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EAWS > BOOK TWO, BLOCK I AIRFRAME > Flashcards

BOOK TWO, BLOCK I AIRFRAME Flashcards

1
Q

P-3 AIRCRAFT SAFETY AREAS (A,B)

A

SAFETY DIAMOND+FIVE FEET, GROUND SAFETY DOWNLOCK PINS IN LANDING GEAR

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2
Q

P-3 AIRCRAFT SAFETY AREAS (C,D)

A

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.

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3
Q

P-8A SAFETY AREAS (A,B)

A

SAFETY DIAMOND AREA, GROUND SAFETY DOWNLOCK PINS ARE INSTALLED ON ALL LANDING GEAR

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4
Q

P-8A SAFETY AREAS (C,D)

A

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.

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5
Q

AIRCRAFT WARNING PLACARDS

A

ON EXTERIOR OF AIRCRAFT ALERT PERSONNEL OF SPECFIC RISK AREAS;INTAKES,WEAPONS BAY.

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6
Q

WING CONTROL SURFACES

A

BE AWARE OF MOVING FLIGHT CONTROL SURFACES AND LOW CLEARANCE,USE OBSERVER, CAN CAUSE SERIOUS INJURY,DEATH,EQUIPMENT DAMAGE

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7
Q

MATERIALS AND CORROSION:P3C

A

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

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8
Q

MATERIALS AND CORROSION:P8A

A

ALL METAL CONSTRUCTION. CORROSION OCCURS OFTEN IN SEAMS OF ALLUMINUM ALLOY, UNPAINTED, ACTUATING MECHANISMS, CREVICES.

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9
Q

FUSELAGE: P3C

A

FORWARD SECTION WITH FLIGHT STATION, MID-BODY SECTION, AFT FUSELAGE SECTION AND TAILCONE

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10
Q

FUSELAGE:P8A

A

FOWARD SECTION ENCOMPASSING THE FLIGHT STATION, MID BODY SECTION, AFT FUSELAGE SECTION INCLUDING TAIL CONE.

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11
Q

WINGS, STABILIZERS, RUDDERS, AILERONS, FLAPS: WINGS P3C

A

WINGS: CENTER-BUILT AS INTEGRAL PART OF THE FUSELAGE, OUTER WINGS: CONSIST OF WING FLAPS, LEADING AND TRAILING EDGE, WINGTIPS, AILERONS, ENGINE NACELLES

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12
Q

WING FLAPS:P3C

A

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.

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13
Q

STABILIZERS:P3C (A) HORIZONTAL

A

(LONGITUDINAL STABILITY) PROVIDE STABILITY ABOUT THE LATERAL AXIS. BASE IN WHICH ELEVATORS ARE ATTACHED.

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14
Q

STABILIZERS:P3C (B) VERTICAL

A

DIRECTIONAL STABILITY.MAINTAINS DIRECTIONAL STABILITY ABOUT THE VERTICAL AXIS.

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15
Q

STABILIZERS:P3C AILERONS

A

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.

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16
Q

stabilizers: P3C ELEVATORS

A

RESPONSIBLE FOR CLIMB. ACHIEVED BY FORE AND AFT MOVEMENT OF CONTROL STICK.

17
Q

stabilizers: P3C AUTOPILOT

A

CONTROLS AND STABILIZE THE AIFCRAFT ABOUT IT’S THREE AXES.

18
Q

p8A: WINGS

A

BOEING 737-900 WINGS. LEADING AND TRAILING EDGE, AILERONS, FLAPS, SLATS, SPOILERS, ENGINE MOUNTS, OPTIONAL WEAPONS PYLONS.

19
Q

P8A: FLAPS AND SLATS

A

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.

20
Q

P8A: flight spoilers

A

four located on upper surface of each wing. speed brakes on ground.

21
Q

p8a: autopilot

A

control and stabilize aircraft about it’s three axes.

22
Q

P3C: LANDING GEAR

A

TWO MLG’S, NOSE GEAR. DUAL WHEELS, FORWARD RETRACTING STRUTS. WEIGHT OF AIRCRAFT KEEPS IT DOWN AND LOCKED.

23
Q

P3C: LANDING GEAR:struts

A

ABSORBS SHOCK THAT OTHERWISE WOULD BE SUSTAINED BY THE AIRCRAFT STRUCTURE DURING TAKEOFF, TAXING, AND LANDING.

24
Q

P3C: LANDING GEAR;BRAKES

A

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.

25
Q

P3C: LANDING GEAR;PARKING BRAKE

A

THE PARKING BRAKES ARE SET BY DEPRESSING THE TOE PEDALS AND PULLING THE T-HANDLE , LOCATED ON THE PILOTS INSTRUMENT PANEL. THIS LOCKS THE BRAKE CONTROL VALVES INTHE OPEN POSITION. THE BRAKE ACCUMULATOR WILL KEEP THE BRAKES CHARGED WITHOUT RECHARGING FOR 8 HOURS.

26
Q

P3C: LANDING GEAR;WHEELS

A

EACH P-3 LANDING GEAR CONSISTS OF A DUAL WHEELS MOUNTED ON EACH STRUT.

27
Q

P8A:LANDING GEAR;

A

FULLY RETRACTABLE TRICYCLE TYPE GEAR DESIGNED WITH AIR/OIL STRUTS CONSISTING OF TWO MAIN LANDING GEAR AND A SINGLE NOSE GEAR. THE NOSE EXTENDS DOWN AND AFT, MAIN EXTENDS DOWN AND SIDEWAYS. TWO WHEEL GEAR UNITS, NOSE IS STEERABLE

28
Q

P8A:LANDING GEAR; STRUTS

A

ABSORBS THE SHOCK THAT OTHERWISE WOULD BE SUSTAINED BY THE AIRCRAFT STRUCTURE DURING TAKEOFF AND TAXING AND LANDING.

29
Q

P8A:LANDING GEAR; BRAKES

A

EACH MAIN GEAR HAS A MULTI-DISC HYDRAULIC POWERED BRAKE.THE BRAKE PEDALS PROVIDE INDIVIDUAL CONTROLOF THE LEFT AND RIGHT BRAKES. NOSE HAS NO BRAKES.

30
Q

P8A:LANDING GEAR; ANTI SKID PROTECTION

A

PROVIDED IN THE NORMAL AND ALTERNATE BRAKE SYSTEM. THE NORMAL BRAKE HYDRAULIC SYSTEM PROVIDES EACH MAIN GEAR WITH INDIVIDUAL ANTISKID PROTECTION. WHEN THE SYTEM DETECTS A SKID, THE ASSOCIATED ANTI SKID VALVE REDUCES BRAKE PRESSURE UNTIL SKIDDING STOPS.

31
Q

P8A:LANDING GEAR; AUTOBRAKE SYSTEM

A

USES HYDRAULIC SYSTEM PRESSURE TO PROVIDE MAXIMUM DECELERATION FOR THE REJECTED TAKEOFF AND AUTOMATIC BRAKING AT PRESELECTED DECELERATION RATES IMMEDIATELY AFTER TOUCHDOWN.

32
Q

P8A:LANDING GEAR; PARKING BRAKE

A

CAN BE SET WITH EITHER HYDRAULIC SYSTEM’S PRESSURE OR FROM THE BRAKE ACCUMULATOR.

33
Q

P8A:LANDING GEAR; WHEELS

A

DUAL WHEEL ASSEMBLY MOUNTED ON STRUT

34
Q

P3C ACCESS POINTS

A

5 AVAILABLE ACCESS POINTS;TWO IN THE FLIGHT STATION,TWO IN MID-BODY, ONE AFT OF PORT WING(MIAN ENTRY)

35
Q

P8A ACCESS POINTS

A

TWO OVER WING EXITS (LEFT AND RIGHT). ONE ENTRY DOOR, ONE SERVICE DOOR, ONE BAILOUT EGRES DOOR, AND ONE CARGO DOOR

EAWS (24 decks)

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