Piper Seminole Aircraft Systems
Instructions. Please read. After completing Unit 3 of the Multiengine Addon Training Course, you must take this quiz. The minimum passing grade is 80%. If you fail the quiz, please review Unit 3. Put special attention on the questions you got wrong in the quiz. You may retake the quiz until you get 80% at least. After successfully completing the quiz, you will get a completion certificate that you must download and keep in your records as proof of passing this quiz. This certificate is a requirement to receive credit for the Unit and graduation of the Course. Please type your name in the fields below for your completion certificate after passing the quiz.
- 1.Which type of engines is the seminole equipped with?
- A.
Lycoming TO-320
- B.
Continental TIO-520
- C.
Lycoming (L)TO-360
- D.
Continental O-200
- 2.What is the rated power of the Piper Turbo Seminole engines?
- A.
200 horsepower at 2700 RPM
- B.
180 horsepower at 2700 RPM
- C.
160 horsepower at 2575 RPM
- D.
180 horsepower at 2575 RPM
- 3.How is the propeller driven on the Piper Turbo Seminole engines?
- A.
Reduction Gearbox Drive
- B.
Direct Drive
- C.
Non-Direct Drive
- 4.The Piper Turbo Seminole engines are not susceptible to induction icing:
- A.
True
- B.
False
- 5.How many blades does the propeller of each engine has?
- A.
1 blade
- B.
2 blades
- C.
3 blades
- D.
4 blades
- 6.This is the capability of a propeller to change the blade angle:
- A.
Full Feathering
- B.
Constant Speed
- C.
Controllable Pitch
- 7.This is the capability of the propeller blades to align with the relative wind to decrease drag:
- A.
Full Feathering
- B.
Constant Speed
- C.
Controlable Pitch
- 8.The propeller governor constantly varies oil pressure into the propeller hub to change the propeller blade pitch. This is known as:
- A.
Full Feathering
- B.
Constant Speed
- C.
Controlable Pitch
- 9.Regardless of the propeller lever position, what will happen when oil pressure is lost?
- A.
Propeller will not feather.
- B.
Propeller will feather if the RPM are above 950
- C.
Propeller will feather if the RPM are below 950
- D.
Propeller will feather regardless of the RPM
- 10.The landing gear on the Seminole is:
- A.
Manually operated
- B.
Electrically operated
- C.
Hydraulically actuated, electrically operated
- D.
Electrically actuated, hydraulically operated
- 11.The landing gear is held up by:
- A.
Mechanical up locks
- B.
Hydraulic pressure
- C.
Electrical actuators
- D.
Spring system
- 12.The landing gear horn will sound:
- A.
When power is approximately below 15” with the landing gear up
- B.
Airspeed is below 88 KIAS and the gear is up
- C.
Flaps 25 or 40 are selected and the landing gear is not down
- D.
Landing gear handle is selected up on ground
- E.
RPMs drop below 2300 and the landing gear is up
- 13.Gear retraction on ground is prevented by:
- A.
Squat switch on the right main landing gear
- B.
Squat switch on the left main landing gear
- C.
Landing gear handle
- D.
Hydraulic pressure trapped by a valve
- 14.If hydraulic pressure is lost, the landing gear:
- A.
Won’t operate up or down
- B.
Will free fall down
- C.
Will stay up
- 15.Emergency landing gear extension is limited to:
- A.
88 KIAS
- B.
100 KTAS
- C.
100 KIAS
- D.
140 KIAS
- 16.The Seminole is equipped with brakes on:
- A.
Main landing gear
- B.
Nose landing gear
- C.
Nose and main landing gear
- 17.Parking brake is permitted to be used during training flights at TecBlue:
- A.
True
- B.
False
- 18.The Seminole is equipped with this type of flap system
- A.
Electrical
- B.
Hydraulic
- C.
Pneumatic
- D.
Manual
- 19.The Piper Seminole has the following wing flaps positions:
- A.
0
- B.
5
- C.
10
- D.
20
- E.
25
- F.
30
- G.
36
- H.
40
- I.
46
- 20.Pitot tube and static port are combined together and located on the:
- A.
Nose
- B.
Left wing
- C.
Right wing
- D.
Tail
- 21.Total usable fuel on the Piper Seminole is:
- A.
100 gals (50 per side)
- B.
108 gals (54 per side)
- C.
110 gals (55 per side)
- D.
116 gals (58 per side
- 22.The electrical system on the Piper Seminole is:
- A.
12 Volt
- B.
14 Volt
- C.
24 Volt
- D.
28 Volt
- 23.How many alternators is the Piper Seminole equipped with?
- A.
1 on the left engine
- B.
1 on the right engine
- C.
2, one on each engine
- D.
None
- 24.The inboard stall warning detector provides stall warning at:
- A.
Flaps 0
- B.
Flaps 10 & 25
- C.
Flaps 25 & 40
- D.
Flaps 40
- 25.The squat switch has two functions on the Piper Seminole when it is on ground:
- A.
Prevents the propeller from feathering
- B.
Removes power from the hydraulic pump
- C.
Disable radio communications
- D.
Deactivates the stall warning
Questions: 186 | Attempts: 17244 | Last updated: Mar 22, 2022
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