Diamond DA42 Twin Star Proficiency Exam

Transcription

Diamond DA42 Twin Star
Proficiency Exam
Name: _____________________________________
Date: ______________________________________
Instructor: __________________________________
CORRECTED TO 100%
Instructor Signature: ______________________________
Pilot Signature: __________________________________
DA42 PROFICIENCY EXAM
1
CHAPTER 1: GENERAL
DIMENSIONS
1. Fill in the numbers where arrows are located.
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2. What type of engines are on the DA42 Twin Star?
___________________________________________________________
___________________________________________________________
3. What type of propellers are installed on the DA42 Twin Star?
___________________________________________________________
___________________________________________________________
4. The DA42 has a maximum rated horsepower for each engine. What is the
horsepower and at what RPM?
___________________________________________________________
___________________________________________________________
5. Define the following with respect to the DA42 Twin Star.
a. CFRP: _______________________________________________
b. GFRP: _______________________________________________
c. ECU: ________________________________________________
d. FADEC: ______________________________________________
e. EPU: ________________________________________________
f. GIA: _________________________________________________
3
CHAPTER 2: OPERATING LIMITATIONS
1. Define and list the following airspeed for the DA42 Twin Star.
VSpeed
Vs
DEFINITION
Vso
Vmca
Vx
Vy
Vyse
Vfe
Vle
Vlo
Va
Vno
Vne
4
SPEED
2. Airspeed Indicator Markings:
a. White Arc: ____________________________________
b. Green Arc: ___________________________________
c. Yellow Arc: ___________________________________
d. Blue Radial: ___________________________________
e. Red Radial (Min): _____________________________
f. Red Radial (Max): _____________________________
3. Power Plant Limitations & Airframe Limitations
RPM (Max): _____________________________________________
RPM (Max Overspeed): ___________________________________
Max Take off power / %Load: ______________________________
Max Continuous Power / % Load: __________________________
Fuel Temp Max: __________________________________________
Fuel Temp Min: ___________________________________________
Oil Pressure Max: _________________________________________
Oil Pressure Min: __________________________________________
Oil Quantity Max: __________________________________________
Oil Quantity Min: ___________________________________________
Gearbox Temp Max: _______________________________________
Coolant Temp Max: ________________________________________
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Coolant Temp Min: ________________________________________
Voltage Max: ______________________________________________
Voltage Min: ___________________________________________
Amperage Max: ___________________________________________
Approved Fuel Grades: ____________________________________
Oil Grades: _______________________________________________
Total Useable Fuel: ________________________________________
Max Fuel Quantity: _________________________________________
Gearbox Oil (Propeller Gearbox):___________________________
Coolant Type: _____________________________________________
Maximum Restart Altitude: _________________________________
Restart Airspeed: __________________________________________
Max Take off Weight: ______________________________________
Zero Fuel Weight: _________________________________________
Max Landing Weight: ______________________________________
Minimum Flight Weight: ____________________________________
Max Baggage Weight: _____________________________________
Nose: ______________________________________________
Cockpit Baggage: ___________________________________
Baggage Extension: _________________________________
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CHAPTER 3: EMERGENCIES
One engine inoperative minimum
control speed (air) Vmca
One engine inoperative speed for best
rate of climb Vyse
1. One engine inoperative during flight – Engine Trouble Shooting
2. Engine Securing (feathering) procedure
3. Unfeathering and restarting engine in flight
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4. Engine failure during takeoff – After Liftoff
5. Engine Feathering Procedure (securing Engine)
6. Engine Failure in Flight – During speeds above Vmca
7. Landing with one engine inoperative
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8. Balked landing with one engine inoperative
9. Flight with one engine inoperative
10. Landing Gear System Failures – Landing gear unsafe warning
11. Landing Gear System Failures – Manual Gear Extension of Landing Gear
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12. Failure of the Electrical System – Complete Failure of the Electrical
System
13. Smoke and Fire – Engine Fire on the Ground
14. Smoke and Fire – Engine Fire in Flight
15. Smoke and Fire – Electrical Fire on Ground
10
16. Smoke and Fire – Electrical Fire in Flight
17. Defective propeller RPM regulating system – Propeller Over Speed
18. Recovery from unintentional spin
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CHAPTER 4: NORMAL PROCEDURES
Airspeed for Rotation
Airspeed for take off climb (Best rate of climb speed)
Airspeed for best angle of climb (NOTE*)
Airspeed for cruise climb
Reference landing approach speed
Final approach speed
Minimum speed during go around
Max structure cruising speed. Do not exceed this speed except
in smooth air, and then only with caution
19. What does the NOTE* signify in the Airspeed chart signify?
20. What are the main points of a daily check, done before the first flight of the
day?
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CHAPTER 5: PERFORMANCE
*
EXAMPLE:
What is the fuel flow at 60% load?
ANSWER:
4.4 US Gal / hour
YOUR QUESTION:
What is the fuel flow at 80 % load?
ANSWER: _____________________
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EXAMPLE
OAT
26 degrees celcius
PRESSURE ALTITUDE
2000 ft
TAKE OFF WEIGHT
1500 kg
WIND COMPONENT
11 knots headwind
ANSWER
1600 feet
YOUR QUESTION
OAT
15 degrees C
PRESSURE ALTITUDE
300 ft
TAKE OFF WEIGHT
1600 kg
WIND COMPONENT
5 knots headwind
ANSWER
_______________
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EXAMPLE
OAT
20 degrees celcius
PRESSURE ALTITUDE
4000 ft
TAKE OFF WEIGHT
1500 kg
WIND COMPONENT
5 knots headwind
ANSWER
1214 feet
YOUR QUESTION
OAT
25 degrees C
PRESSURE ALTITUDE
1000 ft
TAKE OFF WEIGHT
1650 kg
WIND COMPONENT
10 knots headwind
ANSWER
_______________
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ANSWER
_______________
EXAMPLE
OAT
20 degrees celcius
PRESSURE ALTITUDE
6000 ft
TAKE OFF WEIGHT
1640 kg
ANSWER
1000 ft/min
YOUR QUESTION
OAT
15 degrees C
PRESSURE ALTITUDE
2000 ft
TAKE OFF WEIGHT
1500 kg
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EXAMPLE
OAT
17 degrees celcius
PRESSURE ALTITUDE
6000 ft
TAKE OFF WEIGHT
1440 kg
ANSWER
200 ft/min
YOUR QUESTION
OAT
15 degrees C
PRESSURE ALTITUDE
8000 ft
TAKE OFF WEIGHT
1600 kg
ANSWER
_______________
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EXAMPLE
POWER SETTING
70%
PRESSURE ALTITUDE
11000 ft
OAT
ISA STD
ANSWER
150 KTS
YOUR QUESTION
POWER SETTING
60%/70%/80%
PRESSURE ALTITUDE
8000 ft
OAT
ISA 10 deg celcius
ANSWER
_______________
18
EXAMPLE
OAT
20 degrees celcius
PRESSURE ALTITUDE
4000 ft
TAKE OFF WEIGHT
1500 kg
WIND COMPONENT
13 knots
ANSWER
1700 ft
YOUR QUESTION
OAT
10 degrees C
PRESSURE ALTITUDE
2000 ft
TAKE OFF WEIGHT
1600 kg
WIND COMPONENT
15 knots
ANSWER
_______________
19
CHAPTER 6: WEIGHT & BALANCE
COMPLETE THE WEIGHT AND
BALANCE FORM
Front Passengers
360 lbs
Rear Passengers
240 lbs
Nose Baggage
40 lbs
Baggage Compartment
60 lbs (Cockpit)
Fuel
?
YOUR QUESTION
How much fuel can you take
____________
Take off Weight
____________
Zero Fuel Weight
____________
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21
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CHAPTER 7: AIRCRAFT SYSTEMS
1. How many fuel tanks are in your DA42?
2. How many fuel pumps total are in the DA42?
3. What is the purpose of each fuel pump?
4. The DA42 has a ____volt system powered by 2, _____ Ampere
alternators.
5. What does the variable elevator backstop do?
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6. Describe the operation of the cabin heat system on the DA42.
7. Give a brief description for each of the following:
a. Hydraulic Pressure Accumulator (landing gear)
b. Engine Operating Controls
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c. ECU Test Button
d. Alternate Air
8. Describe the operation of the engine cooling system.
25
9. Explain how the Turbo charger system works on the DA42.
10. When the pitot heat is turned on inside the cockpit, what other system is
provided heat from the switch?
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Diamond DA42 Twin Star Proficiency Exam

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