HP d212 Manuel d'utilisateur télécharger pdf (Page 17)

FMS-D212-725-1

Page 1-8

This document is private and confidential and is supplied on the express condition that it is not to be used for any

purpose or copied or communicated to any other person without written permission from Dart Aerospace Ltd.

Revision:

TC Approved Date: 10.05.12

Figure 1-3 – Nine-place passenger loading configuration 3

1 2 ... 12 13 14 15 16 17 18 19 20 21 22 ... 176 177

Shepherd 1
Page Intro-3 3
Revisions 4
Unapproved Date: 07.11.30 5
General Information 5
Terminology 6
Section 1 10
1.4 Flight Crew 14
1.5 Configuration 14
1.5.3 Doors Open/Removed 15
1.5.4 Passengers 15
TC Approved Date: 10.05.12 16
1.5.5 Cargo 18
1.5.5.2 Cargo Compartment 18
1.6.1 Weight 19
1.6.2 Center of Gravity 20
1.7 Airspeed 21
10.05.12 22
1.8 Altitude 23
1.9 Maneuvering 23
TC Approved Date: 08.06.12 25
1.11 Ambient Temperature 26
1.12 Electrical 27
1.13 Power Plant 28
1.13.2 Power Turbine (N 29
Limitations (T5317A Only) 29
1.13.6 Fuel Pressure 30
1.14 Transmission 31
1.15 Rotor 32
1.16 Hydraulic 32
1.17 Fuel and Oil 33
1.18 Rotor Brake 34
1.19 Heater 34
1.20 Additional Placards 35
1.21 Instrument Markings 36
Section 2 45
2.3 Preflight Check 48
2.3.1 Before Exterior Check 49
2.3.2 Exterior Check 51
2.4.1 Pre-start Check 57
2.5 Engine Start 63
2.6 Systems Check 65
2.6.3 Engine Fuel Control 66
2.6.4 Rpm Control 67
2.6.5 Anti-ice Check 67
2.7 Before Takeoff 71
2.8 Takeoff 72
2.9 In-Flight Operation 73
2.10 Descent and Landing 73
2.11 After Landing 74
2.12 Engine Shutdown 74
2.13 Post Flight Check 76
Section 3 77
08.12.17 78
3.3 Engine 80
3.3.4 Engine Underspeed 84
3.3.5 Engine Overspeed 85
3.4 Fire 87
3.4.2 Cabin Smoke or Fumes 89
3.5 Tail Rotor 90
TC Approved Date: 08.12.17 91
3.6 Hydraulic System 96
3.7 Electrical System 97
3.8 Fuel System 97
3.9 Communications System 99
3.10 Cabin Heater 99
3.10.2 Heater Overheat 100
Revision: 101
TC Approved Date: 13.08.09 101
13.08.09 102
TC Approved Date: 09.08.10 103
IF on ground: ENGINE 105
Section 4 108
08.06.12 109
FMS-D212-725-1 113
Page 4-6 113
4.3 Power Assurance Checks 114
Page 4-10 117
4.4 Hover Ceiling Charts 118
4.5 Takeoff Distance 118
4.6 Rate of Climb – Maximum 118
4.7 Landing Distance 119
4.8 Height Velocity 119
Hover Ceiling 122
Takeoff Distance 130
Rate of Climb – Maximum 142
Landing Distance 144
TC Approved Date: 07.06.01 151
Autorotative Glide Distance 152
4,000 feet 153
Height Velocity Chart 154
Section 5 155
07.06.01 156
5.4 Doors Open or Removed 158
5.7 Fuel Loading 159
5.7.1 Computation of CG 160
5.7.2 Sample Loading Problem 160
Unapproved Date: 07.06.01 161

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HP d212 Manuel d'utilisateur Page 17

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