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| Basic empty weight of the t-6? | 4900 lbs
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| Maximum takeoff grossweight? | 6500 lbs
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| Free turbine turboprop eninge fat rated shaft horsepower is? | 1100 SHP
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| What are the two independent sections of the T-6 engine? | Power Turbuine and Gas Generation
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| Oil Capacity of the T-6? | 18.5 Quarts
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| Diameter of the propeller? | 97"
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| Oil level must be serviced within how many minutes? | 30 Min
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| When should you check the oil for most accurate results? | 15-20 Min
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| How long is the T-6? | 33' 4"
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| How wide is the T-6? | 33' 5"
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| How tall is the T-6? | 10' 8"
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| How wide is the horizontal stabilizer? | 11' 4"
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| With oil indicating normal and illuminate of both amber and red OIL PX annunciators, what is is typically caused by? | Signal Conditioning Unit (SCU) Failure
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| What is the power turbine output shaft speed? | 30,000 RPM
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| The Reduction Gearbox reduces turbine output shaft speed to what RPM? | 2,000
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| Oil pressure between 15 and 40 PSI causes which annunciator? after 5 seconds? (at idle power) | Amber OIL PX then Red OIL PX in addtion to the other one after 5 seconds
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| What annunciator will be shown for oil presures less than 15 PSI at idle power? | Red OIL PX
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| Oil presure between 40-90 PSI above idle yields what annunciator? | Amber OIL PX
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| Below 40 PSI above idle power will yield which annunciator? | Red OIL PX
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| 100% torque is available to what altitude? | 12,000-16,000 MSL
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| What provides power to the PMU and at how many volts? | Permanent Magnet Alternator @ 32 VAC
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| IOAT and ITT indications will be unreliable when the PMU is activated above what temperature? | 96 Degrees Celcius
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| What temperature will the PMU shutdown? | IOAT greater than 121 degrees celcius
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| ST ready must be illuminated for how many seconds prior to engine start? | 3 Seconds
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| PMU fail and PMU STATUS annunciators indicate what? | System is in manual mode
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| PMU status illuminartes under what condition? | Fault detected in flight not serious enough to cause the PMU to go into manual mode, and 1 min after WOW is activated
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| What causes a PMU STATUS annunciator in flight? What is a key consideration? | Mismatch in the WOW switch, the PMU will not revert to ground idle when on ground (longer LDG roll)
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| What does the mechanical firewall shutoff handle cutoff? | Fuel, hydraulics and bleed air
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| Fuel System contains how much fuel with single point refueling? what about wingover method of fueling? | 1100 lbs; 1200 lbs
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| How much fuel is in the collector tank? | 40 Lbs
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| What does the auto balance system aim to keep the fuel level between the tanks? | Within 20 lbs
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| When does the transfer valved in the auto balance fuel system activate? | Imbalance of 20 lbs for greater then 30 seconds
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| When will the FUEL BAL annunciator come on? | Fuel balance is not reduced to less than thirty in 2 minutes
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| When dues the red FUEL PX annunciator come on? | Fuel pressure less than 10 PSI
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| When do you get the L/R FUEL LO light? | Fuel less than 110 lbs in the tank
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| When is the amber section range of the fuel tanks? | Less than 150 lbs
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| When should you not manually try to balance the fuel tanks? | With an FP FAIL indication
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| The outer probe provides fuel readings until what reading? | 445 +/- 50
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| The middle probe provides fuel readings until what reading? | 308 +/- 50 lbs
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| The inner probe provides fuel readings until what reading? | 20 lbs
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| How many fuel probes are in the fuel system? | 7
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| How long will the collector tank provide fuel when in inverted flight? | 15 seconds
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| The fuel px low pressure switch is located where? | Motive flow fuel line
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| What is the volts and amps provided by the Generator? | 28 V / 300 Amps
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| What is the volts and amps provvided by the Battery? | 24 v / 42 Amps
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| What is the volts and amps provvided by the Aux Battery? | 24 V / 5 amps
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| Below how many volts indicats there is an issue with the battery being charged by the generator? | 25 Volts
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| Do not connect external power if battery voltage is below? | 22.0 Volts
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| With the bus tie switch open and a generator failure how long can you expect your battery to power the bat bus? | 30 Min
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| How many quarts is the hydraulic system? | 5 qts
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| When does the pressure relief valve in the hydraulic system open? | 3250-3500 PSI
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| What is normal hydraulic pressure? | 3000 +/- 120 PSI
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| What is the minimum hydraulic pressure for the normal system to be useful? | 1800 PSI
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| Below what PSI does the hydraulic system indication go to amber? | Below 1800 PSI
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| When will a HYDR FL LO come on? | Below one quart of hydraulic fluid
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| When is the EHYD PX LO light come on? | Below 2400 PSI +/- 150 in the mergency accumulator
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| What will the fuse in the emergency hydraulic system limit a leak to? | .25 GPM
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| A normal gear extension takes how long? | 6 Seconds
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| What are the three conditions in which the landing gear position warning will sound? | 1. Gear handle not down, flaps up or T/O, PCL below mid range 2. All gear not down and locked with flaps LDG 3. Weight on wheels with the gear handle not down.
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| The Nose wheel is free castoring up to how many degrees? | 160
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| Is normal flap operation available with Aux battery? What about Emergency Flap Operation? | No; No
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| What does the TAD sense? | Torque, altitude, airspeed, and pitch
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| The primpary pitot tube is located on which wing? | The Right
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| The primary static ports are located where? | One on the upper right aft side, and the other the lower left aft port
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| What is powered through the hot battery bus? | Battery Switch ELT FDR OBOGS Ram Air Emergency Flaps Time = Clock BEFORE TIME
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| What is powered by the Aux Bat? | Standbys Lights (STBY) UHF (back up) Fire 1 SLUF
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| After complete electrical failure to the STBY attitude indicator how long will it be working? to what accuracy? | 9 minutes; 6 dgrees
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| Testing the LOW AOA gauge position, what will your indications be? | AOA = 10.5 +/-.25 and an Amber Donut
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| Testing the HIGH AOA gauge position, what will your indications be? | AOA = 18.0 +/-.25 and Green Chevron plus stick shaker
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| Maximum Endurance AOA is? and symbol? | 8.8 White diamond
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| Max Range AOA is? and symbol? | 4.9 and white triangle
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| Stick shaker is activated when? | 5-10 Knots above stall speed, 15.5 AOA
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| The Canopy Fracturing System is made up of what charges and where? | Flexible Linear Shape Change (Front transparency) and Mild Detonating Chord (Rear Transparency)
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| If you pull either CFS handle will both fracture? | No
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| The front windscreen is rated to withstand how heavy of a bird strike at what air speed? | 270 KIAS 4 lbs
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| How many hooks and microswitches on the canopy? | 5 Hooks 4 Micro Switches
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| Which transparency on the canopy is thicker? | The Front Transparancy
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| Can the CFS handle be reset by pushing down? | No
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| How long is the external CFS handle and how many pounds of force to activate it? Will it blow both CFS transparencies? | 10' 15-25 lbs; yes
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| The ejection seat is rated at what altitude and airspeed to a maximum of what altitude and airspeed? | 0 KIAS - 370 KIAS, 0' - 35,000'
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| Mountainous terrain exceeding what altitude should the MOR handle be used? | 8,000 MSL
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| When should the MOR handle be used? | If desired seat CFS seperation is above 14,000 MSL
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| What kind of parachute do we have? | GQ 5000
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| Emergency oxygen will last for how many minutes? | 10 Minutes
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| Emergency Oxygen is pressurized to what? | 1800-2500 PSI
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| There is a what delay between the front and rear ejection seat? | 0.37 seconds
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| What is engine bleed air used for? | Canopy Presuurization seal, anti-g system, cockpit heating + defog, pressurization, OBOGS
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| When does the DUCT TEMP come on? | 300 degrees farenheit
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| The pressure safety valve in the anti g system activates when the pressure exceeds? | 7 PSI
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| The auto control on the ECS panel keeps the cockpit withing how many degrees? | 60 to 90 degrees farenheit
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| When will the heat exchanger bypass valve close? | When the temperature controller detecs a greater than 165 deg farenheit reading
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| When the defog is switched to off how long does it take to close? | 40 seconds
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| Differential pressure of 3.6 +/-0.2 are the highest readings expected up until what altitude? | 18,069 MSL
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| The CKKPT ALT comes on when? | Cockpit Altitude > 19,000
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| The red CKPT PX comes on when? | 3.9 - 4.0 PSI
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| The RMU UHF comm can store how many frequencies? | 20
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| The RMU VHF comm can store how many frequencies? | 20
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| The RMU NAV can store how many frequencies? | 10
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| How long will the ELT transmit for? | 50 hours
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| OBOGS TEMP annunciator will illuminate when? | 200 degrees farenheit
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| What fuels are approved for the T-6? | JP-4, JP-5, JP-8, JP-8+100, JET A, JET A-1, JET B
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| Main geat tire pressure is? | 225 +/-5 or 185+/-5 PSI (USAF)
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| Nosewheel tire pressure is? | 120 +/-5 PSI
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| An Operating procedure or technique which could result in personal injury or loss of life is? | A Warning
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| An Operating procedure or technique which could result in damage to the aircraft is? | A Caution
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| An operating procedure, technique, etc., which is considered essential to emphasize is a? | Note
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| The PT6A-68 free turbine turboprop engine is a reverse flow design with air entering the engine from the front. | False
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| At 100% indicated torque, the engine is producing approximately ________ of torque at the prop shaft | 2900 ft-lbs ≈ 2750 lbs thrust at SL
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| Momentarily placing the starter switch in the AUTO/RESET position ________. | Engages the starter and energizes the spark ignition system
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| What is the only acceptable method for getting a correct indication of oil level? | Dipstick
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| Due to the sensitivity of the SCU, a single, momentary illumination of the amber OIL PX annunciator while maneuvering indicates a system malfunction. | False
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| What does a red CHIP annunciator indicate? | Contaminated Oil
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| What accessories are mounted on the reduction gearbox? | a. Prop interface unit (PIU), torque probe, Permanent magnetic alternator (PMA) (on top), and the air conditioning compressor (belt driven) (on right side)
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| The propeller system is designed to maintain a constant speed of? | 2000 RPM
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| What are the three basic conditions of propeller pitch? | a. Feathered b. low pitch (flat or fine) c. high pitch (coarse)
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| Normally, propeller governing is automatically set by the ____ and ____. | PMU and PIU
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| If oil pressure is lost in the propeller system, what will the prop do? | Feather
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| Power for the feather dump solenoid valve is provided through which circuit breaker? | Prop Sys
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| With the PMU functioning, the _______________ will modulate oil pressure to the prop pitch change piston to limit Np to 106%, while electronic governor will keep Np at 100%. | With the mechanical overspeed governor
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| If PMU is not functioning, the ______________ will modulate oil pressure to maintain Np at or below 100+/-2 %. | Flyweight overspeed governor (checked in hammerhead)
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| During an auto start or normal operations with the ignition set to NORM, the ____ will energize and de-energize the igniters as required. | PMU
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| What items are displayed on the Primary Engine Data Display? | Torque, N1, Np, IOAT, ITT (all processed by PMU)
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| What items are displayed on the Alternate Engine Data Display? | Torque, N1, cockpit press alt, cockpit press differential, fuel flow, fuel quantity, and RITT
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| What is the only item on the AEDD that is processed by the PMU? | Torque
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| What items are on the Engine/Systems/NACWS display? | oil press and temp, hyd press, DC volts and amps, and NACWS traffic alerts
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| True or False. If EDM FAIL, EDM A FAIL, or EDM B FAIL are displayed on any of the respective displays, everything displayed is invalid. | False, only those items replaced by amber dashes and/or with missing pointers are affected
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| Above ______ feet MSL the PMU raises N1 to maintain Np above 80% to avoid stress on the propeller during spins. | 10,000 MSL
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| Relation of PCL position to power setting is _______ with the PMU operating. | Linear
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