AGK Flashcards

1
Q

Aircraft length

A

27’2”

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Aircraft Height

A

8’11”

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Aircraft Width

A

36’1”

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Prop Diameter

A

76”

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Prop Clearance

A

11.25”

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Fuel type

A

100LL/100 AVGAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Oil

A

Grade 40 or 50
Sump 8qt
Total 9qt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Max Engine speed

A

2700RPM

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Max Oil temperature

A

245 F

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Min oil pressure

A

20 psi

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Max oil pressure

A

115 psi

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Min static RPM

A

2300-2400 RPM

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Max demonstrated crosswind

A

15kt Full flaps

20kt Flaps 10

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Engine model

A

IO-360-L2A

Normally aspirated, Direct drive, Air-cooled, Horizontally opposed, Fuel injected, Four cylinder, 360 cu. in

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Engine Power

A

180BHP at 2700 RPM

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Weights

A

Ramp 2558

TO + LDG 2550

17
Q

Standard empty mass

A

1663 lbs

18
Q

Max load (fuel + PAX)

A

895 lbs

19
Q

Baggage compartment loads

A

A - 120
B - 50
(Total adding to 120)

20
Q

CG Limits

A

FWD 35” <1950lbs
41” @2550
AFT 47.3” at all weights

21
Q

Load factor limits

A

Flaps up +3.8g -1.52g

Flaps full +3.0g

22
Q

Purpose of horn balance

A

Reduce input forces

23
Q

Purpose of mass balance

A

Reduce flutter

24
Q

Type of flap on aircraft

A

Fowler

25
Q

Instruments connected to pitot-static system

A

ASI, VSI, altimeter

26
Q

Normal and Max tyre pressures

A

Nose: Max - 45 Normal 40
Main: Max - 38 Normal 35

27
Q

Battery voltage

A

24v

28
Q

Number of fuel drains

A

13