![]() Improvements on the 737, many new types of approaches have been developed. With increased navigational accuracy available and hardware/software A list ofĮach of their features is given in the book. ![]() The latest software is BP 15, introduced in Oct 2016, fitted as standard from L/N 6119 onwards and to earlier aircraft by retrofit. There have been six updates from BP98 to BP15. Each new update is known as a Block Point. Incorporate additional features, improvements to existing features and bugįixes. The 737NG Common Display System has had several software updates to The red line is the angle for stick shaker activation, the green One of the many customer PFD options is an analogue/digital angle of attackĭisplay. Is dependent on gross weight, but in general Vmnver is output below 22,000 feet andĪlthough not used directly in the calculation of Vmnvr, once theĪirplane starts flying, gross weight becomes a factor indirectly (in the calculation of Vmnvr) via the load factor calculation.įMC Gross Weight is used by the SMYD in the switching logic from Vmnvr The first is identified as Vmnvr, the second as Vbl (low speed buffet). Minimum operating speed is computed from the SMYD as follows: The SMYD has Operating speed provides a 0.3g manouvre margin to high speed buffet. The speed tape shows minimum and maximum operating speeds. Switch on the -3/4/500's which was used to switch symbol generators. Note that this is not the same as the EFI The DISPLAYS CONTROL PANEL annunciation merely indicates that an EFISĪn additional, rather bizarre, attention getter because the altimeter willīlank on the failed side, with an ALT flag, until the DISPLAYS - CONTROL PANEL switch Remember that this is a switch that pilots should not touch! This may be why the switch is aĭifferent shape to the other three if not, it is still a good way to ![]() SOURCE selector is only used on the ground for maintenance purposes (to makeĪll 6 DU's be powered by either DEU 1 or 2). “engines running” logic is used in case the air/ground data isn't ![]() Logic as the primary trigger for changing the CDS FAULT message to its One of the inputs used is “engines running”. The air/ground logic system uses a number ofĪirplane state. Intended to be activated on ground, air/ground logic is used by CDS to Since the DISPLAY SOURCE message is intended to be activated in air and
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