POH Section 1 Flashcards

1
Q

Aircraft length

A

27ft 7.2in

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

Wingspan

A

38ft 6.6in

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

Aircraft height

A

8ft 6in

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

Engine make/models

A

Lycoming

Left: 0-360-A1H6
Right: L0-360-A1H6

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

Engine descriptions (excluding make/model)

A
  • Four cylinder
  • Direct drive
  • Horizontally opposed
  • Air cooled
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Engine compression ratio

A

8.5:1

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

Cylinder bore

Also, what is the definition of bore?

A

5.125in

Bore: Diameter of the cylinder

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

Cylinder stroke

Also, definition of stroke

A

4.375in

Stroke: Distance the piston travels in the cylinder

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

Engine displacement

A

361 cubic in

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

Propeller manufacturer

A

Hartzell

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

Propeller diameter, maximum and minimum

A

Max: 74in
Min: 72in

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

Propeller type/description (3 things)

A
  • Constant speed
  • Hydraulically actuated
  • Full feathering
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Total fuel, usable and unusable

A

110 gal (55 either side)

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

Usable fuel

A

108 gal (54 either side)

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

Can 100 octane fuel be used in place of 100LL?

A

Yes

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

Oil capacity (min-max)

A

6-8 quarts

17
Q

Where to check for which grade of oil you need to use?

A

POH 1-4

18
Q

Maximum ramp weight

A

3816lbs

19
Q

Maximum takeoff weight

A

3800 lbs

20
Q

Maximum landing weight

A

3800 lbs

21
Q

Maximum weight in baggage compartment

A

200 lbs

22
Q

Baggage compartment volume

A

24 cu ft

23
Q

Baggage compartment entry dimensions

A

Width: 22in
Height: 20in

24
Q

Wing loading (lbs/square ft)

A

21.1lbs/sq ft

25
Q

Power loading (lbs/hp)

A

10.55lbs/hp

26
Q

14 CFR Part 23: What are the (8) requirements for FAA certification to determine the Vmca of an aircraft?

A
  1. One engine inop and windmilling (or feathered if equipped with autofeather)
  2. No more than 5 degree bank towards operating engine
  3. Takeoff power on operative engine
  4. Landing gear up
  5. Flaps and cowl flaps in takeoff position
  6. Most rearward (unfavorable) CG and maximum takeoff weight
  7. Airborne, out of ground effect
  8. Trim set for takeoffs