BOOK TWO, BLOCK I AIRFRAME Flashcards
(35 cards)
P-3 AIRCRAFT SAFETY AREAS (A,B)
SAFETY DIAMOND+FIVE FEET, GROUND SAFETY DOWNLOCK PINS IN LANDING GEAR
P-3 AIRCRAFT SAFETY AREAS (C,D)
WHEN FLOOR PANELS HAVE BEEN REMOVED A BARRIER AND WARNING PLACARD MUST BE PLACED AROUND OPENING, UTILIZE AN OUTSIDE OBSERVER WHEN OPERATING FLIGHT CONTROL SURFACES.
P-8A SAFETY AREAS (A,B)
SAFETY DIAMOND AREA, GROUND SAFETY DOWNLOCK PINS ARE INSTALLED ON ALL LANDING GEAR
P-8A SAFETY AREAS (C,D)
WHEN FLOOR PANELS HAVE BEEN REMOVED A BARRIER AND WARNING PLACARD MUST BE PLACED AROUND OPENING, UTILIZE AN OUTSIDE OBSERVER WHEN OPERATING FLIGHT CONTROL SURFACES.
AIRCRAFT WARNING PLACARDS
ON EXTERIOR OF AIRCRAFT ALERT PERSONNEL OF SPECFIC RISK AREAS;INTAKES,WEAPONS BAY.
WING CONTROL SURFACES
BE AWARE OF MOVING FLIGHT CONTROL SURFACES AND LOW CLEARANCE,USE OBSERVER, CAN CAUSE SERIOUS INJURY,DEATH,EQUIPMENT DAMAGE
MATERIALS AND CORROSION:P3C
ALL METAL EXCEPT RADOMES,NOSE AND WINGTIPS. CORROSION COMMON IN ALUMINUM ALLOY SEAMS,BOX BEAM SKIN AREAS AROUND PLATED STEEL FASTENERS, UNPAINTED OR AREAS WITH CHIPPED PAINT(ACTUATING MECHANISMS,CREVICES
MATERIALS AND CORROSION:P8A
ALL METAL CONSTRUCTION. CORROSION OCCURS OFTEN IN SEAMS OF ALLUMINUM ALLOY, UNPAINTED, ACTUATING MECHANISMS, CREVICES.
FUSELAGE: P3C
FORWARD SECTION WITH FLIGHT STATION, MID-BODY SECTION, AFT FUSELAGE SECTION AND TAILCONE
FUSELAGE:P8A
FOWARD SECTION ENCOMPASSING THE FLIGHT STATION, MID BODY SECTION, AFT FUSELAGE SECTION INCLUDING TAIL CONE.
WINGS, STABILIZERS, RUDDERS, AILERONS, FLAPS: WINGS P3C
WINGS: CENTER-BUILT AS INTEGRAL PART OF THE FUSELAGE, OUTER WINGS: CONSIST OF WING FLAPS, LEADING AND TRAILING EDGE, WINGTIPS, AILERONS, ENGINE NACELLES
WING FLAPS:P3C
high-lift fowler type, powered by hydraulic systems. uses A COMBO OF AFT MOVEMENT TO INCREASE THE WING AREA, AND A DROOPING MOVEMENT TO CHANGE THE AIRFOIL SECTION.
STABILIZERS:P3C (A) HORIZONTAL
(LONGITUDINAL STABILITY) PROVIDE STABILITY ABOUT THE LATERAL AXIS. BASE IN WHICH ELEVATORS ARE ATTACHED.
STABILIZERS:P3C (B) VERTICAL
DIRECTIONAL STABILITY.MAINTAINS DIRECTIONAL STABILITY ABOUT THE VERTICAL AXIS.
STABILIZERS:P3C AILERONS
OPERATED BY LATERAL SIDE TO SIDE MOVEMENT OF THE CONTROL STICK OR A TURNING MOTION OF THE WHEEL. INTERCONNECTED TO WORK SIMULTANEOUSLY, BUT IN OPPSITE DIRECTION. DOWNWARD TO INCREASE LIFT, OTHER MOVES UPWARD TO DECREASE LIFT. CREATES CONTROLLED ROLL.
stabilizers: P3C ELEVATORS
RESPONSIBLE FOR CLIMB. ACHIEVED BY FORE AND AFT MOVEMENT OF CONTROL STICK.
stabilizers: P3C AUTOPILOT
CONTROLS AND STABILIZE THE AIFCRAFT ABOUT IT’S THREE AXES.
p8A: WINGS
BOEING 737-900 WINGS. LEADING AND TRAILING EDGE, AILERONS, FLAPS, SLATS, SPOILERS, ENGINE MOUNTS, OPTIONAL WEAPONS PYLONS.
P8A: FLAPS AND SLATS
HIGH LIFT DEVICES, INCREASE LIFT AND DECREASE STALL SPEED DURING TAKEOFF, LOW SPEED MANEUVERING AND LANDING. LE DEVICES CONSIST OF FOUR FLAPS AND EIGHT SLATS. TRAILING EDGE DEVICES TWO FLAPS INBOARD AND FOUR SLATS OUTBOARD OF EACH ENGINE.
P8A: flight spoilers
four located on upper surface of each wing. speed brakes on ground.
p8a: autopilot
control and stabilize aircraft about it’s three axes.
P3C: LANDING GEAR
TWO MLG’S, NOSE GEAR. DUAL WHEELS, FORWARD RETRACTING STRUTS. WEIGHT OF AIRCRAFT KEEPS IT DOWN AND LOCKED.
P3C: LANDING GEAR:struts
ABSORBS SHOCK THAT OTHERWISE WOULD BE SUSTAINED BY THE AIRCRAFT STRUCTURE DURING TAKEOFF, TAXING, AND LANDING.
P3C: LANDING GEAR;BRAKES
EACH MAIN GEAR WHEEL HAS A MULTI-DISC HYDRAULIC POWERED BRAKE. THE BRAKE PEDALS PROVIDE INDEPENDENT CONTROL OF THE LEFT AND RIGHT BRAKES. NOSE WHEELS HAVE NO BRAKES.
