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HP d212 Bedienungsanleitung

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FMS-D212-725-1
Page
lntro-1
Eagle
Copters
Ltd.
823
McTavish
Road
NE
Calgary,
Alberta,
Canada
T2E 7G9
Tel:
1
403
250
7370
Fax:
1403
250
7110
http://www.eaglecopters.com
ROTORCRAFT
FLIGHT
MANUAL
SUPPLEMENT
FMS-D212-725-1
Eagle
Single
Bell
212
Models
Sections
1
-
4
of
this
document
comprise
the
Approved
Flight
Manual
Supplement.
Compliance
with
Sectioni,
Limitations
is
mandatory.
Section
5
is
unapproved
and
is
provided
for
information
only.
Transport
Canada
Transports
Canada
AIRCRAFT
CERTIFICATION
DIVISION
APPROVED
VY
-
1,1m
■
DD
Prepared
Reviewed
By;
H.
Siemens
JAerospac/
Ejj.
Shepherd
DE#02
•
COPYRIGHT
©
2007
BY
DART
AEROSPACE
LTD
■
This
documenl
is
private
and
confidenli.il
and
is
supplied
on
Iha
oipress
condition
Ihal
it
is
not
to
bo
used
far
any
purpose
or
cppied
or
mmmLinicjted
to
any
other
person
wilhaul
written
permission
from
Dan
Aerospace
Lid.
TC
Approved
Revision:
G
Date:
13.08.09
Seitenansicht 0
1 2 3 4 5 6 ... 176 177

Inhaltsverzeichnis

Seite 1 - Shepherd

FMS-D212-725-1Pagelntro-1EagleCoptersLtd.823McTavishRoadNECalgary,Alberta,CanadaT2E 7G9Tel:14032507370Fax:14032507110http://www.eaglecopters.comROTORC

Seite 2

FMS-D212-725-1 Page 1-1 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express conditio

Seite 3 - Page Intro-3

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Seite 4 - Revisions

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Seite 5 - General Information

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Seite 6 - Terminology

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Seite 9

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Seite 10 - Section 1

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Seite 14 - 1.5 Configuration

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Seite 15 - 1.5.4 Passengers

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Seite 16 - TC Approved Date: 10.05.12

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Seite 17

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Seite 18 - 1.5.5.2 Cargo Compartment

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Seite 19 - 1.6.1 Weight

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Seite 20 - 1.6.2 Center of Gravity

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Seite 21 - 1.7 Airspeed

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Seite 22 - 10.05.12

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Seite 23 - 1.9 Maneuvering

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Seite 24

FMS-D212-725-1 Page 1-3 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express conditio

Seite 25 - TC Approved Date: 08.06.12

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Seite 26 - 1.11 Ambient Temperature

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Seite 27 - 1.12 Electrical

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Seite 28 - 1.13 Power Plant

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Seite 29 - Limitations (T5317A Only)

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Seite 30 - 1.13.6 Fuel Pressure

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Seite 31 - 1.14 Transmission

FMS-D212-725-1 Page 4-19 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express conditi

Seite 32 - 1.16 Hydraulic

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Seite 33 - 1.17 Fuel and Oil

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Seite 34 - 1.19 Heater

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Seite 35 - 1.20 Additional Placards

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Seite 36 - 1.21 Instrument Markings

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FMS-D212-725-1 Page 4-26 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express conditi

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FMS-D212-725-1 Page 4-28 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express conditi

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FMS-D212-725-1 Page 4-30 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express conditi

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Seite 45 - Section 2

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Seite 46

FMS-D212-725-1 Page 1-5 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express conditio

Seite 47

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Seite 48 - 2.3 Preflight Check

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Seite 49 - 2.3.1 Before Exterior Check

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Seite 50

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Seite 51 - 2.3.2 Exterior Check

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Seite 57 - 2.4.1 Pre-start Check

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Seite 63 - 2.5 Engine Start

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Seite 64

FMS-D212-725-1 Page 5-2 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express condition

Seite 65 - 2.6 Systems Check

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Seite 66 - 2.6.3 Engine Fuel Control

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Seite 67 - 2.6.5 Anti-ice Check

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Seite 71 - 2.7 Before Takeoff

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Seite 72 - 2.8 Takeoff

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Seite 73 - 2.10 Descent and Landing

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Seite 74 - 2.12 Engine Shutdown

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Seite 75

FMS-D212-725-1 Page 5-12 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express condition

Seite 76 - 2.13 Post Flight Check

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Seite 77 - Section 3

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Seite 78 - 08.12.17

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Seite 79

FMS-D212-725-1 Page 1-8 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express conditio

Seite 80 - 3.3 Engine

FMS-D212-725-1 Page 5-16 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express condition

Seite 81

FMS-D212-725-1 Page 5-17 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express condition

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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

Seite 83

FMS-D212-725-1 Page 5-19 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express condition

Seite 84 - 3.3.4 Engine Underspeed

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Seite 85 - 3.3.5 Engine Overspeed

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Seite 86

FMS-D212-725-1 Page 5-22 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express condition

Seite 87 - 3.4 Fire

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Seite 88

FMS-D212-725-1 Page 1-9 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express conditio

Seite 89 - 3.4.2 Cabin Smoke or Fumes

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Seite 90 - 3.5 Tail Rotor

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Seite 91 - TC Approved Date: 08.12.17

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FMS-D212-725-1 Page 1-15 • COPYRIGHT © 2007 BY DART AEROSPACE LTD • This document is private and confidential and is supplied on the express conditi

Seite 96 - 3.6 Hydraulic System

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Seite 97 - 3.8 Fuel System

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Seite 98

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Seite 99 - 3.10 Cabin Heater

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Seite 100 - 3.10.2 Heater Overheat

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Seite 101 - TC Approved Date: 13.08.09

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Seite 102 - 13.08.09

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Seite 103 - TC Approved Date: 09.08.10

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Seite 104

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Seite 105 - IF on ground: ENGINE

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Seite 108 - Section 4

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Seite 109 - 08.06.12

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Seite 113 - Page 4-6

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Seite 114 - 4.3 Power Assurance Checks

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Seite 117 - Page 4-10

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Seite 118 - 4.6 Rate of Climb – Maximum

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Seite 119 - 4.8 Height Velocity

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Seite 122 - Hover Ceiling

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Seite 130 - Takeoff Distance

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Seite 142 - Rate of Climb – Maximum

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Seite 144 - Landing Distance

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Seite 151 - TC Approved Date: 07.06.01

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Seite 152 - Autorotative Glide Distance

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Seite 153 - 4,000 feet

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Seite 154 - Height Velocity Chart

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Seite 155 - Section 5

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Seite 156 - 07.06.01

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Seite 158 - 5.4 Doors Open or Removed

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Seite 159 - 5.7 Fuel Loading

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Seite 160 - 5.7.2 Sample Loading Problem

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Seite 161 - Unapproved Date: 07.06.01

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