RANDOM Flashcards
(296 cards)
1
Q
another term for routine inspection
A
SCHEDULED INSPECTION
2
Q
another term for non-routine inspection
A
UNPLANNED / UNSCHEDULED INSPECTION
3
Q
servicing of aircraft battery
A
- NEW BATTERY - ELECTROLYTE
- OLD BATTERY - DISTILLED WATER
4
Q
2 types of multimeter
A
- ANALOGUE MULTIMETER
- DIGITAL MULTIMETER
5
Q
it describe the operation of some or all of the engine of an aircraft.
A
AIRCRAFT GROUND RUNNING
6
Q
during engine run-up observe the following: (9)
A
- ENGINE OIL TEMPERATURE
- ENGINE OIL PRESSURE
- STATIC PRESSURE
- ENGINE RESPONSE TO CHANGES IN POWER
- ANY UNUSUAL ENGINE NOISE/VIBRATION
- MAGNETO DROP
- IDLE SPEED
- ALTERNATOR AND AMMETER
- SUCTION GAUGE
7
Q
reading of a suction gauge
A
5 - 5.4 INCH/HG
8
Q
power range of mccauley
A
2280 - 2380 RPM
SPECIFIC = 2375 RPM
9
Q
power range of sensenich
A
2175 - 2280 RPM
SPECIFIC = 2275 RPM
10
Q
magneto drop range
A
NOT HIGHER THAN 50
11
Q
they are equipped with FIXED TUBULAR SPRING-STEEL main gear struts and a steerable nose gear.
A
CESSNA MODEL 152 AND F152 SERIES AIRCRAFTS
12
Q
the ________ has an air/hydraulic fluid shock strut.
A
NOSE GEAR
13
Q
airframe components (4)
A
- WINGS
- EMPENNAGE
- LANDING GEAR
- FUSELAGE
14
Q
is a type of fin with a surface that PRODUCES AERODYNAMIC FORCES facilitating movement through air and other gases.
A
WINGS
15
Q
pressure distribution
A
SKIN TO STRINGERS TO RIBS TO SPARS TO FUSELAGE
16
Q
it hinged surface in the trailing edge of an airplane wing, used to control the roll of an aircraft its longitudinal axis.
A
AILERON
17
Q
it is connected in 2 push-pull rods.
A
BELL CRANKS
18
Q
these are a type of HIGH LIFT DEVICE used to increase the lift of an aircraft wing to a given airspeed.
A
FLAPS
19
Q
provides stability for aircraft, in a way similar to the feathers on an arrow.
A
EMPENNAGE
20
Q
the rear section of the airplane’s body.
A
EMPENNAGE
21
Q
its main purpose is to gives stability to the aircraft
A
EMPENNAGE
22
Q
fixed part of an empennage (2)
A
- HORIZONTAL STABILIZER
- VERTICAL STABILIZER / FIN
23
Q
it usually at the rear on an aircraft, which control the aircraft’s pitch and therefore the angle of attack and the lift of the wing.
A
ELEVATOR
24
Q
types of primary fight control surfaces (3)
A
- AILERON
- RUDDER
- ELEVATOR
25
a VERTICAL airfoil pivoted from the tail plane of an aircraft, for controlling movement about the vertical axis.
RUDDER
26
it is the UNDERCARRIAGE of an aircraft or spacecraft.
LANDING GEAR
27
it is used in both landing and takeoff.
LANDING GEAR
28
arrangements of landing gear (3)
1. TRICYCLE
2. CONVENTIONAL / TAIL WHEEL
3. TANDEM
29
classification of landing gear (2)
1. FIXED LANDING GEAR
2. RETRACTABLE LANDING GEAR
30
the _____________ has a single nose wheel in the front and two or more main wheels slightly aft of the center of gravity.
TRICYCLE ARRANGEMENT
31
it provided for the nose offers resistance to shimmy.
SHIMMY DAMPENER
32
the _______________________ is comprised of two cylinders located immediately forward of the pilot's rudder pedals.
HYDRAULIC BRAKE SYSTEM
33
nose gear
NITROGEN + HYDRAULIC (45 PSI)
34
nose gear (omni used)
COMPRESSED AIR + MIL-H-5605
35
brake lining
0.019 INCH
36
connected to the main structure of wing
SPARS
37
it's connect the structure to fuselage
SPARS
38
it protect the airfoil shape
RIBS
39
brand of landing gear used in omni.
1. MCCAULEY (SPOKES)
2. CLEVELAND (PLAIN)
40
it is an aircraft body body section that holds crew and passengers or cargo.
FUSELAGE
41
material used in wind shield
ACRYCLIC PANELS
42
types of fuselage (2)
1. MONOCOQUE
2. SEMI-MONOCOQUE
43
it is a structural approach whereby loads are supported through an object's external skin, SIMILAR TO AN EGG.
MONOCOQUE
44
it is a hybrid combining a TENSILE SHELL and compressive structure made up of longerons and ribs or frames.
SEMI-MONOCOQUE
45
types of airframe inspection (2)
1. 100 HOURS PARTIAL AND PROGRESSIVE AIRFRAME INSPECTION
2. 200 HOURS COMPLETED AIRFRAME INSPECTION
46
what is IRAN?
INSPECT AND REPAIR AS NECESSARY
47
cable size for primary controls
1/8
48
cable size for secondary controls (2)
FLAPS - 3/32
TRIB TABS - 1/16
49
it is a device used to measure tension in wires, cables, textiles, belts, and more.
TENSION METER
50
the nose wheel deflection _______________ each side.
UP TO 30 DEGREES
51
cessna 172 fuel capacity
FULL TANK = 42 GALLONS (21-21)
STANDARD = 30 GALLONS (15-15)
52
cessna 172 fuel capacity extended
52 GALLONS
(26-26)
53
cessna 152 fuel capacity
FULL TANK = 26 GALLONS (13-13)
STANDARD = 16 GALLONS (8-8)
54
cessna 172 oil capacity
8 QT (IN DIPSTICK)
9 QT
55
cessna 152 oil capacity
6 QT (IN DIPSTICK)
7 QT
56
the nose wheel landing gear is deflection up to ______ degrees in each side.
30
57
statement:
THE AMO (APPROVED MAINTENANCE ORGANIZATION) OF OMNI IS AMO 96-10.
58
those are PERIODIC INSPECTION that have to be done on all commercial/civil aircraft after a certain amount of time or usage.
ROUTINE INSPECTION
59
at least ______ percent of all maintenance actions are non-routine, unplanned, unscheduled events.
40%
60
25 / 75 hours engine inspection (6)
1. ENGINE COWLING
2. IGNITION HARNESS
3. SPARK PLUGS
4. CHECK INTAKE MANIFOLD
5. AIR FILTER
6. DRAIN AND CHANGE OIL
61
25 hours landing gear inspection (3)
1. WHEEL REMOVING
2. CLEAN AND INSPECT
3. REPACKING
62
50 hours inspection (10)
1. PROPELLER SECTION
2. COMPRESSION CHECK
3. ENGINE COMPARTMENT
4. CARBURETOR
5. FUEL INLET
6. OIL FILTER
7. CARB HEAT ASSY
8. OIL SUMP SUCTION SCREEN
9. CARB HEAT INDUCTION
10. FUEL STRAINER BOWL
63
100 hours engine inspection (4)
1. PROPELLER SECTION
2. OIL COOLER
3. FUEL STRAINER BOWL
4. MAGNETO TIMING
64
100 partial / complete hours airframe inspection (3)
1. WING SECTION / CHECK FOR BROKEN CABLES AND SECURITY
2. EMPENNAGE AND STABILIZERS CONTROLS
3. CABIN SECTION
65
the name is derived "the back and forth" movement of the pistons which produces mechanical energy.
RECIPROCATING ENGINE
66
the reciprocating engine operates on the basic principle, where in?
CHEMICAL ENERGY (FUEL / AIR MIXTURE) TO MECHANICAL ENERGY
67
most popular reciprocating engines used on small aircraft
OPPOSED ENGINE
68
have high power to weight ratio because they have small and light weight crankcase
OPPOSED ENGINE
69
the compact cylinder arrangement reduces the engine's frontal are and allows a streamlined installation that minimizes aerodynamic drag
OPPOSED ENGINE
70
it compresses fuel/air mixture
PISTON
71
it receive the chemical energy from expansion of gases
PISTON
72
it simply connect piston and crankshaft
CONNECTING ROD
73
it convert the energy from piston into ROTARY MOTION
CRANKSHAFT
74
it is considered as the backbone of the engine
CRANKSHAFT
75
introduction of fuel/air mixture
INTAKE VALVE
76
removal of burned gases
EXHAUST VALVE
77
for ignition
SPARKPLUG
78
types of propellers (7)
1. FIXED PITCH
2. GROUND ADJUSTABLE PITCH
3. CONTROLLABLE PITCH
4. CONSTANT SPEED
5. REVERSE PITCH
6. FEATHERING
7. TEST CLUB
79
types of propeller tip (2)
1. MCCAULEY
2. SENSENICH
80
controls a mixture needle which restricts the amount of fuel flow in the float chamber
MIXTURE KNOB
81
mixture adjustment required for changes in air density (changes in altitude)
MIXTURE KNOB
82
benefits of properly leaned engines (2)
1. BETTER ENGINE PERFORMANCE
2. BETTER FUEL EFFICIENCY
83
mixture too lean (4)
1. HIGH ENGINE TEMPERATURES
2. LOWER ENGINE POWER OUTPUT
3. ROUGH ENGINE AND CAN CAUSE
4. DETONATION AND PRE-IGNITION
84
mixture too rich (3)
1. LOWER ENGINE POWER OUTPUT
2. HIGH FUEL CONSUMPTION
3. POSSIBLE FOULING OF SPARK PLUGS
85
statement:
HOT AIR = LESS DENSE
COLD AIR = MORE DENSE
86
statement:
INTRODUCING HOT AIR MAKES THE MIXTURE RICHER
87
pre-Heats the air before it reaches the carburetor
CARBURETOR HEAT
88
dual magnetos benefits (3)
1. HIGHER POWER OUTPUT
2. MORE EFFICIENT BURNING
3. SAFETY IN THE EVENT OF MAGNETO FAILS
89
it contain large amount of carbon monoxide which is odorless and colorless gas
EXHAUST GASES
90
it measures the temperature of gases at the exhaust manifold
EXHAUST GAS TEMPERATURE (E.G.T.)
91
it can also be used for regulating the fuel/air mixture
EXHAUST GAS TEMPERATURE (E.G.T.)
92
fuel system classification (2)
1. GRAVITY-FEED SYSTEM
2. FUEL-PUMP SYSTEM
93
statement:
"IF THE PROPER GRADE OF FUEL IS NOT AVAILABLE, USE THE NEXT HIGHER GRADE AS A SUBSTITUTE"
94
omni specific fuel used
PETRON BLAZE 100 OCTANE
95
air cooling design (4)
1. SPINNER
2. BAFFLES
3. COOLING FINS
4. COWL FLAPS
96
redirects air into the engine nacelles
SPINNER
97
redirects cold air to the parts of the engine which would not normally be cooled
BAFFLES
98
expand the surface area to improve cooling
COOLING FINS
99
protect cowling incase of bird strikes
COOLING FINS
100
pilot controlled air vents outside the engine to improve cooling
COWL FLAPS
101
reducing temperature (5)
1. REDUCING PITCH FOR BETTER COOLING
2. REDUCE POWER
3. MIXTURE - RICH
4. KEEPING OIL LEVELS HIGH
5. COWL FLAPS - OPEN
102
functions of the oil system (4)
1. ENGINE COOLING
2. ENGINE LUBRICATION
3. PISTON SEALING
4. CARRYING AWAY OF CONTAMINANTS
103
properties of aircraft oil (4)
1. HIGH VISCOSITY
2. LOW POUR POINTS
3. HIGH FLASH POINT
4. OIL SYSTEM IS VITAL TO THE "INTERNAL" COOLING OF THE ENGINE
104
oil system parts (5)
1. OIL SUMP
2. OIL PUMP
3. OIL COOLER
4. OIL FILTER
5. PRESSURE RELIEF VALVE
105
process of dry sump
OIL TANK TO OIL SUMP TO OIL COOLER TO ENGINE TO OIL FILTER
106
the purpose of the manual is to set forth the procedures, the means, and methods of the approved maintenance organization.
MAINTENANCE ORGANIZATION PROCEDURE MANUAL (MOPM)
107
contains factory recommended procedures and instruction for ground handling, servicing and maintaining cessna series model
SERVICE MANUAL
108
presents COMPONENT BREAKDOWNS of structure and equipment in disassembly sequence.
ILLUSTRATED PARTS CATALOG
109
formal description of the aircraft, engine, or propeller
TYPE CERTIFICATE DATA SHEET
110
defines the product design change, states how the MODIFICATION AFFECTS the existing type design.
SUPPLEMENTAL TYPE CERTIFICATE
111
is an official certificate that confirms the part is safe for use in a specific aircraft.
TECHNICAL STANDARD ORDER
112
the document used by MANUFACTURERS OF AIRCRAFT, their engines or their components to communicate details of modifications which can be embodied in aircraft
SERVICE BULLETIN
113
usually pertain to service policies or announce available products or improvements for Lycoming engines.
SERVICE LETTER
114
cover a variety of subjects, such as repair processes, modification procedures, inspection procedures and overhaul methods.
SERVICE INSTRUCTION
115
it is a notification to owners and operators of certified aircraft that a known safety deficiency with a particular model of aircraft, engine, avionics or other system exists and must be corrected.
AIRWORHTINESS DIRECTIVES
116
aircraft journey log filed out by the pilot and handled by aerodrome staff.
LOGBOOK
117
same as task card it is a printed document that needs to be compiled every inspection
WORK DONE
118
types of tags (4)
1. SERVICEABLE TAG (YELLOW)
2. REPAIRABLE TAG (ORANGE)
3. CONDEMNED TAG (RED)
4. BRAND NEW TAG (WHITE)
119
statement:
ALTERNATOR (PRIMARY)
BATTERY (SECONDARY)
120
types of battery (2)
1. PRIMARY (NON-RECHARGEABLE)
2. SECONDARY (RECHARGEABLE)
121
primary batteries (3)
1. LITHIUM
2. ALKALINE
3. MERCURY
122
secondary batteries (4)
1. LITHIUM-IRON
2. NICKEL METAL HYDRIDE
3. NICKEL CADMIUM
4. LEAD ACID
123
non-rechargeable
contains electrolytes
convert chemical to electrical energy
DRY CELL BATTERY
124
gel cell
use for cleaning or maintenance service
SEALED LEAD ACID BATTERY
125
rechargeable
accumulator
secondary cell/supply
one or more electro chemical cells
LEAD ACID BATTERY
126
cessna 152, how many volts?
24 VOLTS
127
cessna 172, how many volts?
12 VOLTS
128
ac to dc, known as?
RECTIFIER
129
dc to ac, known as?
INVERTER
130
mechanical to electrical energy
ALTERNATOR
131
it supports the function of the alternator
ALTERNATOR BELT
132
engine driven electrical generator
firing the sparkplug
MAGNETO
133
a typical ___________ consists of switches, fuses, wiring and some voltage and a current flowing to and from the device.
ELECTRICAL SYSTEM
134
a _________________ or gel cell is a lead acid battery that has the sulfuric acid electrolyte coagulated (thickened) so it cannot spill out.
SEALED LEAD ACID BATTERY
135
the leads serve a dual purpose.
It provides the conductor path for the HIGH-TENSION VOLTAGE to the spark plug.
IGNITION HARNESS
136
it also serves as a shield for stray magnetic fields that surround the wires as they momentarily carry high-voltage current.
IGNITION HARNESS
137
it is a device used to
rotate (crank) an internal-combustion engine so as to initiate the engine's operation
under its own power.
STARTER
138
it provide “on ” and
“off” (left, right, both, start) electrical
control of both magnetos on single
engine aircraft.
IGNITION SWITCH
139
the ______________ controls the operation of the
battery and alternator system.
MASTER SWITCH
140
A ____________ is used as a terminal in the aircraft electrical
system to connect the main electrical system to the equipment
using electricity as a source of power
BUS BAR
141
those are used in the
electrical system to protect the circuits and equipment from
electrical overload
FUSES OR CIRCUIT BREAKERS
142
it is an electrical switch
designed to protect an electrical circuit
from damage caused by
overcurrent/overload or short circuit.
CIRCUIT BREAKERS
143
it is an electrical safety device that operates to
provide overcurrent protection of an electrical circuit.
FUSE
144
it is an electrically-controlled switch used
for switching an electrical power circuit.
CONTACTOR
145
it is used to monitor the performance of the aircraft
electrical system which shows if the alternator/generator is producing
an adequate supply of electrical power
AMMETER
146
it will illuminate when system voltage drops
below normal.
LOW-VOLTAGE WARNING LIGHT
147
it is to maintain a constant alternator voltage with varying engine speed.
VOLTAGE REGULATOR
148
reduce the flow of electrical Current.
AIRCRAFT RESISTOR
149
terminals (3) - create a connection
1. TERMINAL SPADE
2. INSULATED BUTT CONNECTOR
3. RING TERMINAL EYE
150
it is a way of joining
pieces of metal or other ductile
material by deforming one or
both of the pieces to hold the
other,
CRIMPING
151
statement:
ANODE = POSITIVE (+)
CATHODE = NEGATIVE (-)
152
rate of electron/ current flow in an electrical conductor.
AMPERES
153
the pressure from an electrical power circuit source that
pushes charge of electrons (current)
VOLTAGE
154
flow of electricity in an electronic circuit.
CURRENT
155
one in which all circuit
elements are arranged in a
single path. (end to end)
SERIES CIRCUIT
156
one that has two or more paths for
the electricity to flow
PARALLEL CIRCUIT
157
it simply means
that the aircraft is intended to
operate in visual meteorological
conditions (VMC, i.e. nice and
clear weather).
VISUAL FLIGHT RULES
158
these are rules
and regulations to govern flight
under conditions in which flight
by outside visual reference is not
safe.
INSTRUMENT FLIGHT RULES
159
types of flight rules (2)
1. VISUAL FLIGHT RULES
2. INSTRUMENT FLIGHT RULES
160
aircraft instruments categories (3)
1. FLIGHT INSTRUMENTS
2. ENGINE INSTRUMENTS
3. NAVIGATION INSTRUMENTS
161
these are the instruments in
the cockpit of an aircraft that provide the pilot with
data about the flight situation of that aircraft,
FLIGHT INSTRUMENTS
162
designed to measure
operating parameters of the aircraft’s engine(s).
ENGINE INSTRUMENTS
163
those that contribute
information use by the pilot to guide the aircraft
along a determine course.
NAVIGATION INSTRUMENTS
164
The instrument panel assembly consists of a __________________ and ______________.
STATIONARY PANEL AND SHOCK MOUNTED PANEL
165
6 packs / aircraft instruments
1. AIRSPEED INDICATOR
2. VERTICAL SPEED INDICATOR
3. ALTIMETER
4. ATTITUDE INDICATOR
5. HEADING INDICATOR
6. TURN COORDINATOR
166
pitot tube and static instruments (3)
1. AIRSPEED INDICATOR
2. VERTICAL SPEED INDICATOR
3. ALTIMETER
167
gyroscopic instruments (3)
1. ATTITUDE INDICATOR
2. HEADING INDICATOR
3. TURN COORDINATOR
168
it is a flight
instrument indicating
the airspeed of an aircraft in miles
per hour (MPH), knots, or both.
AIRSPEED INDICATOR
169
it is one of the flight instruments in an aircraft used to inform the pilot of the rate of descent or climb.
VERTICAL SPEED INDICATOR
170
it is an instrument used to measure the altitude of an object above a fixed level.
ALTIMETER
171
it is a flight instrument that informs the pilot
of the aircraft orientation relative to Earth's horizon, and gives an immediate indication of the smallest orientation change.
ATTITUDE INDICATOR
172
The attitude indicator (AI), formerly known as ________________________.
GYRO HORIZON OR ARTIFICIAL HORIZON
173
it is a flight instrument used in an aircraft to inform the pilot of the
aircraft's heading.
HEADING INDICATOR
174
heading indicator is sometimes referred to by its older names, the __________________, and also (UK usage) ___________________.
DIRECTIONAL GYRO
DIRECTION INDICATOR
175
One indicates the rate of turn, or the rate of change in the aircraft's heading; the other part indicates whether the aircraft is in coordinated flight, showing the slip or skid of the turn.
TURN COORDINATOR
176
one of the first flight instruments developed
MAGNETIC COMPASS
177
electrical driven instruments (7)
1. VERY HIGH FREQUENCY OMNI DIRECTIONAL RANGE (VOR )
2. INSTRUMENT LANDING SYSTEM (ILS)
3. FUEL QUANTITY INDICATOR
4. TURN COORDINATOR
5. CLOCK
6. AMMETER
7. HOUR METER
178
it is a type of SHORT-RANGE RADIO navigation system
for aircraft, enabling aircraft with a receiving unit to determine its position and stay on course by receiving radio
signals transmitted by a network of fixed ground radio beacons.
VERY HIGH FREQUENCY OMNI DIRECTIONAL RANGE (VOR )
179
it is a precision runway
approach aid employing TWO RADIO BEAMS to provide pilots with
vertical and horizontal guidance during the LANDING APPROACH.
INSTRUMENT LANDING SYSTEM (ILS)
180
it indicates the amount of
current (flow of electrons) from the
alternator to the attached load.
AMMETER
181
it is a genericized trademark for devices used in aviation to measure the time that an aircraft is in use.
The meters typically display hours and tenths of an hour
HOBBS METER
182
engine driven instruments (4)
1. TACHOMETER
2. OIL PRESSURE
3. OIL TEMPERATURE
4. FLAPS LEVER INDICATOR
183
it is an instrument measuring the rotation speed
of a shaft or disk, as in a motor or other machine.
TACHOMETER
184
indicates the supply pressure of the engine lubricant.
OIL PRESSURE
185
controls the operation of the flaps.
FLAPS LEVER INDICATOR
186
aircraft antennas (4)
1. VOR - VERY HIGH FREQUENCY OMNI DIRECTIONAL RANGE
2. VHR - VERY HIGH FREQUENCY
3. TRANSPONDER
4. ELT - EMERGENCY LOCATOR TRANSMITTER
187
it COLLECTS MOISTURE in the aircraft's STATIC system which prevents water damage to panel mounted instruments.
PITOT-STATIC SUMP BOTTLE
188
communications and navigations equipment (6)
1. VHF COMMINICATION SYSTEMS
2. PTT (PUSH TO TALK)
3. TRANSPONDER
4. AUDIO PANEL
5. NOISE FILTER
6. AIRCRAFT ENCODER
189
components of an instrument landing system (ILS) (3)
1. LOCALIZER
2. GLIDE SLOPE
3. OUTER MARKER
190
it is a device that, upon receiving a signal, emits a different signal in response.
TRANSPONDER
191
those are used for audio control and for selections of different audio sources.
AUDIO PANEL
192
aircraft lights (10)
1. NAVIGATION LIGHTS
2. BEACON LIGHT
3. TAIL LIGHT
4. MAP LIGHT
5. DOME LIGHT
6. STROBE LIGHT
7. LANDING LIGHT
8. TAXI LIGHT
9. PANEL LIGHT
10. COURTESY LIGHT
193
those are HIGH INTENSITY LIGHTS used to illuminate the runway surface for takeoff and landing and also to facilitate the aircraft being seen by other
pilots.
LANDING LIGHTS
194
those can be used in a variety of
ways, but they are typically used to direct
people to safety or alert them to danger or
potential hazards.
BEACON LIGHTS
195
those are used to PREVENT COLLISIONS at night or in times of reduced visibility, and are an essential tool in keeping you and your vessel safe.
NAVIGATION LIGHTS
196
those are flashing white lights on the
furthest left, right and, on larger aircraft and some smaller ones, back points of an aircraft.
STROBE LIGHTS
197
those are medium intensity
lights which may be mounted on the nose
landing gear strut, in the aircraft nose or at
the wing roots.
TAXI LIGHTS
198
provides adjustable illuminance, pattern, and
target point.
MAP LIGHTS
199
series of engine (2)
1. L2C
2. N2C
200
firing order
1-3-2-4
201
types of engine (4)
1. IN-LINE ENGINE
2. V-TYPE ENGINE
3. RADIAL ENGINE
4. OPPOSED ENGINE
202
basic parts of reciprocating engines (8)
1. CYLINDER
2. CRANKCASE
3. CRANKSHAFT
4. CAMSHAFT
5. TAPPET VALVE / LIFTER
6. PUSH ROD
7. ROCKER ARM
8. VALVE SPRING
203
statement:
IN THE CYLINDER:
PISTON
CONNECTING RODS
CRANKSHAFT
IGNITION
INTAKE VALVE
EXHAUST VALVE
204
foundation of the engine
CRANKCASE
205
backbone of the engine
CRANKSHAFT
206
responsible for the valves
CAMSHAFT
207
statement:
HALF NANG IKOT NI CRANKSHAFT (50%) SI CAMSHAFT
208
to align the camshaft
DEAD GEAR
209
pushed the tappet valve
6 CAMLOBES
210
clearance to adjust manually and push the rods
TAPPET VALVES / LIFTER
211
transmits the lifting force form the tappet valve
PUSH RODS
212
lifting force
ROCKER ARM
213
hold the valves
VALVE SPRING
214
4 stroke
INTAKE
COMPRESSION
POWER
EXHAUST
215
color of chrome barrel cylinder / piston
ORANGE
216
color of steel barrel cylinder / piston
GREEN
217
color of nitrided
BLACK
218
invented and patented the 4 stroke
ALPHONSE BEAU DE ROCHAS
219
who used the 4 stroke
NIKOLAUS AUGUST OTTO
220
the opening of both intake and exhaust valve
VALVE OVERLAP
221
engine control system (3)
1. THROTTLE
2. MIXTURE
3. CARBURETOR HEAT
222
statement:
CARB HEAT
COLD = PUSH
HOT = PULL
223
fuel system classification (2)
1. FUEL PUMP
2. GRAVITY PUMP
224
fuel system that need electricity and use in low and mid wing aircraft
PUMP FEED
225
fuel system that no need electricity and use in high wing aircraft
GRAVITY FEED
226
types of carburetor (2)
1. PRESSURE CARBURETOR
2. FLOAT TYPE CARBURETOR
227
ignition system (3)
1. MAGNETO
2. IGNITION HARNESS
3. SPARKPLUG
228
support if there's no magneto and use for starting
MAGNETO IMPULSE COUPLING
229
connected in magneto distribution block and proper spark plug
IGNITION HARNESS
230
magneto model 172
LEFT SIDE = 4371
RIGHT SIDE = 4370
231
magneto model 152
LEFT SIDE = 4381
RIGHT SIDE = 4380
232
conduct a short impulse
SPARK PLUG
233
types of spark plugs (3)
1. REM 37BY
2. REM 38E
3. REM 40E
234
it results of too much use of additives
CARBON DEPOSITS
235
statement:
GRAPHITE FOULING = ANTI-SEIZE
236
it is the streamlines bulky engine to reduce drag
COWLING
237
engine manufacturers (4)
1. GE
2. ROYCE
3. FRATT AND WHITNEY
4. LYCOMING
238
founder of cessna
CLYDE CESSNA
239
first production of cessna
1946 MODEL 120
240
materials used in model 120
ALUMINUM (FUSELAGE)
FABRIC (WINGS)
241
models of 152 (4)
1. 152
2. AI52
3. F152
4. FA152
242
when did cessna 150 started?
STARTED ON 1957
243
when did 152 started to use?
1958
244
cessna 152
HORSEPOWER = 110
LYCOMING = 0-235
100 OCTANE FUEL
245
color of octane rating of fuel
RED = 80
BLUE = 100LL
GREEN = 100
COLORLESS = JET
246
production of c152 powerplant
1942
247
reduce stall speeds
VORTEX GENERATOR
248
structures (4)
1. STOL (SHORT TAKE-OFF AND LANDING)
2. VORTEX GENERATOR
3. EXTENDED FUEL TANK
4. AEROBAT 152
249
alternator volts supply
28 VOLTS
250
types of landing gear (2)
1. CLEVELAND
2. MCCAULEY
251
types of wrenches (4)
1. COMBINATION WRENCH
2. OPEN END WRENCH
3. BOX END WRENCH
4. OFFSET WRENCH
252
statement:
WRENCH FOR BOLTS AND NUTS
SCREWDRIVER FOR SCREWS
253
break loose very high fasteners
HINGE HANDLE / POWER HANDLE
254
kinds of socket (2)
1. IMPACT SOCKET
2. CHROME SOCKET
255
types of sockets (4)
1. SHALLOW SOCKET
2. SEMI-DEEP SOCKET
3. DEEP SOCKET
4. UNIVERSAL SOCKET
256
setting and adjust the tightness of nuts and bolts
TORQUE WRENCH
257
it activating adhesive curing epoxy
HEAT GUN
258
inspection program and type operation (4)
1. ANNUAL INSPECTION
2. ANNUAL / 100 HOURS INSPECTION
3. PROGRESSIVE INSPECTION
4. CONTINUOUS AIRWORTHINESS PROGRAM
259
tools that utilizes pressure so a fabricated mechanical joint is made for joining or sealing copper
FLARING TOOL
260
tools that has the appearance of a box end wrench that has been cut open on one end
FLARE NUT WRENCH
261
tool that hand held instruments used to measure the tension of a cable
CABLE TENSION METER
262
it measure the true speed of the propeller
TRUTACH
263
it contains a one way mechanism which allows the socket to be turned without removing it
RATCHET
264
it is a square opening cut in one end to lift a square drive lug
SOCKET
265
a versatile tool to helps do reliable safe wiring
WIRE TWISTER PLIER
266
it is necessary in areas where a bolt could loosen during vibration
SAFETY WIRE
267
for engine timing or perfect timing
MAGNETO SYNCHRONIZER
268
it is used to measure gap widths and used in valve clearance
FEELER GAUGE
269
a device resembling a gun which is used to spray pressurized air
BLOW GUN
270
tools that handles to aid in gripping when opened for larger objects
INTERLOCKING SLIP JOINT PLIERS (PUMP PLIERS)
271
it is used to support the landing gear for inspection
PYRAMID CHOCK
272
to lift heavy loads
HYDRAULIC JACK
273
used to measure the pressure of tires
TIRE PRESSURE GAUGE
274
designed to cut the filter open and visually inspect the filter
OIL FILTER CUTTER
275
checks the compression of aircraft engines
COMPRESSION TESTER
276
tools that use for easiest way to remove a nut of the cylinder
CYLINDER BASE NUT WRENCH (HOLD DOWN WRENCH)
277
hold objects in place when you are working alone
LOCKING PLIERS (VISE GRIPS)
278
tools that used to remove excess material from the edges or surfaces of a raw
DEBURRING TOOL
279
pcar part 5
AIRWORTHINESS
280
year chicago convention held
1944
281
general aviation aircraft re-weighed every?
5 YEARS
282
pcar part number of ato
PART 03
283
annex 7 title
AIRCRAFT NATIONALITY AND REGISTRATION MARKS
284
caap formerly named
AIR TRANSPORTATION OFFICE
285
rp-g classify
GLIDERS
286
pcar part 1
GENERAL POLICIES, PROCEDURES, AND DEFINITIONS
287
annex 1 title
PERSONNEL LICENSING
288
pcar part 6
APPROVED MAINTENANCE ORGANIZATION
289
when was the chicago convention signed by 52 states
DECEMBER 7, 1944
290
commercial operation aircraft re-weighed
3 YEARS
291
pcar part number of operations
PART 08
292
republic act number renamed the ato into caap
REPUBLIC ACT NO.9497
293
rp-c classify
AIRCRAFT EXCEPT GLIDERS
294
validity of ato certificate
5 YEARS
295
in case lost of airman license facsimile valid
60 DAYS
296
amo validity
5 YEARS
