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Instrument > Archer > Flashcards

Archer Flashcards

1
Q

engines

A

1

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2
Q

Engine manufacturer

A

Lycoming

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3
Q

Engine model number

A

IO-360-B4A

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4
Q

Takeoff power

A

180

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5
Q

Speed RPM

A

2700

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6
Q

Engine type

A

Four cylinder, direct drive, horizontally opposed with fuel injection

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7
Q

Number of propellers

A

1

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8
Q

Propeller Manufacturer

A

Sensenich

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9
Q

Propeller model

A

76EM8S14-0-62

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10
Q

Number of blades

A

2

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11
Q

Propeller Diameter Maximum

A

76 inches

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12
Q

Propeller Diameter Minimum

A

76 inches

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13
Q

Propeller Type

A

Fixed Pitch

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14
Q

Fuel Capacity

A

50

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15
Q

Useable fuel

A

48

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16
Q

Minimum octane

A

100 Green or 100LL Blue Aviation Grade

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17
Q

Oil Capacity

A

8

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18
Q

Maximum Ramp Weight

A

Normal: 2558
Utility: 2138

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19
Q

Maximum Takeoff Weight

A

Normal: 2550
Utility:2130

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20
Q

Maximum Landing Weight

A

Normal: 2550
Utility: 2130

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21
Q

Maximum weights Baggage

A

200 pounds

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22
Q

Compartment Volume

A

24 feet

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23
Q

Entry width

A

22 inches

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24
Q

Entry Height

A

20 inches

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25
Q

Wing Loading

A

15 pounds per sq ft

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26
Q

Power Loading

A

pounds per hp 14.2

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27
Q

CAS

A

means the indicated speed of an aircraft, corrected for position and instrument error. Calibrated airspeed is equal to true airspeed in standard atmosphere at sea level

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28
Q

KCAS

A

Calibrated Airspeed expressed in Knots

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29
Q

GS

A

Ground speed is the speed of an airplane relative to the ground

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30
Q

IAS

A

Indicated Airspeed is the speed of an aircraft as shown on the airspeed indicator when corrected for instrument error

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31
Q

KIAS

A

Indicated Airspeed expressed in Knots

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32
Q

TAS

A

True airspeed is the airspeed of an airplane relative to undisturbed air which is the CAS corrected for altitude, temperature and compressibility

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33
Q

Vo

A

Maximum maneuvering speed
113 knots

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34
Q

VFE

A

Maximum Flap extended Speed
102 knots

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35
Q

VNE/MNE

A

Never exceed speed
154 knots

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36
Q

VNO

A

Max structural cruising speed
125 knots

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37
Q

Vs

A

Stalling speed clean configuration
50 knots

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38
Q

Vso

A

Stalling speed landing configuration
45 knots

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39
Q

Vx

A

Best angle of climb is the airspeed which delivers the greatest gain of altitude in the shortest possible horizontal distance
64 knots

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40
Q

Vy

A

Best rate of climb speed is the airspeed which delivers the greatest gain in altitude in the shortest possible time
76 knots

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41
Q

ISA

A

International Standard Atmosphere in which the air is a dry perfect gas; The temperature at sea level is 15 degrees celsius or 59 degrees farenheit. The pressure at sea level is 29.92 inHG

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42
Q

OAT: Outside Air Temperature

A

is the free air static temperature, obtained either from inflight temperature, obtained either from inflight temperature indications or ground meteorological sources, adjusted for instrument error

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43
Q

Indicated pressure Altitude

A

The number read from the altimeter

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44
Q

Pressure Altitude

A

Altitude measured from standard sea level pressure by a pressure or barometric altimeter. It is the indicated pressure altitude corrected for position and instrument error

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45
Q

Station pressure

A

Actual atmospheric pressure at field elevation

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46
Q

wind

A

The wind velocities recorded as variables on the charts of this handbook are to be understood as the headwind or tailwind components of the reported winds

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47
Q

Maximum Continuous Power

A

Maximum power permissible continuously during flight

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48
Q

Takeoff power

A

Maximum power permissible for takeoff

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49
Q

EGT

A

Exhaust Gas Temperature

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50
Q

FFLOW

A

Fuel Flow

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51
Q

RPM

A

Propeller speed

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52
Q

1

A

refers to pilot side

53
Q

2

A

refers to co-pilot’s side

54
Q

ADAHRS

A

Air data, Altitude and Heading Reference system

55
Q

AFCS

A

Automatic Flight Control System

56
Q

CAS

A

Crew Alerting System

57
Q

EBD

A

Evolution Backing Display (Aspen standby Instrument)

58
Q

EIS

A

Engine Indication System

59
Q

ESP

A

Electronic Stability and protection

60
Q

FDE

A

Fault Detection and Exclusion

61
Q

FOB

A

Fuel on Board

62
Q

GDL

A

Garmin Datalink

63
Q

GDU

A

Garmin Display Unit

64
Q

GEA

A

Garmin engine/Airframe Processing Unit

65
Q

GFC

A

Garmin Flight Control System

66
Q

GIA

A

Garmin Integrated Avionics Unit

67
Q

GMA

A

Garmin Audio Panel

68
Q

GMU

A

Garmin Magnetometer Unit

69
Q

GPS

A

Global position system

70
Q

GSU

A

Garmin ADAHRS

71
Q

GTX

A

Garmin Transponder

72
Q

MFD

A

Multi-Function Display

73
Q

PFD

A

Primary Flight Display

74
Q

PFT

A

Preflight Test

75
Q

SBAS

A

Satellite-Based Augmentation System

76
Q

TAWS

A

Terrain Awareness and Warning System

77
Q

USP

A

Underspeed Protection

78
Q

ARM

A

The horizontal distance from the reference datum to the center of gravity (C.G.) of an item

79
Q

Center of Gravity

A

The point at which an airplane would balance if suspended. Distance found by dividing the total moment by total weight

80
Q

C.G. Arm

A

the arm obtained by adding the airplane’s individual moments and dividing the sum by the total weight

81
Q

C.G. Limits

A

The extreme center of gravity locations within which the airplane must be operated at a given weight

82
Q

Datum

A

An imaginary vertical plane from which all horizontal distances are measured for balance purposes

83
Q

Basic Empty Weight

A

Standard empty weight plus optional equipment

84
Q

Maximum Landing Weight

A

Maximum weight approved for the landing touchdown

85
Q

Maximum Ramp Weight

A

weight approved for ground maneuver

86
Q

Maximum Takeoff weight

A

Maximum weight approved for takeoff

87
Q

Maximum zero fuel weight

A

maximum weight exclusive of usable fuel

88
Q

Moment

A

The product of the weight of an item multiplied by its arm

89
Q

payload

A

weight of occupants, cargo and baggage

90
Q

standard empty weight

A

weight of a standard airplane including unusable fuel, full operating fluids and full oil

91
Q

Station

A

A location along the airplane fuselage usually given in terms of distance from the reference datum

92
Q

unusable fuel

A

fuel remaining after a runout test has been completed in accordance with government regulations

93
Q

Usable fuel

A

fuel available for flight planning

94
Q

useful load

A

difference between takeoff weight, or ramp weight is applicable, and basic empty weight

95
Q

Red line (Never Exceed)

A

154 knots

96
Q

Yellow Band ( caution range- smooth Air only)

A

125-154 knots

97
Q

Green band(Normal operating range)

A

50-125 knots

98
Q

White band (Flap Down)

A

45-102 knots

99
Q

Max oil temperature

A

245 degrees

100
Q

Oil pressure

A

Minimum (red line) 25 PSI
Maximum (red line) 115 PSI

101
Q

Tachometer green arc

A

500 to 2700 RPM

102
Q

Oil temperature green band

A

75 degrees- 245 degrees

103
Q

Oil pressure

A

Green band: 55 PSI
Yellow band: 25 PSI-55 PSI
Yellow band (ground warm-up) 95 PSI-115 PSI
Red line (Minimum) 25 PSI
Red line (Maximum) 115 PSI

104
Q

Alternator

A

70 AMPS

105
Q

Emergency Battery minimum

A

23.3 volts

106
Q

Forward Limit inches Aft of Datum

A

2550= 88.6
2050 (or less)= 82.0

107
Q

Rearward Limit Inches AFT of datum

A

2550= 93.0
2050 (or less)= 93.0

108
Q

Utility: Forward limit inches aft datum

A

2130= 83.0
2050 (or less)= 82.0

109
Q

Utility: Rearward limit inches aft of datum

A

2130= 93.0
2050 (or less)= 93.0

110
Q

Positive load factor (maximum)

A

Normal= 3.8G
Utility=4.4G

111
Q

Negative Load factor (maximum)

A

Normal= -1.5G
Utility= -1.7G

112
Q

Placards

A

Limitations: in full view of the pilot
Maneuvering speed: in full view of the pilot
Demonstrated crosswind
No Smoking: on the cockpit overhead panel
Alternate static source: on lower left portion of instrument panel
Air conditioning warning: in full view of the pilot, in the area of the air conditoner control panel when the air conditioner is installed
Strobe light warning: in full view of the pilot
Engage latch before flight: adjacent to upper door latch
Baggage max 200 pounds: on inside of the baggage compartment door or information split into two placards on aft baggage compartment bulkhead
Maximum allowable combined weight: Above right side aft passenger arm rest:
External power 28 volts:on the right side of the fuselage aft of the wing
AVGAS only: adjacent to the filler caps

113
Q

Engine Fire During Start

A

Start switch…… Continue to Crank Engine
Mixture…. Idle
Throttle…….Open
Fuel Pump….. OFF
Fuel selector….OFF

114
Q

Engine Fire in Flight

A

Fuel Selector…..OFF
Throttle……Closed
Mixture……IDLE cut off
Fuel pump…..OFF
Heat/DEF(Defroster)……..OFF
If fire persist
Airspeed……Increase in attempt to blow out fire
Proceed with Power off Landing procedure

115
Q

ELECTRICAL FIRE IN FLIGHT

A

Emergency battery switch……Verify Arm
Battery Master Switch….OFF
Alternator Switch……OFF
Vents……..Open
Heat/DEF(Defroster)…..OFF
Fire……..Extinguish
Emergency descent if needed

116
Q

Engine power loss during takeoff

A

Airspeed…..Maintain safe airspeed
Landing….Land and Stop straight ahead
brakes……as required
If insufficient runway remains:
Airspeed…… Maintain Safe Airspeed
Flaps……. As required
If sufficient altitude has been gained to attempt a restart
Airspeed…. maintain 76 knots
Fuel selector….. switch to tank containing fuel
Fuel pump…… check on
Mixture……. Rich
ALT AIR…. open

117
Q

Engine power loss in Flight

A

Airspeed….. Maintain 76 knots
Fuel selector……Switch to tank containing fuel
Fuel Pump…….ON
Mixture……Rich
ALT AIR………OPEN
Left/Right MAG switches……Turn off then ON one at a time
When power is restored
ALT AIR……Close
Fuel PUMP…….OFF

118
Q

Power off landing

A

Airspeed….Maintain 76 knots
Air conditioning (if installed)…..OFF
Landing pattern…..establish 1000ft above field at downwind position
When committed to landing
Airspeed……66 knots
Flaps….. As Desired
Throttle…….Close
Mixture……..Idle Cut-off
Left/Right MAG Switches…….OFF
Battery Master switch……OFF
Alternator Switch……..OFF
Fuel selector………OFF
Seat belt……fastened

119
Q

Oil Pressure

A

Low Pressure
Throttle…..Minimum
If accompanied by high oil temperature, land as soon as possible
If accompanied by normal oil temperature, land as soon as practical
High oil pressure
Throttle……Minimum
Land as soon as practical

120
Q

Oil Temperature

A

Throttle…..Minimum
Mixture…..Full Rich
Airspeed…..Increase if practical
Land as soon as possible and investigate the problem. Prepare for Power off Landing

121
Q

Loss of Fuel Flow

A

If caused by fuel depletion in One Tank
Fuel pump switch…….ON
Fuel Selector….. Selector other tank (Fullest)
Fuel Pump Switch…..OFF
If caused by engine driven fuel pump failure:
Throttle…….Close
Fuel Pump Switch…..ON
Throttle……Re-establish(as required)
Mixture…..Re-establish(as required)

122
Q

Fuel Quantity Low

A

If one tank has low fuel quantity
Fuel selector……. On Fullest Tank
Land as soon as practical
If both tanks have low fuel quantity
Fuel Selector….. Alternate Tanks to maintain fuel supply to Engine
Land as soon as possible

123
Q

Alternator Failure

A

Verify Failure……Check ALTR AMPS Indication
ALTR switch……OFF
ALTR circuit breaker (Row 1, Col.13)……Reset if Tripped
ALTR FIEL Circuit Breaker (Row 2, Col.13)….Reset
ALTR switch…..ON
If alternator still failed
ALTR switch……OFF
Electrical Power Remaining……OFF
Electrical power Remaining…….30 minutes or less
Electrical Load…….SHED in less than 3 minutes
NON ESS circuit Breaker (ROW 1, Col. 1)…..PULL
Lighting Bus circuit breaker (Row 1, Col,2) PULL
Avionics master switch…..OFF
To ensure 30-minutes of battery life:
Battery discharge….-13 AMPS maximum
pitot heat……14 minutes usage maximum
fuel pump……. 2 mins usage maximum
Land as soon as possible

124
Q

Complete electrical failure

A

Emergency Batt switch……Verify ARM
Standby flight instrument….Verify operational
Aircraft control…..Use PFD and standby instrument
Batt master switch….OFF
ALTR switch……OFF
Prior to Landing
Landing Light……..Inoperative
Approximately 30 minutes of electrical power is available
Land as soon as possible

125
Q

Emergency Battery Voltage

A

Warning: Complete electrical failure is imminent
Land as soon as possible

126
Q

PFD Failure

A

Standby instrument….verify operational
Aircraft control….Use standby instrument
Display backup button on audio panel..Push
Aircraft control….Use MFD and standby instrument
COM2….Activate and Tune as necessary
NAV2…..Activate and TUNE as necessary
COM2/MIC…… Select on audio panel
DME……select NAV2 in DME tuning window
Exit and avoid IFR conditions as soon as practical

127
Q
A
128
Q
A

Instrument (10 decks)

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