Hélicoptères Guimbal
CABRI G2
Issue
Page
number
07
4-2
4-5
4-6
6-5
6-7, 6-8
7-4
7-8
7-12,
7-19
7-13
7-14
8-2
08
C
0-1, 0-2,
0-3, 0-9,
0-10
1-4
2-i, 2-2
2-1
2-3
2-6
2-5, 4-i,
D, 4-2,
4-15
Issue 09
Original issue
Revision object
Performance to
be checked in
chapter 5
Winter air flow
restrictor check
Line shifted from
previous page
Weighing ref.
point
Fuel density
Rotor brake
description +
wording :
transmission
driveshaft
"Interm."
"Avionics" relay
Rotor in Flying
mode is page 7-
17, not 7-16
Sensor page
description
Error in Start
indicator
description
Tie down
Pages # change
Page revisions
FAA engine STC
Page layout
Limitations
Transient low
RPM limit
Lubricating oil
recommendations
Alternate fuel
temporary use
Temporary green
pages integrated.
Approved under DOA EASA.21J.211
INTRODUCTION
Approval
Approval reference (*)
date
05/03/2013
Major Change
Approval EASA
10043929
12/03/2013
Approved under DOA
EASA.21J.211
December
EASA AFM Approval
th
4
, 2014
10051479
0-9
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