Diamond Aircraft DA 40 NG, Руководство по эксплуатации самолета

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DA 40 NG AFM General
Modification Source Installed
Doc. # 6.01.15-E Rev. 3 01-Jul-2014 Page 1 - 3
Shorter NLG Damper
%
MÄM 40-631
%
9
yes
%
9
no
%
Maximum Take-Off Mass 1310 kg
%
MÄM 40-662
%
9
yes
%
9
no
%
Conventional Cockpit DA 40 NG
Club
OÄM 40-321
9
yes
9
no
Emergency Axe
%
OÄM 40-326
%
9
yes
%
9
no
%
Retrofit with Autopilot KAP 140 OÄM 40-329
9
yes
9
no
Retrofit without Autopilot GFC 700 OÄM 40-330
9
yes
9
no
Short Baggage Extension OÄM 40-331
9
yes
9
no
DA 40 NG without Autopilot
GFC 700
OÄM 40-333
9
yes
9
no
Landing Gear with Large Tyres and
%
1280 kg Maximum Landing Mass
%
OÄM 40-334
%
9
yes
%
9
no
%
Diesel Operation
%
OÄM 40-370
%
9
yes
%
9
no
%
This Airplane Flight Manual must be kept on board the airplane at all times. Its designated
place is the side bag of the forward left seat.
CAUTION
The DA 40 NG is a single engine airplane. When the
operating limitations and maintenance requirements are
complied with, it has the high degree of reliability which is
required by the certification basis. Nevertheless, an engine
failure is not completely impossible. For this reason, flights
during the night, on top, under instrument meteorological
conditions (IMC), or above terrain which is unsuitable for a
landing, constitute a risk. It is therefore highly recommended
to select flight times and flight routes such that this risk is
minimized.