Piper Arrow II Flashcards

(67 cards)

0
Q

Describe the engine

A

Lycoming IO-360

Four cylinder, direct drive , horizontally opposed, fuel injected engine

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1
Q

Max gross weight?

A

2650 lbs

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2
Q

Max horsepower for the engine

A

200hp

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3
Q

Maximum RPM of the prop

A

2700 RPM

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4
Q

What is the amperage and voltage of the alternator?

A

60 amp, 14V

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5
Q

Describe the propeller

A

Hartzell two-bladed, constant speed, controllable pitch prop

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6
Q

Describe the landing gear system

A

Retractable tricycle landing gear, hydraulically actuated by an reversible electric pump

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7
Q

What is the approximate landing hear transit time?

A

About 7 seconds

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8
Q

What area the landing gear max retraction and extension speeds?

A

125 MPH - retract

150 MPH extension

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9
Q

Describe the nose gear system. How is it operated?

A

Steed through a 30 degree arc by use of the rudder pedals and brakes. As nose gear retracts, the steerage linkage is disengaged in flight. The nose wheel also contains a hydraulic shimmy damper.

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10
Q

Describe the oleo struts. What is the normal extension.

A

Air-oil type struts. Normal extension is 2.75” for nose gear, 2.0” for the mains.

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11
Q

Describe the brake system.

A

Toe brakes on left side rudder pedals and a hand brake. Toe brakes on the right side are optional. Toe brakes and hand brake have individual cylinders but share one reservoir. Single disk, single puck brake mounted on each main gear.

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12
Q

Describe the horizontal stabilizer

A

Uses a flying tail or stabilator design with a trim tab/servo mounted on the trailing edge.

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13
Q

What is the capacity and useable fuel for the fuel tanks?

A

25 gallon capacity per tank. 24 gals useable per tank.

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14
Q

How is the alternator protected?

A

A voltage regulator and an over voltage relay.

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15
Q

What is the voltage if the battery? How many amp hours can it support?

A

12 volt, 25 AMP hours

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16
Q

What does the vacuum system consist of?

A

Engine-driven vacuum pump, a vacuum regulator, a filter and necessary plumbing

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17
Q

What type of pump is the vacuum pump

A

A dry pump

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18
Q

What protects the vacuum pump from damage?

A

A shear drive

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19
Q

What happens if the vacuum drive shears?

A

The gyros become inoperative

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20
Q

What is the normal operating range for the vacuum system?

A

5.0 In/hg +/- 0.1

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21
Q

An unexpected decrease in vacuum system pressure could indicate what problems?

A

Dirty filter, dirty screens, a sticking vacuum regulator or leak in the system.

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22
Q

What could zero pressure in the vacuum system indicate?

A

A sheared pump drive, defective pump, a defective gauge or collapsed line

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23
Q

What happens if vacuum system pressure is outside the normal operating range?

A

Too high - could damage the gyros.

Too low - gyros are unreliable

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24
Where is the vacuum regulator located?
Behind the instrument panel
25
What annunciations are provided by the annunciation panel?
Alternator, oil pressure or vacuum system malfunctions.
26
What are pitot and static pressure picked up?
From the pitot head on the bottom of the left wing
27
What is the maximum capacity of the baggage area?
200 lbs
28
A what speed is the stall warning indicator activated?
5-10 mph above stall speed
29
How is the stall warning system activated?
By a lift detector on e leading edge of the left wing
30
What are the high and low pitch settings for the propeller?
Hartzell High 29.0 +/- 2.0 Low 14 +/- 0.2 McCauley High 29.8 +/- 0.5 Low 12.5 +/- 0.2
31
What is the diameter of the propellers?
73 - 74"
32
What is the oil temperature normal operating range?
75 - 245 deg F
33
What is the red line temp for the oil temp?
245 deg F
34
What is the green arc (norm operating range) for the oil pressure?
60-90 PSI
35
What is the yellow arc (caution rang) for oil pressure?
25-60 PSI
36
What are the min and max red lines for the oil pressure?
25 PSI | 90 PSI
37
What is the green arc for fuel pressure?
14-45 PSI
38
What are the min and max red lines for fuel pressure?
14 PSI | 45 PSI
39
What are the normal operating ranges for the prop?
For ser numbers below 28R-7635517: 500-2100 2350-2700 For serial numbers 28R-7635517 and up: 500-2700
40
VNE
214 MPH
41
VNO
170MPH
42
VA
131 MPH
43
VFE
125 MPH
44
VLE
150MPH
45
VLR
125 MPH
46
VS
71 MPH
47
VS0
64 MPH
48
Max positive load factor
3.8 G
49
VG
105 MPH
50
What is the arm for the front seat?
80.5"
51
What is the arm for the rear seat?
118.1"
52
What is the arm for the fuel?
95.0
53
What is the arm for the baggage compartment?
142.8
54
What is the change in moment when retracting the landing gear?
819
55
At what RPM setting should the engines be warmed up?
1400-1500 RPM, for not more than 2 mins
56
A what RPM setting should the magnetos be checked?
2000 RPM
57
What is the max RPM drop during the mag check? What is the max differential?
Max drop - 175RPM | Max diff - 50 RPM
58
VR, normal takeoff
60-70 MPH
59
Flap setting for short field takeoff
25 deg
60
VR, short field
60-65 MPH
61
VX (LE)
85 MPH
62
VY (LE)
95 MPH
63
VY
100 MPH
64
VX
96 MPH
65
V(climb)
110 MPH
66
V(app)
90 MPH