DA20-C1 Type Exam
Diamond DA20-C1 Eclipse · Weight And Balance
Overview
The document is a type examination for the Diamond DA20-C1 Eclipse, designed to assess a pilot's knowledge and understanding of the aircraft's systems, performance, and operational procedures. It includes questions on various aspects such as weight and balance, airspeeds, emergency procedures, and aircraft handling. This examination serves as a reference for pilots to ensure they are familiar with the aircraft's specifications and operational limits, which is crucial for safe flying. The questions are structured to cover essential areas of knowledge that a pilot must be proficient in before operating the DA20-C1.
- Maximum take-off weight: [specific weight not provided] lbs.
- Maximum landing weight: [specific weight not provided] lbs.
- Basic empty weight: [specific weight not provided] lbs.
- Weight of full usable fuel: [specific weight not provided] lbs.
- Aircraft useful load: [specific weight not provided] lbs.
Document
Source
Originally published by www.sealandair.ca. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Weight And Balance
- Pages
- 4
- File size
- 765 KB
- Publisher
- www.sealandair.ca
Common. One of the most common aircraft types we track.
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In this document
Weight and Balance
This section covers critical weight and balance parameters for the DA20-C1 Eclipse. Key figures include the maximum take-off weight, maximum landing weight, basic empty weight, weight of full usable fuel, and the aircraft's useful load. Pilots must also determine if the aircraft is within weight and balance limitations under specific loading conditions.
Airspeeds
The airspeeds section outlines important performance metrics such as stall speed in landing configuration, never exceed speed, maximum structural cruising speed, and manoeuvring speed at maximum gross weight. It also includes speeds for take-off and landing flaps, normal rotation speed, and best rate of climb.
Emergency Procedures
This section details the actions pilots should take in various emergency scenarios, including generator failure, engine failure during flight, and indications of high oil temperature or low oil pressure. It emphasizes the importance of knowing emergency procedures to ensure safety during flight.
Aircraft Performance
The performance section requires pilots to understand power settings, fuel consumption, and true airspeed for cruising at different altitudes. It also includes calculations for required take-off distances under various conditions.
Defect Control Procedures
This section provides guidance on how to handle suspected defects in the aircraft, including snagging procedures and the protocol for flying with non-airworthy defects.
Safety notes
- Ensure the aircraft is within weight and balance limitations before flight.
- Follow emergency procedures promptly to ensure safety.
Full document text
DA20-C1 Type Exam DA20-C1 Type Exam Page 1 Pilot: Licence #: Instructor: Date: Reference: DA20-C1 POH, Dispatch form, and DA20-C1 Aircraft Handling Guide General: 1. Is this aircraft certified for: ► Steep turns more than 60 ? YES / NO ► Spins? YES / NO 2. Are aerobatics permitted in this aircraft? ► YES / NO 3. What is the primary type of material used in the aircraft's construction? 4. Are flaps required for take-off? ► YES / NO 5. How are the rudder pedals adjusted? 6. What chapter of the POH lists the "Minimum Operational Equipment"? 7. What type of propeller is installed for DA20-C1 at SLA? __________________________ Fuel System: 1. What is the total usable fuel capacity? 2. What is the correct fuel grade? Colour? 3. Where are the drains located? Oil System: 1. What is the minimum oil level? Max level? 2. What is the recommended oil? Where does Sea Land Air list this information? Weight and Balance: 1. What is the maximum take-off weight? lbs. 2. What is the maximum landing weight? lbs. 3. What is the basic empty weight of the aircraft to be flown? lbs. 4. What is the weight of full usable fuel? lbs. 5. What is the aircraft useful load? lbs. 6. Determine if the aircraft is within the weight and balance limitations given the following conditions: Full fuel, front passengers = 360 lbs, baggage = 40 lbs. ► YES / NO DA20-C1 Type Exam DA20-C1 Type Exam Page 2 Airspeeds: Use indicated airspeeds. 1. Stall speed in the landing configuration (Vso)? 2. Never exceed speed (Vne)? 3. Max structural cruising speed (Vno)? 4. Manoeuvring speed (Va) at max gross weight? Does Va increase / decrease as gross weight decreases? 5. Max flap extended speeds (Vfe) for T/O flaps? LDG flaps? 6. Normal rotation speed? 7. Short field take-off climb speed? 8. At what altitude should the flaps be retracted after departure? 9. Best rate of climb (Vy) at sea level? flaps @ T/O flaps @ CRUISE 10. Maximum demonstrated crosswind component? 11. Short field final approach airspeed? Aircraft configuration? 12. Best power off glide speed with flaps CRUISE? Starting Engine: Describe the procedures for starting this aircraft in cold temperature. Emergency Procedures: 1. What would you do if the Generator Annunciator illuminated? 2. What actions would you take if you experienced an engine failure during flight? 3. What actions would you take if you noticed high oil temperature? 4. What actions would you take if you noticed low oil pressure while in flight? 5. Describe the "Go Around" procedures. DA20-C1 Type Exam DA20-C1 Type Exam Page 3 Aircraft Performance: 1. What is the power setting, fuel consumption and true airspeed for cruising with 70% BHP at 4,000 feet with standard temperature (lean to Best Power)? Use appropriate performance charts for the installed type of propeller. RPM TAS Fuel Consumption 2. What is the required take-off distance to clear a 50ft obstacle using maximum performance procedures with the aircraft at gross weight and an eight knot headwind under the following conditions: ► Sea level, standard temperature? feet ► Pressure altitude = 4,000ft, temperature = 32°C? feet Winter Operations: 1. At what temperature should the baffles be installed? °C Ground / Air 2. What is the recommended oil to be used during winter? Aircraft Handling 1. Why is it important to know the current and forecasted temperature during a walk around for DA20-C1? 2. Under what conditions do the inlet baffles need to be removed? 3. You observe "high oil temperature and low oil pressure" in flight with inlet baffles installed. What should you do? 4. Cylinder Head Temperature is indicating lower than 300°F (green range is between 300°F and 420°F) What should you do? 5. When should you release ignition switch from "START" position to start engine? 6. What checklist should you use when starting a Hot Engine? 7. If you prime a hot engine accidently, what could happen? 8. What should you confirm on Cylinder Head Temperature and oil temperature gauges before takeoff? DA20-C1 Type Exam DA20-C1 Type Exam Page 4 9. Why should you plan a power assist approach? 10. What are the three steps to achieve a power assisted approach on final leg? 11. What will happen if you have higher than 55kt for your final approach speed? 12. What method should you use for cross-wind landing? 13. How can you prevent engine stoppage while turning to taxi out from the runway (especially with a tailwind)? 14. What should your mixture setting be while taxing? Defect Control Procedures: 1. What should you do if you suspect a defect? 2. How do you snag an aircraft? 3. If you have discovered a defect that does not affect the airworthiness of your aircraft, are you allowed to fly the aircraft immediately? Why? DA20-C1 Type Exam Completed Satisfactorily Flight Instructor’s Signature Date Pilot’s Signature Date
What's in the Diamond DA20-C1 Eclipse TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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