曝光台 注意防骗
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every two years.
ATT D-3
Annex 6 - Operation of Aircraft Part I
Table D- 1
Parameters for Flight Data Recorders
Recording
interval
Measurement range (seconds)
Accuracy limits
(sensor input compared
to FDR read-out)
Serial
number Parameter
1 Time (UTC when available, 24 hours
otherwise elapsed time)
33.125% per hour
-300 m (-1 000 ft) to 1
maximum certificated
altitude of aircraft
+1 500 m (+5 000 ft)
f30 m to +200 m
(+I00 ft to +700 ft)
3 Indicated airspeed 95 kmlh (50 kt) to max 1
Vs, (Note I)
VS, to 1.2 V, (Note 2)
4 Heading 360" 1
5 Normal acceleration -3 g to +6 g 0.125 f 1 % of maximum range
excluding datum error of +5%
6 Pitch attitude f7S0 1
7 Roll attitude +18O0 1
8 Radio transmission keying On-off (one discrete) 1
9 Power on each engine Full range
(Note 3)
1 (per
engine)
10 Trailing edge flap or cockpit Full range or each
control selection discrete position
+5% or as pilot's indicator
1 I Leading edge flap or cockpit Full range or each
control selection discrete position
+5% or as pilot's indicator
12 Thrust reverser position Stowed, in transit, and 1 (Per
reverse engine)
13 Ground spoilerlspeed brake Full range or each discrete 1
selection position
+2% unless higher accuracy
uniquely required
14 Outside air temperature Sensor range 2
15 Autopilot/auto A suitable combination of 1
throttle1AFCS discretes
mode and engagement status
Note.- The preceding I5 parameters satisfy the requirements for a Type 11 FDR.
16 Longitudinal acceleration +I g 0.25 +1.5% max range excluding datum
error of k5%
17 Lateral acceleration +1 g 0.25 +1.5% max range excluding datum
error of +5%
18 Pilot input andlor control Full range
surface position-primary
controls (pitch, roll, yaw)
(Note 4)
+2" unless higher accuracy
uniquely required
ATT D-4
Attachment D Annex 6 - Opemtwn of Aircraft
Recording Accuracy limits
interval (sensor input compared
Measurement range (seconds) to FDR read-out)
Serial
number Parameter
19 Pitch trim position Full range 1 +3% unless higher accuracy
uniquely required
20 Radio altitude -6 m to 750 m
(-20 ft to 2 500 ft)
1 kO.6 m (a ft) or k3%
whichever is greater below 150 m
(500 ft) and k5% above 150 rn
(500 ft)
21 Glide path deviation Signal range
22 Localizer deviation Signal range
23 Marker beacon passage Discrete
24 Master warning Discrete
25 NAV 1 and 2 frequency Full range
selection (Note 5)
4 As installed
26 DME 1 and 2 distance 0 - 370 km
(Notes 5 and 6)
4 As installed
27 Landing gear squat switch Discrete
status
28 GPWS (ground proximity Discrete
warning system)
29 Angle of attack Full range 0.5 As installed
30 Hydraulics, each system Discrete 2
(low pressure)
3 1 Navigation data As installed
(latitudellongitude, ground
speed and drift angle) (Note 7)
1 As installed
32 Landing gear or gear Discrete
selector position
4 As installed
Note.- The preceding 32 parameters satisfy the requirements for a Type I FDR.
1. Vso stalling speed or minimum steady flight speed in the landing configuration.
2. VD design diving speed.
3. Record sufficient inputs to determine power.
4. For aeroplanes with conventional control systems "or" applies. For aeroplanes with non-mechanical control systems "and" applies. In
aeroplanes with split surfaces, a suitable combination of inputs is acceptable in lieu of recording each surface separately.
5. If signal available in digital form.
6. Recording of latitude and longitude from INS or other navigation system is a preferred alternative.
7. If signals readily available.
ATT D-5
Annex 6 - Operation of Aircraft Par€ .I
If further recording capacity is available, recording of the following additional information should be considered:
a) operational information from electronic display systems, such as electronic flight instrument systems (EFIS), electronic
centralized aircraft monitor (ECAM) and engine indication and crew alerting system (EICAS). Use the following order of
priority:
1) parameters selected by the flight crew relating to the desired flight path, e.g. barometric pressure setting, selected
altitude, selected airspeed, decision height, and autoflight system engagement and mode indications if not recorded from
another source:
2) display system selection/status, e.g. SECTOR, PLAN, ROSE, NAV, WXR, COMPOSITE, COPY, ETC.;
3) warnings and alerts;
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ICAO 附件6 Operation of Aircraft(73)
