocks -ELT -Battery -OBOGS -Emergency Flaps -FDR Maintenance -Chip Detector |
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What runs off the AUX Battery |
-BFI -Radio relays (transponder/transceiver) -Intertial reference unit -Standby VHF Control -Fire 1 |
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How to adjust MFD Brightness? |
Rocker switches on the middle of the top and bottom of the bezel. |
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Oil Pressure Limits and CAS Messages |
Message is OIL PX, colour varies At Idle: 15-40psi will trigger Amber 15-40psi for 5s will trigger Amber and Red <15psi will trigger Red Above Idle: 40-90psi for 10s will trigger Amber <40psi will trigger Red |
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Oil Pressure Limits and CAS Messages |
Message is OIL PX, colour varies At Idle: 15-40psi will trigger Amber 15-40psi for 5s will trigger Amber and Red <15psi will trigger Red Above Idle: 40-90psi for 10s will trigger Amber <40psi will trigger Red |
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Prop component that control blade angle and speed automatically |
Power Management Unit and Propeller Interface Unit |
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Mechanical Governer limits with PMU on |
106% NP will turn red over 102%. |
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Prop feathering in regards to oil pressure |
If oil pressure is dumped due to PCL off (which activates dump solenoid valve), feathering spring will rotate the prop back to feathered position. |
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PMU is powered by the |
PMA (T-6C FM Pg 1-17) |
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N1 gauge limits |
PMU On: Min 60-61% Ground/67% Flying Max 104%
PMU Off: Min 67% Max 104%(?) |
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When does the HYD FLUID LO message appear on CAS? |
When hydraulic fluid levels reach lower than 1 quart |
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Give two scenarios of the situations when you would use the emergency gear extension procedure |
-Battery bus failure -Engine failure -Primary hydraulics failure |
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Where to check the brake reservoir fluid level |
To the left and rear of the front seat ejector rails. Indicator on top of the filler plug. |
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Flap operation in regards to power loss |
A fail-safe selector valve will cause retraction of the flaps in an electrical outage |
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Hydraulic reservoir inspection panel - what we are looking for, and what to do if it's wrong. |
Below the cockpit, right hand side. Should be between the lines for AC & AD. Pull the discharge handle if indicator is between the desired points. |
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Switches and valves for bleed air into the cockpit. |
Controlled by Defog (ON/OFF) and Bleed Air (HI, NORM, OFF). Bilevel flow control and shut off valve, bilevel flow control bypass valve, heat exchanger bypass valve, firewall shutoff valve. |
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What three things does the defog switch do? |
1) the defog valve (bilevel flow control bypass valve) is opened increasing the bleed air supply 2) inflow valve is automatically set to high, further increasing amount of bleed air entering cockpit 3) air conditioning compressor is automatically turned on to dry the air |
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Do you stay pressurized if you lose electrics? |
No, the dump valve solenoid becomes denergised, opening the valve fully, venting the pressure. |
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How to get max Ram Air in flight? |
Guarded pressurization switch to RAM/DUMP and Ram Air to HI |
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Simple overview of temperature control process |
Heat exchanger takes bleed air from the right hand side P3 port and cools it. If the pilot request hot air the heat exchanger bypass valve will open allowing hot bleed air to mix directly with the cooled heat exchanger air. If the pilot request colder air, the air conditioning unit will be used. |
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Simple overview of temperature control process |
Heat exchanger takes bleed air from the right hand side P3 port and cools it. If the pilot request hot air the heat exchanger bypass valve will open allowing hot bleed air to mix directly with the cooled heat exchanger air. If the pilot request colder air, the air conditioning unit will be used. |
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Defog deice the canopy? |
No |
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What are the guarded pressurisation switch settings |
NORM, DUMP, RAM/DUMP |
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When might you use the manual override handle for ejection |
) If seperation is desired about 15,000 MSL, such as ejecting over mountainous terrain that reaches higher than 8,000ft MSL
2) Faulty seat doesn't separate at 15,000ft automatically.
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When to pull the green ring for OBOGS |
OBOGS failure |
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Emergency oxygen - where to find the pressure and how should it look |
Behind your seat, above the left shoulder. Should read 1800-2500psi, needle close to right. |
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ISS handle settings for ejection |
CMD FWD: Rear seat has solo eject ability but forward position will eject both. BOTH: Either crewmember can initiate ejection of both seats. SOLO: Each seat may choose when to eject but this won't eject the other seat. |
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ISS handle settings for ejection |
CMD FWD: Rear seat has solo eject ability but forward position will eject both. BOTH: Either crewmember can initiate ejection of both seats. SOLO: Each seat may choose when to eject but this won't eject the other seat. |
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Minimum recommended altitude (ft) for ejection AGL, both controlled and uncontrolled. |
2000 controlled 6000 uncontrolled |
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The three specific factors that affect ejection seat performance. |
Sync rate Dive angle Bank angle |
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Time that emergency oxygen lasts |
Up to 10 minutes from ring pull |
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CFS operation |
Piezoelectric crystals generate voltage (mechanically activated), which light flash lamps which activates an optical detonator via laser, which triggers the detonator cord wired through the canopy. FLSC (flexible linear-shaped charge) used for frontage (thicker glass) and MDC (mild detonation cord) used for rear transparency (thinner glass). |
