Airplane Parts

Question 1

Archer
Max Gross Weight (lbs)

Answer 1

2550

Question 2

Primary Flight Controls

Answer 2

Differential Ailerons
Stabilator
Rudder

Question 3

Secondary flight controls

Answer 3

Single-slot type wing flaps
-Manually Actuated
-0°,10°,25°,40°

Question 4

Flight controls
Trim

Answer 4

Elevator

Manually and electronically

Question 5

Propeller

Answer 5

Sensenich
Fixed pitch
76 in
2 blades
Metal

Question 6

Powerplant

Answer 6

Lycoming

IO-360-B4A
I = Fuel Injected
O = Horizontally Opposed Cylinders
360 = Cubic inches of displacement
- _____ = accessory configuration

4 cylinder configuration
Direct propeller drive
Air cooling
Dual magnetos

Question 7

Power plant
Horsepower

Answer 7

180 @ 2700rpm

Question 8

Oil System

Answer 8

Wet sump
8 qt capacity
6 qt min for school

Phillips X/C 20W-50

Question 9

Fuel System

Answer 9

2 fuel pumps
Mechanical and engine driven

50 gal capacity
48 gal usable

Question 10

Hydraulic System

Answer 10

MIL 5606H

Question 11

Landing Gear

Answer 11

Fixed tricycle
Steerable Air / Oil Shock Strut (OLEO)
Brake fluid is red

Question 12

Electrical System

Answer 12

System- 28 volt
Main battery - 24 volt
Emergency battery- 24 volt
Alternator- 70 amp

Question 13

Electrical system
Additional Batteries

Answer 13

1x Emergency (24V approx 30min power to 30min Emergency Bus)

1x Battery for G5 (approx 4 hrs)

Question 14

Deicing and Anti-Icing

Answer 14

Pitot heat
Windscreen defroster
Heated Static Port on Pitot Mast
Alternate static source
Alternate induction air

Question 15

Avionics
Transponder

Answer 15

Mode S with A, C and S functions

Question 16

Avionics
Displays

Answer 16

Garmin G1000 PFD & MFD

Question 17

Avionics

Answer 17

1: Air Data Computer (ADC) + Attitude & Heading Reference System (AHRS) (see 2 for more information)
2: AHRS for gyroscopic instruments uses rate sensors, inclinometers, accelerometers. In conjunction with a magnetometer located in the wing or tail (see POH). ADC provides information for the pitot static instruments via conventional pitot static tubing and translates them to the displays using pressure sensors.
3: The conventional standby instruments include altimeter, airspeed indicator, and attitude indicator with suction provided by an engine driven vacuum pump. 4: G1000 magnetometer in the left wing, G5 in the right

Question 18

Spark plugs

Answer 18

8 spark plugs
2 per cylinder

Question 19

Weight limits

Answer 19

Empty weight ~ 1730lbs
Max weight ~ 2550lbs
Baggage weight~ 200lbs

Question 20

gyroscopic instruments

Answer 20

rigidity in space
precession

Question 21

attitude indicator

Answer 21

rigidity in space
vacuum driven
-bank/pitch

Question 22

heading indicator

Answer 22

rigidity in space
vacuum system

Question 23

turn indicators

Answer 23

precession
*turn coordinators: rate of turn\rate and roll
*turn-and-slip indicators: rate of turn only

Question 24

vertical speed indicator

Answer 24

rate of climb and rate trend
diaphragm to static source
static pressure via calibrated leak
responds to pressure change over time
expands and contracts

Question 25

altimeter

Answer 25

-height above given pressure level
based on standard pressure lapse rate of 1000 per in of mercury
-aneroid wafers expand and contract with changes in pressure received from static port
mechanical linkage between aneroid wafers and display translates the sensed pressure to altitude indication

Question 26

VSI

Answer 26

vertical speed indicator
rate of climb in fpm
rate trend
diaphragm connected to static source
outside diaphragm receives static pressure via calibrated leak
static pressure over time

Question 27

static port blockages
airspeed indicator

Answer 27

indicates correctly only at blockage altitude
lower altitudes- airspeed indicates lower than it should
low altitudes- indicates higher than it should

Question 28

static port blockages
altimeter

Answer 28

will freeze on the altitude where it was blocked

Question 29

static port blockages
VSI

Answer 29

freezes on zero

Question 30

static port blockages
alt air

Answer 30

airspeed indicator- indicate faster airspeed
altimeter- indicate higher
VSI- momentarily show a climb, then to 0