曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

synchronization reference
- Autopilot/autothrottlelAFCS mode and engagement
status*
- Selected barometric setting*: pilot, first officer
- Selected altitude (all pilot selectable modes of
operation)*
1/11/01
No. 21
Annex 6 - Operation of Aircraft Part II
- Selected speed (all pilot selectable modes of operation)*
- Selected mach (all pilot selectable modes of operation)*
- Selected vertical speed (all pilot selectable modes of
operation)*
- Selected heading (all pilot selectable modes of
operation)*
- Selected flight path (all pilot selectable modes of
operation)*: course/DSTRK, path angle
- Selected decision height*
- EFIS display format*: pilot, first officer
- Multi-function/engine/alerts display format*
- GPWS/TAWS/GCAS status*: selection of terrain display
mode including pop-up display status, terrain alerts, both
cautions and warnings, and advisories, on/off switch
position
- Low pressure warning*: hydraulic pressure, pneumatic
pressure
- Computer failure*
- Loss of cabin pressure*
- TCASIACAS (traffic alert and collision avoidance
system/airborne collision avoidance system)*
- Ice detection*
- Engine warning each engine vibration*
- Engine warning each engine over temperature*
- Engine warning each engine oil pressure low*
- Engine warning each engine over speed*
- Wind shear warning*
- Operational stall protection, stick shaker and pusher
activation*
- All cockpit flight control input forces*: control wheel,
control column, rudder pedal cockpit input forces
- Vertical deviation*: ILS glide path, MLS elevation,
GNSS approach path
- Horizontal deviation*: ILS localizer, MLS azimuth.
GNSS approach path
- DME 1 and 2 distances*
- Primary navigation system reference*: GNSS, INS,
VORIDME, MLS, Loran C, ILS
- Brakes*: left and right brake pressure, left and right brake
pedal position
- Date*
- Event marker*
- Head up display in use*
- Para visual display on*
Note 1.- Parameter requirements, including range,
sampling, accuracy and resolution, as contained in the
Minimum Operational Performance Specification (MOPS)
document for Flight Recorder Systems of the European
Organization for Civil Aviation Equipment (EUROCAE) or
equivalent documents.
6.10.2 Flight data recorders - duration
Types I and I1 flight data recorders shall be capable of
retaining the information recorded during at least the last
25 hours of their operation.
6.10.3 Flight data recorders - aeroplanes for
which the individual certificate of airworthiness
is first issued on or after 1 January 1989
6.10.3.1 All aeroplanes of a maximum certificated takeoff
mass of over 27 000 kg shall be equipped with a Type I
flight data recorder.
6.10.3.2 Recommendation.- All aeroplanes of a
maximum certificated take-off mass of over 5 700 kg up to and
including 27 000 kg should be equipped with a Type II jlight
data recorder.
6.10.4 Flight data recorders - aeroplanes for which
the individual certificate of airworthiness
is first issued after 1 January 2005
All aeroplanes of a maximum certificated take-off mass of
over 5 700 kg shall be equipped with a Qpe IA flight data
recorder.
6.10.5 Cockpit voice recorders - aeroplanes
for which the individual certificate of airworthiness
is first issued on or after 1 January 1987
Note.- Cockpit voice recorder performance requirements
are as contained in the Minimum Operational Performance
Specifications (MOPS) document for Flight Recorder Systems
of the European Organization for Civil Aviation Equipment
(EUROCAE) or equivalent documents.
6.10.5.1 All aeroplanes of a maximum certificated takeoff
mass of over 27 000 kg shall be equipped with a cockpit
voice recorder, the objective of which is the recording of the
aural environment on the flight deck during flight time.
6.10.5.2 Recommendation.- All aeroplanes of a
maximum certificated take-off mass of over 5 700 kg up to and
including 27 000 kg should be equipped with a cockpit voice
recorder; the objective of which is the recording of the aural
environment on the jlight deck during jlight time.
Note 2.- The number of parameters to be recorded will
depend on aeroplane complexity. Parameters without an (*) 6.10.6 Cockpit voice recorders - duration
are to be recorded regardless of aeroplane complexity. Those
parameters designated by an (*) are to be reconied if an 6.10.6.1 A cockpit voice recorder shall be capable of
information source for the parameter is used by aeroplane retaining the information recorded during at least the last 30
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：附件6--航空器的運行an06_P2_6ed(48)