BGSU Archer EP SIM Flashcards 2220

Wing Span

35' 6''

Number of engines

1

Engine Manufacturer

Lycoming

Engine Model Number

IO-360-B4A (Fuel Injected)

Takeoff Power (BHP)

180 hp

Takeoff Power Engine Speed

2700 rpm

Bore

5.125

Stroke

4.375

Displacement

361.0

Compression Ratio

8.5:1

Engine Type

Four Cylinder, direct drive, horizontally opposed, fuel injected, naturally aspirated

Number of Propellers

1

Prop manufacturer

Sensenich

Number of Blades

2

Prop Diameter

76/76 in

Prop Type

Fixed Pitch

fuel capacity total

50 gal

Useable Fuel

48 gal

Fuel Types and Color

100LL Blue 100 Green

Oil type BG uses

20w-50 Ashless Dispersent OR Mineral Oil

Oil Capacity

8 qrts

Max Ramp weight (Normal)

2558 lbs

Max Ramp Weight (Utility)

2138 lbs

Max TO/LND weight (Normal)

2550 lbs

Max TO/LND weight (Utility)

2130 lbs

Max baggage compartment (Normal)

200 lbs

Max baggage compartment (Utility)

0 lbs

Baggage space

Volume: 24 cu. ft.

width: 22 in

height: 20 in

Wing Loading

15.0 lbs/sq ft

Power Loading

14.2 lbs/HP

Calibrated Air Speed (CAS)

Indicated Airspeed corrected for position and instrument error

Ground Speed (GS)

Speed of the airplane relative to the ground

Indicated Airspeed (IA)

Speed of the aircraft shown on the airspeed indicator corrected for instrument error

True Airspeed (TAS)

CAS corrected for altitude, temperature, and compressibility

Vo

Max operating maneuvering speed. Full aerodynamic control will not overstress the airplane.

Vfe

Maximum Flaps Extend Speed (102 KIAS)

Vne

Never Exceed Speed (154 KIAS)

Vno

Max Structural Cruising Speed (125 KIAS)

Vs

Stall Speed in Clean Configuration 50 KIAS

Vso

Stall Speed in Landing Configuration 45 KIAS

Vx

Best angle of Climb Speed. Greatest altitude gain in shortest horizontal distance 64 KIAS

Vy

Best rate of Climb Speed. Best altitude gain in shortest possible time 76 KIAS

International Standard Atmosphere

29.92/1013.2 15C/59F

OAT

Outside air temperature

Indicated Pressure altitude

Number read from altimeter when set to 29.92

Pressure Altitude

Altimeter corrected for Position and Instrument error

Station Pressure

Actual Pressure at field elevation

EGT

Exhaust Gas Temperature

FFLOW

Fuel Flow

RPM

Prop Speed (Revolutions per Minute)

1

Pilot Side

2

Co Pilot Side

ADAHARS

Air Data, attitude, heading, reference system

AFCS

Automatic Flight Control System

CAS

Crew Alerting System

EBD

Evolutionary Backup Display

EIS

Engine Indication System

ESP

Electronic Stability and Protection

FDE

Fault Detection and Exclusion

FOB

Fuel on board

GDL

Garmin Datalink

GDU

Garmin Display Unit

GEA

Garmin Engine Airframe processing unit

GFC

Garmin Flight Control system

GIA

Garmin Integrated Avionics

GMA

Garmin Audio Panel

GMU

Garmin Magnetometer Unit

GPS

Global Positioning System

GTX

Garmin Transponder

MFD

Multi Function Display

PFD

Primary Flight Display

PFT

Preflight Test

SBAS

Satellite Based Augmentation System

TAWS

Terrain Awareness and Warning system

USP

Underspeed Protection

Datum (Def)

Imaginary vertical plane from which all horizontal distances are measured for balance

Basic Empty Weight (BEW)

Standard Empty Weight plus optional equipment

Standard Empty Weight

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

Station

Location along the airplane fuselage given in terms of the distance from the reference datum

Never Exceed Speed (Vne)

154 KIAS

Maximum Structural Cruising Speed (Vno)

125 KIAS

Maneuvering Speed Formula

113 + sqrt of weight/max gross weight

Vo @ 2550

113 KIAS

Vo @1917

98 KIAS

Maximum Flaps Extended Speed (Vfe)

102 KIAS

Red Line (Never Exceed Speed)

154 KIAS

Yellow Band (Caution Range - Smooth Air Only)

125-154 KIAS

Green Band (Normal Operating Range)

50-125 KIAS

White Band (Flaps Down)

45-102 KIAS

Tach: Green Arc (normal operating range)

500-2700 rpm

Tach: Red Line (Max)

2700 rpm

Oil Temp Green Band (Normal Operating Range)

75-245 F

Oil Temp: Red line (maximum)

245 F

Oil Pressure: Green Band (Normal Operating)

55-95 PSI

Oil Pressure: Yellow Band (Caution Range-Idle)

25-55 PSI

Oil Pressure: Yellow Band (Ground Warmup)

95-115 PSI

Oil Pressure: (Red line Max)

115 PSI

Oil Pressure: (Rex line Min)

25 PSI

Propeller tolerance @ ISA Conditions

Not above 2340 RPM

Not below 2240 RPM

Alternator amps

70 Amps