EAWS P8 Specifics || All Answers Are Correct 100%.
Dimensions of the p8 correct answers 123 ft 6 inches -wing span
129 ft 5 inches- length 42 ft 9 inches- height
Safety Diamond correct answers nose , wingtips and act of tail
Ground Run-Up Danger Areas correct answers Engine and ApU noise, Radiation Hazard, landing gear areas, wagons bay, flight controls, sonobuoy chut are, lock pins not in, removed floor panels,
Aircraft safety Placards correct answers on exterior of plane to alert personnel to specific risk areas. on engine intakes and weapons bay
Wing Control Surfaces correct answers flaps and slats( movable) can cause damage
Protective finish for corrosion on surface of wings and stabilizer correct answers Cadmium Titanium plating, titanium repairs, aluminum, composites
where are composite materials primarily used correct answers high strength, stiffness and low density requirements
Fuselage Structures correct answers semi-monocoque structure . most materials used are aluminum. attached to fuselage : Nose Radome, wing to body fairing , tailcone
Nose RADOME correct answers fiberglass material.
has navigation and surveillance radar antennas
- has 8 lightning diverted strips .
Primary Flight Controls correct answers Ailerons(2), Rudder(graphite material) ,Elevator(2)
secondary flight controls correct answers Leading edge flaps and slats(12), trailing edge flaps(4) , spoilers and speed brakes (12), Horizontal stab
flight control system components correct answers flight control cables, flight control panel, flight
control hydraulic module package
Flight control Hydraulic Modular Packages correct answers two controls. each has flight shutoff valve, low pressure switch, and spoiler shutoff valve
Stew detection system correct answers used FSEU to monito alignment of TE flaps . uses data from flap skew sensors and flap position transmission LE Autopilot system correct answers if airplane comes to near stall then autoslats function fully extends to LE slats. helps recent stall
Autopilot correct answers to control aircraft about three axis upon pilots selection
Landing Gear correct answers Air/ground system, main landing gear and doors, nose landing gear and doors, landing gear extension and retraction system, wheels and brakes, LG position indicating and earning system, tail skid
Landing gear extension and retraction system correct answers landing gear control system, main landing gear extension and retraction, nose landing gear extension and retraction, main landing gear manual extension system
Wheels and Brakes includes correct answers tires and wheels, hydraulic brake system, parking brake system, anti skid/autobrake system
Tail skid correct answers protects stabilizer bulkhead and fuselage structure when main landing gear shock struts are extended and airplane roared during tskeoff
Autoflight system correct answers DFCS , Yaw damper system, auto throttle
DFCS( digital flight control system) functions correct answers autopilot, flight director, altitude alert, speed trim, mach trim
autopilot correct answers FCC receive inputs from ADIRS and FMC . FCC sends commands to ailerons and elevators . two autopilots / A and B
Flight Director correct answers FCC receive inputs from many systems and send flight director commands to common display system to give guidance for pilots
Altitude alert correct answers when airplane moves from MCP selected altitude and alert occurs
Speed trim correct answers when engine thrust is high and airspeed is low it keeps speed set by pilots to command horizontal stabilizer
Much trim correct answers when speed of the airplane increased the nose starts to go down.
(mach tuck) when the airspeed is more than .615 the mach trim function gives an up elevator to keep nose of airplane level
DFCS( digital flight control system) correct answers had a Mode control Panel(MCP) , two flight
control computers(FCC), and actuator inputs to flight control system . only FCC A does auto throttle
what does the ice and rain protection system keep ice frim correct answers win leading edges, engine inlet cowls, raked wingtips, horizontal stabilizer, air data probe, flight compartment windows, observer window, water and waste system lines and drains, WTAI correct answers wing thermal anti icing . prevents ice on leading edge of wings . uses hot air from pneumatic system to heat three inboard slats
which system use extra mechanical expulsive de icing shstem correct answers raked wingtips and horizontal stabilizer
flight compartment windows correct answers use electric heat to prevent. ice formation, fog, and for impact strength
Crew/service doors correct answers consists of three doors which are hinges , inward- outward opening , plug type doors. forward entry door, forward service door, aft egress doors
Emergency exit doors correct answers two located above each wing. open inside and outside plane. spring loaded vent panel at the top of hatch which is connected to door warning system
Cargo compartment door correct answers right side of fuselage on lower side. door is plug type. opens inward and hinges at top
weapons bay doors correct answers electronically controlled and hydraulically operates .
Miscellaneous exterior service doors correct answers ground air conditioning door, waster device
door, section 48 access and blowout door, engine oil tank access door, external power receptacle door, center fuel tank sump access door, hydraulic brake accumulator access door, waste service panel
Hazards around wmgine correct answers engine inlet suction area, engine exhaust area, anti collision lights
type of Engine on P8 correct answers CFM56-7B . high bypass, dual rotor, axial flow turbofan . it's produces 27300 pounds of trust
Engine sections correct answers Fan and booster, high pressure compressor, combustor, HPT, LPT, accessory drive
Fan and Booster correct answers four stage compressor . the fan is the first stage and the booster is a three stage . fan increases speed of the air and a splitter sends it to primary and secondary air flows
Primary correct answers air flows goes into core of engine . the booster increases pressure of air and send to HPC
Secondary correct answers air flow goes into fan duct . 80 percent of thrust in engine take off is supplies here
