CAAP EQC Flashcards by Jl Almaden

Q

engine manufacturer

A

avco lycoming

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Q

engine model

A

O-235-L2C

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Q

engine is equipped with a__________ and is __________

A

carburetor, normally aspirated

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Q

engine displacement

A

233.3 cubic inches

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Q

engine horsepower

A

110 hp

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Q

maximum rpm

A

2550 rpm

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Q

propeller manufacturer

A

mccauley/sensenich

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Q

blade and pitch of propeller

A

two-blade, fixed pitch

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Q

propeller model

A

1A103 / TCM6958

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Q

propeller diameter

A

at least 67.5 inches but no more than 69 inches

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Q

total fuel capacity - standard tanks

A

26 US gallons, 13 US gallons per tank

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Q

total usable fuel - standard tanks

A

24.5 US gallons

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Q

total fuel capacity long range tanks

A

39 US gallons, 19.5 US gallons per tank

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Q

total usable fuel - long range tanks

A

37.5 US gallons

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Q

approved avgas fuel grade

A

100LL Blue / 100 Green

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Q

oil system capacity

A

6 quarts

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Q

oil system capacity with oil filter

A

7 quarts

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Q

oil type

A

MIL-L-22851 ashless dispersant oil

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Q

MIL-L-22851 ashless dispersant oil mus be used after

A

first 50 hours or oil consumption has stabilized

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Q

main landing gear tire size and tire pressure

A

6.00 - 6 | 21 psi

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Q

nose landing gear tire size and tire pressure

A

5.00 - 5 | 30 psi

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Q

alternator voltage & amperes

A

28-volt, 60-amp

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Q

battery voltage & amperes

A

24-volt, 14-amp/hour

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Q

white arc airspeed

A

full flap operating speed / 35kn-85kn

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Q

green arc airspeed

A

normal operating speed / 40kn-111kn

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Q

yellow arc airspeed

A

caution range / 111kn-149kn

Q

red line airspeed

A

never exceed / 149kn

Q

never exceed speed

A

149 KIAS

Q

max structural cruising speed

A

111 KIAS

Q

maneuvering speed at maximum weight

A

104 KIAS

Q

max flap extend speed

A

85 KIAS

Q

max window open speed

A

143 KIAS

Q

wingspan

A

33 feet 4 inches

Q

length

A

24 feet 1 inch

Q

height

A

8 feet 6 inches

Q

wheel base length

A

58 inches

Q

propeller ground clearance

A

12 inches

Q

maximum turning radius

A

24 feet 8 inches

Q

total wing area

A

160 square feet

Q

maximum weight on both takeoff and landing

A

1670 lbs

Q

standard empty weight

A

1081 lbs

Q

maximum useful cargo weight

A

589 lbs

Q

maximum cargo/baggage weight

A

< 120 lbs

Q

max weight in baggage area 1

A

120 lbs

Q

max weight in baggage area 2

A

40 lbs

Q

Vx

A

55 knots

Q

Vy

A

67 knots

Q

maximum demonstrated crosswind velocity

A

12 knots

Q

wing loading

A

10.5 psf

Q

power loading

A

15.2 lbs / hp

Q

load factor limits

A

positive 4.4g || positive 3.5g (flaps down) || negative 1.76g

Q

Fuel Burn 2300RPM | 35C | 2000FT PA

A

5.1 GPH

Q

maximum glide speed

A

60 KIAS

Q

precautionary landing with engine power

A

55 KIAS

Q

landing without engine power - wing flaps up

A

65 KIAS

Q

landing without engine power - wing flaps down

A

60 KIAS

Q

tachometer normal operating range

A

1900 RPM - 2550 RPM

Q

tachometer maximum limit

A

2550 RPM

Q

oil temperature normal operating range

A

100F - 245F

Q

oil temperature maximum limit

A

245F

Q

oil pressure minimum limit

A

25 psi

Q

oil pressure normal operating range

A

60psi - 90 psi

Q

oil pressure maximum limit

A

100psi

Q

max entry speed for chandelles, lazy 8s, steep turns

A

95 knots