FAA sets new minimum requirements for 737 MAX
autopilot
The FAA's Master Minimum Equipment List for the
737 MAX now features new requirements tied to autopilot and flight
controls
Airlines flying the 737 MAX will face new restrictions on
the operation of some autopilot-related systems when the type returns to
service. The changes are detailed in revision 2 of the Master Minimum Equipment
List (MMEL), published by the Federal Aviation Administration on 10 April 2020.
The new rules remove exemptions for several systems, in effect increasing the
required redundancies for dispatching the MAX when it returns to
service.
The revised MMEL includes 12 changes to required equipment or
redundancies on board. Previously, for example, a 737 MAX could be dispatched
with no working autopilot systems so long as en route operations and approach
minimums did not require the system, and the total amount of flying was
acceptable to the flight crew. Under the new rules at least one of the two
autopilot computers on board must be functional for an aircraft to
depart.
The audible warning system for autopilot disengage and warning
lights tied to Speed Trim Fail and Stabilizer out of Trim must now also be
functional for a MAX to depart. Under the prior rules these were not required so
long as autopilot was not in use or the the trim system was "verified to operate
normally."
Similarly, at least one of the autopilot command switches and
lights must now function, tied to the working autopilot system on board. Ditto
for the autopilot disengage light and Control Wheel Autopilot Disengage
Switches. As the autopilot requirements increase these warning and control
systems can no longer be exempted.
Just a few of the revisions to the minimum
equipment list for the 737 MAX, increasing redundancy and alerts related to the
aircraft's autopilot system
Finally, the Flight Controls section of
the document was updated to require both of the Control Wheel Trim Switch
Systems be operating properly. Previously the MMEL allowed for one "inoperative
on non-flying pilot's side provided control wheel trim switch operates normally
on flying pilot's side."
The pilots of both the LionAir and Ethiopian
Airlines fought against incorrect trim settings as the Maneuvering
Characteristics Augmentation System (MCAS) erroneously pushed the aircraft into
the ground. Given the critical nature of trim control in both accidents this
change increases the odds that pilots could overcome another runaway trim issue.
Or at least ensures that both have the necessary control systems in place to do
so.
All of the MMEL changes are secondary, however, to the other
revisions Boeing is making to the MCAS system and other facets of autopilot as
it works to bring the MAX back to the skies. These include not allowing MCAS to
repeatedly override pilot inputs.
It will also include as standard
(previously only an add-on feature) an alert for angle-of-attack (AOA) disagree
between the redundant sensors on board. MCAS depends on the AOA system to
trigger its controls. In both crashes it activated when one of the AOA sensors
indicated problems while the other reported normal flight. Lack of notification
regarding that disagreement between the AOA sensors is believed to have
contributed to the pilots' inability to regain control in both
crashes.
The new rules apply to both the MAX 8 and MAX 9 models.
Presumably the MAX 10 will include similar requirements when its MMEL is
released as part of the type's certification.
Abonner på:
Legg inn kommentarer (Atom)
Ingen kommentarer:
Legg inn en kommentar
Merk: Bare medlemmer av denne bloggen kan legge inn en kommentar.