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496 Cards in this Set
- Front
- Back
- 3rd side (hint)
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What are the four inspections concepts? |
Periodic, phased, Isochronal, and programmed Depot maintenance |
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What are the basic scheduled inspections that are common to the four inspection concepts? |
Preflight, end of runway, thru flight, basic post fight. |
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When are TH inspections performed? |
Between flights |
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which basic scheduled inspection is a more thorough check in the PR or TH inspections? |
BPO |
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What three inspections are based on hours of operation |
Hourly postflight, periodic, phase |
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Which inspection is a combination of the BPO, PE and or HPO inspection requirements |
Phase inspection |
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What three inspections are peculiar to the Isochronal inspection system |
Minor, major, home station check |
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What is the AFTO form 781A used for |
To document discrepancies it discovered by aircrew or maintenance personnel |
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When can you erase symbols in the symbol block |
Never |
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What is required in the corrective action block when clearing a red X discrepancy |
A complete TO reference |
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What documentation is required if you cannot accomplish the operational check immediately after completion of the maintenance |
Close out the original entry by describing the corrective action |
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What is the purpose of AFTO form 781C |
Provides avionic configurations and load statuses |
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What is the aircraft commander's role relating to the AFTO form 781C |
Check forms to ensure equipment and configurations conform to mission needs |
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What is the role of maintenance personnel for the AFTO form 781C |
To ensure the validity in the legibility of all required entries |
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What is the purpose of the AFTO form 781H |
Used to document maintenance status and servicing information |
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What is the purpose of the exceptional release |
Certification that the authorized individual who enters the minimum signature has reviewed the active forms to ensure the aircraft a safe for flight |
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What is block 11 used for on the AFTO Form 781H |
To document servicing data for fuel, oil, oxygen, and nitrogen/water |
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What is the purpose of the AFTO form 781J |
To document airframe time and engine data |
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Who is responsible for making entries on the AFTO form 781J |
The aircraft maintenance technician |
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Which AFTO forms are used to document oil servicing |
781J and 781H |
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What is the purpose of the AFTO form 781K |
To record essential inspection and delayed maintenance data |
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What is block D used for |
All delayed discrepancies, urgent action TCTOs, category one routine action safety modification TCTOs, outstanding routine action TCTOs, or commercial equivalents |
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At what point are red X entries entered on the AFTO form 781K |
Never |
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What type of equipment is the AFTO form 244 used for |
AGE and support equipment |
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What does part V of the AFTO form 244 provide |
A means to document equipment discrepancies and corrective actions |
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What is the AFTO form 245 used for |
A continuation of the afto form 244 |
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What is the purpose of AF Form 1492 |
To flag a condition that could cause damage or injury if ignored |
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Where are warning tags placed on an aircraft |
At a point where undesirable activation of a system is possible |
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The perforated bottom portion of the tag is used for what purpose |
To provide a crosscheck with the aircraft forms |
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When is the basic postflight inspection performed |
After the last flight of the specified flying period |
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The home station check inspection can be accomplished in conjunction with |
Minor and major inspections |
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How do you document the malfunction on the AFTO 781A that is found during an operational check |
Document the finding and refer to a new write up |
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Which AFTO 781 forms are used to document airframe time |
H and J |
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How what a system be deactivated if it fails during flight |
A circuit breaker collar or other approved method will be used to lock out the system circuit breaker and an applicable warning statement written |
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What is the most common type of insulated wire used on aircraft called |
Kapton wiring |
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What does a coaxial cable consist of |
An inner conductor and an outer conductor separated by an insulated dielectric |
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What type of impedance do coaxial cable's have |
50 ohms |
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When is triaxial cable used |
When further shielding is required |
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What is the most common type of thermocouple wiring |
Alumel/Chromel |
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Why is it important to make sure equal links of both wires are removed when cutting thermocouple wiring |
If links are not equal wrong temperature indications will occur |
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What are some precautions to observe during maintenance of thermocouple wiring |
Do not bend thermocouple leads Route wiring away from hotspots |
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What is a major factor to consider when using fiber optic cable's in place of conventional wire |
Elasticity |
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Twisting a fiber optic cable during installation can have what effect |
Disturbances and lay uniformity resulting in reduced optical power transmission |
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What are some sources of EMI |
Lightning, powerlines, engines, generators, radar |
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Describe a simple way to identify sources of EMI |
Turn on other devices or systems one at a time until interference symptoms return |
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What are the advantages of fiber optics |
Small size, safety, security, lightweight, speed |
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Which components protect the fiber optic cable and add tensile strength |
Outer jacket, strength members, buffer jacket |
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What is the active component in a fiber optic communication system |
Optical source |
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What are the two types of light sources used in a fiber optic system |
Light emitting diode or injection laser diode |
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What two types of photodiodes are used in a fiber optic system |
Pin photodiode and avalanche photodiode |
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What does proper use of a wire stripping tool accomplish |
Removes insulation without damaging the wire |
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What is the first step to ensure the wire is properly stripped |
Select the correct size |
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What are wire splices used for |
To join wires together |
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What must you do after the crimp barrel is properly installed |
Ensure the wires cannot be pulled out of the splice |
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What is an EMP cable |
Nuclear hardened wire |
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What is the first thing you must do before repairing an EMP cable jacket |
Examine the damaged area to determine if it's limited to only the jacket |
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What is the final step in outer cable shield repair |
Wrap repaired area with at least half inch of cable on each side of the repair with self bonding silicone tape |
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What must you do prior to repairing a wire at an EMP connector |
Check TO to ensure you have proper materials for the job |
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What does lacing and tying provide |
Ease of installation, maintenance, and inspection |
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What is the recommended type of material for lacing and tying |
Narrow flat tape |
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When can continuous lacing be used |
Only on wire groups or bundles which are installed in panels or junction boxes |
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What are the spacing requirements for tying wire groups or bundles |
12 inches or less apart |
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What warning must you always heed when you are using cable straps |
The strap must always be cut flush with the boss surface in order to eliminate painful cuts and scratches from protruding strap ends |
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What are torque wrench designed to measure |
The specific degree of tightness of nuts or bolts |
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What is the working range of a torque wrench |
Not lower than 20% nor greater than the rated capacity of the torque wrench |
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How do you prepare a torque wrench for storage |
Set it to its lowest increment torque value or mechanical stop which ever comes first |
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What does a cable tensiometer measure |
Specific degree of tightness of aircraft cable's |
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Why is important to check flight control cables for proper tension |
Can lead to increased cable wear sluggish flight control surface response to pilot input or cause vibration |
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Why are panels sealed |
To protect against corrosion and to fill and level out gaps between the panel and airframe |
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What is used to prevent sealant from contacting adjacent areas during application |
Masking tape |
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What needs to be avoided when applying sealent |
Entrapment of air |
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What is a gasket |
A mechanical seal which fills the space between two or more mating surfaces generally to prevent leakage |
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Why must you and share gaskets are properly seated during installation |
To avoid leaks and proper operation of equipment |
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Which type of cable is primarily used to carry radiofrequency power from one point to another |
Coaxial |
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What type of cable is not affected by electromagnetic interference |
Fiber optic |
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What is used to convert fiber optic light transmissions back to electrical signals |
Photodiode |
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What must be done before installing a wire splice |
Remove the insulation from the wire |
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Why are environmental splices The preferred method of wire splicing |
Weather resistant |
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How many outer protective layers does an electromagnetic pulse cable have |
3 |
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What percentage of minor shield damage can the flightline technician repair on an electromagnetic pulse cable |
Up to 25% of the outer shield circumference |
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Which of the following is not a type of tape used in outer shield repair of electromagnetic pulse cable |
Electrical |
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When tying wire bundles behind connectors start ties far enough back from the connector to |
Avoid putting tension on the wires and pins |
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Cotton or linen cord or tape must be pre-waxed to make it |
Moisture and fungus resistant |
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What does an aircraft air-conditioning system provide |
Conditioned air for crew, cooling for avionics systems, defogging of windows, and cabin pressurization |
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Where does the aircraft receive power from in flight |
AC generators |
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What system provides the power to move flight control surfaces and landing gear |
Hydraulics |
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What is the function of the propulsion system |
To provide thrust, or thrust and lift on rotary devices |
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What systems provide line of sight, air to air, and air to ground voice communications |
VHF UHF HF |
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Which navigation system is an independent system |
Inertial navigation system |
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What ground-based transmitting stations does ILS operate in conjunction with |
Localizer, glide-slope, and marker Beacon signals |
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What system provides steering data to the autopilot |
Inertial navigation system |
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What is the purpose of engine indicating instrumen |
To monitor vital signs of engines |
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What components are attached to the fuselage |
Wings, engines, and empennage |
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What do the engine nacelles provide |
Smooth airflow around and into engines |
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What flight controls are included on the wings |
Ailerons flaps and spoilers |
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What does the empennage consist of |
Horizontal stabilizer, elevator, vertical stabilizer, and rudder |
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Name the four aerodynamic forces that affect aircraft flight |
Gravity lift thrust and drag |
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What produces thrust |
Aircraft engines |
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When an aircraft is fine at a constant altitude with a constant airspeed what does a lift and thrust equal |
Lift=gravity and thrust=drag |
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What must be increased for airspeed to increase |
Thrust to a point where it exceeds drag |
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What are the three axis of rotation and what motions doesn't aircraft make on these axis |
Longitudinal lateral and vertical. Roll pitch and yaw |
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What takes place on the X axis |
Roll |
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At what point on the aircraft do all three axis meet |
Center of gravity |
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What do the primary flight controls consist of |
Ailerons elevators and rudder |
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What controls roll motion of the aircraft |
Ailerons |
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What is used to control the pitch attitude of the aircraft |
Elevators |
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What provides the directional control for yaw of the aircraft |
Rudder |
Elevator trim and position in degrees nose up or knows them from the neutral position |
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Why is the cable system the most widely used type of mechanical flight control |
Deflections of the structure to which it is attached do not affect its operation |
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Why do some aircraft incorporate flight control systems that automatically revert to servo tab control |
In case of total hydraulic failure |
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What links the flight controls with the hydraulic system |
Conventional cable or push pull tube system |
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Why are artificial feel systems incorporated into the design of hydromechanical flight control systems |
To provide increased resistance to the controls at higher speeds |
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Why does an electro mechanical system eliminate the need for high-pressure hydraulic lines |
The actuator uses electric power instead of hydraulic power |
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What can be prevented through electronic flight control computer programming |
Undesirable and dangerous characteristics |
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What is the flap position indicator designed to display |
Percentage of flap extension from 0 to 100% |
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What does the elevator trim indicator display |
Elevator trim and position in degrees nose up or knows them from the neutral position |
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What do synchros convert |
Mechanical shift angles to electrical signals or electrical signals to mechanical shift degrees |
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What is one main difference between a Synchro and selsyn system |
28 VDC is used instead of the 115 or 26 VAC a Synchro system uses |
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What does the selsyn system transmitter consist of |
A circular resistance winding with three taps positioned 120° apart |
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Why must selsyn transmitters and indicators be replaced together |
They often come in matched sets |
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What does autopilot control to automatically correct for any out of trim condition in the pitch exes |
The elevator trim tabs |
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What ensures the autopilot system engages and operates correctly during all functions |
Electrical mechanical interlocks |
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What controls the activation of engage signals, switch hold signals, and clutches for the rudder, aileron, and elevator servos |
The automatic flight control process AFCP |
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Where are lateral guidance commands derived from |
Inertial navigation,flight director, and radio navigation systems |
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What is annunciated on the flight progress/warning unit |
The AFSC flight progress, cautions, and warnings |
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What does an auto trim fail Annunciation indicate |
A pitch axis out of trim condition may exist |
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What does the FCP provide |
Autopilot engagement and displacement, pitch and lateralcouple control, pitch or lateral axis disengage Control altitude hold mode engagement and the BIT initiate |
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When will the picture will be in operative |
Whenever the altitude hold or speed on pitch modes are selected after glideslope capture, or when the pitch axis is in the off position |
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What will automatically deselect the speed on pitch mode, if active, and deactivate the pitch wheel on the flight control panel |
Selection of altitude hold |
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What is the purpose of the three identical servos |
To position the aircraft control surfaces in response to AFCP guidance commands |
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What a AFCS modes are considered both lateral and vertical modes |
Flight director and approach |
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Which switches determine what flight data controls AFCS mode selection |
The autopilot one and autopilot two switches |
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How are navigation system interfaces to the autopilot determined |
By the pilot and copilot flight director switch positions |
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When does the power on state occur |
Immediately following application of power to the automatic flight control processor |
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What is the normal state for the AFCS |
The flight control state |
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What must the calibrated airspeed be in order to activate the maintenance BIT |
Less than 50 knots |
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How far to the rear of an engine may be required to be considered a safe distance away from engine exhaust |
Up to 600 feet |
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How far to the rear of an engine may be required to be considered a safe distance away from engine exhaust |
Up to 600 feet |
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How can you determine the point of rotation of an engine |
Buy a red or black band around the fuselage |
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How far to the rear of an engine may be required to be considered a safe distance away from engine exhaust |
Up to 600 feet |
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How can you determine the point of rotation of an engine |
Buy a red or black band around the fuselage |
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How long should you remain clear of the 300 foot hazard area after an aircraft has stopped during a hot brakes situation |
At least 45 to 60 minutes |
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How far to the rear of an engine may be required to be considered a safe distance away from engine exhaust |
Up to 600 feet |
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How can you determine the point of rotation of an engine |
Buy a red or black band around the fuselage |
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How long should you remain clear of the 300 foot hazard area after an aircraft has stopped during a hot brakes situation |
At least 45 to 60 minutes |
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From which direction should you approach and aircraft with hot breaks? Why? |
From the nose or tail. The areas on the side are where fragments could be hurled if the tire explodes |
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How far to the rear of an engine may be required to be considered a safe distance away from engine exhaust |
Up to 600 feet |
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How can you determine the point of rotation of an engine |
Buy a red or black band around the fuselage |
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How long should you remain clear of the 300 foot hazard area after an aircraft has stopped during a hot brakes situation |
At least 45 to 60 minutes |
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From which direction should you approach and aircraft with hot breaks? Why? |
From the nose or tail. The areas on the side are where fragments could be hurled if the tire explodes |
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What can happen if you operate power actuated surfaces carelessly |
You can damage equipment, severely injure, or kill someone |
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How far to the rear of an engine may be required to be considered a safe distance away from engine exhaust |
Up to 600 feet |
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How can you determine the point of rotation of an engine |
Buy a red or black band around the fuselage |
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How long should you remain clear of the 300 foot hazard area after an aircraft has stopped during a hot brakes situation |
At least 45 to 60 minutes |
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From which direction should you approach and aircraft with hot breaks? Why? |
From the nose or tail. The areas on the side are where fragments could be hurled if the tire explodes |
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What can happen if you operate power actuated surfaces carelessly |
You can damage equipment, severely injure, or kill someone |
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What must you first do prior to performing any maintenance on the aircraft |
Review aircraft forms |
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How far to the rear of an engine may be required to be considered a safe distance away from engine exhaust |
Up to 600 feet |
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How can you determine the point of rotation of an engine |
Buy a red or black band around the fuselage |
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How long should you remain clear of the 300 foot hazard area after an aircraft has stopped during a hot brakes situation |
At least 45 to 60 minutes |
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From which direction should you approach and aircraft with hot breaks? Why? |
From the nose or tail. The areas on the side are where fragments could be hurled if the tire explodes |
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What can happen if you operate power actuated surfaces carelessly |
You can damage equipment, severely injure, or kill someone |
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What must you first do prior to performing any maintenance on the aircraft |
Review aircraft forms |
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What is the purpose of landing gear safety pins? |
To prevent inadvertent retraction of the landing gear while the aircraft is on the ground |
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How far to the rear of an engine may be required to be considered a safe distance away from engine exhaust |
Up to 600 feet |
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How can you determine the point of rotation of an engine |
Buy a red or black band around the fuselage |
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How long should you remain clear of the 300 foot hazard area after an aircraft has stopped during a hot brakes situation |
At least 45 to 60 minutes |
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From which direction should you approach and aircraft with hot breaks? Why? |
From the nose or tail. The areas on the side are where fragments could be hurled if the tire explodes |
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What can happen if you operate power actuated surfaces carelessly |
You can damage equipment, severely injure, or kill someone |
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What must you first do prior to performing any maintenance on the aircraft |
Review aircraft forms |
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What is the purpose of landing gear safety pins? |
To prevent inadvertent retraction of the landing gear while the aircraft is on the ground |
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What is the purpose of grounding an aircraft |
To dissipate dangerous built up static electricity |
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How far to the rear of an engine may be required to be considered a safe distance away from engine exhaust |
Up to 600 feet |
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How can you determine the point of rotation of an engine |
Buy a red or black band around the fuselage |
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How long should you remain clear of the 300 foot hazard area after an aircraft has stopped during a hot brakes situation |
At least 45 to 60 minutes |
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From which direction should you approach and aircraft with hot breaks? Why? |
From the nose or tail. The areas on the side are where fragments could be hurled if the tire explodes |
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What can happen if you operate power actuated surfaces carelessly |
You can damage equipment, severely injure, or kill someone |
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What must you first do prior to performing any maintenance on the aircraft |
Review aircraft forms |
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What is the purpose of landing gear safety pins? |
To prevent inadvertent retraction of the landing gear while the aircraft is on the ground |
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What is the purpose of grounding an aircraft |
To dissipate dangerous built up static electricity |
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Why is RF radiation a particularly dangerous hazard |
Because it can't be seen or heard |
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How far to the rear of an engine may be required to be considered a safe distance away from engine exhaust |
Up to 600 feet |
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How can you determine the point of rotation of an engine |
Buy a red or black band around the fuselage |
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How long should you remain clear of the 300 foot hazard area after an aircraft has stopped during a hot brakes situation |
At least 45 to 60 minutes |
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From which direction should you approach and aircraft with hot breaks? Why? |
From the nose or tail. The areas on the side are where fragments could be hurled if the tire explodes |
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What can happen if you operate power actuated surfaces carelessly |
You can damage equipment, severely injure, or kill someone |
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What must you first do prior to performing any maintenance on the aircraft |
Review aircraft forms |
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What is the purpose of landing gear safety pins? |
To prevent inadvertent retraction of the landing gear while the aircraft is on the ground |
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What is the purpose of grounding an aircraft |
To dissipate dangerous built up static electricity |
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Why is RF radiation a particularly dangerous hazard |
Because it can't be seen or heard |
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A sound level of how many decibels can rupture the eardrum and cause permanent damage |
100 dB |
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How far to the rear of an engine may be required to be considered a safe distance away from engine exhaust |
Up to 600 feet |
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What is the typical operating pressure of hydraulic systems |
3000 pounds per square inch |
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How can you determine the point of rotation of an engine |
Buy a red or black band around the fuselage |
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How long should you remain clear of the 300 foot hazard area after an aircraft has stopped during a hot brakes situation |
At least 45 to 60 minutes |
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From which direction should you approach and aircraft with hot breaks? Why? |
From the nose or tail. The areas on the side are where fragments could be hurled if the tire explodes |
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What can happen if you operate power actuated surfaces carelessly |
You can damage equipment, severely injure, or kill someone |
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What must you first do prior to performing any maintenance on the aircraft |
Review aircraft forms |
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What is the purpose of landing gear safety pins? |
To prevent inadvertent retraction of the landing gear while the aircraft is on the ground |
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What is the purpose of grounding an aircraft |
To dissipate dangerous built up static electricity |
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Why is RF radiation a particularly dangerous hazard |
Because it can't be seen or heard |
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A sound level of how many decibels can rupture the eardrum and cause permanent damage |
100 dB |
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How far to the rear of an engine may be required to be considered a safe distance away from engine exhaust |
Up to 600 feet |
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What is the typical operating pressure of hydraulic systems |
3000 pounds per square inch |
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What is the process for storing flammable liquids in buildings |
They will be in approved containers and stored in areas specifically approved by Fire Chief |
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How can you determine the point of rotation of an engine |
Buy a red or black band around the fuselage |
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How long should you remain clear of the 300 foot hazard area after an aircraft has stopped during a hot brakes situation |
At least 45 to 60 minutes |
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From which direction should you approach and aircraft with hot breaks? Why? |
From the nose or tail. The areas on the side are where fragments could be hurled if the tire explodes |
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What can happen if you operate power actuated surfaces carelessly |
You can damage equipment, severely injure, or kill someone |
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What must you first do prior to performing any maintenance on the aircraft |
Review aircraft forms |
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What is the purpose of landing gear safety pins? |
To prevent inadvertent retraction of the landing gear while the aircraft is on the ground |
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What is the purpose of grounding an aircraft |
To dissipate dangerous built up static electricity |
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Why is RF radiation a particularly dangerous hazard |
Because it can't be seen or heard |
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A sound level of how many decibels can rupture the eardrum and cause permanent damage |
100 dB |
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Besides lift, what else does the main rotor provided on a helicopter |
Lateral and longitudinal movement |
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Besides lift, what else does the main rotor provided on a helicopter |
Lateral and longitudinal movement |
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What is the purpose of the tail rotor on a helicopter |
To stabilize the aircraft and can move the aircraft |
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Besides lift, what else does the main rotor provided on a helicopter |
Lateral and longitudinal movement |
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What is the purpose of the tail rotor on a helicopter |
To stabilize the aircraft and can move the aircraft |
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What are the three controls used to maneuver a helicopter |
Collective, cyclic, footpedals |
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Besides lift, what else does the main rotor provided on a helicopter |
Lateral and longitudinal movement |
|
|
|
What is the purpose of the tail rotor on a helicopter |
To stabilize the aircraft and can move the aircraft |
|
|
|
What are the three controls used to maneuver a helicopter |
Collective, cyclic, footpedals |
|
|
|
Raising what helicopter control will cause a helicopter to increase in altitude |
Collective |
|
|
|
Besides lift, what else does the main rotor provided on a helicopter |
Lateral and longitudinal movement |
|
|
|
What is the purpose of the tail rotor on a helicopter |
To stabilize the aircraft and can move the aircraft |
|
|
|
What are the three controls used to maneuver a helicopter |
Collective, cyclic, footpedals |
|
|
|
Raising what helicopter control will cause a helicopter to increase in altitude |
Collective |
|
|
|
What did the foot pedals on a helicopter control |
Yaw |
|
|
|
Besides lift, what else does the main rotor provided on a helicopter |
Lateral and longitudinal movement |
|
|
|
What is the purpose of the tail rotor on a helicopter |
To stabilize the aircraft and can move the aircraft |
|
|
|
What are the three controls used to maneuver a helicopter |
Collective, cyclic, footpedals |
|
|
|
Raising what helicopter control will cause a helicopter to increase in altitude |
Collective |
|
|
|
What did the foot pedals on a helicopter control |
Yaw |
|
|
|
To tilt a helicopter forward what must the pilot do |
Push the cyclic forward |
|
|
|
Besides lift, what else does the main rotor provided on a helicopter |
Lateral and longitudinal movement |
|
|
|
What is the purpose of the tail rotor on a helicopter |
To stabilize the aircraft and can move the aircraft |
|
|
|
What are the three controls used to maneuver a helicopter |
Collective, cyclic, footpedals |
|
|
|
Raising what helicopter control will cause a helicopter to increase in altitude |
Collective |
|
|
|
What did the foot pedals on a helicopter control |
Yaw |
|
|
|
To tilt a helicopter forward what must the pilot do |
Push the cyclic forward |
|
|
|
Which AHHS component is the brain of the system |
System interface unit (SIU) |
|
|
|
Besides lift, what else does the main rotor provided on a helicopter |
Lateral and longitudinal movement |
|
|
|
What is the purpose of the tail rotor on a helicopter |
To stabilize the aircraft and can move the aircraft |
|
|
|
What are the three controls used to maneuver a helicopter |
Collective, cyclic, footpedals |
|
|
|
Raising what helicopter control will cause a helicopter to increase in altitude |
Collective |
|
|
|
What did the foot pedals on a helicopter control |
Yaw |
|
|
|
To tilt a helicopter forward what must the pilot do |
Push the cyclic forward |
|
|
|
Which AHHS component is the brain of the system |
System interface unit (SIU) |
|
|
|
What controls the AHHS fail and boost servo off light on the caution advisory panel |
The forward relay unit FRU |
|
|
|
Besides lift, what else does the main rotor provided on a helicopter |
Lateral and longitudinal movement |
|
|
|
What is the purpose of the tail rotor on a helicopter |
To stabilize the aircraft and can move the aircraft |
|
|
|
What are the three controls used to maneuver a helicopter |
Collective, cyclic, footpedals |
|
|
|
Raising what helicopter control will cause a helicopter to increase in altitude |
Collective |
|
|
|
What did the foot pedals on a helicopter control |
Yaw |
|
|
|
To tilt a helicopter forward what must the pilot do |
Push the cyclic forward |
|
|
|
Which AHHS component is the brain of the system |
System interface unit (SIU) |
|
|
|
What controls the AHHS fail and boost servo off light on the caution advisory panel |
The forward relay unit FRU |
|
|
|
What VSI indication is illuminated when AHHS is engaged |
Go around light |
|
|
|
Besides lift, what else does the main rotor provided on a helicopter |
Lateral and longitudinal movement |
|
|
|
What is the purpose of the tail rotor on a helicopter |
To stabilize the aircraft and can move the aircraft |
|
|
|
What are the three controls used to maneuver a helicopter |
Collective, cyclic, footpedals |
|
|
|
Raising what helicopter control will cause a helicopter to increase in altitude |
Collective |
|
|
|
What did the foot pedals on a helicopter control |
Yaw |
|
|
|
To tilt a helicopter forward what must the pilot do |
Push the cyclic forward |
|
|
|
Which AHHS component is the brain of the system |
System interface unit (SIU) |
|
|
|
What controls the AHHS fail and boost servo off light on the caution advisory panel |
The forward relay unit FRU |
|
|
|
What VSI indication is illuminated when AHHS is engaged |
Go around light |
|
|
|
What information does the collective command pointer provide |
Indicates AHHS vertical velocity up to 500 ft./m |
|
|
|
Besides lift, what else does the main rotor provided on a helicopter |
Lateral and longitudinal movement |
|
|
|
How are the four modes of AHHS operation selected |
The system control unit (SCU) |
|
|
|
What is the purpose of the tail rotor on a helicopter |
To stabilize the aircraft and can move the aircraft |
|
|
|
What are the three controls used to maneuver a helicopter |
Collective, cyclic, footpedals |
|
|
|
Raising what helicopter control will cause a helicopter to increase in altitude |
Collective |
|
|
|
What did the foot pedals on a helicopter control |
Yaw |
|
|
|
To tilt a helicopter forward what must the pilot do |
Push the cyclic forward |
|
|
|
Which AHHS component is the brain of the system |
System interface unit (SIU) |
|
|
|
What controls the AHHS fail and boost servo off light on the caution advisory panel |
The forward relay unit FRU |
|
|
|
What VSI indication is illuminated when AHHS is engaged |
Go around light |
|
|
|
What information does the collective command pointer provide |
Indicates AHHS vertical velocity up to 500 ft./m |
|
|
|
When cycled what AHHS component decreases the aircraft speed to zero knots |
The AHHS zero button |
|
|
|
When cycled what AHHS component decreases the aircraft speed to zero knots |
The AHHS zero button |
|
|
|
What does the BAR ALT hold mode control |
The collectives position to maintain selected altitude |
|
|
|
When cycled what AHHS component decreases the aircraft speed to zero knots |
The AHHS zero button |
|
|
|
What does the BAR ALT hold mode control |
The collectives position to maintain selected altitude |
|
|
|
What is operational range of the barometric altimeter mode |
-1000 feet to 10,000 feet |
|
|
|
When cycled what AHHS component decreases the aircraft speed to zero knots |
The AHHS zero button |
|
|
|
What does the BAR ALT hold mode control |
The collectives position to maintain selected altitude |
|
|
|
What is operational range of the barometric altimeter mode |
-1000 feet to 10,000 feet |
|
|
|
What is operational range of the radar altimeter mode |
0 to 1500 feet |
|
|
|
When cycled what AHHS component decreases the aircraft speed to zero knots |
The AHHS zero button |
|
|
|
What does the BAR ALT hold mode control |
The collectives position to maintain selected altitude |
|
|
|
What is operational range of the barometric altimeter mode |
-1000 feet to 10,000 feet |
|
|
|
What is operational range of the radar altimeter mode |
0 to 1500 feet |
|
|
|
What must the helicopters groundspeed be for hover stabilization mode activation |
Less than 20 kn |
|
|
|
When cycled what AHHS component decreases the aircraft speed to zero knots |
The AHHS zero button |
|
|
|
What does the BAR ALT hold mode control |
The collectives position to maintain selected altitude |
|
|
|
What is operational range of the barometric altimeter mode |
-1000 feet to 10,000 feet |
|
|
|
What is operational range of the radar altimeter mode |
0 to 1500 feet |
|
|
|
What must the helicopters groundspeed be for hover stabilization mode activation |
Less than 20 kn |
|
|
|
Which helicopter control mode provides control of the left and right, forward and aft, and altitude axis |
Hover radar (HOV RA) |
|
|
|
When cycled what AHHS component decreases the aircraft speed to zero knots |
The AHHS zero button |
|
|
|
What does the BAR ALT hold mode control |
The collectives position to maintain selected altitude |
|
|
|
What is operational range of the barometric altimeter mode |
-1000 feet to 10,000 feet |
|
|
|
What is operational range of the radar altimeter mode |
0 to 1500 feet |
|
|
|
What must the helicopters groundspeed be for hover stabilization mode activation |
Less than 20 kn |
|
|
|
Which helicopter control mode provides control of the left and right, forward and aft, and altitude axis |
Hover radar (HOV RA) |
|
|
|
What interrupt the AHHS system from driving if the helicopter lands with the HOV/RA mode engaged |
The loss of weight on wheels |
|
|
|
When cycled what AHHS component decreases the aircraft speed to zero knots |
The AHHS zero button |
|
|
|
What does the BAR ALT hold mode control |
The collectives position to maintain selected altitude |
|
|
|
What is operational range of the barometric altimeter mode |
-1000 feet to 10,000 feet |
|
|
|
What is operational range of the radar altimeter mode |
0 to 1500 feet |
|
|
|
What must the helicopters groundspeed be for hover stabilization mode activation |
Less than 20 kn |
|
|
|
Which helicopter control mode provides control of the left and right, forward and aft, and altitude axis |
Hover radar (HOV RA) |
|
|
|
What interrupt the AHHS system from driving if the helicopter lands with the HOV/RA mode engaged |
The loss of weight on wheels |
|
|
|
What provides the SRU with a WOW discreet |
The stability augmentation system/flightpath stabilization |
|
|
|
When cycled what AHHS component decreases the aircraft speed to zero knots |
The AHHS zero button |
|
|
|
What does the BAR ALT hold mode control |
The collectives position to maintain selected altitude |
|
|
|
What is operational range of the barometric altimeter mode |
-1000 feet to 10,000 feet |
|
|
|
What is operational range of the radar altimeter mode |
0 to 1500 feet |
|
|
|
What must the helicopters groundspeed be for hover stabilization mode activation |
Less than 20 kn |
|
|
|
Which helicopter control mode provides control of the left and right, forward and aft, and altitude axis |
Hover radar (HOV RA) |
|
|
|
What interrupt the AHHS system from driving if the helicopter lands with the HOV/RA mode engaged |
The loss of weight on wheels |
|
|
|
What provides the SRU with a WOW discreet |
The stability augmentation system/flightpath stabilization |
|
|
|
What component tells the SIU which mode has been selected |
SCU |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What force allows an aircraft to overcome gravity during flight |
Lift |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What force allows an aircraft to overcome gravity during flight |
Lift |
|
|
|
The longitudinal or Rolexes extends lengthwise from the |
Nose to tail |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What force allows an aircraft to overcome gravity during flight |
Lift |
|
|
|
The longitudinal or Rolexes extends lengthwise from the |
Nose to tail |
|
|
|
The ailerons are moved by |
Turning the control wheels |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What force allows an aircraft to overcome gravity during flight |
Lift |
|
|
|
The longitudinal or Rolexes extends lengthwise from the |
Nose to tail |
|
|
|
The ailerons are moved by |
Turning the control wheels |
|
|
|
What produces a nose up or nose down attitude of the aircraft |
Elevators simultaneously deflected up or down |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What force allows an aircraft to overcome gravity during flight |
Lift |
|
|
|
The longitudinal or Rolexes extends lengthwise from the |
Nose to tail |
|
|
|
The ailerons are moved by |
Turning the control wheels |
|
|
|
What produces a nose up or nose down attitude of the aircraft |
Elevators simultaneously deflected up or down |
|
|
|
What is the purpose of aircraft flaps |
Increase or decrease lift |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What force allows an aircraft to overcome gravity during flight |
Lift |
|
|
|
The longitudinal or Rolexes extends lengthwise from the |
Nose to tail |
|
|
|
The ailerons are moved by |
Turning the control wheels |
|
|
|
What produces a nose up or nose down attitude of the aircraft |
Elevators simultaneously deflected up or down |
|
|
|
What is the purpose of aircraft flaps |
Increase or decrease lift |
|
|
|
What is the only intended use for manual movement of the |
Ground operation |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What force allows an aircraft to overcome gravity during flight |
Lift |
|
|
|
The longitudinal or Rolexes extends lengthwise from the |
Nose to tail |
|
|
|
The ailerons are moved by |
Turning the control wheels |
|
|
|
What produces a nose up or nose down attitude of the aircraft |
Elevators simultaneously deflected up or down |
|
|
|
What is the purpose of aircraft flaps |
Increase or decrease lift |
|
|
|
What is the only intended use for manual movement of the |
Ground operation |
|
|
|
What type of flight control system is the most commonly used |
Hydromechanical |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What force allows an aircraft to overcome gravity during flight |
Lift |
|
|
|
The longitudinal or Rolexes extends lengthwise from the |
Nose to tail |
|
|
|
The ailerons are moved by |
Turning the control wheels |
|
|
|
What produces a nose up or nose down attitude of the aircraft |
Elevators simultaneously deflected up or down |
|
|
|
What is the purpose of aircraft flaps |
Increase or decrease lift |
|
|
|
What is the only intended use for manual movement of the |
Ground operation |
|
|
|
What type of flight control system is the most commonly used |
Hydromechanical |
|
|
|
What device will limit the external wind forces from damaging the aircraft while it is parked or tied down |
Gust locks |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
Hydraulic powered actuators convert hydraulic pressure into |
Control surface movements |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What force allows an aircraft to overcome gravity during flight |
Lift |
|
|
|
The longitudinal or Rolexes extends lengthwise from the |
Nose to tail |
|
|
|
The ailerons are moved by |
Turning the control wheels |
|
|
|
What produces a nose up or nose down attitude of the aircraft |
Elevators simultaneously deflected up or down |
|
|
|
What is the purpose of aircraft flaps |
Increase or decrease lift |
|
|
|
What is the only intended use for manual movement of the |
Ground operation |
|
|
|
What type of flight control system is the most commonly used |
Hydromechanical |
|
|
|
What device will limit the external wind forces from damaging the aircraft while it is parked or tied down |
Gust locks |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
Hydraulic powered actuators convert hydraulic pressure into |
Control surface movements |
|
|
|
The aileron trim indicator displays the aileron trim tab position in degrees up or down from the |
Neutral position |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What force allows an aircraft to overcome gravity during flight |
Lift |
|
|
|
The longitudinal or Rolexes extends lengthwise from the |
Nose to tail |
|
|
|
The ailerons are moved by |
Turning the control wheels |
|
|
|
What produces a nose up or nose down attitude of the aircraft |
Elevators simultaneously deflected up or down |
|
|
|
What is the purpose of aircraft flaps |
Increase or decrease lift |
|
|
|
What is the only intended use for manual movement of the |
Ground operation |
|
|
|
What type of flight control system is the most commonly used |
Hydromechanical |
|
|
|
What device will limit the external wind forces from damaging the aircraft while it is parked or tied down |
Gust locks |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
Hydraulic powered actuators convert hydraulic pressure into |
Control surface movements |
|
|
|
The aileron trim indicator displays the aileron trim tab position in degrees up or down from the |
Neutral position |
|
|
|
The automatic flight control system is capable of maintaining an aircraft at a constant heading, pitch or roll attitude and, |
Altitude |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What force allows an aircraft to overcome gravity during flight |
Lift |
|
|
|
The longitudinal or Rolexes extends lengthwise from the |
Nose to tail |
|
|
|
The ailerons are moved by |
Turning the control wheels |
|
|
|
What produces a nose up or nose down attitude of the aircraft |
Elevators simultaneously deflected up or down |
|
|
|
What is the purpose of aircraft flaps |
Increase or decrease lift |
|
|
|
What is the only intended use for manual movement of the |
Ground operation |
|
|
|
What type of flight control system is the most commonly used |
Hydromechanical |
|
|
|
What device will limit the external wind forces from damaging the aircraft while it is parked or tied down |
Gust locks |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
Hydraulic powered actuators convert hydraulic pressure into |
Control surface movements |
|
|
|
The aileron trim indicator displays the aileron trim tab position in degrees up or down from the |
Neutral position |
|
|
|
The automatic flight control system is capable of maintaining an aircraft at a constant heading, pitch or roll attitude and, |
Altitude |
|
|
|
The automatic flight control processor will position the servos in response to guidance commands or manual commands from the |
Flight control panel |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What force allows an aircraft to overcome gravity during flight |
Lift |
|
|
|
The longitudinal or Rolexes extends lengthwise from the |
Nose to tail |
|
|
|
The ailerons are moved by |
Turning the control wheels |
|
|
|
What produces a nose up or nose down attitude of the aircraft |
Elevators simultaneously deflected up or down |
|
|
|
What is the purpose of aircraft flaps |
Increase or decrease lift |
|
|
|
What is the only intended use for manual movement of the |
Ground operation |
|
|
|
What type of flight control system is the most commonly used |
Hydromechanical |
|
|
|
What device will limit the external wind forces from damaging the aircraft while it is parked or tied down |
Gust locks |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
Hydraulic powered actuators convert hydraulic pressure into |
Control surface movements |
|
|
|
The aileron trim indicator displays the aileron trim tab position in degrees up or down from the |
Neutral position |
|
|
|
The automatic flight control system is capable of maintaining an aircraft at a constant heading, pitch or roll attitude and, |
Altitude |
|
|
|
The automatic flight control processor will position the servos in response to guidance commands or manual commands from the |
Flight control panel |
|
|
|
What switch commands the automatic flight control system to capture and maintain the aircraft airspeed at the time of engagement |
Speed on pitch |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What force allows an aircraft to overcome gravity during flight |
Lift |
|
|
|
The longitudinal or Rolexes extends lengthwise from the |
Nose to tail |
|
|
|
The ailerons are moved by |
Turning the control wheels |
|
|
|
What produces a nose up or nose down attitude of the aircraft |
Elevators simultaneously deflected up or down |
|
|
|
What is the purpose of aircraft flaps |
Increase or decrease lift |
|
|
|
What is the only intended use for manual movement of the |
Ground operation |
|
|
|
What type of flight control system is the most commonly used |
Hydromechanical |
|
|
|
What device will limit the external wind forces from damaging the aircraft while it is parked or tied down |
Gust locks |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
Hydraulic powered actuators convert hydraulic pressure into |
Control surface movements |
|
|
|
The aileron trim indicator displays the aileron trim tab position in degrees up or down from the |
Neutral position |
|
|
|
The automatic flight control system is capable of maintaining an aircraft at a constant heading, pitch or roll attitude and, |
Altitude |
|
|
|
The automatic flight control processor will position the servos in response to guidance commands or manual commands from the |
Flight control panel |
|
|
|
What switch commands the automatic flight control system to capture and maintain the aircraft airspeed at the time of engagement |
Speed on pitch |
|
|
|
What is not a vertical mode of the automatic flight control system |
Heading |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What force allows an aircraft to overcome gravity during flight |
Lift |
|
|
|
The longitudinal or Rolexes extends lengthwise from the |
Nose to tail |
|
|
|
The ailerons are moved by |
Turning the control wheels |
|
|
|
What produces a nose up or nose down attitude of the aircraft |
Elevators simultaneously deflected up or down |
|
|
|
What is the purpose of aircraft flaps |
Increase or decrease lift |
|
|
|
What is the only intended use for manual movement of the |
Ground operation |
|
|
|
What type of flight control system is the most commonly used |
Hydromechanical |
|
|
|
What device will limit the external wind forces from damaging the aircraft while it is parked or tied down |
Gust locks |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
Hydraulic powered actuators convert hydraulic pressure into |
Control surface movements |
|
|
|
The aileron trim indicator displays the aileron trim tab position in degrees up or down from the |
Neutral position |
|
|
|
The automatic flight control system is capable of maintaining an aircraft at a constant heading, pitch or roll attitude and, |
Altitude |
|
|
|
The automatic flight control processor will position the servos in response to guidance commands or manual commands from the |
Flight control panel |
|
|
|
What switch commands the automatic flight control system to capture and maintain the aircraft airspeed at the time of engagement |
Speed on pitch |
|
|
|
What is not a vertical mode of the automatic flight control system |
Heading |
|
|
|
Flight control system attitude source selection is done |
Automatically |
|
|
|
What provides access the platform aircraft engine maintenance and service |
Cargo door |
|
|
|
What force allows an aircraft to overcome gravity during flight |
Lift |
|
|
|
The longitudinal or Rolexes extends lengthwise from the |
Nose to tail |
|
|
|
The ailerons are moved by |
Turning the control wheels |
|
|
|
What produces a nose up or nose down attitude of the aircraft |
Elevators simultaneously deflected up or down |
|
|
|
What is the purpose of aircraft flaps |
Increase or decrease lift |
|
|
|
What is the only intended use for manual movement of the |
Ground operation |
|
|
|
What type of flight control system is the most commonly used |
Hydromechanical |
|
|
|
What device will limit the external wind forces from damaging the aircraft while it is parked or tied down |
Gust locks |
|
|
|
What is not monitored by the engine indicating system |
Hydraulic temperature |
|
|
|
Hydraulic powered actuators convert hydraulic pressure into |
Control surface movements |
|
|
|
The aileron trim indicator displays the aileron trim tab position in degrees up or down from the |
Neutral position |
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The automatic flight control system is capable of maintaining an aircraft at a constant heading, pitch or roll attitude and, |
Altitude |
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The automatic flight control processor will position the servos in response to guidance commands or manual commands from the |
Flight control panel |
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What switch commands the automatic flight control system to capture and maintain the aircraft airspeed at the time of engagement |
Speed on pitch |
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What is not a vertical mode of the automatic flight control system |
Heading |
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Flight control system attitude source selection is done |
Automatically |
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Before working in a flight control surface area |
Disable and tag the system |
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What provides access the platform aircraft engine maintenance and service |
Cargo door |
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What force allows an aircraft to overcome gravity during flight |
Lift |
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The longitudinal or Rolexes extends lengthwise from the |
Nose to tail |
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The ailerons are moved by |
Turning the control wheels |
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What produces a nose up or nose down attitude of the aircraft |
Elevators simultaneously deflected up or down |
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What is the purpose of aircraft flaps |
Increase or decrease lift |
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What is the only intended use for manual movement of the |
Ground operation |
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What type of flight control system is the most commonly used |
Hydromechanical |
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What device will limit the external wind forces from damaging the aircraft while it is parked or tied down |
Gust locks |
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Increased |
Increased |
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