HP d212 Manual do Utilizador Página 95
- Página / 177
- Índice
- MARCADORES
Avaliado. / 5. Com base em avaliações de clientes
FMS-D212-725-1
Page 3-19
• COPYRIGHT © 2007 BY DART AEROSPACE LTD •
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:
D
TC Approved Date: 08.12.17
to a complete stop.
Left Pedal Locked Forward of Neutral:
Reduce power and maintain ENG RPM (N
2
) within the green arc. Normal
turns can be safely made under these conditions, although the helicopter
nose may be displaced to left.
On final approach, begin a slow deceleration so as to arrive at a point about
four to five feet above intended touchdown area as effective translational lift
is lost.
Apply collective to stop rate of descent and forward speed, and to align
helicopter with intended landing path. Allow helicopter to touchdown at near
zero ground speed, maintaining alignment with throttle.
Pedals Locked in Neutral:
Reduce power and maintain ENG RPM (N
2
) within green arc. Normal turns
can be safely made under these conditions.
Execute a normal to shallow approach, holding AIRSPEED at 60 KIAS during
initial part of approach. Adjust power as necessary to minimize or prevent
right yaw.
At 50 to 75 feet AGL and when landing area can be made, start a
deceleration to arrive at intended landing point with AIRSPEED at 25 KIAS.
At 2 to 5 feet AGL, use throttle slowly as necessary to maintain alignment
with landing area and to control yaw; do not allow helicopter to settle until
alignment is assured, then touchdown.
After ground contact, use collective and throttle as necessary to minimize
forward speed and to maintain alignment. Move cyclic as necessary to follow
turn until helicopter has come to a complete stop.
- 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
Manuais e produtos relacionados com Barebones PC/estação de trabalho HP d212
(18 páginas)© 2020, manymanuals-pt.com. Todos os direitos reservados. | 0.099 s |
Manymanuals.com
Manymanuals.de
Manymanuals.fr
Manymanuals.it
Manymanuals.pl
Manymanuals.cz
Manymanuals.es
Manymanuals-pt.com
Comentários a estes Manuais