Page 804 - UK Air Operations Regulations 201121

~ Regulation SPO - ANNEX VIII - Specialised Operations n trik

46 b Co-pilot
47 Mult Hunction/engjn e/ alerts display format, show ing the display system status
4S Alternating cun-ent {AC) electrical bus status - each bu.s.
49 Direct current (DC) electrical bus status - each bus
50 engine bleed valve(s) position
No* Parameter
51 Auxiliary power unit (APU) bleed valve(s) position
52 Computer failure - all critical flight and engine control systems
53 Engine t hrust command
54 Engine t hrust target
55 Computed centre of gravity (CG)
56 Fuel quant ity in CG trim tank
57 Head-up display in use
58 Paravisua 1 display on
59 Operat ional stall protection, s.tick shaker and pusher activation
60 Primary navigatio n system reference :
60a GNSS
60b Inertial navigational system (INS)
60c VHF omnidirectional radio range {VOR)/dis,tance measuring equipment (DME)
60d MIS
60e Loran C
60f 115
61 Ice detection
62 Engine w arning - each engine vibration
63 Engine warning - each engine over temperature
64 Engine w arning - each engine oil pressure low
65 Engine w arning - each engine overspeed
66 Yaw t rim surface position
67 Roll trim surface position
68 Yaw or sideslip angle
69 De-icing and/or anti-icing systems selection
70 Hydraulic press.ure - each system
71 Loss of cabin pressure

No* Parameter
72 Trim cont rol input position in the fl ight crew compartment, pitch - when mechanical means
for control inputs. are not available, di.splayed tri m position or t rim command should be
recorded.
73 Trim control input position in th e fl ight crew compartm ent, roll - when mechaniail means
for control inputs. are not available, di.splayed tri m position or t rim command should be
recorded.
74 Trim control input position in the flight crew compartment, yaw - w hen mechanical means
for control inputs. are not available, displayed t rim position or t rim command should be
recorded.
75 All flight control input forces {for f ly-by-wire fligl,t control systems, where cont rol surface
position is a function of the displacement of the cont rol input device on ly, it is not necessary
to record t his parameter):
75a Control wheel input forces
75b Control column input forces
75c Rudder pedal input forces
76 Event marker
77 Date
78 Actual navigation performance (ANP) or estimat e of position error (EPE) or estimate of
position uncertainty (EPU)
79 Cabin pressure altitude - for aeroplanes type certified before 1 January 2023, to be
recorded onty if this does not require extensive modification
80 Aeroplane computed w eight - for aeroplanes type certified before 1 January 2023, t o be
recorded onty if this does not require extensive modification
81 Flight direct.or command:
81 a Left flight director pitch command - for aeroplanes type certified before 1 January 2023,
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