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66 Cards in this Set
- Front
- Back
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What are the 7 primary mission areas of Maritime Patrol Aircraft(MPA)?
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1.Anti Surface Warfare(ASU)
2.Anti Submarine Warfare(ASW) 3.Command & Control(C2W) 4.Command, Control, Communication(CCC) 5.Intelligence(INT) 6.Mine Warfare(MIW) 7.Mobility(MOB) |
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What are the 5 conditions of flight according to NATOPS?
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Condition 1-Battle
Condition 2-Transit/High alt ASW Condition 3-Equipment Status Check Condition 4-Aircraft Status Inspection Condition 5- Taxi/Takeoff/Landing/Turbulance |
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Purpose of Search Stores?
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Localize and track enemy submarines and other sea going vessels.
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Purpose of Kill Stores.
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Attack and destroy enemy subs
and sea going vessels. |
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AGM
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Air launched, surface attack, guided missile
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ATM
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Air launched, training, guided missile
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CATM
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Captive air launched, training missile
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What types of air laid mines are used by the P-3 aircraft?
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-MK-55: 2200 lbs.
-MK-60: 2500 lbs. -MK-62/63/64: Quickstrike, 500-1000 lbs. -MK-25/36/65:Quckstrike, 200 lbs. |
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AGM-84 Harpoon
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All weather anti-ship missile
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AGM-65 Maverick
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Laser guided, rocket propelled, air to ground missile.
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AGM-84E SLAM
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Standoff land-attack missile.
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What two types of torpedoes are used by the P-3C aircraft?
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-MK-50
-MK-46 |
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What are the 3 basic types of sonobouys?
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-Passive
-Active -Special Purpose |
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What is the purpose of the MK-84 Signal Underwater Sound(SUS)?
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Signal underwater targets/friendly subs during ASW.
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What are the 3 types of deployable countermeasures?
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-Chaffs
-Flares -Jammers |
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What is a pyrotechnic device?
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Items that produce bright light for illumination or colored lights/smoke for signaling.
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What are the 2 types of marine location markers?
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-MK-25:13.5-18.5 min.
-MK-58: 40-60 min. |
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LAU-117 missile launcher
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Maverick launch rack
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Bomb rack
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Carry, arm, and release kill stores from wings stations.
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Pylon
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Suspend launchers or bombs.
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Corrosion prone areas of the P-3C aircraft.
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Metal surfaces exposed to the environment.
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Purpose of the Aircraft Automatic Flight Control System(AFCS) or autopilot.
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Ease pilot workload and provide aircraft stability.
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Type and model of the P-3C engine.
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-T-56A-14
-Provides 4,600 Shaft Horsepower(SHP) for takeoff |
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Purpose of the constant speed propeller.
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Allows engine to maintain 100% RPM.
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P-3C fueling methods
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-Overwing Gravity feed
-Center Point Pressure Fueling |
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Discuss the type of construction used by the P-3C.
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-All metal construction
-Wings: box beam with two main spars -Fuselage: semi monocoque construction consisting of skins, stringers, longerons, and bulkheads or frames. |
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Discuss the landing gear used by the P-3C.
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Fully retractable tricycle type landing gear.
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Discuss the purpose of aircraft cabin pressurization and air conditioning.
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Maintain comfortable environment for aircrew and cooling of avionics.
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Discuss the purpose of aircraft oxygen systems.
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-Survival if cabin pressure is lost.
-3.5 hours for flight station @ 25,000 ft. -7 portable O2 bottles for crew lasting 5-10 min or 22 min max. |
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Foward body section.
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Up to flight station
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Fuselage:Midbody section
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Midsection
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Fuselage:Aft fuselage section
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Tail cone
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Wings: Center section
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Box type beam
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Wings: Outer panels
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Leading edge, trailing edge, flaps, ailerons, wing tips, nacels
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Horizontal stabilizers
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-Located on aft tail cone
-Provide longitudinal stability along the lateral axis |
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Vertical Stabilizer
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-Located on aft tail cone
-Provides directional stability along the vertical axis |
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Flaps
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High lift fowler type.
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Ailerons
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Controls aircraft roll.
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Rudder
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Controls aircraft yaw.
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Elevators
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Controls aircraft pitch
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Trim tabs
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-Neutralize unbalanced conditions
-Recessed in trailing edge of any control surface. |
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Landing gear struts
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-Air oil shock strut
-Absorbs shock otherwise sustained by airframe |
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Brakes
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-4 multiple disc brake assemblies, 1 per each main gear wheel
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Wheels
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-Aluminium or magnesium alloy
-2 types and demounted flange -36 ply tires |
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Hydraulic Pumps
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-Located in HSC
-Electrically Driven variable displacement pumps -Usable output of 8gpm -2gpm tapped off for motor cooling -Low pressure warning @ 1800 psi. |
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Hydraulic reservoirs
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-Located in HSC
-1=5.6 gallons or 5 gallons with filled brake accum and must be services if it falls below -2=1 gallon -must be serviced @ .75 gallon |
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Hydraulic boosters assemblies
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-Ensures pilot has normal feel of control surfaces
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Hydraulic Actuators
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-Transforms hydraulic fluid pressure into mechanical force
-2 types:Actuating cylinders and hydraulic motors |
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Forward radome
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-150 lbs.
-Rain and erosion/ antistatic coating -Braided copper lightning -Houses radar antenna, ESM, and countermeasures sensors |
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Aft radome
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-Houses radar antenna, mad and countermeasure sensors
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Engine Driven Compressor(EDC)
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-Engines 2 and 3
-Heated, compressed air is ducted through two air-cycle cooling units in nose wheel well |
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Cabin exhaust fan
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Draws cooled air through the cabin to keep avionics cool.
Air is then sent out through through outflow valve. |
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Refrigeration Turbine
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Compresses air to 2x it's temp and then cools via rapid expansion.
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Heat exchanger
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Combines het engine bleed air with ram air to cool it.
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Hight Rate Discharge(HRD) bottles
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Engine-2 Bromotriflouromethane bottles. 1 for each pair of engines
-10.5 lbs 600 psi -1 for APU |
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Engine Ice control
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14th stage bleed air prevents ice on:
-Engine air scoop -torque meter -shroud -compressor inlet assembly |
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propeller ice control
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continuous heat applied to front of spinners.
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Wing deice
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14th stage bleed air runs to 6 piccolo tubes along the leading edge.
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Empennage(EMP) deice.
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Stabilizers are electrically heated in system anti-ices parting strips and 20 cycling strips.
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What type of aviators breathing oxygen is used on P-3?
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MIL-0-2721OD
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Engine power section
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-Axial flow compressor
-combustion chamber -multi-stage turbine -exhaust |
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Torque meter
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measures torsional deflection(twist) and it is recorded as horsepower.
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Reduction gear system
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Reduces engine rpm within range of efficient prop rpm.
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Propeller blades
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-Hamilton Standard
-54H60-77 5=Mod# 4=# of blades H=Shank size 60=Spline size 77=minor mod # |
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Who is the SECDEF?
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Leon Penetta
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Who is the SECNAV?
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Ray Mabus
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