POH Section 1 Flashcards
Aircraft length
27ft 7.2in
Wingspan
38ft 6.6in
Aircraft height
8ft 6in
Engine make/models
Lycoming
Left: 0-360-A1H6
Right: L0-360-A1H6
Engine descriptions (excluding make/model)
- Four cylinder
- Direct drive
- Horizontally opposed
- Air cooled
Engine compression ratio
8.5:1
Cylinder bore
Also, what is the definition of bore?
5.125in
Bore: Diameter of the cylinder
Cylinder stroke
Also, definition of stroke
4.375in
Stroke: Distance the piston travels in the cylinder
Engine displacement
361 cubic in
Propeller manufacturer
Hartzell
Propeller diameter, maximum and minimum
Max: 74in
Min: 72in
Propeller type/description (3 things)
- Constant speed
- Hydraulically actuated
- Full feathering
Total fuel, usable and unusable
110 gal (55 either side)
Usable fuel
108 gal (54 either side)
Can 100 octane fuel be used in place of 100LL?
Yes
Oil capacity (min-max)
6-8 quarts
Where to check for which grade of oil you need to use?
POH 1-4
Maximum ramp weight
3816lbs
Maximum takeoff weight
3800 lbs
Maximum landing weight
3800 lbs
Maximum weight in baggage compartment
200 lbs
Baggage compartment volume
24 cu ft
Baggage compartment entry dimensions
Width: 22in
Height: 20in
Wing loading (lbs/square ft)
21.1lbs/sq ft
Power loading (lbs/hp)
10.55lbs/hp
14 CFR Part 23: What are the (8) requirements for FAA certification to determine the Vmca of an aircraft?
- One engine inop and windmilling (or feathered if equipped with autofeather)
- No more than 5 degree bank towards operating engine
- Takeoff power on operative engine
- Landing gear up
- Flaps and cowl flaps in takeoff position
- Most rearward (unfavorable) CG and maximum takeoff weight
- Airborne, out of ground effect
- Trim set for takeoffs