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