532
14 CFR Ch. I (1–1–19 Edition)
Pt. 135, App. F
The recorded values must meet the designated range, resolution and accuracy requirements during static and dynamic condi-
tions. Dynamic condition means the parameter is experiencing change at the maximum rate attainable, including the maximum
rate of reversal. All data recorded must be correlated in time to within one second.
Parameters Range
Accuracy (sensor
input)
Seconds per
sampling interval
Resolution Remarks
36. Landing Gear
Position or
Landing gear
cockpit control
selection.
Discrete .............
...........................
4 ........................
...........................
A suitable combination of
discretes should be re-
corded.
37. Drift Angle
15
As installed ........
As installed ........
4 ........................
0.1
°
38. Wind Speed
and Direction.
As installed ........
As installed ........
4
1 knot, and 1.0
°
.
39. Latitude and
Longitude.
As installed ........
As installed ........
4 ........................
0.002
°
, or as in-
stalled.
Provided by the Primary
Navigation System Ref-
erence. Where capacity
permits latitude/longitude
resolution should be
0.0002
°
.
40. Stick shaker
and pusher acti-
vation.
Discrete(s) ‘‘on’’
or ‘‘off’’.
...........................
1 ........................
...........................
A suitable combination of
discretes to determine acti-
vation.
41. Windshear
Detection.
Discrete ‘‘warn-
ing’’ or ‘‘off’’.
...........................
1.
42. Throttle/power
lever position
16
.
Full Range .........
±
2% ...................
1 for each lever
2% of full range
For airplanes with non-me-
chanically linked cockpit
engine controls.
43. Additional En-
gine Param-
eters.
As installed ........
As installed ........
Each engine
each second.
2% of full range
Where capacity permits, the
preferred priority is indi-
cated vibration level, N2,
EGT, Fuel Flow, Fuel Cut-
off lever position and N3,
unless engine manufac-
turer recommends other-
wise.
44. Traffic Alert
and Collision
Avoidance Sys-
tem (TCAS).
Discretes ...........
As installed ........
1 ........................
...........................
A suitable combination of
discretes should be re-
corded to determine the
status of—Combined Con-
trol, Vertical Control, Up
Advisory, and down advi-
sory. (ref. ARINC Char-
acteristic 735 Attachment
6E, TCAS VERTICAL RA
DATA OUTPUT WORD.)
45. DME 1 and 2
Distance.
0–200 NM; ........
As installed ........
4 ........................
1 NM .................
1 mile.
46. Nav 1 and 2
Selected Fre-
quency.
Full range ..........
As installed ........
4 ........................
...........................
Sufficient to determine se-
lected frequency.
47. Selected baro-
metric setting.
Full Range .........
±
5% ...................
(1 per 64 sec.) ..
0.2% of full
range.
48. Selected alti-
tude.
Full Range .........
±
5% ...................
1 ........................
100 ft.
49. Selected
speed.
Full Range .........
±
5% ...................
1 ........................
1 knot.
50. Selected
Mach.
Full Range .........
±
5% ...................
1 ........................
.01.
51. Selected
vertical speed.
Full Range .........
±
5% ...................
1 ........................
100 ft./min.
52. Selected
heading.
Full Range .........
±
5% ...................
1 ........................
1
°
.
53. Selected flight
path.
Full Range .........
±
5% ...................
1 ........................
1
°
.
54. Selected deci-
sion height.
Full Range .........
±
5% ...................
64 ......................
1 ft.
55. EFIS display
format.
Discrete(s) .........
...........................
4 ........................
...........................
Discretes should show the
display system status (e.g.,
off, normal, fail, composite,
sector, plan, nav aids,
weather radar, range,
copy.
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