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** ON A/C POST SB 31-1319 for A/C 025-025, 027-028, 108-109, 452-452
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| ** ON A/C
POST SB 31-1319 for A/C 025-025, 027-028, 108-109, 452-452 POST SB 31-1391 for A/C 025-025, 027-028, 108-109, 452-452 EMB SB 31-1168 for A/C 108-109 EMB SB 31-1179 for A/C 108-109 (5)
Load Report Logic <15> +----------------------------------------------------------------------+ Customer : AEE Type : A318/A319/A320/A321 Rev. Date : Aug 01, 2017 Manual : AMM Selected applicability : ALL 31-37-51 PB 001 CONF 00 - AIDS - STRUCTURE REPORTS - DESCRIPTION AND OPERATION Print Date: September 27, 2018 Page 55 of 83 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT. !Code!Item ! !Progr.!Standard ! ! No.!No. ! Description of Function Item !MCDU !Value ! !----!------!-----------------------------------------!------!---------! ! !A ! Report Format ! ! ! ! ! ! ! ! ! ! !B ! Parameter Table ! ! ! ! ! ! ! ! ! ! !C ! First three lines of Report ! ! Blank ! ! ! ! ! ! ! ! !D ! Print Out Rules ! C ! PH10 see! ! ! ! (PH9,PH10, Immediately, Manually) ! ! separate! ! ! ! ! ! list ! ! !E ! Transfer to ACARS MU (yes/no) ! C ! see ! ! ! ! ! ! separate! ! ! ! ! ! list ! ! !F ! Increment of the report counter (yes/no)! C ! Yes ! ! ! ! ! ! ! ! !G ! Inhibit report triggers (yes/no) ! C ! No ! ! ! ! ! ! ! ! !H ! 'Y15.0' sec before land/event A320! C ! 1 ! ! ! ! A321! C ! 1 ! ! ! ! A319! C ! 1 ! ! ! ! A318! C ! 1 ! ! ! ! ! ! ! ! !I ! 'Y15.1' sec before land/event A320! C ! 1 ! ! ! ! A321! C ! 1 ! ! ! ! A319! C ! 1 ! ! ! ! A318! C ! 1 ! ! ! ! ! ! ! ! !J ! 'Y15.2' sec after land/event A320! C ! 3 ! ! ! ! A321! C ! 3 ! ! ! ! A319! C ! 3 ! ! ! ! A318! C ! 3 ! ! ! ! ! ! ! ! !K ! 'Y15.3' sec before bounced A320! C ! 1 ! ! ! ! A321! C ! 1 ! ! ! ! A319! C ! 1 ! ! ! ! A318! C ! 1 ! ! ! ! ! ! ! ! !L ! 'Y15.4' sec before bounced A320! C ! 1 ! ! ! ! A321! C ! 1 ! ! ! ! A319! C ! 1 ! ! ! ! A318! C ! 1 ! ! ! ! ! ! ! ! !M ! 'Y15.5' sec after bounced A320! C ! 3 ! ! ! ! A321! C ! 3 ! ! ! ! A319! C ! 3 ! ! ! ! A318! C ! 3 ! ! ! ! ! ! ! ! !N ! N dataset time (sample) at landing ! C ! 1 ! ! ! ! to check for RALR trigger ! ! ! ! ! ! Note: -N dataset time is programmable ! ! ! ! ! ! from 0 to 5. ! ! ! ! ! ! -1 sample is 1/16 second (16 Hz) ! ! ! Customer : AEE Type : A318/A319/A320/A321 Rev. Date : Aug 01, 2017 Manual : AMM Selected applicability : ALL 31-37-51 PB 001 CONF 00 - AIDS - STRUCTURE REPORTS - DESCRIPTION AND OPERATION Print Date: September 27, 2018 Page 56 of 83 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT. !----!------!-----------------------------------------!------!---------! !1000! ! Not applicable ! ! ! !----!------!-----------------------------------------!------!---------! !2000! ! Not applicable ! ! ! !----!------!-----------------------------------------!------!---------! !3000!3 ! Programmable Start Logic ! ! ! ! !3.1 ! Logic algorithm ! ! ! ! !3.2 ! Logic criteria values ! !not prog.! !----!------!-----------------------------------------!------!---------! ! ! ! The parameters which are used for logic ! ! ! ! ! ! items described as follows are observed ! ! ! ! ! ! with a rate of 16 Hz. ! ! ! ! ! ! Exceptions: ! ! ! ! ! ! At landing (0.5 sec before and 0.5 sec ! ! ! ! ! ! after landing or bounce), the non- ! ! ! ! ! ! filtered acceleration VRTA and the non- ! ! ! ! ! ! filtered landing gear status (see to ! ! ! ! ! ! item no. 4.7) are observed with a rate ! ! ! ! ! ! of 32 Hz. ! ! ! !----!------!-----------------------------------------!------!---------! ! !4 ! Report is generated if one of the ! ! ! ! ! ! following logic items is present during ! ! ! ! ! ! landing: ! ! ! !4100! ! RALR < RALRL ! ! ! ! ! ! calculated between Start Sample Number ! ! ! ! ! ! S1 and Stop Sample Number S2 ! ! ! ! ! ! or ! ! ! !4400! ! VRTA > VRTAL1.1 ! ! ! ! ! ! (during +/- 0.5 seconds before and after! ! ! ! ! ! landing) calculated between Start ! ! ! ! ! ! Sample Number S3 and Stop Sample ! ! ! ! ! ! Number S4 ! ! ! ! ! ! or ! ! ! !4800! ! GW > GWL (at landing) and RALR < RALRLG ! ! ! ! ! ! (at dataset time at landing (see item ! ! ! ! ! ! no. L)). ! ! ! ! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! ! ! ! ! GWL4) is taken depending on if an ! ! ! ! ! ! aircraft is equipped with or without ACT! ! ! ! ! ! (Additional Center Tanks). ! ! ! ! ! ! ! ! ! ! ! ! Logic for ACT detection ! ! ! ! ! ! GW ! ! ! ! ! ! FWC 26.1.276.01.26 26.1.276.01.27 Limit! ! ! ! ! ! 26.1.276.10.26 26.1.276.10.27 ! ! ! ! ! ! ! ! ! ! ! ! 0 0 GWL1 ! ! ! ! ! ! 1 0 GWL2 ! ! ! ! ! ! 0 1 GWL3 ! ! ! ! ! ! 1 1 GWL4 ! ! ! ! ! ! ! ! ! ! ! ! or ! ! ! ! ! ! ! ! ! !4900! ! GW > GWL (at landing) and VRTA > VRTALG ! ! ! Customer : AEE Type : A318/A319/A320/A321 Rev. Date : Aug 01, 2017 Manual : AMM Selected applicability : ALL 31-37-51 PB 001 CONF 00 - AIDS - STRUCTURE REPORTS - DESCRIPTION AND OPERATION Print Date: September 27, 2018 Page 57 of 83 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT. ! ! ! (during +/- 0.5 sec before and after ! ! ! ! ! ! landing). ! ! ! ! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! ! ! ! ! GWL4) is taken depending on if an ! ! ! ! ! ! aircraft is equipped with or without ACT! ! ! ! ! ! (Additional Center Tanks). Logic for ACT! ! ! ! ! ! detection like Code No. 4800. ! ! ! ! ! ! ! ! ! !4500! ! Report will be generated if one of the ! ! ! ! ! ! following logic items is present during ! ! ! ! ! ! the bouncing: ! ! ! ! ! ! ! ! ! ! ! ! VRTA > VRTAL1.2 during +/- 0.5 sec at ! ! ! ! ! ! landing (1st touchdown) ! ! ! ! ! ! ! ! ! ! ! ! or ! ! ! ! ! ! ! ! ! ! ! ! VRTA > VRTAL1.3 during +/- 0.5 sec at ! ! ! ! ! ! landing (2nd touchdown). ! ! ! ! ! ! ! ! ! ! !4.1 ! RALRL limit (ft/sec) A320 ! C ! -9.0 ! ! ! ! A321 ! C ! -9.0 ! ! ! ! A319 ! C ! -9.0 ! ! ! ! A318 ! C ! -9.0 ! ! !4.2 ! RALT ! ! ! ! !4.2.1 ! RALTL1 limit (ft) A320 ! C ! 150.0 ! ! ! ! A321 ! C ! 150.0 ! ! ! ! A319 ! C ! 150.0 ! ! ! ! A318 ! C ! 150.0 ! ! !4.3 ! RALR ! ! ! ! !4.3.1 ! D geometrical correction factor for ! ! ! ! ! ! ROLR (ft/deg) A320 ! C ! 0.0 ! ! ! ! A321 ! C ! 0.0 ! ! ! ! A319 ! C ! 0.0 ! ! ! ! A318 ! C ! 0.0 ! ! !4.3.2 ! DX lever arm correction (x-axis) ! ! ! ! ! ! for R/A RALT (ft) A320 ! C ! 18.0 ! ! ! ! A321 ! C ! 28.8 ! ! ! ! A319 ! C ! 18.5 ! ! ! ! A318 ! C ! 16.8 ! ! !4.3.3 ! DZ lever arm correction (z-axis) ! ! ! ! ! ! for R/A RALT (ft) A320 ! C ! 7.1 ! ! ! ! A321 ! C ! 7.8 ! ! ! ! A319 ! C ! 7.2 ! ! ! ! A318 ! C ! 7.6 ! ! !4.3.4 ! DXTPIR lever arm correction (x-axis) ! ! ! ! ! ! for PTCH (ft) A320 ! C ! 39.0 ! ! ! ! A321 ! C ! 53.1 ! ! ! ! A319 ! C ! 33.8 ! ! ! ! A318 ! C ! 29.5 ! ! ! ! ! ! ! ! !4.3.5 ! FC filter frequency (Hz) A320 ! C ! 0.3 ! ! ! ! A321 ! C ! 0.3 ! ! ! ! A319 ! C ! 0.3 ! Customer : AEE Type : A318/A319/A320/A321 Rev. Date : Aug 01, 2017 Manual : AMM Selected applicability : ALL 31-37-51 PB 001 CONF 00 - AIDS - STRUCTURE REPORTS - DESCRIPTION AND OPERATION Print Date: September 27, 2018 Page 58 of 83 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT. ! ! ! A318 ! C ! 0.3 ! ! ! ! ! ! ! ! !4.3.6 ! K1 filter constant A320 ! C ! 5.2 ! ! ! ! A321 ! C ! 5.2 ! ! ! ! A319 ! C ! 5.2 ! ! ! ! A318 ! C ! 5.2 ! ! ! ! ! ! ! ! !4.3.7 ! K2 filter constant A320 ! C ! 25.0 ! ! ! ! A321 ! C ! 25.0 ! ! ! ! A319 ! C ! 25.0 ! ! ! ! A318 ! C ! 25.0 ! ! ! ! ! ! ! ! !4.3.8 ! K3 filter constant A320 ! C ! 5.0 ! ! ! ! A321 ! C ! 5.0 ! ! ! ! A319 ! C ! 5.0 ! ! ! ! A318 ! C ! 5.0 ! ! ! ! ! ! ! ! !4.3.9 ! THETA0 (averaged pitch at A320 ! C ! 6.0 ! ! ! ! touchdown) deg A321 ! C ! 4.5 ! ! ! ! A319 ! C ! 2.0 ! ! ! ! A318 ! C ! 6.0 ! ! ! ! ! ! ! ! !4.3.10! S1 (sample) A320 ! C ! -4.0 ! ! ! ! A321 ! C ! -4.0 ! ! ! ! A319 ! C ! -4.0 ! ! ! ! A318 ! C ! -4.0 ! ! ! ! ! ! ! ! !4.3.11! S2 (sample) A320 ! C ! 4.0 ! ! ! ! A321 ! C ! 4.0 ! ! ! ! A319 ! C ! 4.0 ! ! ! ! A318 ! C ! 4.0 ! ! ! ! ! ! ! ! !4.4 ! VRTAL1.1 limit at landing (g) A320 ! C ! 2.6 ! ! ! ! A321 ! C ! 2.6 ! ! ! ! A319 ! C ! 2.6 ! ! ! ! A318 ! C ! 2.6 ! ! ! ! ! ! ! ! !4.4.1 ! S3 (sample) A320 ! C ! -16 ! ! ! ! A321 ! C ! -16 ! ! ! ! A319 ! C ! -16 ! ! ! ! A318 ! C ! -16 ! ! ! ! ! ! ! ! !4.4.2 ! S4 (sample) A320 ! C ! 16 ! ! ! ! A321 ! C ! 16 ! ! ! ! A319 ! C ! 16 ! ! ! ! A318 ! C ! 16 ! ! ! ! ! ! ! ! !4.5 ! VRTAL1.2 limit at landing-1st touchdown ! ! ! ! ! ! from bounced land/event (g) A320 ! C ! 2.6 ! ! ! ! A321 ! C ! 2.6 ! ! ! ! A319 ! C ! 2.6 ! ! ! ! A318 ! C ! 2.6 ! ! ! ! ! ! ! ! !4.5.1 ! VRTAL1.3 limit at bounce (2nd touchdown)! ! ! Customer : AEE Type : A318/A319/A320/A321 Rev. Date : Aug 01, 2017 Manual : AMM Selected applicability : ALL 31-37-51 PB 001 CONF 00 - AIDS - STRUCTURE REPORTS - DESCRIPTION AND OPERATION Print Date: September 27, 2018 Page 59 of 83 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT. ! ! ! from bounced land/event (g) A320 ! C ! 2.6 ! ! ! ! A321 ! C ! 2.6 ! ! ! ! A319 ! C ! 2.6 ! ! ! ! A318 ! C ! 2.6 ! ! !4.6 ! GW Overweight landing ! ! ! ! !4.6.1 ! GWL1, GWL2, GWL3, GWL4 limit (kg) A320 ! C ! 64500 ! ! ! ! A321 ! C ! 73500 ! ! ! ! A319 ! C ! 61000 ! ! ! ! A318 ! C ! 56000 ! ! ! ! ! ! ! ! !4.6.2 ! RALRLG limit (ft/sec) A320 ! C ! -6.0 ! ! ! ! A321 ! C ! -6.0 ! ! ! ! A319 ! C ! -6.0 ! ! ! ! A318 ! C ! -6.0 ! ! ! ! ! ! ! ! !4.6.3 ! VRTALG limit (g) A320 ! C ! 1.7 ! ! ! ! A321 ! C ! 1.7 ! ! ! ! A319 ! C ! 1.7 ! ! ! ! A318 ! C ! 1.7 ! ! ! ! ! ! ! ! !4.7 ! Landing detection ! ! ! ! ! ! Landing is detected when in PH7 or PH8 ! ! ! ! ! ! 6D.1.021.01.13 = 1 (LH gear) ! ! ! ! ! ! or ! ! ! ! ! ! 6D.1.021.01.14 = 1 (RH gear) ! ! ! ! ! ! ! ! ! ! !4.8 ! Bounced landing detection ! ! ! ! ! ! A bounced landing is detected when in ! ! ! ! ! ! PH7 or PH8 parameter 6D.1.021.01.11 is ! ! ! ! ! ! set to 1 for longer than 'Y15.6'*(1/32) ! ! ! ! ! ! seconds ! ! ! ! ! ! and ! ! ! ! ! ! then one or both of 6D.1.021.01.13 or ! ! ! ! ! ! 6D.1.021.01.14 is set to 0 for longer ! ! ! ! ! ! than 'Y15.7'*(1/32) seconds ! ! ! ! ! ! and ! ! ! ! ! ! then the one which was set to 0 or the ! ! ! ! ! ! first one of 6D.1.021.01.13 or ! ! ! ! ! ! 6D.1.021.01.14 is set to 1 again within ! ! ! ! ! ! within 'Y15.8'*(1/32) seconds. ! ! ! ! ! ! ! ! ! ! !4.9 ! 'Y15.6' landing gear compress time ! ! ! ! ! ! (1st touchdown) (sample) A320 ! ! 16 ! ! ! ! A321 ! ! 16 ! ! ! ! A319 ! ! 16 ! ! ! ! A318 ! ! 16 ! ! ! ! ! ! ! ! !4.10 ! 'Y15.7' time between bounces (sample) ! ! ! ! ! ! A320 ! ! 32 ! ! ! ! A321 ! ! 32 ! ! ! ! A319 ! ! 32 ! ! ! ! A318 ! ! 32 ! ! ! ! ! ! ! ! !4.11 ! 'Y15.8' landing gear compress time ! ! ! Customer : AEE Type : A318/A319/A320/A321 Rev. Date : Aug 01, 2017 Manual : AMM Selected applicability : ALL 31-37-51 PB 001 CONF 00 - AIDS - STRUCTURE REPORTS - DESCRIPTION AND OPERATION Print Date: September 27, 2018 Page 60 of 83 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT. ! ! ! (2nd touchdown) (sample) A320 ! ! 320 ! ! ! ! A321 ! ! 320 ! ! ! ! A319 ! ! 320 ! ! ! ! A318 ! ! 320 ! ! ! ! NOTE: 1 sample is 1/32 second (32 Hz) ! ! ! !----!------!-----------------------------------------!------!---------! ! !5 ! Report is generated if one of the ! ! ! ! ! ! following logic items is present during ! ! ! ! ! ! flight (PH5, 5.1, 6, 7, 7.1). There is a! ! ! ! ! ! spacing time TURBWAIT (sec.) to enable ! ! ! ! ! ! the trigger logic again after the ! ! ! ! ! ! previous report generation. ! ! ! ! ! ! ! ! ! !5100!5.1 ! VRTA > VRTAL2.1 if FLAP < FLAPL ! ! ! ! ! ! ! ! ! !5200!5.2 ! VRTA < VRTAL2.2 if FLAP < FLAPL ! ! ! ! ! ! ! ! ! !5300!5.3 ! VRTA > VRTAL2.3 if FLAP >= FLAPL OR ! ! ! ! ! ! VRTA < VRTAL2.4 if FLAP >= FLAPL ! ! ! ! ! ! ! ! ! ! ! ! Limitation for Code 5100, 5200, 5300: ! ! ! ! ! ! W15 TURBWAIT spacing time for re- ! ! ! ! ! ! activating the trigger logic after the ! ! ! ! ! ! previous report generation within the ! ! ! ! ! ! same flight leg. ! ! ! ! ! ! ! ! ! !5400!5.4 ! If one of the 5 spoiler excursion ! ! ! ! ! ! counters has an overflow (999 is ! ! ! ! ! ! reached). ! ! ! ! ! ! ! ! ! ! !5.5 ! VRTAL2.1 limit (g) A320 ! C ! 2.5 ! ! ! ! A321 ! C ! 2.5 ! ! ! ! A319 ! C ! 2.5 ! ! ! ! A318 ! C ! 2.5 ! ! ! ! ! ! ! ! !5.6 ! VRTAL2.2 limit (g) A320 ! C ! -1.0 ! ! ! ! A321 ! C ! -1.0 ! ! ! ! A319 ! C ! -1.0 ! ! ! ! A318 ! C ! -1.0 ! ! ! ! ! ! ! ! !5.7 ! VRTAL2.3 limit (g) A320 ! C ! 2.0 ! ! ! ! A321 ! C ! 2.0 ! ! ! ! A319 ! C ! 2.0 ! ! ! ! A318 ! C ! 2.0 ! ! ! ! ! ! ! ! !5.8 ! VRTAL2.4 limit (g) A320 ! C ! 0.0 ! ! ! ! A321 ! C ! 0.0 ! ! ! ! A319 ! C ! 0.0 ! ! ! ! A318 ! C ! 0.0 ! ! ! ! ! ! ! ! !5.9 ! TURBWAIT (sec.) A320 ! C ! 10 ! ! ! ! A321 ! C ! 10 ! ! ! ! A319 ! C ! 10 ! ! ! ! A318 ! C ! 10 ! Customer : AEE Type : A318/A319/A320/A321 Rev. Date : Aug 01, 2017 Manual : AMM Selected applicability : ALL 31-37-51 PB 001 CONF 00 - AIDS - STRUCTURE REPORTS - DESCRIPTION AND OPERATION Print Date: September 27, 2018 Page 61 of 83 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT. ! ! ! ! ! ! ! !5.10 ! FLAPL (deg) A320 ! C ! 0.5 ! ! ! ! A321 ! C ! 0.5 ! ! ! ! A319 ! C ! 0.5 ! ! ! ! A318 ! C ! 0.5 ! !----!------!-----------------------------------------!------!---------! !8100!8.1 !ACARS MU uplink request with IMI 'REQ15':! ! ! ! ! !The report <15> is immediately generated ! ! ! ! ! !and transmitted to the ACARS MU ! ! ! !----------------------------------------------------------------------! ! A = Programmable by Airbus ! ! C = Programmable by Customer ! +----------------------------------------------------------------------+
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