Help
Options
Didn't know it?
click below
click below
Knew it?
click below
click below
Don't Know
Remaining cards (0)
Know
retry
shuffle
restart
0:00
Embed Code - If you would like this activity on your web page, copy the script below and paste it into your web page.
Normal Size Small Size show me how
Normal Size Small Size show me how
Dash 1: Chapter 1
Finished
| Question | Answer |
|---|---|
| Basic empty weight of the t-6? | 4900 lbs |
| Maximum takeoff grossweight? | 6500 lbs |
| Free turbine turboprop eninge fat rated shaft horsepower is? | 1100 SHP |
| What are the two independent sections of the T-6 engine? | Power Turbuine and Gas Generation |
| Oil Capacity of the T-6? | 18.5 Quarts |
| Diameter of the propeller? | 97" |
| Oil level must be serviced within how many minutes? | 30 Min |
| When should you check the oil for most accurate results? | 15-20 Min |
| How long is the T-6? | 33' 4" |
| How wide is the T-6? | 33' 5" |
| How tall is the T-6? | 10' 8" |
| How wide is the horizontal stabilizer? | 11' 4" |
| 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 |
| What is the power turbine output shaft speed? | 30,000 RPM |
| The Reduction Gearbox reduces turbine output shaft speed to what RPM? | 2,000 |
| 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 |
| What annunciator will be shown for oil presures less than 15 PSI at idle power? | Red OIL PX |
| Oil presure between 40-90 PSI above idle yields what annunciator? | Amber OIL PX |
| Below 40 PSI above idle power will yield which annunciator? | Red OIL PX |
| 100% torque is available to what altitude? | 12,000-16,000 MSL |
| What provides power to the PMU and at how many volts? | Permanent Magnet Alternator @ 32 VAC |
| IOAT and ITT indications will be unreliable when the PMU is activated above what temperature? | 96 Degrees Celcius |
| What temperature will the PMU shutdown? | IOAT greater than 121 degrees celcius |
| ST ready must be illuminated for how many seconds prior to engine start? | 3 Seconds |
| PMU fail and PMU STATUS annunciators indicate what? | System is in manual mode |
| 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 |
| 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) |
| What does the mechanical firewall shutoff handle cutoff? | Fuel, hydraulics and bleed air |
| Fuel System contains how much fuel with single point refueling? what about wingover method of fueling? | 1100 lbs; 1200 lbs |
| How much fuel is in the collector tank? | 40 Lbs |
| What does the auto balance system aim to keep the fuel level between the tanks? | Within 20 lbs |
| When does the transfer valved in the auto balance fuel system activate? | Imbalance of 20 lbs for greater then 30 seconds |
| When will the FUEL BAL annunciator come on? | Fuel balance is not reduced to less than thirty in 2 minutes |
| When dues the red FUEL PX annunciator come on? | Fuel pressure less than 10 PSI |
| When do you get the L/R FUEL LO light? | Fuel less than 110 lbs in the tank |
| When is the amber section range of the fuel tanks? | Less than 150 lbs |
| When should you not manually try to balance the fuel tanks? | With an FP FAIL indication |
| The outer probe provides fuel readings until what reading? | 445 +/- 50 |
| The middle probe provides fuel readings until what reading? | 308 +/- 50 lbs |
| The inner probe provides fuel readings until what reading? | 20 lbs |
| How many fuel probes are in the fuel system? | 7 |
| How long will the collector tank provide fuel when in inverted flight? | 15 seconds |
| The fuel px low pressure switch is located where? | Motive flow fuel line |
| What is the volts and amps provided by the Generator? | 28 V / 300 Amps |
| What is the volts and amps provvided by the Battery? | 24 v / 42 Amps |
| What is the volts and amps provvided by the Aux Battery? | 24 V / 5 amps |
| Below how many volts indicats there is an issue with the battery being charged by the generator? | 25 Volts |
| Do not connect external power if battery voltage is below? | 22.0 Volts |
| With the bus tie switch open and a generator failure how long can you expect your battery to power the bat bus? | 30 Min |
| How many quarts is the hydraulic system? | 5 qts |
| When does the pressure relief valve in the hydraulic system open? | 3250-3500 PSI |
| What is normal hydraulic pressure? | 3000 +/- 120 PSI |
| What is the minimum hydraulic pressure for the normal system to be useful? | 1800 PSI |
| Below what PSI does the hydraulic system indication go to amber? | Below 1800 PSI |
| When will a HYDR FL LO come on? | Below one quart of hydraulic fluid |
| When is the EHYD PX LO light come on? | Below 2400 PSI +/- 150 in the mergency accumulator |
| What will the fuse in the emergency hydraulic system limit a leak to? | .25 GPM |
| A normal gear extension takes how long? | 6 Seconds |
| 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. |
| The Nose wheel is free castoring up to how many degrees? | 160 |
| Is normal flap operation available with Aux battery? What about Emergency Flap Operation? | No; No |
| What does the TAD sense? | Torque, altitude, airspeed, and pitch |
| The primpary pitot tube is located on which wing? | The Right |
| The primary static ports are located where? | One on the upper right aft side, and the other the lower left aft port |
| What is powered through the hot battery bus? | Battery Switch ELT FDR OBOGS Ram Air Emergency Flaps Time = Clock BEFORE TIME |
| What is powered by the Aux Bat? | Standbys Lights (STBY) UHF (back up) Fire 1 SLUF |
| After complete electrical failure to the STBY attitude indicator how long will it be working? to what accuracy? | 9 minutes; 6 dgrees |
| Testing the LOW AOA gauge position, what will your indications be? | AOA = 10.5 +/-.25 and an Amber Donut |
| Testing the HIGH AOA gauge position, what will your indications be? | AOA = 18.0 +/-.25 and Green Chevron plus stick shaker |
| Maximum Endurance AOA is? and symbol? | 8.8 White diamond |
| Max Range AOA is? and symbol? | 4.9 and white triangle |
| Stick shaker is activated when? | 5-10 Knots above stall speed, 15.5 AOA |
| The Canopy Fracturing System is made up of what charges and where? | Flexible Linear Shape Change (Front transparency) and Mild Detonating Chord (Rear Transparency) |
| If you pull either CFS handle will both fracture? | No |
| The front windscreen is rated to withstand how heavy of a bird strike at what air speed? | 270 KIAS 4 lbs |
| How many hooks and microswitches on the canopy? | 5 Hooks 4 Micro Switches |
| Which transparency on the canopy is thicker? | The Front Transparancy |
| Can the CFS handle be reset by pushing down? | No |
| 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 |
| 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' |
| Mountainous terrain exceeding what altitude should the MOR handle be used? | 8,000 MSL |
| When should the MOR handle be used? | If desired seat CFS seperation is above 14,000 MSL |
| What kind of parachute do we have? | GQ 5000 |
| Emergency oxygen will last for how many minutes? | 10 Minutes |
| Emergency Oxygen is pressurized to what? | 1800-2500 PSI |
| There is a what delay between the front and rear ejection seat? | 0.37 seconds |
| What is engine bleed air used for? | Canopy Presuurization seal, anti-g system, cockpit heating + defog, pressurization, OBOGS |
| When does the DUCT TEMP come on? | 300 degrees farenheit |
| The pressure safety valve in the anti g system activates when the pressure exceeds? | 7 PSI |
| The auto control on the ECS panel keeps the cockpit withing how many degrees? | 60 to 90 degrees farenheit |
| When will the heat exchanger bypass valve close? | When the temperature controller detecs a greater than 165 deg farenheit reading |
| When the defog is switched to off how long does it take to close? | 40 seconds |
| Differential pressure of 3.6 +/-0.2 are the highest readings expected up until what altitude? | 18,069 MSL |
| The CKKPT ALT comes on when? | Cockpit Altitude > 19,000 |
| The red CKPT PX comes on when? | 3.9 - 4.0 PSI |
| The RMU UHF comm can store how many frequencies? | 20 |
| The RMU VHF comm can store how many frequencies? | 20 |
| The RMU NAV can store how many frequencies? | 10 |
| How long will the ELT transmit for? | 50 hours |
| OBOGS TEMP annunciator will illuminate when? | 200 degrees farenheit |
| What fuels are approved for the T-6? | JP-4, JP-5, JP-8, JP-8+100, JET A, JET A-1, JET B |
| Main geat tire pressure is? | 225 +/-5 or 185+/-5 PSI (USAF) |
| Nosewheel tire pressure is? | 120 +/-5 PSI |
| An Operating procedure or technique which could result in personal injury or loss of life is? | A Warning |
| An Operating procedure or technique which could result in damage to the aircraft is? | A Caution |
| An operating procedure, technique, etc., which is considered essential to emphasize is a? | Note |
| The PT6A-68 free turbine turboprop engine is a reverse flow design with air entering the engine from the front. | False |
| At 100% indicated torque, the engine is producing approximately ________ of torque at the prop shaft | 2900 ft-lbs ≈ 2750 lbs thrust at SL |
| Momentarily placing the starter switch in the AUTO/RESET position ________. | Engages the starter and energizes the spark ignition system |
| What is the only acceptable method for getting a correct indication of oil level? | Dipstick |
| Due to the sensitivity of the SCU, a single, momentary illumination of the amber OIL PX annunciator while maneuvering indicates a system malfunction. | False |
| What does a red CHIP annunciator indicate? | Contaminated Oil |
| 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) |
| The propeller system is designed to maintain a constant speed of? | 2000 RPM |
| What are the three basic conditions of propeller pitch? | a. Feathered b. low pitch (flat or fine) c. high pitch (coarse) |
| Normally, propeller governing is automatically set by the ____ and ____. | PMU and PIU |
| If oil pressure is lost in the propeller system, what will the prop do? | Feather |
| Power for the feather dump solenoid valve is provided through which circuit breaker? | Prop Sys |
| 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 |
| If PMU is not functioning, the ______________ will modulate oil pressure to maintain Np at or below 100+/-2 %. | Flyweight overspeed governor (checked in hammerhead) |
| During an auto start or normal operations with the ignition set to NORM, the ____ will energize and de-energize the igniters as required. | PMU |
| What items are displayed on the Primary Engine Data Display? | Torque, N1, Np, IOAT, ITT (all processed by PMU) |
| What items are displayed on the Alternate Engine Data Display? | Torque, N1, cockpit press alt, cockpit press differential, fuel flow, fuel quantity, and RITT |
| What is the only item on the AEDD that is processed by the PMU? | Torque |
| What items are on the Engine/Systems/NACWS display? | oil press and temp, hyd press, DC volts and amps, and NACWS traffic alerts |
| 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 |
| Above ______ feet MSL the PMU raises N1 to maintain Np above 80% to avoid stress on the propeller during spins. | 10,000 MSL |
| Relation of PCL position to power setting is _______ with the PMU operating. | Linear |
Created by:
1214
Popular Aviation sets