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- Selected heading (all pilot selectable modes of oper- 25 hours of their
ation)*
- Selected flight path (all pilot selectable modes of
operation)*: courseDSTRK, path angle
6.10.3 Flight data recorders - aeroplanes for
-- ESeFlIeSc tdedis pdleacyi sfioornm haet*ig: hpti*l ot, first officer which the individual certificate of airworthiness
is first issued on or after 1 January 1989
- Multi-function/engine/alerts display format*
- GPWSEAWSIGCAS status*: selection of terrain
display mode including pop-up display status, terrain 6.10.3.1 All aeroplanes of a maximum certificated takeoff
mass of over 27 000 kg shall be equipped with a Type I alerts, both cautions and warnings, and advisories, onloff
switch position flight data recorder.
- Low pressure warning*: hydraulic pressure, pneumatic
6.10.3.2 Recommendation.- All aeroplanes of a
pressure
maximum certificated take-off mass of over 5 700 kg up to and
- Computer failure*
- Loss of cabin pressure*
including 27 000 kg should be equipped with a Type Ilflight
- TCASIACAS (traffic alert and collision avoidance data recorder.
system/airbome collision avoidance system)*
- Ice detection*
- Engine warning each engine vibration* 6.10.4 Flight data recorders - aeroplanes for which
- Engine warning each engine over temperature* the individual certificate of airworthiness
- Engine warning each engine oil pressure low* is first issued after I January 2005
- Engine warning each engine over speed*
- Wind shear warning* All aeroplanes of a maximum certificated take-off mass of
- Operational stall protection, stick shaker and pusher Over 5 700 kg shall be equipped with a Type 1.4 flight data
activation* recorder.
- All cockpit flight control input forces*: control wheel,
control column, rudder pedal cockpit input forces
- Vertical deviation*: ILS glide path, MLS elevation, 6.10.5 Cockpit voice recorders - aeroplanes
GNSS approach path for which the individual certificate of airworthiness
- Horizontal deviation*: ILS localizer, MLS azimuth, is first issued on or after I January 1987
GNSS approach path
- DME 1 and 2 distances* Note.- Cockpit voice recorder performance requirements
- Primary navigation system reference*: GNSS, INS, are as contained in the Minimum Operational Performance
VORIDME, MLS, Loran C, ILS Specjfications (MOPS) document for Flight Recorder Systems
- Brakes*: left and right brake pressure, left and right brake of the European Organization for Civil Aviation Equipment
pedal position (EUROCAE) or equivalent documents.
- Date*
- Event marker* 6.10.5.1 All aeroplanes of a maximum certificated take-
- Head up display in use* off mass of over 27 000 kg shall be equipped with a cockpit
- Para visual display on* voice recorder, the objective of which is the recording of the
aural environment on the flight deck during flight time.
Note 1.- Parameter requirements, including range.
samplir~g, accuracy and resolution, as contained in the 6.10.5.2 Recommendation.- All aeroplanes of a
Minimum Operational Pelformarzce Spect$cation (MOPS) max-irn~mce~r tijicated take-off mass of over 5 700 kg up to arrd - document for Flight Recorder Systenzs of the Eltropearz irlcl~rdirlg2 7 000 kg sho~~lbde equipped with a cockpit voice
0rgani;ation for Civil Aviation Equiprnetlt (EUROCAE) or recordel; the objective of which is the recording of the a~rml
equivalerlt documents. erzvironrizer~ot r1 the flight deck during jlight time.
28/11/02
No. 22
Chapter 6 Annex 6 - Operation of Aircraft
6.10.6 Cockpit voice recorders - duration
6.10.6.1 A cockpit voice recorder shall be capable of
retaining the information recorded during at least the last 30
minutes of its operation.
6.10.6.2 Recommendation.- A cockpit voice recorder;
installed in aeroplanes of a maximum cert$cated take-off
mass of over 5 700 kg for which the individual certificate of
airworthiness is first issued on or after I January 1990, should
be capable of retaining the information recorded during at
least the last two hours of its operation.
6.10.6.3 A cockpit voice recorder, installed in aeroplanes
of a maximum certificated take-off mass of over 5 700 kg for
which the individual certificate of airworthiness is first issued
after 1 January 2003, shall be capable of retaining the
information recorded during at least the last two hours of its
operation.
6.10.9 Flight recorder records
The pilot-in-command shall ensure, to the extent possible, in
the event the aeroplane becomes involved in an accident or
incident, the preservation of all related flight recorder records,
and if necessary the associated flight recorders, and their
retention in safe custody pending their disposition as
　
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