EASA: Problemi di pitch eccessivo anche per l’A320 NEO


TW 843

Senior Member
6 Novembre 2005
32,801
786
0
49
Azionista LibertyLines
CIVIL AVIATION
EASA finds excessive pitch issue in second Airbus A320 family jet

The Airbus A320neo has been found to be potentially subject to an angle-of-attack protection weakness, which, under certain circumstances, could lead to excessive pitch and higher flight crew workload conditions. The notification by the European Union Aviation Safety Agency (EASA) comes weeks after a similar excessive pitch anomaly was discovered on the A321neo.

The Airbus A320neo has been found to be potentially subject to an angle-of-attack protection weakness, which, under certain circumstances, could lead to excessive pitch and higher flight crew workload conditions. The notification by the European Union Aviation Safety Agency (EASA) comes weeks after a similar excessive pitch anomaly was discovered on the A321neo.

According to the Airworthiness Directive (AD), issued by the EASA on July 31, 2019, a “reduced efficiency” of the A320neo angle-of-attack (AOA) protection under certain flight configurations, and in combination with specific commanded maneuvers from the flight crew, could lead to excessive pitch attitudes, possibly resulting in increased workload.

This “potentially unsafe” condition, although never encountered during operations, was discovered during analysis and laboratory testing of the A320neo flight control laws, the EASA says.

Airbus has issued temporary revisions to the A320neo flight manual (AFM TR) to address the situation, and the EASA has ordered operators of the type to revise their manuals accordingly. The revisions limit the center-of-gravity envelope for the plane. In addition, the manufacturer has provided loading recommendations.

The regulator’s instructions for the type come after a similar issue was found in another member of the Airbus A320 Family, the A321neo. In that case, Airbus’ temporary revisions to the A321neo flight manuals were necessitated after analysis of the elevator and aileron computer installed on the aircraft. A behavior anomaly in these computer units was also found to potentially lead to an excessive pitch scenario.

In the AD, issued by the EASA on July 17, 2019, operators of the A321neo were also urged to update their flight manuals according to temporary revisions developed by Airbus. The directive, considered as an “interim action”, has since been revised and published again on July 31, 2019. Operators must comply with a 30 day ‘window’ starting August 7, 2019.

As for the instructions regarding the A320neo, the AD comes into effect on August 14, 2019, already, with the commentary period postponed after its publication.

Aerotime
 
Confermo, sono terribilmente pesanti nel "posteriore", VY ad esempio ha emesso da poco delle procedure specifiche per i loro NEO, riguardo accettazone passeggeri e carico bagagli (sostanzialmente tutto davanti!)
 
Confermo, sono terribilmente pesanti nel "posteriore", VY ad esempio ha emesso da poco delle procedure specifiche per i loro NEO, riguardo accettazone passeggeri e carico bagagli (sostanzialmente tutto davanti!)
Non credo sia un problema di peso del "posteriore", trattasi piuttosto di una mera taratura di software, anche perché pure i CEO 186pax sono pesanti in coda se pieni e con pochi bagagli in stiva (tipo una tratta con pax medio business MXP CDG con 30 bagagli alla 1):
. Laboratory analysis by Airbus of the behaviour of the ELAC STD installed on the A320 NEO revealed that excessive pitch attitude can occur in the following conditions:
• Aircraft with actual CG of 32.5% and
• the aircraft is in CONF 1+F, 2, 3, or FULL and
• the aircraft is decelerating and
• the application of full back stick and TOGA
thrust
 
Non credo sia un problema di peso del "posteriore", trattasi piuttosto di una mera taratura di software, anche perché pure i CEO 186pax sono pesanti in coda se pieni e con pochi bagagli in stiva (tipo una tratta con pax medio business MXP CDG con 30 bagagli alla 1):

Confermo la questione legata al software dei controlli di volo. Con il nuovo ELAC Software che dovrebbe arrivare quest´inverno il problema dovrebbe essere risolto. Da sottolinerare la lista elencata da OneShot. Per far sí che il comportamento del 320/321NEO diventi eccessivo attorno all´asse laterale devono succedere tutti i punti riportati contemporaneamente..non impossibile ma abbastanza improbabile..soprattutto un input "full back" sul sidestick mentre si applica TOGA.