PRE-SOLO KNOWLEDGE TEST
Diamond DA20-C1 Eclipse · Checklist
Overview
This document is a pre-solo knowledge test specifically designed for pilots training on the Diamond DA20-C1 Eclipse. It covers essential operational knowledge required before solo flight, including airspeeds, weight and balance calculations, fuel requirements, and emergency procedures. The test format encourages pilots to demonstrate their understanding of the aircraft's performance characteristics and operational limits, ensuring they are well-prepared for solo flight. Key topics include takeoff and landing distances, required documentation, and safety protocols, making it a vital resource for student pilots and instructors alike.
- Maximum gross weight: 1764 lbs
- Center of gravity range: 7.95 in – 12.48 in
- Usable fuel capacity: 24 gallons
- Landing distance over a 50 ft obstacle: approx. 1360 ft
- Landing roll distance: approx. 661 ft
Document
Source
Originally published by www.sweetaviation.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Checklist
- Pages
- 5
- File size
- 389 KB
- Publisher
- www.sweetaviation.com
Common. One of the most common aircraft types we track.
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In this document
Airspeeds and Definitions
The document lists various airspeeds critical for the Diamond DA20-C1, including VSO, VS1, VR, VX, VY, VFE, VA, VNO, and VNE. Each airspeed is associated with its visual indication on the airspeed indicator, which is essential for safe flight operations.
Weight and Balance
The weight and balance section provides calculations for the Diamond DA20-C1, including empty weight, pilot and passenger weight, baggage limits, and fuel weight. The maximum gross weight is 1764 lbs, with a center of gravity range from 7.95 in to 12.48 in.
Fuel Requirements
The document specifies the fuel capacity of the Diamond DA20-C1, which is 24 gallons usable. It also outlines the rate of fuel consumption and minimum fuel requirements for solo flight.
Takeoff and Landing Distances
Takeoff ground roll and landing distances are detailed under specific conditions. The landing distance over a 50 ft obstacle is approximately 1360 ft, while the landing roll distance is about 661 ft.
Emergency Procedures
The document includes questions regarding actions to take in the event of an engine failure during takeoff and climb, emphasizing the importance of understanding emergency protocols.
Safety notes
- Ensure all required documents are on board before flight.
- Understand emergency procedures for engine failure during takeoff.
Full document text
PRE-SOLO KNOWLEDGE TEST Diamond Eclipse DA20-C1 Name Date 1 List the airspeeds and their definitions for your airplane. Airspeed Visual Indication on the Definition KIAS Airspeed Indicator (color) VSO VS1 VR VX T/O VX CRUISE VY T/O VY CRUISE VFE T/O VFE LND VA VNO VNE 2. Calculate the gross weight and Center of Gravity for this aircraft with the aircraft having full tanks and you as the pilot. WEIGHT AND BALANCE DIAMOND DA20-C1 N476DC Serial Number C0276 Weight x Arm = Moment 1. Empty Weight 1202.0 lbs. x8.34 in. = 10024.7 in lbs. 2. Pilot & Passenger x 5.63 in. = Center of Gravity= Total Moment Total Weight 3. Baggage (44lbs max) 4. Fuel (6.01 lbs/gal) x 32.44 in. = x 32.44 in. = Limits: Gross Weight: 1764 lbs. (Take off & Landing) (24 gal. usable) Center of Gravity: 7.95 in. – 12.48 in. 5. Total = 3 Fuel: Maximum capacity gallons, of which _ gallons is usable. Rate of fuel consumption _ gal/hr. Minimum fuel required at the start of this solo flight _. Grade of fuel used by this aircraft _ . Color of the fuel used by this aircraft . 4 Oil Maximum capacity of oil qts. Minimum capacity of oil at the start of solo flight _ _ qts. Grade of oil used in this aircraft . 5. What is the takeoff ground roll for this aircraft today? Pressure Altitude Outside Air Temp Aircraft Weight lbs Head Wind Component Obstacle Height Zero feet Ground Roll SENSENICH PROPELLER W69EK7-63, W69EK7-63G and W69EK-63 6 What is the ground roll distance for a landing today? _ 5.3.11. Landing Distance Conditions: - Throttle: Idle - Maximum T/O Weight - Approach Speed 55 KIAS - Level Runway, paved - Wing Flaps in Landing position (LDG) - Standard Setting, MSL Landing distance over a 50 ft (15 m) obstacle: approx. 1360 ft (414m) Landing roll distance: approx. 661 ft (201m) Height above ft. 0 1000 2000 3000 4000 5000 6000 7000 MSL (m) (0) (305) (610) (914) (1219) (1524) (1829) (2134) Landing Distance ft. 1360 1387 1417 1447 1478 1511 1545 1580 (m) 415 423 432 441 450 461 471 782 Landing Roll Distance ft. 661 680 701 722 744 767 791 815 (m) 201 207 214 220 227 234 241 248 7 What would be an indication to use Alternate Air? 8 What are the radio frequencies used at this airport? UNICOM ATIS Fort Wayne International Tower Frequency Approach Control Emergency 9 What airplane certificates and documents must be on board your airplane prior to every flight? A R O W 10 What personal documents and endorsements must you have before beginning a solo flight? 11 Who is directly responsible and is the final authority as to the operation of your airplane when you are flying solo? 12 Except for takeoff and landing, what are the minimum safe altitudes you may operate your airplane? Over congested area feet above the highest obstacle. Other than congested area _ feet above the surface or away from any person, vessel, vehicle, or structure. 13 Explain the actions you would take if the airplane engine failed in the following situations: a. During the takeoff roll b. During the takeoff climb at an altitude of 1200 feet msl? 14 What is the day-VFR fuel requirement? What is the minimum amount of fuel you must have on board in minutes _? In gallons? Fuel gauge? 15 What is the maximum number of passengers you can have in your airplane when you are flying solo in the pattern doing takeoffs and landings? 16 You have been authorized to solo the Diamond DA-20 and want to solo the Cessna 172. What needs to be done before you can solo the Cessna 172? 17 Your approval to solo the Diamond DA-20 was today. For how many days is this approval valid? 18 What is density altitude at Smith Field if the elevation is 834 ft, the barometric pressure is 29.62 inches of mercury, and the temperature is 95º F? Pressure Altitude Density Altitude How will this density altitude affect the performance of this airplane? 19 What are the weather minimums you need to fly solo per the FAA? FAA Visibility Ceiling Height Max Wind Velocity _ Cross Wind Component What is a stall? How will you recognize when the aircraft is about to stall? How do you recover? 21 Label each leg of the traffic pattern (upwind, crosswind, downwind, base, final). Picture of the traffic pattern with questions about airspeed and flap settings for different legs. Airspeed KIAS Flap Setting: Cruise T/O LND Airspeed _KIAS Flap Setting: Cruise T/O LND Altitude AGL Airspeed KIAS Flap Setting: Cruise T/O LND 22. From the aircraft position draw the correct flight path to land on the appropriate runway. Picture of the runways with an airplane and the direction of the wind. Wind Sock 23 13 5 31 23. From the aircraft position draw the correct flight path to land on the appropriate runway. Picture of the runways with an airplane and the direction of the wind going in an opposite direction from the previous question . Wind Sock 13 23 31 5
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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