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Note.-For IFR operations the safety area wiil be larger than depicted. See Annex 14, Volume I/, for details.
Figure A 4
ATT A-9
Annex 6 - Operation of Aircraft Part 111
PERFORMANCE CLASS 2 HELICOPTERS
ELEVATED HELlPORTlHELlDECK
TAKE-OFF
10.7 m for VFR operations
10.7 m * 0.01 DR for IFR operations
L = The maxlmum dlrnension of the helicopter
Figure A-5
ATT A-10
Aijklament A Annex 6 - Opem&ion of Aircmft
PERFORMANCE CLASS 3 HELICOPTERS
SURFACE LEVEL HELIPORT
TAKE-OFF
r (Obstacle)
Area permitting a safe forced landing
available
30 m or 1.5L
I
SAFETY AREA &
' 2L for water hellports
L = The maxlmum dlmenslon of the hellcopter
Figure A-6
ATT A-11
Annex 6 - Opemiion of AhmP Part IZI
Figure A-7
PERFORMANCE CLASS I HELICOPTERS
SURFACE LEVEL HELIPORT
LANDING
A
ATT A-12
>10.7 m + 0.01 DR*
)anding distance required,
Landing distance available
300 m or 900 rn
Sultable area
- - - - - - - - - - - - - - - - - - - - - - - - - - * - * -
10.7 m for VFR operatlons
10.7 m t 0.01 DR for IFR operations
L = The maximum dimension of the hellcopter
Note.-For IFR operations the safety area will be larger than depicted. See Annex 14, Volume /I, for details.
Attachment A Annex 6 - Operation of Aircraft
PERFORMANCE CLASS I HELICOPTERS
ELEVATED HELlPORTlHELlDECK
LANDING
SAFETY AREA
10.7 m far VFR operations
10.7 m + 0.01 DR for IFR operations
L =The maxlmum dimension of the helicopter
Figure A-8
ATT A-13
Annex 6 - Operation of Aircmfl Pnrl 111
Figure A-9
PERFORMANCE CLASS 2 HELICOPTERS
SURFACE LEVEL HELIPORT
LANDING
&fid +t bef~bnd ing
ting or H%a\ ,\ne taw pm A
ATT A-14
mu~nes
ba\kd \8nd\n99
~10.7m +
Defined point before landing
0.01 DR'
!
V I (Obstacle)
4
DR w
Landing dlstance available
SAFETY AREA
" 10.7 rn for VFR operations
10.7 m t 0.01 DR for IFR operations
L = The maximum dimension of the helicopter
Note.-For IFR operations the safety area will be lagar than depicted. See Annex 14, Volume /I, for details.
Amchment A Annex 6 - Opemtian of Aircmfr
PERFORMANCE CLASS 2 HELICOPTERS
ELEVATED HELlPORTlHELlDECK
LANDING
' 10.7 m for case of engine failure before defined point and for VFR operations wlth all engines operating
L = The maximum dimension of the helicopter
Figure A-10
Annex 6 - Operation of Aircmjl PuH I12
Figure A-1 1
PERFORMANCE CLASS 3 HELICOPTERS
SURFACE LEVEL HELIPORT
LANDING
erathe
\anding an en9\nes OP A
ATT A-16
rl0.7 m
Area permitting a safe forced landing
b
Landing distance available i -
Fl --+A-----2---*+--+---
I
30m 7R
-------- ------ 1 ---------
SAFETY AREA L 3 10%
L The maximum dimension of the hellcopter
ATTACHMENT B. FLIGHT RECORDERS
Supplementary to Section 11, Chapter 4. 4.3 and Section Ill, Chapter 4, 4.9
The material in this Attachment concerns flight recorders
intended for installation in helicopters engaged in international
air navigation. Flight recorders comprise two systems - a
flight data recorder and a cockpit voice recorder. Flight data
recorders for helicopters are classified as Type IV and Type V
depending upon the number of parameters to be recorded.
1. Flight data recorder (FDR)
1.1 General requirements
1.1.1 The FDR is to record continuously during flight
time.
1.1.2 The FDR container is to:
a) be painted a distinctive orange or yellow wlour;
b) carry reflective material to facilitate its location; and
c) have securely attached an automatically activated
underwater locating device.
1.1.3 The FDR is to be installed so that:
a) the probability of damage to the recording is minimized;
b) it receives its electrical power from a bus that provides
the maximum reliability for operation of the FDR
without jeopardizing service to essential or emergency
loads; and
c) there is an aural or visual means for pre-flight checking
that the FDR is operating properly.
1.2 Parameters to be recorded
1.2.1 Type IV FDR. This FDR will be capable of
recording, as appropriate to the helicopter, at least the thirty
parameters in Table B-1. However, other parameters may be
substituted with due regard to the helicopter type and the
characteristics of the recording equipment.
1.2.2 Type V FDR. This FDR will be capable of recording,
as appropriate to the helicopter, at least the first fifteen
parameters in Table B-1. However, other parameters may be
　
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