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4.2.4.2 If the comer markings are more than 2 m apart,
intermediate lines 9 cm x 3 cm shall be inserted so that there
is no more than 2 m between adjacent markings.
Note.- This Standard does not require any helicopter to
lzave break-in areas.
a) the operations manual prescribed in 2.2.2; or those parts
of it that pertain to flight operations;
4.3 Flight recorders
b) the helicopter flight manual for the helicopter, or other
documents containing performance data required for the
application of Chapter 3 and any other information
necessary for the operation of the helicopter within the
terms of its certificate of airworthiness, unless these data
are available in the operations manual; and
c) current and suitable charts to cover the route of the
proposed flight and any route along which it is
reasonable to expect that the flight may be diverted.
4.2.4 Marking of break-in points
4.2.4.1 If areas of the fuselage suitable for break-in by
rescue crews in an emergency are marked on a helicopter, such
areas shall be marked as shown below (see figure following).
Note 1.- Flight recorders comprise two systems, a flight
dnta recorder (FDR) and a cockpit voice recorder (CVR).
Note 2.- Combination recorders (FDWCVR) can only be
used to meet the jlight recorder equipage requirements as
speciJically indicated in this Annex.
Note 3.- Detailed guidance onflight recorders is contained
in Attachment B.
4.3.1 Flight data recorders - types
4.3.1.1 A Type IV FDR shall record the parameters
required to determine accurately the helicopter flight path,
speed, attitude, engine power and operation.
MARKING OF BREAK-IN POINTS (see 4.2.4)
Section 11, Chapter 4 Annex 6 - Operation of Aircraft
4.3.1.2 A Type V FDK shall record the parameters
required to determine accurately the helicopter flight path,
speed, attitude and engine power.
4.3.1.3 Tlie use of cngraving metal foil FDRs shall be
discontinued by 1 January 1995.
4.3.1.4 Recommendation.- The use of analogue FDRs
using frequency modulation (FM) should he discontinued by 5
November 1998.
- Pressure altitude
- Indicated airspee,d
- Outside air temperature
- Heading
- Normal acceleration
- Lateral acceleration
- Longitudinal acceleration (body axis)
- Time or relative time count
- Navigation data*: drift angle, wind speed, wind
direction, latitudetlongitude
- Radio altitude*
4.3.1.4.1 The use of photographic film FDRs shall be
discontinued from 1 January 2003. 4.3.1.7.2 The following parameters satisfy the requirements
for attitude:
4.3.1.5 All helicopters for which the individual certificate
of airworthiness is first issued after 1 January 2005, which - Pitch attitude
utilize data link communications and are required to carry a - Roll attitude
CVR, shall record on a flight recorder, all data link - Yaw rate -
communications to and from the helicopter. The minimum
recording duration shall be equal to the duration of the CVR, 4.3.1.7.3 The following parameters satisfy the requireand
shall be correlated to the recorded cockpit audio. ments for engine power:
- Power on each engine: free power turbine speed (Nr),
4.3.1.5.1 From 1 January 2007, all helicopters which engine torque, engine gas generator speed (Xg). cockpit
utilize data link communications and are required to carry a power control position
CVR. shall record on. a flight recorder, all data link - Rotor: main rotor speed, rotor brake
communications to and from the helicopter. The minimuin - Main gearbox oil pressure*
recording duration shall be equal to the duration of the CVR, - Gearbox oil temperature*: main gearbox oil temperaand
shall be correlated to the recorded cockpit audio.
ture, intermediate gearbox oil temperature, tail rotor
gearbox oil temperature
4.3.1.5.2 Sufficient information to derive the content of - Engine exhaust gas temperature (T4)*
the data link communications message, and, whenever
- Turbine inlet temperature (TT)*
practical. the time the message was displayed to or generated
by the crew shall be recorded. 4.3.1.7.4 The following parameters satisfy the requirements
for configuration:
Note.- Data link conznzunicatiorzs include, but trre not
limited to, automatic dcpentlent surveillance (ADS), - Landing gear or gear selector position*
controller-pilot data link commrinications (CPDLC), data lcnk- - Fuel quantity*
flight information services (D-FJS) and aeronautical - Ice detector liquid water content*
operational control (AOC) messages.
4.3.1.6 Recommendation.- All helicopters of a
muximum certificated take-on mass over 2 700 kg, required to
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