HP d212 Manual do Utilizador Página 175
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FMS-D212-725-1
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• 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:
A
Unapproved Date: 07.06.01
Table 5-12 – Fuel Loading (Cont’d)
Helicopter serial numbers 35049 and subsequent
Metric
ASTM D-1655 Type A, A-1, JP-5,
and JP-8
(0.815 Kg/L)
ASTM D-1655 Type B and JP-4
(0.779 Kg/L)
Quantity
(Liters)
Weight
(Kg)
CG
(MM)
Moment
(Kg-
MM/100)
Quantity
(Liters)
Weight
(Kg)
CG
(MM)
Moment
(Kg-
MM/100)
40 32.6 3655 1191.5 40 31.2 3655 1140.4
80 65.2 3658 2385.0 80 62.3 3658 2278.9
120 97.8 3561 3482.7 120 93.5 3561 3329.5
160 130.4 3421 4461.0 160 124.6 3421 4262.6
200 163.0 3340 5444.2 200 155.8 3340 5203.7
240 195.6 3284 6423.5 240 187.0 3284 6141.1
280 228.2 3246 7407.4 280 218.1 3246 7079.5
*297.1 242.1 3233 7827.1 *297.1 231.4 3233 7481.2
320 260.8 3249 8473.4 320 249.3 3249 8099.8
360 293.4 3343 9808.4 360 280.4 3343 9373.8
400 326.0 3434 11194.8 400 311.6 3434 10700.3
440 358.6 3515 12604.8 440 342.8 3515 12049.4
480 391.2 3579 14001.1 480 373.9 3579 13381.9
520 423.8 3635 15405.1 520 405.1 3635 14725.4
560 456.4 3683 16809.2 560 436.2 3683 16065.3
600 489.0 3721 18195.7 600 467.4 3721 17392.0
640 521.6 3757 19596.5 640 498.6 3757 18732.4
680 554.2 3790 21004.2 680 529.7 3790 20075.6
720 586.8 3818 22404.0 720 560.9 3818 21415.2
760 619.4 3843 23803.5 760 592.0 3843 22750.6
800 652.0 3866 25206.3 800 623.2 3866 24092.9
827.4 674.3 3876 26135.9 827.4 644.5 3876 24980.8
* Most critical fuel amount for most forward flight condition.
Note: All data above represents usable fuel based on nominal density at
15°C (59°F)
- 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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