曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

FDR are listed in the paragraphs below. The parameters
24/11/05
No. 10
Section 111, Chapter 4 Annex 6 - Opemtion of Aircmp
without an asterisk (*) are mandatory parameters which shall
be recorded. In addition, the parameters designated by an
asterisk (*) shall be recorded if an information data source for
the parameter is used by helicopter systems or the flight crew
to operate the helicopter.
4.9.1.7.1 The following parameters satisfy the requirements
for flight path and speed:
- Pressure altitude
- Indicated airspeed - 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,
latitudellongitude
- Radio altitude*
4.9.1.7.2 The following parameters satisfy the requirements
for attitude:
- Pitch attitlidc
- Roll attitude
- Yaw rate
4.9.1.7.3 The following parameters satisfy the requirements
for engine power:
- Power on each engine: free power turbine speed (Nf).
engine toque, engine gas generator speed (Ng). cockpit
power control position
- Rotor: main rotor speed, rotor brake
- Main gearbox oil pressure* - Gearbox oil temperature*: main gearbox oil temperature,
intermediate gearbox oil temperature, tail rot~r-~earbox
oil temperature
- Engine exhaust gas temperature (TJ*
- Turbine inlet temperature (TIT)*
4.9.1.7.4 The following parameters satisfy the requirements
for configuration:
- Landing gear or gear selector position*
- Fuel contents* - Ice detector liquid water content*
4.9.1.7.5 The following parameters satisfy the requirements
for operation:
- Hydraulics low pressure
- warnings
- Primary Flight Controls - Pilot input andlor control
output position: collective pitch, longitudinal cyclic
pitch, lateral cyclic pitch, tail rotor .pedal, controllable
stabilator, hydraulic selection
- Marker beacon passage
- Each navigation receiver frequency selection - AFCS mode and engagement status*
- Stability augmentation system engagement*
- Indicated sling load force* - Vertical deviation*: ILS glide path, MLS elevation.
GNSS approach path
- Horizontal deviation*: ILS localizer. MLS azimuth.
GNSS approach path - DME 1 and 2 distances*
- Altitude rate*
- Ice detector liquid water content*
- Helicopter health and usage monitor system (HUMS)*:
engine data, chip detectors, track timing, exceedance
discretes, broadband average engine vibration
Note 1.- Parameter requirements, including range,
sampling, accumcy and resolution, as .contained in the
Minimum Operatiom1 Performance Specification (MOPS)
document for Flight Recorder Systems of the European
Organization for Civil Aviation Equipment (EUROCAE) or
equivalent documents.
Note 2.- The number of parameters to be recorded will
depend on helicopter complexity. Parameters without an (*)
are to be recorded regardless of helicopter complexity. Those
pammeten designated by an (*) are to be recorded if an
information source for the parameter is used by helicopter
systems a d o r flight crew to operate the helicopter.
4.9.2 Flight data recorders - duration
Types IV and V FDRs shall be capable of retaining the
information recorded during at least the last tea hours of their
operation.
4.9.3 Flight data recorders - helicopters
for which the individual certificate
of airworthiness is first issued
on or after 1 January 1989
4.9.3.1 All helicopters of a maximum certificated take-off
mass of over 7 000 kg shall be equipped with a Type N FDR.
4.9.3.2 Recommendation.- All helicopters of a
marimurn certificated take-off mass of over 2 700 kg up to and
including 7 000 kg should be equipped with a Type V FDR.
4.9.4 Flight data recorders - helicopters
for which the individual certificate
of airworthiness is first issued after 1 January 2005
4.9.4.1 All helicopters of a maximum certificated take-off
mass of over 3 180 kg shall be equipped with a Type IVA
FDR with a recording duration of at least 10 hours.
Note.- A single, combination CVWFDR is acceptable.
W1 YO5
No. 10
Annex 6 - weration of Aircmfl Part ZZZ
4.9.5 Cockpit voice recorders - helicopters
for which the individual certificate
of airworthiness is first issued
on or after 1 January 1987
Note.- CVR 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
　
中國航空網(wǎng) www.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_P3_5ed_amend_10(7)