Diamond DA 42 NG, Maintenance Manual

Page: 326 / 2339

AIRCRAFT
Placards and Markings
DA 42 NG AMM
Page 2
15 Mar 2018
11-30-00
Doc # 7.02.15
Rev. 4
(Inside door behind handle)
ELT
LOCATED
MAX. 45 kg [100 lb]
ARM: 3 89 m [153 1"]
COCKPIT BAGGAGE
MAX BAGGAGE TOTAL (COCKPIT BAGGAGE
CAUTION: OBSERVE WEIGHT AND BALANCE LIMITATIONS
SEE AI PLANE FLIGHT MANUAL CHAPTER R 6
ARM: 4.54 m [178.7"]
BAGGAGE
MAX. 18 kg [40 lb]
COMPARTMENT & EXTENSION): 45 kg [100 lb]
COMPARTMENT
EXTENSION
Max Baggage:
30 kg [66 lb]
LH & RH
PEDAL SLIDE
SWITCH
Optional
(On underside of canopy)
during
parallel to this
position line
TAKE-OFF & LANDING
SET SEAT BACKRESTS
UPRIGHT
during
parallel to this
position line
TAKE-OFF & LANDING
SET SEAT BACKRESTS
UPRIGHT
OXYGEN
DO NOT SMOKE!
DO NOT TRANSPO RT FLAMMABLE FLUIDS, OILS AND
GREASES IN THE NO SE BAGG AGE COMPARTMENT!
DE-ICING FLUID
Max. 31.6 liters (8.3 US gal)
Useable 30 liters (7.9 US gal)
Refer to AFM for approved fluids
This airplane may only be operated in accordance with the Airplane
Flight Manual in the "Normal" category. Provided that national
operational requirements are met and the appropriate equipment is
installed and operational, this airplane is approved for the following
kinds of operation: day VFR, night VFR, IFR and flight into known or
forecast icing conditions. All aerobatics manouvers including spinning
are prohibited. For further operational limitations refer to the Airplane
Flight Manual.
Operating manouvering speed:
=122 KIAS (above 1800 kg / 3968 lb)
=119 KIAS (above 1700 kg / 3748 lb to 1800 kg / 3968 lb)
=112 KIAS (above 1700 kg / 3748 lb)
V
V
V
o
o
o
Limitations for GFC 700 Autopilot System:
Autopilot / Yaw Damper DISC during take-off and
landing.
Do not use AP during single engine operation.
Maximum speed for autopilot operation is 180 KIAS.
Minimum speed for autopilot operation is 90 KIAS.
Minimum altitude for autopilot operation:
Cruise, Climb, Descent and Maneuvering:
Approach:
Departure:
800 feet AGL
200 feet AGL
200 feet AGL
Alternate Static
OPEN
CLOSED
If Alternate Static is open
Emer gency Window and
Cockpit Vent must be closed
Optional
(If OÄM 42-207 is installed)
SHORT BAGG AG E
EXTENSIO N
MAX 15 kg [33 lb]
ARM: 3.97 m [156.3 in] STANDARD BAG GAGE
COMPARTMENT
MAX 30 kg [66 lb]
ARM: 3.65 m [143.7 in]
CAUTION: OBSERVE WEIG HT AND BALANCE LIMITATIONS
SEE AIRPLANE FLIGHT MANUAL CHAPTER 6
Hydraulic Fluid
AeroShell Fluid 41
AMG-10
CAUTION: Mixing of different fluid-types is not permitted!
Refer to AMM for refilling or fluid change
No engine start
below
No take-off below Diesel Fuel Class
-5°C (+23°F) +5°C (+41°F)
-10°C (+14°F) -5°C (+23°F) Diesel Fuel Class C
-15°C (+5°F) -10°C (+14°F) Diesel Fuel Class D, E or F
Diesel Fuel of unknown class or
unknown fuel blend
If OÄM 42-251 is installed
If OÄM 42-067 or
OÄM 42-259 is installed
If OÄM 42-067 or
OÄM 42-259 is installed
TABLET MOUNT:
- SIZE MAX: 255mm BY 200mm (10.03" BY 7.87")
- WEIGHT MAX: 1,1kg (2.43lb)
- INTERCONNECTING ARM LENGTH MAX: 76.2mm (3")
Optional
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
Figure 1: Interior Placards and Markings