A320/ Prevention Of Tailstrikes - Airbus

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A320/Preventionof tailstrikesBy: Michel PALOMEQUEA320 Flight Safety Director & Chief Engineer AdvisorA320 Program1 IntroductionLike the preceding paper on VMO/MMO exceedance, this article is a follow up on the presentationtitled “A320 ELAC” given at the last Flight SafetyConference in Barcelona on October 2007.It will look as well at the safety improvementsbrought to the ELAC in the form of the latestL84 and L93 standards, which bring additionalprevention means against tailstrikes during landing.Two other modifications will also be described,concerning the pilot awareness of a too high pitchin the landing phase.Pitch attitude limitwith MLG fully compressedPitch attitude limitwith MLG fully extended2 Description of typicaltailstrike scenarioMost of the tailstrikes on A320 family aircraft occurduring landing in manual mode (Auto Pilot OFF),when the sidestick is maintained in the aft positionafter touch down (Fig1).The importance of this subject is obviouslycorrelated to the fuselage length. It is, therefore,particularly important to A320 and A321 operators.A318A319A320A32115.7 13.9 11.7 9.7 17.3 15.5 13.5 11.2 Safety first #06 July 2008 - 1/5

NormallawFlare lawTailstrikeGround lawGround spoilersdeflection50 ft20 ft to 30 ftTouch downnThrust leversset to idleFlareA/C on the ground for5s and - θ 2.5 AFTStickFWDStickPitch sidestick ordersFigure 1: Normal landing with sidestickmaintained AFT after the touch down.3 Flight control lawimprovementIn order to avoid the above scenario, it was decidedto improve the flare law of the flight control law ofthe A320 and A321. This was done by introducinga limitation of the side stick nose up inputs duringlanding.Full UpPitch attitude commanded (deg)1816-16-2Sidestickdeflection(deg)3.1 Flare law before L84 and L93standardsThe principle is as follows: A pitch sidestick deflection corresponds to acommanded pitch attitude. The maximum commanded pitch attitude withfull back stick is 18 degrees (fig. 2).Figure 2: Flare lawbefore L84 and L93standards-22Full DownSafety first #06 July 2008 - 2/5

3.2 Flare law in L84 and L93 standardsWith the new law introduced in the latest ELAC standards (fig. 3), the maximum commanded pitchattitude on ground is limited to the values indicated in the table below:Pitch rate change 3 /s 3 /sA3209 6 A3217 4 Full UpPitch attitude commanded (deg)187 (Max limitation: pitch rate 0)4 (Max limitation: pitch rate 3%)This limitation is triggered by the ground spoilerextension, thus ensuring that it will be active onlyduring landing. It is therefore deactivated duringthe take off and go-around phases.Simulations with the improved control laws haveconfirmed the following: No impact on the landing performance The usual flare is not modified No interference in case of go-around or duringtake off due to the ground spoiler condition16-16-7.2 -4.8-2Sidestickdeflection(deg)-22Full DownFigure 3: A321 pitchattitude control lawon groundELAC hardwareELAC softwareMod. numberService BulletinA or A’L84 standard38105Not yet availableBL93 standard3800827-1182Safety first #06 July 2008 - 3/5

4 Additional alertsto impeding tailstrikeIn order to further increase pilot awareness to animpeding tailstrike, the following modifications havebeen developed for the A320 and A321: A pitch limit indicator on the Primary Flight Display,which is displayed at landing (below 400 feetAGL in both manual and automatic modes)when the thrust levers are below the FLEX/MCTsetting.Pitch limit indicatoron PFD“Pitch, Pitch”audio call-outNote: due to the below FLEX/MCT condition,the pitch limit indicator is not displayedduring the T/O phase.(This modification is available onlyfor aircraft with the EIS2 standard) A “PITCH, PITCH” call out, activated when thepitch is greater than a certain threshold and ifTOGA is not selected.(Th

Most of the tailstrikes on A320 family aircraft occur during landing in manual mode (Auto Pilot OFF), when the sidestick is maintained in the aft position after touch down (Fig1). The importance of this subject is obviously correlated to the fuselage length. It is, therefore, particularly important to A320 and A321 operators. A318 A319 A320 A321

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