Piper Seminole: PA-44-180

Description

Specifications
Sean Furio
Quiz by Sean Furio, updated 7 months ago
Sean Furio
Created by Sean Furio 7 months ago
42
0

Resource summary

Question 1

Question
Wing area
Answer
  • 183.8 square feet
  • 182.8 square feet
  • 183.6 square feet
  • 182.6 square feet

Question 2

Question
Wing span
Answer
  • 38 ft. 8 in
  • 36 ft. 8 in
  • 38 ft. 7 in
  • 36 ft. 7 in

Question 3

Question
Wing tip
Answer
  • 2 ft 1.20 in
  • 2 ft 1.18 in
  • 3 ft 1.20 in
  • 3 ft 1.16 in

Question 4

Question
Width
Answer
  • 27 ft 7.20 in
  • 25 ft 7.18 in
  • 28 ft 7.20 in
  • 26 ft 7.18 in

Question 5

Question
Height
Answer
  • 8 ft 6 in
  • 6 ft 8 in
  • 7 ft 6 in
  • 8 ft 7 in

Question 6

Question
Elevator height
Answer
  • 10 ft
  • 11 ft
  • 12 ft
  • 9 ft

Question 7

Question
Minimum turning radius
Answer
  • 33 ft
  • 32 ft
  • 34 ft
  • 36 ft

Question 8

Question
Propeller Manufacturer
Answer
  • Hartzell
  • Heartzel
  • McCauley
  • Airmaster

Question 9

Question
Propeller Max Diameter
Answer
  • 74 in
  • 72 in
  • 75 in
  • 77 in

Question 10

Question
Propeller Min Diameter
Answer
  • 72 in
  • 71 in
  • 74 in
  • 75 in

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

Question
Engine MAX HP
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

Question
Engine Type
Answer
  • Four cylinder, direct-drive
  • horizontally opposed, air-cooled
  • Six cylinder, direct-drive
  • horizontally opposed, air-cooled, fuel injected

Question 19

Question
Oil Quantity
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

Question
Total Fuel
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

Question
Usable Fuel
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
Unusable Fuel
Answer
  • 2 GAL
  • 1 GAL
  • 3 GAL
  • 4 GAL

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

Question
Battery
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

Question
Max Ramp weight
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

Question
Wing Loading
Answer
  • 21.1 lbs/sq. ft.
  • 21.2 lbs/sq. ft.
  • 22.1 lbs/sq. ft.
  • 23.1 lbs/sq. ft.

Question 32

Question
Power Loading
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

Question
VYSE
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)
Answer
  • 83
  • 82
  • 81
  • 75

Question 46

Question
Best Rate of Climb Speed (VY)
Answer
  • 88
  • 90
  • 81
  • 85

Question 47

Question
Stall Speed (VS0)
Answer
  • 55
  • 57
  • 60
  • 61

Question 48

Question
Stall Speed (VS1)
Answer
  • 57
  • 55
  • 60
  • 58

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)
Answer
  • 202
  • 201
  • 222
  • 212

Question 54

Question
Red Radial Line (One Engine Inop., air min. control speed)
Answer
  • 56
  • 55
  • 51
  • 53

Question 55

Question
Blue Radial Line (One Engine Inop., best rate of climb speed)
Answer
  • 88
  • 90
  • 70
  • 67

Question 56

Question
Engine Maximum Rotation Speed (RPM)
Answer
  • 2700
  • 2600
  • 2500
  • 2650

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?
Answer
  • 30°
  • 20°
  • 33°
  • 31°

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?
Answer
  • OIL PRESSURE GAUGE
  • CYLINDER HEAD TEMPERATURE
  • OIL TEMPERATURE
  • FUEL PRESSURE

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?
Answer
  • 2
  • 1
  • 3
  • 4

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
Answer
  • will free fall down
  • will remain retracted
  • will get stuck mid extension
  • will explode

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:
Answer
  • Main landing gear
  • Nose landing gear
  • Nose and main landing gear

Question 83

Question
How many blades does the propeller of each engine has?
Answer
  • 2
  • 1
  • 3
  • 4

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:
Answer
  • 0
  • 10
  • 20
  • 25
  • 30
  • 35
  • 40

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
Answer
  • 0 and 10
  • 25 and 40
  • 25
  • 10

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
Answer
  • 10 and 0
  • 25 and 40
  • 10
  • 25

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

Question
Alternator
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]
Answer
  • 15psi
  • 20psi
  • 21psi
  • 22psi

Question 99

Question
OIL PRESSURE: Red Line (Minimum) [right engine]
Answer
  • 25psi
  • 23psi
  • 21psi
  • 26psi

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
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