Page 641 - UK Air Operations Regulations (Consolidated) 201121

~ Regulation NCC - ANNEX VI - Non-Commercial Complex Operations n trik

No' Parameter
I Time or relative time count
2 Pressure altitude
3 Indicated airspeed
4 Heading
5 Norma I acceleration
6 Pitch attitude
7 Roll attitude
8 Manual radio transmission keying CVR/FOR synchronisation reference
9 Power on each engine:
9a free power turbine speed (NF)
9b Engine torque
9c Engine gas gerierator speed (NG)
9d fligh·t crew corn pa rtment power control position
9e Other parameters to enable engine power to be determined
10 Rotor:
!Oa Main rotor speed
!Ob Rotor brake I f inst a I led)
i
11 l'mlal)' ftigtO: cootrols - Pilot i"plJt ar,c\lor cmtrd outpUt position flf appicable):
lla Collective pitch
lib Longitudinal cyclic pitch
lie Lateral cyclic pitch
lid Ta il rotor pedal
lie Controllable stabilator (if applicable)
11f Hydraulic selection
12 Hydraulics low pressure (each system should be recorded.)
B Outside air temperature
18 Yaw rate or yaw acceleration
20 longitudinal acceleration (body axis)
21 Lateral acceleratlOn
25 Marker beacon passage
26 W arnings - a discrete should be recorded for the master warning, gearbox low oil
pressure and stability augmentation system as fa ilure. Other 'red' warnings should be
recorded where the warning cond ition cannot be determined from other para meters
or from the cockpit voice r ecorder.
27 Each navigation receiver frequency selectton
37 Engine control modes
The number in the left hand column reflects the serial number depicted in EUROCAE ED-
112.
Table 2: FOR parameters - Helicopters for whkh the data source for the pa rameter is either
used by helicopter systems or is available on the instrument panel for use by the f light
crew to operate the helicopter
No' Parameter
14 AFCS mode and engagement status
IS Stability augmentation system ef'\gagement (each system should be recorded)
16 Main gear box oil pre.ssure
17 Gear box oil temperature:
17a Main gear box oil temperaru re
17b Intermediate gear box o il temperature
17c Ta il rotor gear box oil temperature
19 Ind icated sling load force (if signals readily available)
22 Radio altitude
23 Venical deviation - the approach aid in use shou ld be recorded:
23a ILS glide path
23b MLS elevation
23c GNSS a pp roach path
24 Horizof'\tal deviatiof'\ - the approach aid in use should be recorded:
24a IL.S localiser
24b MLS azimuth
24c GNSS a pp roach path
28 DM E 1 & 2 distances
29 Navigation data:
29a Drift angle
29b Wind speed
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