Page 808 - UK Air Operations Regulations 201121
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~          Regulation SPO - ANNEX VIII - Specialised Operations                                              n trik



                                      11   Graphics   Weather  maps  &  Graphics  exchanged  in  the  fra me\vork  of
                                                  other graphics   procedure5 w ithin the  operational control, as.
                                                             specified in Part-ORO.
                                                             Information that enables correlation w ith any
                                                             associated records  stored separately from the
                                                             aerop lane.
                                      12   AOC    Aeronautical   Messages  exchanged  in  the  framework  of
                                                  operational  control  procedures. within  the  operational control, as
                                                  messages   specified in Part-ORO.
                                                             Information that enables correlation w ith any
                                                             associated records  stored separately from the
                                                             aeroplane.  Definition  in  EUROCAE  ED-112,
                                                             dated March 2003.
                                      13   Surveillance   Downlinked aircraft  As  defined  in  ICAO  Annex  10  Volume  IV
                                                  parameters IDAP)   (Surveillance systems and ACAS).
             SPO.IDE.A.150(a) GM1    Data Link Recording
                                      APPLICABILITY OF THE DATA LINK RECORDING REQUIREMENT
                                          (a)  If it is certain that the aeroplane cannot use data link communication messages for ATS
                                             communications corresponding to any application designated by SPO.IDE.A.150(1), then
                                             the data link recording requirement does not apply.
                                          (b)  Examples where the aeroplane cannot use data link communication messages for ATS
                                             communications include but are not limited to the cases where:
                                              (1)  the aeroplane data link communication capability is disabled permanently and in a
                                                 way that it cannot be enabled again during the flight;
                                              (2)  data link communications are not used to support air traffic service (ATS) in the area
                                                 of operation of the aeroplane; and
                                              (3)  the aeroplane data link communication equipment cannot communicate with the
                                                 equipment used by ATS in the area of operation of the aeroplane
             SPO.IDE.A.155           Flight data and cockpit voice combination recorder
                                      Compliance with CVR requirements and FDR requirements may be achieved by:
                                          (a)  one flight data and cockpit voice combination recorder if the aeroplane has to be equipped
                                             with a CVR or an FDR; or
                                          (b)  two flight data and cockpit voice combination recorders if the aeroplane has to be equipped
                                             with a CVR and an FDR.
             SPO.IDE.A.155 AMC1      Flight Data And Cockpit Voice Combination Recorder
                                      GENERAL
                                      When two flight data and cockpit voice combination recorders are installed, one should be located
                                      near the flight crew compartment in order to minimise the risk of data loss due to a failure of the wiring
                                      that gathers data to the recorder. The other should be located at the rear section of the aeroplane, in
                                      order to minimise the risk of data loss due to recorder damage in the case of a crash
             SPO.IDE.A.155 GM1       Flight data and cockpit voice combination recorder
                                      GENERAL
                                          (a)  A flight data and cockpit voice combination recorder is a flight recorder that records:
                                              (1)  all voice communications and the aural environment required by SPO.IDE.A.140;
                                                 and
                                              (2)  all parameters and specifications required by SPO.IDE.A.145, with the same
                                                 specifications required by SPO.IDE.A.140 and SPO.IDE.A.145.
                                          (b)  In addition a flight data and cockpit voice combination recorder may record data link
                                             communication messages and related information required by SPO.IDE.A.150.
             SPO.IDE.A.160           Seats, seat safety belts and restraint systems
                                      Aeroplanes shall be equipped with:
                                          (a)  a seat or station for each crew member or task specialist on board;
                                          (b)  a seat belt on each seat, and restraint devices for each station;
                                          (c)  for other-than-complex motor-powered aeroplanes, a seat belt with upper torso restraint
                                             system on each flight crew seat, having a single point release for aeroplanes having a
                                             CofA first issued on or after 25 August 2016;
                                          (d)  for complex motor-powered aeroplanes, a seat belt with upper torso restraint system,
                                             incorporating a device that will automatically restrain the occupant's torso in the event of
                                             rapid deceleration:
                                              (1)  on each flight crew seat and on any seat alongside a pilot's seat; and
                                              (2)  on each observer's seat located in the flight crew compartment.
                                          (e)  The seat belt with upper torso restraint system required under point (d) shall have:
                                              (1)  a single point release;
                                              (2)  on flight crew members seats and on any seat alongside a pilot's seat, either of the
                                                 following:
                                                  (i)  two shoulder straps and a seat belt that may be used independently;
                                                  (ii)  a diagonal shoulder strap and a seat belt that may be used independently for
                                                     the following aeroplanes:
                                                      (A)  aeroplanes with an MCTOM of 5 700 kg or less and with an MOPSC of
                                                         nine or less that are compliant with the emergency landing dynamic
                                                         conditions defined in the applicable certification specification;
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