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Diamond DA 40-TDI- G1000 Systems Version 1.0

DIAMOND DA40 · Systems Description

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Overview

The document provides technical specifications and details about the Diamond DA40-NG aircraft, including its dimensions, weight, speeds, and various systems. It serves as a reference for understanding the aircraft's capabilities and operational limits.

  • The Diamond DA40-NG has a glide ratio of 1:9.7.
  • The maximum takeoff weight is 1310 kg.
  • The maximum landing weight is 1216 kg.
  • The empty weight of the aircraft is 944.9 kg.
  • The aircraft features multiple antennas for communication and navigation.
  • The stall speed varies with weight, ranging from 58 KIAS to 66 KIAS.
  • The VNO speed is 130 KIAS and VNE is 172 KIAS.
  • The baggage compartment can hold a maximum of 45 kg.

Document

Source

Originally published by salt.aero. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
·
Systems Description
File size
·
17 MB
Publisher
·
salt.aero
Language
·
en

Specifications & performance

Extracted from this document.

Specifications

Height m
·
1.97
Length m
·
8.06
Wingspan m
·
11.63
Baggage capacity kg
·
45

Performance

Glide ratio
·
1:9.7

V-speeds

VNE_KIAS
·
172
VNO_KIAS
·
130
VS_1000_KG_KIAS
·
58
VS_1100_KG_KIAS
·
61
VS_1200_KG_KIAS
·
64
VS_1310_KG_KIAS
·
66
VFE_FLAPS_T_O_KIAS
·
110
VFE_FLAPS_L_DG_KIAS
·
98
VO_1080_1180_KG_KIAS
·
108
VO_ABOVE_1180_KG_KIAS
·
113
VO_UP_TO_1080_KG_KIAS
·
101

Weight & balance

Empty weight kg
·
944.9
Max landing weight kg
·
1216
Max takeoff weight kg
·
1310
About this document
What is the Diamond DA 40-TDI- G1000 Systems Version 1.0?

The Diamond DA 40-TDI- G1000 Systems Version 1.0 is a systems description for the DIAMOND DA40.

Where does the Diamond DA 40-TDI- G1000 Systems Version 1.0 come from?

This copy of the Diamond DA 40-TDI- G1000 Systems Version 1.0 was originally published by salt.aero and is hosted on Sprinkle as a free, searchable reference copy.

Documentation completeness
4/7

Most owners only have the POH. Here's the essential set for the DIAMOND DA40.

More DIAMOND DA40manuals & documents

In this document

Dimensions

The Diamond DA40-NG has a wingspan of 11.63 m, a length of 8.06 m, and a height of 1.97 m.

Mass

The empty weight is 944.9 kg, with a maximum takeoff weight of 1310 kg and a maximum landing weight of 1216 kg.

Speeds

Characteristic speeds include VNO at 130 KIAS, VNE at 172 KIAS, and various stall speeds depending on weight.

Flight Controls

The aircraft uses push rods for ailerons and elevator control, with rudder control via cables.

Antenna Systems

The aircraft is equipped with multiple antennas for VHF communication, GPS, and weather information.

Baggage Compartment

The baggage compartment can accommodate a maximum of 45 kg, with specific limits for the aft compartment.

Safety notes

  • JET fuel is heavier than AVGAS.
  • Typical fuel weight for JET A1 is 0.8 kg/ltr and for AVGAS is 0.72 kg/ltr.

Full document text

Diamond DA 40-NG Diamond DA40-NG Dimensions Dimensions 11,63 m Gllide Ratio: 1:9,7 Dimensions 1,68 m 8,06 m 1,97 m Dimensions 2,97 m Diamond DA40-NG Exterior VHF COM 1 Antenna VHF COM 1 Antenna VHF COM 2 antenna VHF NAV in the horizontal stabilizer WX 500 Antenna The Stormscope Model WX-500 displays lightning information at ranges of 25 nm to 200 nm and easily interfaces with most popular Multi-Function Displays Marker Antenna GPS Antennas DME, XPDR Antennas ADF antenna TAS 600 antenna upper TAS 600 antenna lower Pitot Probe Lift Detector (Stall Warning) Engine Oil Engine Oil Gearbox Oil Air Inlets Cabin heat Intercooler Gearbox cooler Radiator Engine air intake RH cabin Ventilation LH cabin Ventilation Diamond DA40 NG Mass Mass (Weight) Empty SP-MKD 944,9 kg Max T/OFF 1310 kg Max LDG 1216 kg Max Baggage with „Baggage Extension“ 45 kg (max 18 kg in aft compartment) Baggage Compartment Baggage Compartment Attention! JET fuel is heavier than AVGAS! Typical fuel weight: JET A1: 0,8 kg/ltr 3,03 kg/USG AVGAS: 0,72 kg/ltr 2,8 kg/USG Diamond DA40-NG Speeds Characteristic Speeds VNO 130 KIAS VNE 172 KIAS Vo up to 1080 kg 101 KIAS Vo 1080-1180 kg 108 KIAS Vo above 1180 113 KIAS VFE (Flaps T/O) 110 KIAS VFE (Flaps LDG) 98 KIAS AFM str. 198 Vs 1000 kg 58 KIAS Vs 1100 kg 61 KIAS Vs 1200 kg 64 KIAS Vs 1310 kg 66 KIAS Stalling Speeds Stalling Speeds Diamond DA40-NG Flight Controls Ailerons, Elevator: push rods Flight Control Operation Rudder: cables Flight Control Operation Flaps: electrically by push rods, left and right mechanically interconnected Diamond DA40-NG Instrument Panel