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FMS-D212-725-1
Page 5-18
• 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 5-9 – Fuel Loading
Helicopter serial numbers prior to 35049
English
ASTM D-1655 Type A, A-1, JP-5,
and JP-8
(6.8 Lbs/Gal)
ASTM D-1655 Type B and JP-4
(6.5 Lbs/Gal)
Quantity
(US
Gal)
Weight
(Lb)
CG
(In)
Moment
(In-Lb)
Quantity
(US
Gal)
Weight
(Lb)
CG
(In)
Moment
(In-Lb)
10 68 143.6 9765 10 65 143.6 9334
20 136 143.6 19530 20 130 143.6 18668
30 204 140.2 28601 30 195 140.2 27339
40 272 134.8 36666 40 260 134.8 35048
50 340 131.6 44744 50 325 131.6 42770
60 408 129.4 52795 60 390 129.4 50466
70 476 127.9 60880 70 455 127.9 58195
*72.6 494 127.6 63034 *72.6 472 127.6 60227
80 544 128.3 69795 80 520 128.3 66716
90 612 130.6 79927 90 585 130.6 76401
100 680 134.6 91528 100 650 134.6 87490
110 748 137.8 103074 110 715 137.8 98527
120 816 140.4 114566 120 780 140.4 109512
130 884 142.6 126058 130 845 142.6 120497
140 952 144.6 137659 140 910 144.6 131586
150 1020 146.1 149022 150 975 146.1 142448
160 1088 147.6 160589 160 1040 147.6 153504
170 1156 148.8 172013 170 1105 148.8 164424
180 1224 149.9 183478 180 1170 149.9 175383
190 1292 150.9 194963 190 1235 150.9 186362
200 1360 151.9 206584 200 1300 151.9 197470
210 1428 152.7 218056 210 1365 152.7 208436
**216.8 1474 153.3 225964 **216.8 1409 153.3 216000
* 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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