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FMS-D212-725-1
Page 5-5
• 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
5.5.2 Internal Cargo Loading Table
Weights at various arms and their moments are listed in 50 pound
increments from 50 pounds through 2000 pounds and in 25 kilogram
increments from 25 kilograms through 900 kilograms (Table 5-4).
5.6 Cargo Compartment Loading
Cargo compartment is accessible from right side of tailboom and contains
approximately 28 cubic feet of space. Cargo compartment has a load limit of
400 pounds (181.4 kilograms) not to exceed 100 pounds per square foot
(0.048 kilograms per square centimeter). These are structural limitations
only and do not infer that CG will remain within approved limits. When
weight is loaded into Cargo compartment the pilot must compute GW CG to
ensure that the loading is within approved limits.
5.6.1 Cargo Loading
Loading of cargo compartment should be from front to rear. Load shall be
secured to tiedown fittings if shifting of load in flight could result in structural
damage to cargo compartment or in GW CG limits being exceeded. If cargo
is not secured, CG shall be computed with load in most adverse position.
5.6.2 Cargo Loading Table
Weights at various arms and their moments are listed in 20 pound
increments from 20 pounds through 400 pounds and in 10 kilogram
increments from 10 kilograms through 181.4 kilograms (Table 5-8)
5.7 Fuel Loading
At beginning of any flight with full fuel on board, helicopter CG will move
forward due to the fact that the CG of fuel on board moves forward as it is
consumed. This occurs because fuel is consumed from rear (upper) fuel
cells first. Maximum forward CG condition of fuel on board occurs when 72.6
U.S. gallons (274.8 liters) remain for helicopter serial numbers prior to 35049
and at 78.5 U.S. gallons (297.1 liters) for helicopter serial numbers 35049
- 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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