MCAS

E552017

MCAS (Maneuvering Characteristics Augmentation System) is an automated flight-control feature on the Boeing 737 MAX designed to adjust the aircraft’s nose-down pitch under certain conditions to improve handling characteristics.

All labels observed (1)

Label Occurrences
MCAS canonical 4

How this entity was disambiguated

Statements (48)

Predicate Object
instanceOf flight control system ⓘ
software-controlled augmentation system ⓘ
abbreviationOf Maneuvering Characteristics Augmentation System ⓘ
activationCondition flaps up configuration ⓘ
high angle of attack ⓘ
manual flight ⓘ
associatedWith Boeing 737 MAX safety crisis ⓘ
canBeOverriddenBy manual stabilizer trim wheel ⓘ
pilot use of stabilizer trim cutout switches ⓘ
certificationAuthority Federal Aviation Administration ⓘ
contributedToAccident Ethiopian Airlines Flight 302 ⓘ
Lion Air Flight 610 ⓘ
controls stabilizer trim ⓘ
controversy delegation of certification tasks to manufacturer ⓘ
insufficient disclosure to pilots before accidents ⓘ
designCharacteristic automatic repeated nose-down trim commands ⓘ
no dedicated cockpit annunciation in original design ⓘ
designedTo adjust aircraft nose-down pitch ⓘ
enhance pitch stability ⓘ
improve handling characteristics ⓘ
developedForAircraftModel Boeing 737 MAX ⓘ
documentationIssue limited mention in original flight crew operations manual ⓘ
fullName Maneuvering Characteristics Augmentation System ⓘ
implementation flight control computer software ⓘ
inputSensor angle of attack sensor ⓘ
introducedOn Boeing 737 MAX 8 ⓘ
Boeing 737 MAX 9 ⓘ
manufacturer Boeing ⓘ
operatesOn horizontal stabilizer ⓘ
operationalStatus modified and active on recertified Boeing 737 MAX aircraft ⓘ
postAccidentChange enhanced pilot training requirements ⓘ
limited authority over stabilizer movement ⓘ
limited number of repeated activations ⓘ
updated flight crew procedures ⓘ
use of two angle of attack sensors for activation logic ⓘ
primaryPurpose compensate for aerodynamic changes due to larger engines ⓘ
make 737 MAX handling similar to earlier 737 models ⓘ
regulatoryResponse EASA additional certification conditions ⓘ
FAA software modification requirements ⓘ
global grounding of Boeing 737 MAX fleet in 2019 ⓘ
relatedConcept augmentation system ⓘ
fly-by-wire control laws ⓘ
stability augmentation ⓘ
relatedTo Boeing 737 MAX design changes ⓘ
riskFactor single point of failure in original design ⓘ
safetyIssue erroneous activation due to faulty angle of attack data ⓘ
softwareUpdate Boeing 737 MAX return-to-service modifications ⓘ
timePeriodIntroduced 2010s ⓘ

How these facts were elicited

Referenced by (4)

Full triples — surface form annotated when it differs from this entity's canonical label.