Page 800 - UK Air Operations Regulations 201121

~ Regulation SPO - ANNEX VIII - Specialised Operations n trik

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44a Course/desired track (DSTRK)
44b Path angle
44c Coordinates of final approach path (IRNAV/IAN)
45 Selected decision height - t.o be reco rded for the aeroplane w here the parameter is
displayed electronically
46 Electronic fiight instrument system (EFIS) display format:
46a Pilot
46b Co-pilot
No' Parameter
47 Multi-function/engine/alerts display format
48 AC electrical bu5 status - each bus
49 DC electrica I bus status - each bus
50 Engine bleed valve pos.it io n
51 Auxiliary power unit (APU) bleed valve position
52 Com puter failure - (all critical flight and engine control systems)
53 Engine thrust command
54 Engine thrust target
55 Computed centre of gravity (CG)
56 fu el quant ity in CG t rim tank
57 Head-up display in use
58 Para vi.s.ua1 di.s.play on
59 Operationa l stall protection, stick shaker and pus.her activation
60 Primary navigation system refe rence:
60a GNSS
60b Inertial navigational system (INS)
60c VHF omnidirectional radio range {VOR)/DME
60d Ml.S
60e Loran C
60f ILS
61 Ice detection
62 Engine wam ing - each engine vibration
63 Engine wam ing - each engine ove r tem perature
64 Engine warn ing - each engine oil pressure low
65 Engine warn ing - each engine ove r speed
66 Yaw t rim surface position
67 Roll t rim surface position
No Parameter
68 Yaw or s.ideslip angle
69 De-icing and/or anti-icing systems selection
70 Hydraulic pressure - each system
71 Loss of cabin pressure
72 Trim control input position in the flight crew compartment, pitch - when mechanical
means for control inputs are not available, displayed trim position or t rim command
should be recorded
73 Trim control input position in t he flight cr ew compartment, roll - when mechanical
means for control inputs are not available, displayed trim position or t rim command
should be recorded
74 Trim control input position in the flight crew compartment , yaw - wh en mechanical
means for control inputs are not available, displayed trim position or t rim command
should be recorded
75 All flight control input forces {for fly-by-wire flight control systems, w here control
surface position is a function of th e disp lacement of th e control input device onJy, it
is not necessary to record t his parameter):
75a Control w heel
75b Control column
75c Rudder pedal
76 Event marker
77 Date
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20th November 2021 800 of 856