DA40 TDI Diamond Star FACT SHEET
Diamond DA40 TDI · Specifications
Overview
This document provides specifications for the Diamond DA40 TDI, a light aircraft designed for efficiency and performance. It includes detailed performance metrics, dimensions, weight specifications, and fuel requirements. The information is intended for pilots, aviation enthusiasts, and potential buyers who are interested in understanding the capabilities and characteristics of the DA40 TDI. Key performance figures such as take-off distances, climb rates, and fuel consumption rates are highlighted, along with the aircraft's dimensions and weight limits.
- Take-off distance (ground roll): 335 m
- Max cruise speed at 10,000 ft: 246 km/h
- Fuel consumption at 70% power: 18.5 lt/h
- Max take-off weight (MTOW): 1,150 kg
- Range with standard tank: 1,372 km
Document
Source
Originally published by www.aeroclub-sommer.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Specifications
- Year
- 2005
- Pages
- 2
- File size
- 166 KB
- Publisher
- www.aeroclub-sommer.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 641
- Engine (hp)
- 135
- Height (ft)
- 6
- Length (ft)
- 26
- Propeller
- MT 3-blade Hydraulic Constant Speed
- Wingspan (ft)
- 39
- Engine model
- THIELERT Centurion 1.7
- Max speed (kt)
- 133
- Cruise speed (kt)
- 125
- Empty weight (lb)
- 1,753
- Fuel capacity (gal)
- 30
- Rate of climb (fpm)
- 650
- Max takeoff weight (lb)
- 2,535
Performance
- Fuel burn (gph)
- 4.9
- Landing over 50ft
- 2,083
- Takeoff over 50ft
- 1,099
Weight & balance
- Useful load (lb)
- 782
- Max takeoff weight (lb)
- 2,535
Most owners only have the POH. Here's the essential set for the Diamond DA40 TDI.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
More Diamond DA40 TDImanuals & documents
See all 20 →- Type Acceptance Report TAR 3/21B/34 – Diamond DA40 SeriesMaintenance Manual
- Checklist für Diamond DA40 TDI Diamond StarFlight Manual
- Check-List Diamond DA-40 TDiChecklist
- Diamond DA40-TDI G1000Performance Data
- DA 40 NG AFMPilot's Operating Handbook
- TYPE-CERTIFICATE DATA SHEET EASA.A.022 DA 40Parts Catalog
- DA 40 D AFMFlight Manual
- PH-TDS Procedures Quick Reference GuideChecklist
- Canadian Aviation Service Difficulty ReportsService Bulletins
- DA 40 D AFMPilot's Operating Handbook
- G1000 System Maintenance ManualFlight Manual
- Garmin G1000 Cockpit Reference Guide for the DA40/40FV Speeds Reference
In this document
Performance/Consumption
The DA40 TDI has a take-off distance of 335 meters for ground roll and 635 meters when considering a 50 ft obstacle at maximum take-off weight (MTOW). The rate of climb at sea level is 3.3 m/s, decreasing to 1.9 m/s at 10,000 ft. The maximum cruise speed at 10,000 ft is 246 km/h, with a cruise speed of 232 km/h at 70% power and 211 km/h at 60% power. Fuel consumption varies from 18.5 liters per hour at 70% power to 15.1 liters per hour at 60% power, providing a range of 1,372 km with the standard tank and 2,006 km with the long-range tank.
Dimensions/Weights
The DA40 TDI measures 8.06 meters in length, 1.97 meters in height, and has a wingspan of 11.94 meters. The wing area is 13.54 m², and the aircraft accommodates four seats. The empty weight is 795 kg, while the maximum take-off weight (MTOW) is 1,150 kg, allowing for a payload of 355 kg. Fuel capacity is 114 liters for the standard tank and 155 liters for the long-range tank.
Engine and Propeller
The aircraft is powered by a THIELERT Centurion 1.7 engine, producing 135 horsepower. It is equipped with a 3-blade hydraulic constant speed propeller, which contributes to its efficient performance.
Full document text
DA40 TDI Diamond Star FACT SHEET Take-off Distance (Ground Roll) MTOW Take-off Distance (50 ft Obstacle) MTOW Rate of Climb at Sea Level MTOW Rate of Climb in 10.000 ft MTOW Max. Cruise Speed in 10.000 ft Cruise Speed @ 70% in 10.000 ft Fuel Consumption Cruise Speed @ 60% in 10.000 ft Fuel Consumption Range @ 60% in 10.000 ft Standard/Long Range Tank THIELERT Centurion 1.7 (135 hp) MT 3-blade Hydraulic Constant Speed Propeller 335 m 635 m 3.3 m/s 1.9 m/s 246 km/h TAS 232 km/h TAS 18.5 lt/h 211 km/h TAS 15.1 lt/h 1,372 km/2,006 km Specifications apply to standard equipped aircraft, if not otherwise stated. Specification may change without notice. Status: March 1, 2005 Power Plant Engine Propeller Performance/Consumption Dimensions/Weigths Length Height Wing Span Wing Area Seats Empty Weight Max. Take-off Weight (MTOW) Payload Fuel Capacity Standard/Long Range Tank Fuel Grades 8.06 m 1.97 m 11.94 m 13.54 m² 4 795 kg 1,150 kg 355 kg 114 lt/155 lt Jet A1/Diesel 26 ft 5 in 6 ft 6 in 39 ft 2 in 145.7 sq ft 4 1,753 lbs 2,535 lbs 782 lbs 30 US gal/41 US gal Jet A1/Diesel 1,099 ft 2,083 ft 650 fpm 374 fpm 133 kts TAS 125 kts TAS 4.9 US gal/hr 114 kts TAS 4.0 US gal/hr 741 nm/1,083 nm DA40 TDI Diamond Star D I A M O N D A I R C R A F T I N D U S T R I E S G M B H Verkauf/Sales F +43-26 22-26 700-355 sales@diamond-air.at Diamond Aircraft Industries GmbH N. A. Otto-Straße 5 A-2700 Wiener Neustadt, Austria T +43 26 22 26 700 F +43 26 22 26 780 www.diamond-air.at 8.06 m / 26 ft 5 in 1.97 m / 6 ft 6 in 11.94 m / 39 ft 2 in