Skip to main content

Maneuvering Characteristics Augmentation System (MCAS)

 
MCAS, or Maneuvering Characteristics Augmentation System, provides consistent airplane handling characteristics in a very specific set of unusual flight conditions. MCAS now contains multiple enhanced protections:

  • Measurements from two Angle of Attack (AOA) sensors will be compared.
  • Each sensor will submit its own data to the airplane’s flight control computer.
  • MCAS will only be activated if both sensors agree.
  • MCAS will only be activated once.
  • MCAS will never override the pilot’s ability to control the airplane using the control column alone.

MCAS ON 737 Max
The Maneuvering Characteristics Augmentation System (MCAS) flight control law was implemented on the 737 MAX to mitigate the aircraft's tendency to pitch up because of the aerodynamic effect of its larger, heavier, and more powerful CFM LEAP-1B engines and nacelles. The stated goal of MCAS, according to Boeing, was to provide consistent aircraft handling characteristics at elevated angles of attack in certain unusual flight conditions only and hence make the 737 MAX perform similarly to its immediate predecessor, the 737NG



MCAS role on Accidents
Investigators determined that MCAS was triggered by falsely high angle of attack (AoA) inputs, as if the plane had pitched up excessively. On both flights, shortly after takeoff, MCAS repeatedly actuated the horizontal stabilizer trim motor to push down the airplane nose. Satellite data for the flights, ET 302 and JT 610, showed that the planes struggled to gain altitude. Pilots reported difficulty controlling the airplane and asked to return to the airport.

On March 11, 2019, after China had grounded the aircraft, Boeing published some details of new system requirements for the MCAS software and for the cockpit displays, which it began implementing in the wake of the prior accident five months earlier:

  • If the two AoA sensors disagree with the flaps retracted, MCAS will not activate and an indicator will alert the pilots.
  • If MCAS is activated in non-normal conditions, it will only "provide one input for each elevated AoA event."
  • Flight crew will be able to counteract MCAS by pulling back on the column.

On March 27, Daniel Elwell, the acting administrator of the FAA, testified before the Senate Committee on Commerce, Science, and Transportation, saying that on January 21, "Boeing submitted a proposed MCAS software enhancement to the FAA for certification. the FAA has tested this enhancement to the 737 MAX flight control system in both the simulator and the aircraft. The testing, which was conducted by FAA flight test engineers and flight test pilots, included aerodynamic stall situations and recovery procedures." After a series of delays, the updated MCAS software was released to the FAA in May 2019. On May 16, Boeing announced that the completed software update was awaiting approval from the FAA.The flight software underwent 360 hours of testing on 207 flights. Boeing also updated existing crew procedures. The implementation of MCAS has been found to disrupt autopilot operations.

On April 4, 2019 Boeing publicly acknowledged that MCAS played a role in both accidents

Why do newer 737s need MCAS?
U.S. Federal Aviation Administration (FAA) regulations require that all commercial jetliners have smooth handling characteristics in all flight conditions. This includes rare instances where the nose of the airplane is unusually high, such as when it is climbing aggressively or performing excessively tight turns with high bank angles.

When does MCAS activate?
MCAS was designed to activate only when all three of the following conditions occur at the same time:

  1. The pilot is flying the airplane manually.
  2. The airplane nose approaches a higher-than-usual angle.
  3. The pilot has the wing flaps up.


How did MCAS initially work?
Prior to being enhanced, MCAS relied on information from a single Angle of Attack (AOA) sensor to monitor the angle of the airplane. In the two accidents, a single AOA sensor gave incorrect information to MCAS, which caused it to activate. In both cases, MCAS engaged repeatedly when the sensor continued to incorrectly report a high AOA.



Popular posts from this blog

Gas Turbine Compressor

PURPOSE OF COMPRESSOR                                     The compressor section of the gas turbine engine has many functions. Its primary function is to supply air in sufficient quantity to satisfy the requirements of the combustion burners. Specifically, to fulfill its purpose, the compressor must increase the pressure of the mass of air received from the air inlet duct, and then, discharge it to the burners in the quantity and at the pressures required.                               A secondary function of the compressor is to supply bleed-air for various purposes in the engine and aircraft. The bleed-air is taken from any of the various pressure stages of the compressor.                              The exact location of the bleed ports is dependent on the pressure or temperature required for a particular job. The ports are small openings in the compressor case adjacent to the particular stage from which the air is to be bled                                Air is often bled

Lockheed Martin F-35 Lightning II

Ø   The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, all-weather stealth multirole fighters. Ø   The fifth-generation combat aircraft is designed to perform ground attack and air superiority missions. Ø   It has three main models: ·        the F-35A conventional takeoff and landing (CTOL) variant, ·        the F-35B short take-off and vertical-landing (STOVL) variant, ·        the F-35C carrier-based Catapult Assisted Take-Off But Arrested Recovery (CATOBAR) variant.                                      Role Stealth   multirole fighter National origin United States Manufacturer Lockheed Martin Aeronautics First flight 15 December 2006 (F-35A) Introduction F-35B: 31 July 2015 ( USMC ) F-35A: 2 August 2016 ( USAF ) F-35C: 2018 ( USN ) Status In service Primary users United States Air Force United States Marin

ATA Chapters

Air transportation Association (ATA) published a numbering system to learn and understand the technical features of an Aircraft The standard numbering system was published by the   Air Transport Association   on June 1, 1956.  While the   ATA 100   numbering system has been superseded, it continued to be widely used until it went out of date back in 2015, especially in documentation for   general aviation   aircraft, on aircraft Fault Messages (for Post Flight Troubleshooting and Repair) and the electronic and printed manuals. This commonality permits greater ease of learning and understanding for   pilots ,   aircraft maintenance technicians , and   engineers . The Joint Aircraft System/Component (JASC) Code Tables was a modified version of the Air Transport Association of America (ATA), Specification 100 code. It was developed by the FAA's, Regulatory Support Division (AFS-600). This code table was constructed by using the new JASC code four digit format, along with an abbreviate