HP d212 Manual do Utilizador Página 173
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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 5-10 – Fuel Loading (Cont’d)
Helicopter serial numbers prior to 35049
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 3647 1188.9 40 31.2 3647 1137.9
80 65.2 3647 2377.8 80 62.3 3647 2272.1
120 97.8 3541 3463.1 120 93.5 3541 3310.8
160 130.4 3399 4432.3 160 124.6 3399 4235.2
200 163.0 3322 5414.9 200 155.8 3322 5175.7
240 195.6 3272 6400.0 240 187.0 3272 6118.6
*274.8 224.0 3241 7259.8 *274.8 214.1 3241 6939.0
280 228.2 3246 7407.4 280 218.1 3246 7079.5
320 260.8 3277 8546.4 320 249.3 3277 8169.6
360 293.4 3368 9881.7 360 280.4 3368 9443.9
400 326.0 3470 11312.2 400 311.6 3470 10812.5
440 358.6 3541 12698.0 440 342.8 3541 12138.5
480 391.2 3609 14118.4 480 373.9 3609 13494.1
520 423.8 3665 15532.3 520 405.1 3665 14846.9
560 456.4 3708 16923.3 560 436.2 3708 16174.3
600 489.0 3744 18308.2 600 467.4 3744 17499.5
640 521.6 3777 19700.8 640 498.6 3777 18832.1
680 554.2 3805 21087.3 680 529.7 3805 20155.1
720 586.8 3833 22492.0 720 560.9 3833 21499.3
760 619.4 3858 23896.5 760 592.0 3858 22839.4
800 652.0 3884 25323.7 800 623.2 3884 24205.1
**820.7 668.9 3894 26047.0 **820.7 639.3 3894 24894.3
* Most critical fuel amount for most forward flight condition.
** Most critical fuel amount for most aft 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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