Question 1
Answer
-
183.8 square feet
-
182.8 square feet
-
183.6 square feet
-
182.6 square feet
Question 2
Answer
-
38 ft. 8 in
-
36 ft. 8 in
-
38 ft. 7 in
-
36 ft. 7 in
Question 3
Answer
-
2 ft 1.20 in
-
2 ft 1.18 in
-
3 ft 1.20 in
-
3 ft 1.16 in
Question 4
Answer
-
27 ft 7.20 in
-
25 ft 7.18 in
-
28 ft 7.20 in
-
26 ft 7.18 in
Question 5
Answer
-
8 ft 6 in
-
6 ft 8 in
-
7 ft 6 in
-
8 ft 7 in
Question 6
Question 7
Question
Minimum turning radius
Question 8
Question
Propeller Manufacturer
Answer
-
Hartzell
-
Heartzel
-
McCauley
-
Airmaster
Question 9
Question
Propeller Max Diameter
Question 10
Question
Propeller Min Diameter
Question 11
Question
Left Propeller Model No
Answer
-
HC-C2Y (K,R) – 2CEUF
-
FC 7666 A - 2R
-
HC-C2Y (K,R) – 2CLEUF
-
HC-C2Y (K,R) – 2CUEF
-
HC-C2Y (K,R) – 2CLUEF
Question 12
Question
Right Propeller Model No.
Answer
-
HC-C2Y (K,R) – 2CLEUF
-
FJC 7666 A – 2R
-
HC-C2Y (K,R) – 2CEUF
-
FC 7666 A - 2R
Question 13
Question
Engine Manufacturer
Answer
-
Lycoming
-
Lycuming
-
Cummins
-
Rolls-Royce
Question 14
Answer
-
180 HP
-
190 HP
-
170 HP
-
200 HP
Question 15
Question
Engine Max Speed
Answer
-
2700 rpm
-
2800 rpm
-
2750 rpm
-
2600 rpm
Question 16
Question
Engine Model No. (Left)
Answer
-
O-360-E1A6D
-
O-370-E1A6D
-
O-360-E1A5D
-
LO-360-E1A6D
Question 17
Question
Engine Model No. (Right)
Answer
-
LO-360-E1A6D
-
O-360-E1A6D
-
O-360-E1A0D
-
LO-360-E10D
Question 18
Answer
-
Four cylinder, direct-drive
-
horizontally opposed, air-cooled
-
Six cylinder, direct-drive
-
horizontally opposed, air-cooled, fuel injected
Question 19
Answer
-
6 QTS (max), 4 QTS (min)
-
7 QTS (max), 5 QTS (min)
-
5 QTS (max), 3 QTS (min)
-
8 QTS (max), 6 QTS (min)
Question 20
Question
Recommended Fuel
Answer
-
100LL (BLUE)
-
100/130 (minimum grade)
-
Jet Fuel
-
G100UL
Question 21
Answer
-
110 US GAL, 55 GAL per tank
-
100 US GAL, 50 GAL per tank
-
120 US GAL, 60 GAL per tank
-
90 US GAL, 45 GAL per tank
Question 22
Answer
-
110 GAL, 55 GAL per tank
-
108 GAL, 54 GAL per tank
-
120 GAL, 60 GAL per tank
-
106 GAL, 53 GAL per tank
Question 23
Question 24
Question
Fuel Consumption
Answer
-
26 GPH, 13 GPH per engine
-
28 GPH, 14 GPH per engine
-
30 GPH, 15 GPH per engine
-
24 GPH, 12 GPH per engine
Question 25
Answer
-
12 V | 35 amp/hr
-
12 V | 60 amp/hr
-
14 V | 60 amp/hr
-
14 V | 35 amp/hr
Question 26
Question
MAX GROSS WEIGHT
Answer
-
3800 LBS
-
3900 LBS
-
4800 LBS
-
2800 LBS
Question 27
Question
Max Take-off weight
Answer
-
3800 LBS
-
4800 LBS
-
3816 LBS
-
3000 LBS
Question 28
Answer
-
3816 LBS
-
3800 LBS
-
3815 LBS
-
3850 LBS
Question 29
Question
Max Landing weight
Answer
-
3800 LBS
-
3870 LBS
-
3100 LBS
-
3300 LBS
Question 30
Question
Baggage Area and weight capacity
Answer
-
24 cu. Ft, 200 LBS
-
25 cu. Ft, 180 LBS
-
24 cu. Ft, 300 LBS
-
26 cu. Ft, 200 LBS
Question 31
Answer
-
21.1 lbs/sq. ft.
-
21.2 lbs/sq. ft.
-
22.1 lbs/sq. ft.
-
23.1 lbs/sq. ft.
Question 32
Answer
-
10.56 lbs/hp
-
10.55 lbs/hp
-
11.55 lbs/hp
-
20.55 lbs/hp
Question 33
Question
Maneuvering Speed 3800lbs (VA)
Answer
-
135 KIAS
-
136 KIAS
-
145 KIAS
-
112 KIAS
Question 34
Question
Maneuvering Speed 2700lbs (VA)
Answer
-
112 KIAS
-
120 KIAS
-
135 KIAS
-
113 KIAS
Question 35
Question
Never Exceed Speed (VNE)
Answer
-
202 KIAS
-
203 KIAS
-
169 KIAS
-
205 KIAS
Question 36
Question
Maximum Structural Cruising Speed (VNO)
Answer
-
169 KIAS
-
179 KIAS
-
202 KIAS
-
160 KIAS
Question 37
Question
Maximum Flaps Extended Speed (VFE)
Answer
-
111 KIAS
-
110 KIAS
-
131 KIAS
-
101 KIAS
Question 38
Question
Maximum Gear Extended Speed (VLE)
Answer
-
140 KIAS
-
160 KIAS
-
150 KIAS
-
142 KIAS
Question 39
Question
Maximum Landing Gear Extending Speed (VLO)
Answer
-
140 KIAS
-
150 KIAS
-
180 KIAS
-
110 KIAS
Question 40
Question
Maximum Landing Gear Retracting Speed (VLO)
Answer
-
102 KIAS
-
109 KCAS
-
109 KIAS
-
101 KIAS
Question 41
Question
Air Minimum Control Speed (VMCA)
Answer
-
55 KIAS
-
56 KIAS
-
57 KIAS
-
66 KIAS
Question 42
Question
Decision Speed (V1)
Answer
-
56 KIAS
-
55 KIAS
-
54 KIAS
-
57 KIAS
Question 43
Answer
-
88 KIAS
-
98 KIAS
-
80 KIAS
-
85 KIAS
Question 44
Question
Rotation Speed (VR)
Answer
-
70 (short field)
-
75 (normal)
-
80 (loaded)
-
60 (short field)
-
70 (normal)
-
90 (loaded)
Question 45
Question
Best Angle of Climb Speed (VX)
Question 46
Question
Best Rate of Climb Speed (VY)
Question 47
Question
Stall Speed (VS0)
Question 48
Question
Stall Speed (VS1)
Question 49
Question
Maximum Demonstrated Crosswind
Answer
-
17 KTS
-
15 KTS
-
12 KTS
-
18 KTS
Question 50
Question
White Arc (Flap Operating Range)
Answer
-
55-111 kts
-
50-110 kts
-
65-111 kts
-
50-111 kts
Question 51
Question
Green Arc (Normal Operating Range)
Answer
-
57-169
-
58-170
-
57-110
-
55-169
Question 52
Question
Yellow Arc (Caution Range)
Answer
-
169-202
-
170-201
-
169-201
-
170-202
Question 53
Question
Red Radial Line (VNE)
Question 54
Question
Red Radial Line (One Engine Inop., air min. control speed)
Question 55
Question
Blue Radial Line (One Engine Inop., best rate of climb speed)
Question 56
Question
Engine Maximum Rotation Speed (RPM)
Question 57
Question
Maximum Manifold Pressure
Answer
-
FULL THROTTLE
-
15" MP
-
24" MP
-
20" MP
Question 58
Question
Maximum Cylinder Head Temperature (CHT)
Answer
-
500° F
-
550° F
-
600° F
-
540° F
Question 59
Question
Maximum Oil Temperature
Answer
-
245° F
-
255° F
-
260° F
-
215° F
Question 60
Question
FUEL PRESSURE: Normal Operating Range (Green Arc)
Answer
-
0.5-8 psi
-
0.5-9 psi
-
0.8-8 psi
-
1.5-8 psi
Question 61
Question
TACHOMETER: Green Arc (Normal Operating Range)
Answer
-
500-2700rpm
-
500-2800rpm
-
600-2700rpm
-
100-2700rpm
Question 62
Question
OIL TEMPERATURE: Green Arc (Normal Operating Range)
Answer
-
75°-245° F
-
75°-255° F
-
85°-245° F
-
75°-245° C
Question 63
Question
OIL PRESSURE: Green Arc (LEFT ENGINE)
Answer
-
55-90psi
-
60-90psi
-
15-60psi
-
25-60psi
Question 64
Question
OIL PRESSURE: Green Arc (RIGHT ENGINE)
Answer
-
60-90psi
-
55-90psi
-
90-100psi
-
90-115psi
Question 65
Question
OIL PRESSURE: Yellow Arc (Caution/Idle) [LEFT ENGINE]
Answer
-
55-90psi
-
15-60ps
-
90-115psi
-
90-100psi
Question 66
Question
OIL PRESSURE: Yellow Arc (Caution/Idle) [RIGHT ENGINE]
Answer
-
90-100psi
-
25-60psi
-
55-90psi
-
60-90psi
Question 67
Question
OIL PRESSURE: Yellow Arc (Warm-up/Taxi/Takeoff) [LEFT ENGINE]
Answer
-
90-115psi
-
15-60psi
-
25-60psi
-
90-100psi
Question 68
Question
OIL PRESSURE: Yellow Arc (Warm-up/Taxi/Takeoff) [RIGHT ENGINE]
Answer
-
90-100psi
-
25-60psi
-
90-115psi
-
15-60psi
Question 69
Question
CYLINDER HEAD TEMPERATURE
Green Arc
Answer
-
200°-435° F
-
200°-500° F
-
200°-435° C
-
200-435 K
Question 70
Question
CYLINDER HEAD TEMPERATURE
Red Line (maximum)
Answer
-
500° F
-
500 K
-
500° C
-
435° F
Question 71
Question
The nose gear must not exceed a turning angle of how many degrees when towed?
Question 72
Question
What is the maximum allowable
RPM drop when checking the
feathering of the propeller?
Answer
-
175rpm
-
200rpm
-
150rpm
-
100rpm
Question 73
Question
What is the first instrument you
should check after starting the
engine?
Question 74
Question
What type of fuel system is
normally used to supply fuel to
the engine of the PA-44-180?
Answer
-
Engine-driven fuel pumps
-
Fuel Injected
-
Gravity Fed
Question 75
Question
What is the normal enroute or
cruise climb speed of the PA-44-180?
Answer
-
105 kts
-
200 kts
-
100 kts
-
110 kts
Question 76
Question
Normal operating range of the
vacuum system
Answer
-
4.8-5.2 in. Hg.
-
5-6.2 in. Hg.
-
4.6-5.2 in. Hg.
-
4.8-5.8 in. Hg.
Question 77
Question
How many voltage regulators are
equipped in the PA-44-180 to maintain
effective load sharing in their electrical
system?
Question 78
Question
Squat switch locations for stall warning system and landing gear
Answer
-
left wing and left main gear
-
right wing and right main gear
-
right wing and left main gear
-
left wing and right main gear
Question 79
Question
The squat switch has two functions on the Piper Seminole when it is on ground
Answer
-
Removes power from the hydraulic pump
-
Deactivates the stall warning
-
Activates pitot heat
-
Gives power to the hydraulic pump
Question 80
Question
If hydraulic pressure is lost, the landing gear
Question 81
Question
Emergency landing gear extension is limited to
Answer
-
100 kts
-
200 kts
-
110 kts
-
90 kts
Question 82
Question
The Seminole is equipped with brakes on:
Question 83
Question
How many blades does the propeller of each engine has?
Question 84
Question
This is the capability of a propeller to change the blade angle:
Answer
-
Controllable Pitch
-
Constant Speed
-
Full Feathering
Question 85
Question
How many alternators is the Piper Seminole equipped with?
Answer
-
2, one on each engine
-
1 on left engine
-
1 on the right engine
-
none
Question 86
Question
This is the capability of the propeller blades to align with the relative wind to decrease drag:
Answer
-
Full Feathering
-
Constant Speed
-
Controllable Pitch
Question 87
Question
The Seminole is equipped with this type of flap system
Answer
-
Manual
-
Pneumatic
-
Hydraulic
-
Electrical
Question 88
Question
The landing gear on the Seminole is:
Answer
-
Hydraulically actuated, electrically operated
-
Manually operated
-
Electrically operated
-
Electrically actuated, hydraulically operated
Question 89
Question
The propeller governor constantly varies oil pressure into the propeller hub to change the propeller blade pitch. This is known as:
Answer
-
Constant Speed
-
Full Feathering
-
Controllable Pitch
Question 90
Question
The Piper Seminole has the following wing flaps positions:
Question 91
Question
Pitot tube and static port are combined together and located on the:
Answer
-
Left wing
-
Right wing
-
Nose
-
Tail
Question 92
Question
Regardless of the propeller lever position, what will happen when oil pressure is lost?
Answer
-
Propeller will feather if the RPM are above 950
-
Propeller will not feather.
-
Propeller will feather regardless of the RPM
-
Propeller will feather if the RPM are below 950
Question 93
Question
The stall warning horn is activated by two lift detectors on the leading
edge of the left wing, outboard of the engine nacelle. The inboard detector
activates the horn when the flaps are in the
Question 94
Question
The stall warning horn is activated by two lift detectors on the leading
edge of the left wing, the outboard activates the horn when the flaps are in positions
Question 95
Question
The landing gear warning system will be activated under any of the following conditions:
Answer
-
Gear not locked down with throttle below 15" MP
-
Gear not locked down with wing flaps selected from 25 - 40 degrees
-
Gear handle up position when on ground
-
Airspeed is below 88 KIAS and the gear is up
-
RPMs drop below 2300 and the landing gear is up
Question 96
Answer
-
14 V | 60 amp/hr
-
14 V | 35 amp/hr
-
12 V | 60 amp/hr
-
12 V | 35 amp/hr
Question 97
Question
Safe Speed for intentional engine failure
Answer
-
82 kts
-
83 kts
-
81 kts
-
84 kts
Question 98
Question
OIL PRESSURE: Red Line (Minimum) [left engine]
Question 99
Question
OIL PRESSURE: Red Line (Minimum) [right engine]
Question 100
Question
OIL PRESSURE: Red Line (Maximum) [left engine]
Answer
-
115psi
-
215psi
-
105psi
-
110psi
Question 101
Question
OIL PRESSURE: Red Line (Maximum) [right engine]
Answer
-
110psi
-
100psi
-
105psi
-
102psi