a320 system configuration guide
DESCRIPTION
A320 System Configuration GuideTRANSCRIPT
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Authorized by BSMC
System Configuration GuideA320 FamilyIssue 6, Revision 1January 2012Document in accordance with the following Standard Specifications:
A318-100 P 000 01000 issue 04A319-100 J 000 01000 issue 07A320-200 D 000 02000 issue 08A321-200 E 000 02000 issue 05
CC1200001
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A320 Family
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Issue 6 Revision 1, January 2012
[ REF-2]
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Is
A320 Family Table of contents
T ATAInCGPAACEEFFHIcInLLNO
38ms 46nit (APU) 49
51 52 53 55 56 57 72
ontrol 73 79
ATAitle Titletroduction 00ertification and external livery 02eneral aircraft design criteria 03lacards and markings 11ir conditioning 21uto flight 22ommunications 23lectrical power 24quipment/furnishings 25ire protection 26uel 28ydraulic power 29e and rain protection 30
Water/wasteInformation systeAuxiliary Power UStructuresDoorsFuselageStabilizersWindowsWingsEnginesEngine fuel and cOilsue 6 Page TOC-1
dicandighavixyg Revision 1, January 2012
ating/recording systems 31ing gear 32ts 33gation 34en 35
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Page TOC-2Issue 6 Revision 1, January 2012
Table of Contents
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A320 FamilyTable of contents
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Page DTOC-1Issue
Detailed table of contentsTIT Page ATA ref
A320 Family
In 1 [00]00 2 [00-2]
Ce 9 [02]02 10 [02-2]02 12 [02-4]02 16 [02-8]02 20 [02-12]02 22 [02-14]02 24 [02-16]02 30 [02-22]02 32 [02-24]02 / PFC 34 [02-26]
02 36 [02-28]
Ge 39 [03]03 40 [03-2]03 44 [03-6] 6 Revision 1, January 2012
LE
troduction .00.200 - Introduction
rtification and external livery .10.104 - Certification of dynamically tested passenger seats .10.111 - Compliance with FAA type certification requirements .10.112 - Partial compliance with FAA type certification requirements .10.120 - 15 knots tailwind certification .10.123 - Operation on runways with reduced width .10.190 - ETOPS 120/180 min .12.122 - Compliance status with EU-OPS 1 .12.123 - Compliance with CS25/FAR 25.562 (Head Injury Criteria - HIC) .12.130 - EASA certification of Take Off/Landing operation on wet grooved
runways .40.101 - External livery
neral aircraft design criteria .20.300 - Design weights (A318) .20.400 - Design weights (A319)
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Page DTOC-2Issue
DDetailed table of contents A320 FamilyTIT Page ATA ref03 48 [03-10]03 52 [03-14]
Pl 57 [11]11 58 [11-2]11 ings 60 [11-4]11 62 [11-6]11 64 [11-8]11 or warning 68 [11-12]
11 72 [11-16]11 76 [11-20]11 holds 78 [11-22]11 82 [11-26]11 86 [11-30]11 90 [11-34]
Ai 93 [21]21 94 [21-2]21 98 [21-6]21 102 [21-10] 6 Revision 1, January 2012
etailed table of contentsLE
.20.500 - Design weights (A320)
.20.600 - Design weights (A321)
acards and markings .00.124 - Installation of leasing identification plates .20.100 - Second language for door operation external placards and mark.20.110 - Second language for selected external placards and markings .20.119 - Nose Landing Gear (NLG) permanent steering markers .20.135 - Second language for residual cabin & cargo pressure exterior do
placards .21.101 - Emergency cut-out markings .22.100 - Landing gear placards .30.100 - Installation of additional access placards in forward and aft cargo.30.121 - Second language for cargo compartment placards .30.136 - US and metric units for cargo compartment height placards .33.101 - Placard for flight crew oxygen system
r conditioning .20.108 - Cabin air recirculation filter cartridges equipment selection .22.100 - Installation of electrical heaters for foot air outlets in the cockpit .26.110 - Avionics ventilation fan automatic speed reduction
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Page DTOC-3Issue
A320 Family Detailed table of contents
TIT Page ATA ref21 106 [21-14]21 110 [21-18]21 114 [21-22]21 118 [21-26]21 120 [21-28]21 124 [21-32]21 128 [21-36]
Au 131 [22]22 132 [22-2]22 134 [22-4]22 138 [22-8]22 ) 142 [22-12]
Co 145 [23]23 cator 148 [23-4]
23 152 [23-8]23 156 [23-12]23 160 [23-16]23 (SFE) 162 [23-18] 6 Revision 1, January 2012
LE .27.108 - Avionics ventilation air filter alternate equipment .28.201 - Installation of ventilation system for forward cargo hold .28.210 - Installation of ventilation system for complete aft cargo hold .41.100 - Installation of front air outlets at flight crew foot level .43.201 - Installation of heating system for forward cargo hold .43.204 - Installation of heating system for complete aft cargo hold .70.109 - Installation of ozone catalytic converters
to flight .00.104 - Automatic landing capability .70.100 - Flight Management (FM) kits alternate equipment .81.143 - Inhibition of the expedite pushbutton .82.103 - Installation of third Multipurpose Control and Display Unit (MCDU
mmunications .00.132 - Installation (based on basic common provision) of Emergency Lo
Transmitter (ELT) .11.102 - Full provision for single HF system .11.111 - Full provision for dual HF system .11.116 - Installation of single HF system (SFE) .11.131 - Installation of single HF system and full provision for second one
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Page DTOC-4Issue
DDetailed table of contents A320 FamilyTIT Page ATA ref23 166 [23-22]23 170 [23-26]23 172 [23-28]23 174 [23-30]23 178 [23-34]23 180 [23-36]23 184 [23-40]23 186 [23-42]23 188 [23-44]23 192 [23-48]23 el 196 [23-52]23 200 [23-56]23 204 [23-60]23 206 [23-62]23 210 [23-66]23 214 [23-70]23 218 [23-74]23 nt 220 [23-76]23 ply for CVR 224 [23-80]23 226 [23-82]23 Project) 228 [23-84] 6 Revision 1, January 2012
etailed table of contentsLE
.11.155 - Installation of dual HF system (SFE)
.11.167 - Additional wiring for HF Data Link (HFDL) function
.11.169 - Activation of HF Data Link (HFDL) function
.12.130 - VHF Data Radio (VDR) alternate equipment
.13.100 - Installation of alternate Radio Management Panel (RMP)
.13.101 - Installation of third Radio Management Panel (RMP)
.13.105 - Activation of RMP std 4 frequency load function
.28.170 - Installation of AERO H+/SBB SATCOM cockpit voice interface
.28.210 - Installation of SATCOM AERO H+ SRT 2100B system
.28.211 - Installation of SwiftBroadband (SBB) SATCOM system
.50.110 - Installation of additional Audio Control Panel (ACP) and jack pan
.50.135 - Installation of headset for fourth occupant
.50.138 - Cockpit hand microphone alternate equipment
.51.103 - Installation of active noise canceling boomsets (SFE)
.51.136 - Boomsets alternate equipment
.51.139 - Boomsets alternate equipment with two jack plugs
.70.110 - Installation of a video monitoring system
.71.103 - Solid State Cockpit Voice Recorder (SSCVR) alternate equipme
.71.110 - Recorder Independent Power Supply (RIPS) - 28VDC power sup
.71.120 - System provision for CVR capable of data link recording
.73.200 - Installation of cockpit and cabin alert switches (Aircraft Security
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Page DTOC-5Issue
A320 Family Detailed table of contents
TIT Page ATA ref
El 231 [24]24 ith batteries 232 [24-2]
Eq 235 [25]25 238 [25-4]25 240 [25-6]25 244 [25-10]25 e door area 248 [25-14]25 252 [25-18]25 254 [25-20]25 lds 258 [25-24]25 ard and aft 262 [25-28]
25 d cargo hold 268 [25-34]
25 d cargo hold 272 [25-38]
25 old - sliding 274 [25-40] 6 Revision 1, January 2012
LE
ectrical power .55.101 - Passenger Address (PA) power supply in emergency condition w
OFF
uipment/furnishings .10.108 - Installation of paper holder on the glareshield .11.102 - Pilot seats alternate covers - sheepskin .11.208 - Installation of fourth occupant seat in cockpit .27.100 - Installation of heated floor panels for fwd passenger/crew/servic.27.101 - Installation of On/off switch for heated floor panels .50.137 - Rubber seal profile for cargo compartment floor panels .50.510 - Basic full bulk configuration selection in forward and aft cargo ho.50.520 - Installation of reinforced floor panels for heavy bulk usage in forw
cargo holds .52.190 - System provision for mechanized bulk loading systems in forwar
(A320) .52.191 - System provision for mechanized bulk loading systems in forwar
(A321) .52.202 - Installation of mechanized bulk loading system in forward cargo h
carpet system
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Page DTOC-6Issue
DDetailed table of contents A320 FamilyTIT Page ATA ref25 go hold 278 [25-44]
25 go hold 282 [25-48]
25 - sliding 284 [25-50]
25 ward and aft 288 [25-54]
25 argo holds 294 [25-60]
25 298 [25-64]25 ty in fwd and 300 [25-66]
25 Ds (A319) 304 [25-70]25 , door area 308 [25-74]
25 312 [25-78]25 316 [25-82]
Fi 319 [26]26 320 [26-2]26 324 [26-6] 6 Revision 1, January 2012
etailed table of contentsLE
.52.204 - System provision for mechanized bulk loading systems in aft car(A319/A320)
.52.205 - System provision for mechanized bulk loading systems in aft car(A321)
.52.212 - Installation of mechanized bulk loading system in aft cargo hold carpet system
.52.304 - Installation of semi-automatic Cargo Loading System (CLS) in forcargo holds (A320/A321)
.52.310 - Fixed provision for occasional bulk capability in forward and aft c(A320/A321)
.52.315 - Full electrical provision for semi-automatic CLS
.52.404 - Installation of Cargo Loading System (CLS) with full bulk capabiliaft cargo holds
.52.407 - Bulk loading capability in aft cargo hold door area behind two UL
.52.410 - Full provision for installation of special container in aft cargo hold(A319)
.52.500 - Installation of continuous side guides in forward cargo hold
.52.511 - Installation of continuous side guides in aft cargo hold
re protection .20.103 - Auxiliary Power Unit (APU) fire extinguisher alternate equipment.21.104 - Engine fire extinguishers alternate equipment
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Page DTOC-7Issue
A320 Family Detailed table of contents
TIT Page ATA ref26 328 [26-10]26 min 330 [26-12]26 min 334 [26-16]
Fu 337 [28]28 ) in aft cargo 338 [28-2]
28 ACTs) in aft 342 [28-6]
28 346 [28-10]28 ld 352 [28-16]28 356 [28-20]28 360 [28-24]28 364 [28-28]
Hy 367 [29]29 368 [29-2]29 372 [29-6] 6 Revision 1, January 2012
LE .23.103 - Cargo holds fire extinguisher alternate equipment .23.111 - Cargo holds fire extinguishers extended duration for ETOPS 120.23.112 - Cargo holds fire extinguishers extended duration for ETOPS 180
el .11.133 - Full provision for installation of one Additional Center Tank (ACT
hold .11.140 - Full provision for installation of two/one Additional Center Tanks (
cargo hold .11.225 - Installation of one Additional Center Tank (ACT) in aft cargo hold.11.235 - Installation of two Additional Center Tanks (ACTs) in aft cargo ho.25.107 - Installation of additional refuel/defuel coupling in LH wing .25.110 - Installation of fuel quantity preselector in cockpit .25.130 - Relocation of refuel/defuel control panel
draulic power .10.110 - Hydraulic Engine Driven Pumps (EDPs) alternate equipment .21.104 - Electropumps alternate equipment
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Page DTOC-8Issue
DDetailed table of contents A320 FamilyTIT Page ATA refIce 375 [30]30 376 [30-2]30 380 [30-6]30 382 [30-8]
In 387 [31]31 388 [31-2]31 392 [31-6]31 quipment 396 [31-10]31 402 [31-16]31 406 [31-20]31 410 [31-24]31 412 [31-26]31 416 [31-30]31 420 [31-34]31 isplay (ND) 422 [31-36]
La 425 [32]32 426 [32-2]32 nt 430 [32-6] 6 Revision 1, January 2012
etailed table of contentsLE and rain protection
.41.102 - Installation of intermittent function of windshield wipers
.70.108 - Extended freezing protection
.81.105 - Installation of dual advisory ice detection system
dicating/recording systems .00.107 - US units for indicators and labels .14.103 - Overhead panel toggle switches re-orientation .33.051 - Flight Data Interface and Management Unit (FDIMU) alternate e.33.132 - Installation of Quick Access Recorder (QAR/WGL-QAR) .33.200 - Solid State Flight Data Recorder (SSFDR) alternate equipment .33.210 - Digital Flight Data Recorder System (DFDRS) capabilities .36.161 - Installation of Digital AIDS Recorder (DAR/WGL-DAR) (BFE) .60.114 - Indication of metric altitude on Primary Flight Display (PFD) .60.120 - Installation of Electronic Instrument System (EIS2) .65.100 - Activation of Minimum Off Route Altitude (MORA) on Navigation D
nding gear .40.113 - Wheels and brakes alternate equipment .41.111 - Main Landing Gear (MLG) tires selection and alternate equipme
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Page DTOC-9Issue
A320 Family Detailed table of contents
TIT Page ATA ref32 434 [32-10]32 438 [32-14]32 eel 442 [32-18]
Li 445 [33]33 lighting) 446 [33-2]33 448 [33-4]33 450 [33-6]
Na 453 [34]34 456 [34-4]34 460 [34-8]34 464 [34-12]34 468 [34-16]34 472 [34-20]34 476 [34-24]34 em 478 [34-26]34 480 [34-28]34 484 [34-32]34 488 [34-36] 6 Revision 1, January 2012
LE .41.120 - Nose Landing Gear (NLG) tires selection .48.200 - Installation of universal brake cooling fans .49.109 - Installation of Tire Pressure Indicating System (TPIS) on twin wh
ghts .12.109 - Changes in cockpit illumination (excluding instrument and panel.43.000 - Runway turnoff lights .46.000 - Taxi and take-off lights
vigation .00.108 - QNH/QFE BARO setting .13.105 - Installation of aspirated Total Air Temperature (TAT) probes .13.106 - Pitot probes alternate equipment .15.101 - Angle Of Attack (AOA) sensors alternate equipment .20.203 - Integrated Standby Instrument System (ISIS) optional functions .35.109 - System provision for Head Up Display (HUD) system installation.35.110 - Installation (based on provision) of Head Up Display (HUD) syst.41.302 - Full single Weather Radar (WXR) system alternate equipment .41.310 - Installation of dual Weather Radar (WXR) System .42.101 - Radio altimeters alternate equipment
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Page DTOC-10Issue
DDetailed table of contents A320 FamilyTIT Page ATA ref34 492 [34-40]34 quipment 496 [34-44]
34 500 [34-48]34 502 [34-50]34 504 [34-52]34 ) 506 [34-54]34 508 [34-56]34 ate 510 [34-58]
34 e warnings 512 [34-60]34 al functions 514 [34-62]34 uipment 516 [34-64]34 520 [34-68]34 tion 522 [34-70]34 524 [34-72]34 m 528 [34-76]34 ent 532 [34-80]34 536 [34-84]34 quipment 540 [34-88]34 544 [34-92]34 548 [34-96] 6 Revision 1, January 2012
etailed table of contentsLE
.42.117 - Radio altitude automatic call-outs
.43.203 - Traffic Alert and Collision Avoidance System (TCAS) alternate e(SFE)
.43.250 - Installation of T2CAS
.43.260 - T2CAS - Activation of alternate warnings
.43.270 - Wiring provision for T3CAS
.43.290 - Wiring provision for Aircraft Traffic Situation Awareness (ATSAW
.43.295 - Activation of ATSAW function
.48.124 - Enhanced Ground Proximity Warning System (EGPWS) - alternequipment
.48.127 - Enhanced Ground Proximity Warning System (EGPWS) alternat
.48.132 - Enhanced Ground Proximity Warning System (EGPWS) - option
.51.101 - Distance Measuring Equipment (DME) interrogators alternate eq
.52.117 - Automatic Dependent Surveillance - Broadcast (ADS-B OUT)
.52.133 - Compliance with European enhanced surveillance (EHS) regula
.52.140 - Air Traffic Control (ATC) control panel alternate equipment
.53.109 - Full provision for second Automatic Direction Finder (ADF) syste
.53.111 - Single Automatic Direction Finder (ADF) system alternate equipm
.53.119 - Installation of dual Automatic Direction Finder (ADF) system
.55.102 - VHF Omnidirectional Range (VOR)/Marker receivers alternate e
.58.313 - Multi Mode Receiver (MMR) alternate equipment
.58.316 - Activation of GLS function
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Page DTOC-11Issue
A320 Family Detailed table of contents
TIT Page ATA ref34 550 [34-98]34 MR 552 [34-100]
Ox 555 [35]35 inder 556 [35-2]35 560 [35-6]35 564 [35-10]35 566 [35-12]35 570 [35-16]
W 573 [38]38 574 [38-2]38 zation 576 [38-4]
In 579 [46]46 tion (AOC) 580 [46-2]
46 584 [46-6]46 586 [46-8] 6 Revision 1, January 2012
LE .58.317 - Activation of FLS function .58.340 - Installation of MLS function for cat IIIb operation hosted by the M
ygen .11.102 - Installation of in-situ replenishment facility for cockpit oxygen cyl.11.201 - Cockpit oxygen cylinder alternate equipment .20.010 - Installation of four oxygen masks per box .20.113 - Extended supply duration for passenger chemical oxygen system.20.114 - Extended supply duration for passenger gaseous oxygen system
ater/waste .10.104 - Installation of water conditioner in potable water system .41.101 - Installation of auxiliary compressor in the potable water pressuri
system
formation systems .21.102 - Installation of AIRBUS standard Airline Operational Communica
software for ATSU .21.105 - Activation of ARINC 623 ATS applications in the ATSU .21.111 - Activation of VHF Data Link (VDL) Mode 2 function
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Page DTOC-12Issue
DDetailed table of contents A320 FamilyTIT Page ATA ref46 588 [46-10]46 590 [46-12]
Au 593 [49]49 594 [49-2]
St 597 [51]51 598 [51-2]51 604 [51-8]51 (3 coats) 608 [51-12]
Do 611 [52]52 612 [52-2]52 itions) 616 [52-6]52 618 [52-8]
Fu 621 [53]53 622 [53-2]53 626 [53-6] 6 Revision 1, January 2012
etailed table of contentsLE
.21.140 - Installation of Future Air Navigation System (FANS) A+
.21.142 - Installation of Future Air Navigation System (FANS) B+
xiliary Power Unit (APU) .00.105 - Auxiliary Power Unit (APU) alternate equipment
ructures .00.115 - Fuselage and wings extended corrosion prevention .22.250 - External livery decorative adhesive film .22.710 - Alternate paint system (CF primer/strippable) on standard areas
ors .22.200 - Installation of additional emergency exits (A319) .51.100 - Installation of cockpit door release back-up system (MMEL cond.51.106 - Installation of modified door lock mechanism
selage .30.050 - Belly fairing panels - extrusion strips .35.100 - Ram air inlet leading edge protection
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Page DTOC-13Issue
A320 Family Detailed table of contents
TIT Page ATA refSt 629 [55]55 e 630 [55-2]
W 633 [56]56 634 [56-2]
W 639 [57]57 640 [57-2]57 642 [57-4]
En 645 [72]72 646 [72-2]72 650 [72-6]72 654 [72-10]72 658 [72-14]
En 661 [73]73 662 [73-2] 6 Revision 1, January 2012
LE abilizers .30.101 - Installation of erosion protection on vertical stabilizer leading edg
indows .10.102 - Cockpit windows alternate equipment
ings .40.100 - Leading edge and leading edge devices .49.101 - Wing leading edge access panels - miscellaneous changes
gines .00.118 - Engines selection and alternate equipment (A318) .00.119 - Engines selection and alternate equipment (A319) .00.120 - Engines selection and alternate equipment (A320) .00.121 - Engines selection and alternate equipment (A321)
gine fuel and control .21.100 - Installation of additional sensors for engine health monitoring
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Page DTOC-14Issue
DDetailed table of contents A320 FamilyTIT Page ATA refOi 665 [79]79 rnate 666 [79-2]
79 port on 670 [79-6] 6 Revision 1, January 2012
etailed table of contentsLE l .00.101 - Engine, engine accessories and Auxiliary Power Unit (APU) alte
lubricating oil .40.101 - Installation of Integrated Drive Generator (IDG) oil level viewing
engine RH fan cowl
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Issue 6 Revision 1, January 2012
[ 00-1]
A320 Family Introduction 00
Reference Title00.00.200 Introduction
Page 1
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00 Introduction A320 Family
Is [ 00-2]
0
D1TmeTaWtiotoseso
2TsiaSM
r use n Guide encompasses a wide range of me circumstances, it is possible that a ation of options cannot be achieved. onfiguration Guide must be used in he expertise and assistance of Airbus.
n Guide shows items for which a pre- solution has been developed and for mes have been studied. Provided the ined in the customer definition mile-spected, these items can be installed the delivery lead time.
ire longer lead-time than normal, and er decisions prior to Contractual Defi-F) deadlines. These items are high-logue by a special remark: "Subject to ints". For these items, specific deci-all be identified in customer definition
Page 2sue 6 Revisio
0.00.20
escriptio) General his Configodels and
d on the fihis Configs "Airbus hen usedn and themization lection oflutions.
) Basic airhis Configc aircraft nd perfortandard Sanufacturn 1, January 2012 00.00.200
0 - Introduction
n
uration Guide is dedicated to the aircraft associated Standard Specifications indicat-rst page. uration Guide offers various options defined preferred solutions" to the customer. in conjunction with the Standard Specifica- other Configuration Guides a complete cus-of the Aircraft is possible through the
the different items and associated technical
craft uration Guide starts from the theoretical ba-as shown in the reference layout for weight mance calculations of the corresponding pecification and incorporating any relevant er Specification Change Notice (MSCN).
3) Instructions foThis Configuratiooptions and in soparticular combinTherefore, the Cconjunction with t
4) Lead-times This Configuratiodefined technicalwhich the lead tischedule as defstone chart is rewithout affecting
Caution: Some items requtherefore customnition Freeze (CDlighted in this catalead-time constrasion deadlines shmilestones.
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Introduction 00A320 Family
Issue 6 Rev
00.00.2
[ 00-3]
5) CataloOn each Air Tr
sectio date o option
For each object basic descr
someby dra
EPACitem isChangproce
technilutionssociat
Note: Fothe basicthe TDU
, the arrangement of the items follows sification. The items are sorted by nu-eference numbers within a given ATA
ions bear a 7-digit reference number: howing first the ATA (e.g. 26) and sub-ssification, followed by a running num-
olution (TDU) is referenced by a two-. 02). d in the Table Of Content (TOC) and beginning of each chapter.
: ection", "... alternate equipment", "pro-stallation of...". . equipment selection" relate to items rd specification offers a choice of basic uch items the customer is requested to f the choices on offer, unless alternate uired.
Page 3ision 1, January 2012 00.00.200
00 - Introduction (Continued)gue presentation
page, the following information is provided: ansport Association of America (ATA) title and n number f the issue of the catalogue reference
item, the description is structured in subparts: ive of the item aircraft definition related to the item iption of the item in terms of modifications, in cases commented by a note and/or illustrated wings selection mode for the item shows whether the selectable by individual or global Request For e (RFC)/Specification Change Notice (SCN)
dure cal solutions: a table describes all technical so- (called TDU: Technical Description Unit) as-ed to the item.
r comparison purposes, some tables also show aircraft equipment, labelled Std (Standard) in
column.
As far as possiblethe ATA 100 clasmerical order of rchapter.
The different opt(e.g: 26.24.600) sATA (e.g. 24) claber (e.g. 600).
Each technical sdigit number (e.gAll items are listeduplicated at the
Definition of titles"... equipment selvisions for...", "Ina) items titled "..where the standaequipment. For sselect from one oequipment is req
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00 Introduction A320 Family
Issue 6 Rev [ 00-4]
00.00.2
b) itemswhere ththat defin
c) items the custosions to
d) items customeof the sta
SelectionSpecific item andvisible inafter).
Such solment or items copabilities
ful product qualification and proof of Airbus performance requirements and tions.
s are as follows: f RFC/SCN on Manufacturer's Weight
of RFC/SCN on Operator's Weight
RFC/SCN on Available Payload d are for one off unless otherwise stat-
cts have yet to be determined for RFC/
ct is small and will be taken as zero for CN. native items are delta weights to the andard Specification unless otherwise
selection mode is Global the weight of part of the relevant Global RFC/SCN. n in the catalogue for such items are
.
Page 4ision 1, January 2012 00.00.200
00 - Introduction (Continued) titled "...alternate equipment" relate to items e customer can choose equipment alternate to ed in the Standard Specification.
titled "Provisions for..." relate to items where mer can add structural and/or system provi-
prepare the a/c for later installation.
titled "Installation of..." relate to items where the r can add functions/equipment/systems on top ndard definition.
conditions selection conditions may be associated to an are identified by an icon and a special remark the TDU table (see example in the figure here-
utions may be at the initial phases of develop-first application on Airbus aircraft. For these
mmitment to quality, industrial and technical ca-, on time delivery and customer support de-
pend on successcompliance with customer expecta
Weights Weight definition MWE: Effect o
Empty OWE: Effect
Empty APL: Effect of All weights quoteed. TBD: Weight effeSCN. Negl: Weight effeindividual RFC/SWeights for altercorresponding Ststated. Where the EPACthe item shall be Any weights showfor guidance only
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Introduction 00A320 Family
Issue 6 Rev
00.00.2
[ 00-5]
For somon custoweights and will b
6) DefiniThe custforms. Then, a SRFC, anThese Rcustomeed.
Global RThe globwith conlead-timewhich gr
IndividuaThe seleRFC/SC
r request ot mentioned in this Guide, or corre-dified item, require specific customer cial feasibility study has to be initiated. ential for customers to review the Con-s soon as possible to identify which of s are covered and which are not. customers, with the assistance of Air-e the necessary specific requests re-
ich are not covered by this Guide. uests shall necessarily have an impact times and resources and shall conse-onstraints and decisions that shall be d faith between the customer and Air-y forewarns that this may lead to the rtain requests.
sibility equipment by any entity other than the luding but not limited to the Buyer) for are made or which are post-delivery of e made under the sole and full respon-er.
Page 5ision 1, January 2012 00.00.200
00 - Introduction (Continued)e individual RFC/SCN the weight is dependent mer requirements, e.g. certain BFE items. The for such items shall be taken for guidance only e identified as such.
tion handling omer's selection is recorded by Airbus in RFC
CN is issued by Airbus, based on a customer's d is submitted for customer's signature. FCs/SCNs are issued before CDF directly on r request except if their content is to be adapt-
FC/SCN al RFC consists of a checklist containing items siderable interdependence and equivalent s. The global RFC leads to the global SCN
oups all selected items.
l RFC/SCN ction of individual items not covered by global N is achieved via individual RFCs/SCNs.
Specific customeItems that are nsponding to a morequests as a speIt is therefore essfiguration Guide atheir requirementThis will allow thebus, to raise in timlated to items whSuch specific reqin terms of lead quently lead to cdiscussed in goobus. Airbus herebunfeasibility of ce
7) Buyer's responAll installation of Manufacturer (incwhich provisions the aircraft shall bsibility of the Buy
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00 Introduction A320 Family
Issue 6 Rev [ 00-6]
00.00.2
The Buyufacturerrectly orequipmetive or no
Page 6ision 1, January 2012 00.00.200
00 - Introduction (Continued)er shall hold harmless and indemnify the Man- against any claims or/and damages related di- indirectly to an incorrect installation of an nt or to such equipment itself, whether defec-t.
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Introduction 00
Issue 6 Revision 1, January 2012 00.00.200
A320 Family
[ 00-7]
Figure 00-1 - Typical page description
25 Equipment/furnishings A320 Family
25.52.212 Installation of mechanized bulk loading system in aft cargo hold - sliding carpet system25.52.304 Installation of semi-automatic Cargo Loading System (CLS) in forward and aft cargo
holds (A320/A321)25.52.310 Fixed provision for occasional bulk capability in forward and aft cargo holds (A320/A321)25.52.315 Full electrical provision for semi-automatic CLS25.52.404 Installation of Cargo Loading System (CLS) with full bulk capability in fwd and aft cargo
holds25.52.407 Bulk loading capability in aft cargo hold door area behind two ULDs (A319)25.52.410 Full provision for installation of special container in aft cargo hold, door area (A319)25.52.500 Installation of continuous side guides in forward cargo hold25.52.511 Installation of continuous side guides in aft cargo hold
Reference Title
25 Equipment/furnishings A320 Family25.52.404 - Installation of Cargo Loading System (CLS) with full bulk capability in
fwd and aft cargo holdsObjective for A319-100 and A320-200 and A321-200To provide operational capability either to transport ULDs and/or bulk freight up to a maximum average den-sity of 15 lb/cu ft.
Basic aircraft for A319-100 and A320-200 and A321-200Full bulk configuration and structural provision for at-taching optional divider nets in the forward and aft cargo holds.System provision for CLS plus minimum electrical pro-vision for mechanized bulk loading system.
Description for A319-100 and A320-200 and A321-200The modification consists of the installation of:
electrically powered semi-automatic CLS additional tie-down fittings door nets with stanchions and divider nets for the for-
ward and aft cargo holds reinforced cargo floor panels for heavy bulk usage for
the forward and aft cargo holds, flat parts only drainage system side wall/ceiling panels for bulk loading in the forward
and aft cargo holds
fender for protection devices for the rapid decom-pression at frame 24 A.
EPAC selection mode Global CARGO
.
ATA title and section number
(ATA section + page number within the section)Date of the issue of the cataloguepage numberOption reference
Detailed description pageChapter cover pagewith a list of available items
Option reference and title
Issue 6 Revision 01, January 2012 [ 26-1]Page 243Issue 6 Revision 01, January 2012 25.52.404 [ 26-4]Page 246
.
Page 7
-
00 Introduction A320 Family
Issue 6 Revision 1, January 2012 00.00.200
[ 00-8]
Figure 00-2 - Example of technical solutions description table
Table 25-21 - Technical solutions description
TDU Title (Remarks) Appl. Weight (kg)MWE/OWE/APL
Equipmentreference
Equipmentsupplier
EquipmentPN
QTY STS
01 Semi-automatic CLS in fwdand aft cargo holds - without ACT provision (A320/A321)
A320-200A321-200
122.0/122.0/-122.0102.0/102.0/-102.0
02 Semi-automatic CLS in fwdand aft cargo holds - with full provision for one ACT (A320) Requires prior acceptance of CN28.11.133/02 - Full provision for instal-lation of one ACT in aft cargo hold (A320).Due to ACT, lead-time constraints for thisoption are 9 months.
A320-200
03 Semi-automatic CLS in fwdand aft cargo holds - with full provision for one ACT (A321) Requires prior acceptance of CN28.11.133/01 - Full provision for instal-lation of one ACT in aft cargo hold (A321)
A321-200
04 Semi-automatic CLS in fwdand aft cargo holds - with full provision for two ACTs (A320) Requires prior acceptance of CN28.11.140/03 - Full provision for instal-lation of two/one ACTs in aft cargo hold (A320).
A320-200
Due to ACT, lead-time constraints for thisoption are 8 months.
Due to ACT, lead-time constraints for thisoption are 9 months.
153.0/153.0/-153.0
133.0/133.0/-133.0
177.0/177.0/-177.0
Title of the technicalsolution and optionalremarks
Equipment information:Technical solution
Applicableseries
identifier (TDU)Weights informationper series
reference vendor PN (part numbers) quantity status (BFE or SFE)
MWE: Manufacturers Weight EmptyOWE: Operational Weight EmptyAPL: Allowable Payload Change
Selectioncondition
Selectionconditionremark
Page 8
-
Issue 6 Revision 1, January 2012
[ 02-1]
A320 Family Certification and external livery 02
Reference Title02.10.104 Certification of dynamically tested passenger seats02.10.111 Compliance with FAA type certification requirements02.10.112 Partial compliance with FAA type certification requirements02.10.120 15 knots tailwind certification02.10.123 Operation on runways with reduced width02.10.190 ETOPS 120/180 min02.12.122 Compliance status with EU-OPS 102.12.123 Compliance with CS25/FAR 25.562 (Head Injury Criteria - HIC)02.12.130 EASA certification of Take Off/Landing operation on wet grooved / PFC runways02.40.101 External livery
Page 9
-
02 Certification and external livery A320 Family
Is [ 02-2]
0 r seats
OTfrte
B2APfrAPfrte
D2Pfrte
00 and A320-200 and A321-200ynamically tested passenger seats is A certification on A319 and A321, but luded in the following option: - Compliance with FAA type certifica-.
mode
Page 10sue 6 Revisio
2.10.10
bjective fo certify ame specsted pass
asic aircr00319/A320assenger ame spec318assenger ame specsted pass
escriptio00assenger ame specsted passn 1, January 2012 02.10.104
4 - Certification of dynamically tested passenge
or A319-100 and A320-200 and A321-200passenger seats in accordance with seat ification AI 2521M1F100000 for dynamically enger seats.
aft for A319-100 and A320-200 and A321-
/A321seats are certified in accordance with seat ification AI 2520M1F000100.
seats are certified in accordance with seat ification AI 2521M1F000500 for dynamically enger seats.
n for A319-100 and A320-200 and A321-
seats are certified in accordance with seat ification AI 2521M1F100000 for dynamically enger seats.
Note for A319-1Certification of dmandatory for FAis already incCN02.10.111/01 tion requirements
EPAC selection Individual
-
Certification and external livery 02
Issue 6 Revision 1, January 2012 02.10.104
A320 Family
[ 02-3]
Table 02-1 - Technical solutions descriptionTDU Title (Remarks) Appl. Weight (kg)
MWE/OWE/APLEquipmentreference
Equipmentsupplier
EquipmentPN
QTY STS
05 Certification of dynamically tested passenger seats B/C
A319-100A320-200A321-200
0.0/0.0/0.00.0/0.0/0.00.0/0.0/0.0
06 Certification of dynamically tested passenger seats Y/C
A319-100A320-200A321-200
0.0/0.0/0.00.0/0.0/0.00.0/0.0/0.0
Page 11
-
02 Certification and external livery A320 Family
Is [ 02-4]
0 irements
OTty
BTwfo
DTpcrA
A
modified emergency exit inscription
ynamically tested passenger seats as specification 2520 M1F 0005 00 (or assageways to emergency exits.
zone converters modified emergency exit inscription
aximum 179 passenger seatsassageways to emergency exits.
zone converters ynamically tested passenger seats as specification 2520 M1F 0005 00 (or assageways to emergency exits.
a/c the installation of variable geome-junction with photoluminescent floor- is prohibited.
Page 12sue 6 Revisio
2.10.11
bjectiveo install alpe certific
asic aircrhe aircraftith JAR-2r US impo
escriptiohe followinliance withaft type:318-100installatiinstallatiand marinstallatiper seatequivaleinstallatiinstallati
319-100installatin 1, January 2012 02.10.111
1 - Compliance with FAA type certification requ
l modifications to be in compliance with FAA ation requirements.
aft is designed and constructed in accordance 5 airworthiness requirements, and FAR-25 rtation (see type certificate data sheet).
ng changes shall be carried-out to be in com- the FAA Type Design of the respective Air-
on of ozone converters on of modified emergency exit inscription kingon of dynamically tested passenger seats as frame specification 2520 M1F 0005 00 (or nt)on of weight placard on each overwing hatchon of passageways to emergency exits.
on of ozone converters
installation of and marking
installation of dper seat frameequivalent)
installation of p
A320-200 installation of o installation of
and marking installation of m installation of p
A321-200 installation of o installation of d
per seat frameequivalent)
installation of p
NoteOn US registeredtry seats in conmounted EEPMS
-
Certification and external livery 02A320 Family
Issue 6 Rev
02.10.1 irements (Continued)
[ 02-5]
EPAC seIndividua
Page 13ision 1, January 2012 02.10.111
11 - Compliance with FAA type certification requ
lection mode l
-
02 Certification and external livery A320 Family
Issue 6 Revision 1, January 2012 02.10.111
[ 02-6]
Table 02-2 - Technical solutions descriptionTDU Title (Remarks) Appl. Weight (kg)
MWE/OWE/APLEquipmentreference
Equipmentsupplier
EquipmentPN
QTY STS
01 Compliance with FAA type cer-tification requirements (A319/A320/A321)For A319 and A321, not compatible with CN02.10.104 - 16 g Certification of dynamically passenger seats.Requires prior acceptance of CN21.70.109 - Installation of ozone cata-lytic converters.Selection of CN11.30.131/05 - Installation of weight placards on overwing hatch is recommended.
A319-100A320-200A321-200
20.0/20.0/-20.020.0/20.0/-20.020.0/20.0/-20.0
08 Compliance with FAA type cer-tification requirements (A318)Requires prior acceptance of CN21.70.109 - Installation of ozone cata-lytic converters.Requires prior acceptance of CN11.30.131/05 - Installation of weight placards on overwing hatch.
A318-100 20.0/20.0/-20.0
Page 14
-
Certification and external livery 02A320 Family
Issue 6 Revision 1, January 2012
02.10.111 [ 02-7]
Intentionally left blank
Page 15
-
02 Certification and external livery A320 Family
Is [ 02-8]
0 n requirements
OTqce
BTwfo
DTlyspA
A
zone converters modified emergency exit inscription
zone converters.
red a/c the installation of variable ge-in conjunction with photoluminescent EEPMS is prohibited. tion of this option, AIRBUS will, no lat-ths before aircraft Industrial Delivery, Type Design Statement to the end ding: atus to the FAA Type Design" (List of uired to meet US Type Design) irements to obtain a US Standard Air-
icate" (Customization status for US op-
f this option ensures the partial compli-ividual aircraft MSN to the FAA Type
exclusion of the cabin layout.
Page 16sue 6 Revisio
2.10.11
bjectiveo install aluirementsrtification
asic aircrhe aircraftith JAR-2r US impo
escriptiohe followin in complective air
318-100 installatiinstallatiand marinstallatihatch.
319-100 installatiinstallatiand marn 1, January 2012 02.10.112
2 - Partial compliance with FAA type certificatio
l modifications except cabin arrangement re-, to be partially in compliance with FAA type requirements.
aft is designed and constructed in accordance 5 airworthiness requirements, and FAR-25 rtation (see type certificate data sheet).
ng changes shall be carried-out to be partial-
iance with the FAA Type Design of the re-craft type:
on of ozone converters on of modified emergency exit inscription kingon of weight placard on each overwing
on of ozone converters on of modified emergency exit inscription king.
A320-200 installation of o installation of
and marking.
A321-200 installation of o
Note on US registe
ometry seats floor-mounted
upon the selecer than 6 monissue the FAAcustomer inclu
- "Compliance StModifications req- "Additional Requworthiness Certiferations). the selection o
ance of the indDesign, at the
-
Certification and external livery 02A320 Family
Issue 6 Rev
02.10.1 n requirements (Continued)
[ 02-9]
the decate aproceBUS wvided monthmarksMSN.changModiflay of
a reviof del
EPAC seIndividua
Page 17ision 1, January 2012 02.10.112
12 - Partial compliance with FAA type certificatio
livery of a US Standard Airworthiness Certifi-t Aircraft ID is subject to a prior FAA validation ss of the Aircraft customized definition. AIR-
ill timely initiate and control this process pro-the end customer delivers, no later than 6 s before Aircraft ID, the final N-Registration allocated by the FAA to the individual aircraft Failure to meet this objective may generate es to the contractual definition (de-validation of
ications not timely approved by the FAA or De-the aircraft ID sed FAA TD Statement will be provided at time ivery.
lection mode l
-
02 Certification and external livery A320 Family
Issue 6 Revision 1, January 2012 02.10.112
[ 02-10]
Table 02-3 - Technical solutions descriptionTDU Title (Remarks) Appl. Weight (kg)
MWE/OWE/APLEquipmentreference
Equipmentsupplier
EquipmentPN
QTY STS
04 Partial compliance with FAA type certification require-ments (without seat arrange-ment requirements)Requires prior acceptance of CN21.70.109 - Installation of ozone cata-lytic converters.Selection of CN11.30.131/05 - Installation of weight placards on overwing hatch is recommended.
A319-100A320-200A321-200
20.0/20.0/-20.020.0/20.0/-20.020.0/20.0/-20.0
06 Partial compliance with FAA type certification require-ments (without seat arrange-ment requir) (A318)Requires prior acceptance of CN21.70.109 - Installation of ozone cata-lytic converters.Requires prior acceptance of CN11.30.131/05 - Installation of weight placards on overwing hatch.
A318-100 20.0/20.0/-20.0
Page 18
-
Certification and external livery 02A320 Family
Issue 6 Revision 1, January 2012
02.10.112 [ 02-11]
Intentionally left blank
Page 19
-
02 Certification and external livery A320 Family
Is [ 02-12]
0
OT1
BIntath1
DInuthow
To
ine characteristics justifications with ticular in terms of engine inlet.
sensitivity of the engine inlet charac-ilwind, a slower thrust application at
necessary, which in turn may require rocedure". Both effects may require ances and consequent aircraft gross for a given runway length.
mode
Page 20sue 6 Revisio
2.10.12
bjectiveo be able5 knots de
asic aircr the absetion of thee tailwind
0 knots.
escriptio order to
p to 15 kne aircraft
nstrationsind.
he certificff shall inc
new permanual aadditionaincludingthe comsettings,n 1, January 2012 02.10.120
0 - 15 knots tailwind certification
to take off with a tailwind component up to pending on engine type.
aftnce of specific flight tests, the usual interpre- current certification requirements is to limit operations to a maximum component of
noperate the aircraft at a tailwind component ots, severe conditions shall be conducted by manufacturer. This includes flight test dem- with 1.5 x the desired limit in terms of tail-
ation dossier for tailwind operations at take-lude: formance justifications, updating of flight nd flight crew operating manual l handling qualities demonstrations in flight, justification/modifications (if necessary) of puters settings (angle of attack protection windshear warning ...)
additional engtailwind, in par
NoteDepending on theteristics with a tatake-off may be "rolling take-off plong take-off distweight penalties
EPAC selection Individual
-
Certification and external livery 02
Issue 6 Revision 1, January 2012 02.10.120
A320 Family
[ 02-13]
Table 02-4 - Technical solutions descriptionTDU Title (Remarks) Appl. Weight (kg)
MWE/OWE/APLEquipmentreference
Equipmentsupplier
EquipmentPN
QTY STS
01 15 knots tailwind certification at take-off
A318-100A319-100A320-200A321-200
0.0/0.0/0.00.0/0.0/0.00.0/0.0/0.00.0/0.0/0.0
Page 21
-
02 Certification and external livery A320 Family
Is [ 02-14]
0
OTco
BTw
DC44tio
NFdlo
mode
Page 22sue 6 Revisio
2.10.12
bjectiveo authorizmprised
asic aircrhe standaays with a
escriptioertification5 meters 5 m) is acns:new permanualsnew defiuments adjustmeupdating
oteor aircraftuced runwading optn 1, January 2012 02.10.123
3 - Operation on runways with reduced width
e aircraft operation on runways with a width between 30 m and 45 m.
aftrd aircraft is certificated for operation on run- minimum width of 45 m.
n for operation on runways less than
wide (width comprised between 30 m and hieved by performing the following modifica-
formance justifications, updating of flight and TLC nition of MMEL, updating of certification doc-
nt of limitations (e.g. crosswind, autoland), of MEL and CDL.
equipped with a CLS and operating on re-ay width, it is recommended to select a bulk ion.
EPAC selection Individual
-
Certification and external livery 02
Issue 6 Revision 1, January 2012 02.10.123
A320 Family
[ 02-15]
Table 02-5 - Technical solutions descriptionTDU Title (Remarks) Appl. Weight (kg)
MWE/OWE/APLEquipmentreference
Equipmentsupplier
EquipmentPN
QTY STS
01 Aircraft Operation on runways less than 45m wideNot applicable in conjunction with PW engines
A318-100A319-100A320-200A321-200
0.0/0.0/0.00.0/0.0/0.00.0/0.0/0.00.0/0.0/0.0
Page 23
-
02 Certification and external livery A320 Family
Is [ 02-16]
0
OTdg
BB
DMeretea
NTle
n authorization can only be obtained on by the operator to its national au-e operational life of the aircraft, addi-ns may be necessary to maintain
y at the required level. They are not hange.cceptance of CN26.23.111 - Cargo ishers extended duration for ETOPS .23.112 - Cargo holds fire extinguish-ation for ETOPS 180 min.o have at least one HF installed for . Therefore, this option requires prior N23.11.116 - Installation of single HF r CN23.11.131 - Installation of single ull provision for second one (SFE), or stallation of dual HF system (SFE).es extended over water flights, under
rements, it is the responsibility of the l slide rafts (EECG item CN25.62.102) ELTs (EECG item CN25.65.305).
mode
Page 24sue 6 Revisio
2.10.19
bjectiveo make thiversion tiine inoper
asic aircrasic certif
escriptioodification
lectrical equired bynance an
ircraft deli
otehe precisected confapplicabengine mAPU typcargo hon 1, January 2012 02.10.190
0 - ETOPS 120/180 min
e design capable of 120/180 min maximum me from diversion airport at normal one en-ative cruise speed.
aftication is with class C cargo holds.
ns concern the supply of some systems in
mergency conditions and their reliability as the applicable ETOPS Configuration Main-d Procedure (CMP) document at the time of very.
list of modifications depends upon the se-iguration of the aircraft: le airworthiness requirement odel
e ld ventilation, heating.
ETOPS operatiothrough applicatithority. During thtional modificatiosystems reliabilitcovered by this cRequires prior aholds fire extingu120 min or CN26ers extended durIt is mandatory tETOPS 120/180acceptance of Csystem (SFE), oHF system and fCN23.11.155 - InIf the aircraft makEU-OPS 1 requioperator to instaland two portable
EPAC selection Individual
-
Certification and external livery 02
Issue 6 Revision 1, January 2012 02.10.190
A320 Family
[ 02-17]
Figure 02-1 - ETOPS - area of operation
One engine failure flight path (condition of ETOPS requirement)
(Non ETOPS twins) Typical single engine speed
60 minute rule
Typical single engine speed
180 minute rule
Typical single engine speed
120 minute rule
Page 25
-
02 Certification and external livery A320 Family
Issue 6 Revision 1, January 2012 02.10.190
[ 02-18]
Figure 02-2 - ETOPS 120/180 min options (A318)
Certified = SCG item(no lead-time constraint)
Not certified (lead-time constraint)
EASA/JAA FAA EASA/JAA FAA
A318 - ETOPS 120 min A318 - ETOPS 180 min
CFM56-5B8/3 CN02.10.200/05 CN02.10.200/06 CN02.10.300/05 CN02.10.300/06
CFM56-5B9/3 CN02.10.200/07 CN02.10.200/08 CN02.10.300/07 CN02.10.300/08
PW6122A CN02.10.200/11 CN02.10.200/12 CN02.10.300/11 CN02.10.300/12
PW6124A CN02.10.200/13 CN02.10.200/14 CN02.10.300/13 CN02.10.300/14
Page 26
-
Certification and external livery 02
Issue 6 Revision 1, January 2012 02.10.190
A320 Family
[ 02-19]
Figure 02-3 - ETOPS 120/180 min options (A319)
Certified = SCG item(no lead-time constraint)
EASA/JAA FAA EASA/JAA FAA
A319 - ETOPS 120 min A319 - ETOPS 180 min
CFM56-5B5/3 CN02.10.210/03 CN02.10.210/04 CN02.10.310/03 CN02.10.310/04
CFM56-5B6/3 CN02.10.210/15 CN02.10.210/16 CN02.10.310/15 CN02.10.310/16
CFM56-5B7/3 CN02.10.210/37 CN02.10.210/38 CN02.10.310/37 CN02.10.310/38
IAE V2522-A5 CN02.10.210/41 CN02.10.210/42 CN02.10.310/41 CN02.10.310/42
IAE V2524-A5 CN02.10.210/51 CN02.10.210/52 CN02.10.310/51 CN02.10.310/52
IAE V2527M-A5 CN02.10.210/61 CN02.10.210/62 CN02.10.310/61 CN02.10.310/62
Page 27
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02 Certification and external livery A320 Family
Issue 6 Revision 1, January 2012 02.10.190
[ 02-20]
Figure 02-4 - ETOPS 120/180 min options (A320)
Certified = SCG item(no lead-time constraint)
N/A
N/A
N/A = Not Applicable
EASA/JAA FAA EASA/JAA FAA
A320 - ETOPS 120 min A320 - ETOPS 180 min
CFM56-5B4/3 CN02.10.220/03 CN02.10.220/04 CN02.10.320/03 CN02.10.320/04
CFM56-5B5/3 CN02.10.220/05 CN02.10.320/05
CFM56-5B6/3 CN02.10.220/07 CN02.10.320/07
IAE V2527-A5 CN02.10.220/41 CN02.10.220/42 CN02.10.320/41 CN02.10.320/42
IAE V2527E-A5 CN02.10.220/51 CN02.10.220/52 CN02.10.320/51 CN02.10.320/52
N/A
N/A
N/A
N/A
Page 28
-
Certification and external livery 02
Issue 6 Revision 1, January 2012 02.10.190
A320 Family
[ 02-21]
Figure 02-5 - ETOPS 120/180 min options (A321)
Certified = SCG item(no lead-time constraint)
EASA/JAA FAA EASA/JAA FAA
CFM56-5B1/3 CN02.10.240/09 CN02.10.240/10 CN02.10.330/09 CN02.10.330/10
CFM56-5B2/3 CN02.10.240/30 CN02.10.240/31 CN02.10.330/30 CN02.10.330/31
CFM56-5B3/3 CN02.10.240/13 CN02.10.240/14 CN02.10.330/13 CN02.10.330/14
IAE V2530-A5 CN02.10.240/21 CN02.10.240/22 CN02.10.330/21 CN02.10.330/22
IAE V2533-A5 CN02.10.240/11 CN02.10.240/12 CN02.10.330/11 CN02.10.330/12
A321 - ETOPS 120 min A321 - ETOPS 180 min
Page 29
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02 Certification and external livery A320 Family
Is [ 02-22]
0
OTsu
BTpcy7
DAEp
NTeEan
EIn
Page 30sue 6 Revisio
2.12.12
bjectiveo provide bparts K
asic aircrhe basic aarts K, L & Locator
.0, ...).
escriptiot aircraft dU-OPS 1,rovided.
otehe operatrational auU-OPS 1.l complianon-compli
PAC seledividualn 1, January 2012 02.12.122
2 - Compliance status with EU-OPS 1
compliance status report against EU-OPS 1, & L or subparts K, L & S, at aircraft delivery.
aftircraft does not comply with EU-OPS 1, sub- S (cabin emergency equipment, Emergen-
Transmitter (ELT) installation, TCAS change
nelivery, a compliance status report against
subparts K & L or subparts K, L & S, shall be
or is responsible to show to their national op-thority the compliance of their aircraft with
AIRBUS is providing help by raising a factu-ce review and cannot be responsible for the ance which may be identified.
ction mode
-
Certification and external livery 02
Issue 6 Revision 1, January 2012 02.12.122
A320 Family
[ 02-23]
Table 02-6 - Technical solutions descriptionTDU Title (Remarks) Appl. Weight (kg)
MWE/OWE/APLEquipmentreference
Equipmentsupplier
EquipmentPN
QTY STS
01 Compliance status with EU-OPS 1 - subpart K plus L requirements
A318-100A319-100A320-200A321-200
0.0/0.0/0.00.0/0.0/0.00.0/0.0/0.00.0/0.0/0.0
02 Compliance with EU-OPS 1 - subpart K, L and S require-ments
A318-100A319-100A320-200A321-200
0.0/0.0/0.00.0/0.0/0.00.0/0.0/0.00.0/0.0/0.0
Page 31
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02 Certification and external livery A320 Family
Is [ 02-24]
0 ury Criteria - HIC)OTari
BN
DTrareInseco
NAucete
EIn
Page 32sue 6 Revisio
2.12.12
bjectiveo certify pccordancea - HIC).
asic aircrone.
escriptiohe passention shagulation. particulaats and mpliance
oteirbus comlation at dssful seasts.
PAC seledividualn 1, January 2012 02.12.123
3 - Compliance with CS25/FAR 25.562 (Head Inj
assenger seats and cabin attendant seats in with CS25/FAR 25.562 (Head Injury Crite-
aft
nger seat and cabin attendant seat configu-
ll be compliant with CS25/FAR 25.562
r, dynamic tests are required on passenger cabin attendant seats to demonstrate such for the agreed validated cabin layout.
mitment to show compliance with such reg-elivery remains subject to the on-time suc-t supplier results of passenger seat dynamic
ction mode
-
Certification and external livery 02
Issue 6 Revision 1, January 2012 02.12.123
A320 Family
[ 02-25]
Table 02-7 - Technical solutions descriptionTDU Title (Remarks) Appl. Weight (kg)
MWE/OWE/APLEquipmentreference
Equipmentsupplier
EquipmentPN
QTY STS
03 Compliance with CS25/FAR 25.562 (Head Injury Criteria - HIC)
A318-100A319-100A320-200A321-200
0.0/0.0/0.00.0/0.0/0.00.0/0.0/0.00.0/0.0/0.0
Page 33
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02 Certification and external livery A320 Family
Is [ 02-26]
0 ation on wet grooved / PFC
OTw(gpstTaw
B2N
D2TlimmcoTaOo
account the specific braking friction co-imum OCTOPUS version needed for Landing A/C performance is V25.
mode
Page 34sue 6 Revisio
2.12.13
bjective fo allow Taet runwayrooved o
avementsandard smhe groovessociated et runway
asic aircr00one.
escriptio00he modifi
itations ent to conditions o
he minimullows as aff A/C pern a smootn 1, January 2012 02.12.130
0 - EASA certification of Take Off/Landing operrunways
or A318-100 and A319-100 and A320-200ke-Off/Landing performance calculation on taking credit of specific runway pavement
r Porous Friction Course). On those specific , a higher braking friction coefficient, than on
ooth runways, can be reached. d/PFC (Porous Friction Course) runway is to a specific braking friction coefficient on .
aft for A318-100 and A319-100 and A320-
n for A318-100 and A319-100 and A320-
cation consists in introducing the relevant and performance through the AFM supple-ver Take-Off/Landing operations under wet n grooved/PFC runways.m OCTOPUS version needed is V23.1 that
n option to select the calculation of the Take formance (Accelerate Stop Distance) either h runway state or on a grooved/PFC runway
state, taking into efficient. The mincalculation of the
EPAC selection Individual
-
Certification and external livery 02
Issue 6 Revision 1, January 2012 02.12.130
A320 Family
[ 02-27]
Table 02-8 - Technical solutions descriptionTDU Title (Remarks) Appl. Weight (kg)
MWE/OWE/APLEquipmentreference
Equipmentsupplier
EquipmentPN
QTY STS
01 EASA certification of Take-Off operation on wet grooved / PFC runways
A318-100A319-100A320-200
0.0/0.0/0.00.0/0.0/0.00.0/0.0/0.0
02 EASA certification of Landing operation on wet grooved / PFC runways
A318-100A319-100A320-200
0.0/0.0/0.00.0/0.0/0.00.0/0.0/0.0
Page 35
-
02 Certification and external livery A320 Family
Is [ 02-28]
0
OTEn
BTticzoE
DTsha
NNS
of slats lips and exhaust, parts of pylons
ilizer shield ading edge
fairings ails such as angle of attack sensors, lected antennas etc.
issued for drawing identification.
f each external livery (design, paint ading, number of colours, product se-ffect the paint production cycle. Con-external livery is investigated on an and relevant terms and conditions will the corresponding SCN (Specification
mode
Page 36sue 6 Revisio
2.40.10
bjectiveo deliver txternal livacelles.
asic aircrhe aircraftal stabilizntal Stab
xternal ma
escriptiohe aircrafall be pa
s defined a drawininstructioetc.) painted con instrusamples
oteote 1:ome metan 1, January 2012 02.40.101
1 - External livery
he aircraft painted in the livery of the buyer. ery means fuselage, vertical stabilizer and
aft is delivered painted in white (fuselage, ver-er), and light grey (wings, Trimmable Hori-ilizer (THS) and nacelles).rkings are in English only.
nt fuselage, vertical stabilizer and nacelles inted according to the livery of the customer by:g prepared by AIRBUS, based on decorative ns from the customer (paper, floppy disk, olour samples prepared by AIRBUS, based ctions from the customer (colour references, ).
llic areas are and remain unpainted:
leading edges engine intake scuff plates horizontal stab THS forward le forward pylon equipment det
static ports, se
Note 2:One RFC will be
Note 3:The complexity oblending and/or flection, ...), can asequently, each individual basis, be mentioned in Change Notice).
EPAC selection Individual
-
Certification and external livery 02
Issue 6 Revision 1, January 2012 02.40.101
A320 Family
[ 02-29]
Figure 02-6 - External livery (A319)
anti-skid paint
Grey M9004 (upper wing coating)Grey M9001 (polyurethane top coat)
A319 shownPrinciples valid for all A320 Family versions
White M8002Metallic unpainted
IAE engine nacelle
CFM engine nacelleTHS leading edge
unpainted
Slat leading edge unpainted
Apron fairing
THS travel area
Page 37
-
02 Certification and external livery A320 Family
Issue 6 Revision 1, January 2012 02.40.101
[ 02-30]
Table 02-9 - Technical solutions descriptionTDU Title (Remarks) Appl. Weight (kg)
MWE/OWE/APLEquipmentreference
Equipmentsupplier
EquipmentPN
QTY STS
01 External livery A318-100A319-100A320-200A321-200
TBD/TBD/TBDTBD/TBD/TBDTBD/TBD/TBDTBD/TBD/TBD
External livery TBD TBD SFE
Page 38
-
Issue 6 Revision 1, January 2012
[ 03-1]
A320 Family General aircraft design criteria 03
Reference Title03.20.300 Design weights (A318)03.20.400 Design weights (A319)03.20.500 Design weights (A320)03.20.600 Design weights (A321)
Page 39
-
03 General aircraft design criteria A320 Family
Is [ 03-2]
0
OTsiae
BTa
D
mode
Page 40sue 6 Revisio
3.20.30
bjective fo allow thegn weightble weightngines/air
asic aircrhe aircrafre as follo
MaximumMaximumMaximumMaximum
escriptiochangesual, Weition Manmodificachangesware to aMLW, replacemindicatinpossiblyn 1, January 2012 03.20.300
0 - Design weights (A318)or A318-100 customer to select predefined alternate de-
variants as shown in following table (select- variants associated with basic and optional craft models).
aft for A318-100t basic design weights (weight variant 000) ws:
Taxi Weight (MTW) 59.4 t Take-Off Weight (MTOW) 59 t Landing Weight (MLW) 56 t Zero Fuel Weight (MZFW) 53 t.
n for A318-100 in the aircraft manuals (Aircraft Flight Man-ght & Balance Manual, Flight Crew Opera-ual, ...)tion of the CG diagram in all performance related manuals and soft-dapt to the new maximum weights (MTOW, )ent of labels bonded to the MLG main fitting
g MTOW and tire pressure, changes of the wheels when necessary.
EPAC selectionIndividual
-
General aircraft design criteria 03
Issue 6 Revision 1, January 2012 03.20.300
A320 Family
[ 03-3]
Figure 03-1 - Design weight options (A318)Weightvariant
A318
-111
CFM
56-5B
8/3
A318
-112
CFM5
6-5B9
/3
A318
-121
PW 6
122A
Design weights (t)
CN03.20.311 CN03.20.312 CN03.20.321 TDU
000MTOW 59MLW 56 Basic Basic Basic Basic 20MZFW 53
001MTOW 61.5MLW 56 Certified 01MZFW 53
002MTOW 63MLW 57.5 Certified Certified Certified Certified 02MZFW 54.5
003MTOW 64.5MLW 57.5 Certified Certified 03MZFW 54.5
004MTOW 66MLW 57.5 Certified Certified
Certified
04MZFW 54.5
005MTOW 68MLW 57.5 Certified 05MZFW 54.5
006MTOW 56MLW 56 Certified Certified 06
MZFW 53
MZFW 53
007MTOW 61MLW 56 Certified Certified 07
Certified Certified
A318
-122
PW 6
124A
CN03.20.322
08008MTOW 64MLW 56MZFW 53
Certified Certified
Certified Certified
Certified Certified
CertifiedCertified
Certified Certified
Certified Certified
Certified Certified
Certified
Certified = SCG item (no lead-time constraint)
Page 41
-
03 General aircraft design criteria A320 Family
Issue 6 Revision 1, January 2012 03.20.300
[ 03-4]
Figure 03-2 - Basic CG limits diagram (A318)25232119171513 27 29 31 33 35 37 4139
15 17 1911090705 13 21 23 25 27 29 31 33 35 4537 39 41 43 35
40
45
50
55
60
65
70
75
80
35
40
45
50
55
60
65
70
75
80
%RC
%RCAircraft weight (kg x 1000) Aircraft weight (kg x 1000)
42.6
MTOW 59 000 kg
MLW 56 000 kg
MZFW 53 000 kg
Flight Flight
Landing3
2
.
2
Landing
5657
Take-off
Page 42
-
General aircraft design criteria 03
Issue 6 Revision 1, January 2012 03.20.300
A320 Family
[ 03-5]
Figure 03-3 - CG limits diagram with max. optional MTOW (A318)
25232119171513 27 29 31 33 35 37 4139
15 17 1911090705 13 21 23 25 27 29 31 33 35 4537 39 41 43 35
40
45
50
55
60
65
70
75
80
35
40
45
50
55
60
65
70
75
80
%RC
%RCAircraft weight (kg x 1000) Aircraft weight (kg x 1000)
40.6
3
1
.
1
8
Take-off
MTOW 68 000 kg
MLW 57 500 kg
MZFW 54 500 kg
Flight
Flight
Landing
Landing
63
1
6
.
7
Take-off
1
8
.
7
63
57
3
3
.
0
3
2
.
0
56
Page 43
-
03 General aircraft design criteria A320 Family
Is [ 03-6]
0
OTsiae
BTa
D
00ure Indication System (TPIS) is in-
computer pin programming has to be gly.
mode
Page 44sue 6 Revisio
3.20.40
bjective fo allow thegn weightble weightngines/air
asic aircrhe aircrafre as follo
MaximumMaximumMaximumMaximum
escriptiochangesual, Weition Manmodificachangesware to aMLW, ...replacemfitting indpossiblywhen nen 1, January 2012 03.20.400
0 - Design weights (A319)or A319-100 customer to select predefined alternate de-
variants as shown in following table (select- variants associated with basic and optional craft models).
aft for A319-100t basic design weights (weight variant 000) ws:
Taxi Weight (MTW) 64.4 t Take-Off Weight (MTOW) 64 t Landing Weight (MLW) 61 t Zero Fuel Weight (MZFW) 57 t.
n for A319-100 in the aircraft manuals (Aircraft Flight Man-ght & Balance Manual, Flight Crew Opera-ual, ...)tion of the CG diagram in all performance related manuals and soft-dapt to the new maximum weights (MTOW,
) ent of labels bonded to the NLG/MLG main icating MTOW and tire pressure
, changes of the brakes, wheels and tires cessary.
Note for A319-1If the Tire Pressstalled, the TPISmodified accordin
EPAC selection Individual
-
General aircraft design criteria 03
Issue 6 Revision 1, January 2012 03.20.400
A320 Family
[ 03-7]
Figure 03-4 - Design weight options (A319)Weight variant A3
19-1
11CF
M 56
-5B5
/3
A319
-112
CFM
56-5
B6/3
A319
-115
CFM
56-5
B7/3
A319
-131
IAE
V252
2-A5
A319
-132
IAE
V252
4-A5
A319
-133
IAE
V252
7M-A
5
Design weights (t)
CN03.20.411 CN03.20.412 CN03.20.415 CN03.20.431 CN03.20.432 CN03.20.433 TDU
000MTOWMLWMZFW MTOWMLWMZFW MTOWMLWMZFW MTOWMLWMZFW MTOWMLWMZFW MTOWMLWMZFW MTOWMLWMZFW MTOWMLWMZFW MTOWMLWMZFW MTOWMLWMZFW MTOWMLWMZFW MTOWMLWMZFW
646157
Basic Basic Basic Basic Basic Basic 20
0017061 Certified Certified Certified Certified Certified Certified 0157
00275.562.5 Certified Certified Certified Certified Certified Certified
Certified Certified Certified Certified Certified Certified
Certified Certified Certified
Certified Certified Certified Certified Certified Certified
Certified Certified Certified Certified Certified Certified
0258.5
0036861 0357
00468
62.5 Certified Certified Certified 0458.5
00570
62.5 0558.5
00673.562.558.5
06
Certified Certified Certified Certified Certified Certified00775.56157
07
Certified Certified Certified Certified Certified Certified00864
62.558.5
08
Certified Certified Certified Certified Certified Certified00966
62.558.5
09
Certified Certified Certified Certified Certified Certified011666157
11
Certified Certified Certified Certified Certified Certified012626157
12
Certified = SCG item (no lead-time constraint)
Page 45
-
03 General aircraft design criteria A320 Family
Issue 6 Revision 1, January 2012 03.20.400
[ 03-8]
Figure 03-5 - Basic CG limits diagram (A319)
21191715 23 25 27 29 31 33 35 37 3980
75
70
65
60
55
50
45
40
35
41% RCAircraft weight (kg x 1 000) Aircraft weight (kg x 1 000)
11090705 13 15 17 19 21 23 25 %RC27 29 31 33 35 37 39 41 43 45
80
75
70
65
60
55
50
45
40
35
49.6
MTOW 64 000kgMLW 61 000kg
MZFW 57 000kg
Take-off
Take-off/landingFlight
Flight
Landing35.4
Page 46
-
General aircraft design criteria 03
Issue 6 Revision 1, January 2012 03.20.400
A320 Family
[ 03-9]
Figure 03-6 - CG limits diagram with max. optional MTOW (A319)
25232119171513 27 29 31 33 35 37 4139
15 17 1911090705 13 21 23 25 27 29 31 33 35 4537 39 41 4335
40
45
50
55
60
65
70
75
80
35
40
45
50
55
60
65
70
75
80
%RC
%RC
Aircraft weight (kg x 1000) Aircraft weight (kg x 1000)
65.3
MTOW 75 500 kg
MLW 62 500 kg
MZFW 58 500 kg
Take-off/landing
Flight
Flight
Landing
3
6
3
7
2
6
2
4
74.5
2
5
49.6
Take-off
35.4
Page 47
-
03 General aircraft design criteria A320 Family
Is [ 03-10]
0
OTsiae
BTa
D
ations associated to high design ample maximum taxiing speed during
00ure Indication System (TPIS) is in-
computer pin programming has to be gly.
mode
Page 48sue 6 Revisio
3.20.50
bjective fo allow thegn weightble weightngines/air
asic aircrhe aircrafre as follo
MaximumMaximumMaximumMaximum
escriptiochangesual, Weition Manmodificachangesware to aMLW, replacemfitting indpossiblywhen nen 1, January 2012 03.20.500
0 - Design weights (A320)or A320-200 customer to select predefined alternate de-
variants as shown in following table (select- variants associated with basic and optional craft models).
aft for A320-200t basic design weights (weight variant 008) ws:
Taxi Weight (MTW) 73.9 t Take-Off Weight (MTOW) 73.5 t Landing Weight (MLW) 64.5 t Zero Fuel Weight (MZFW) 61.0 t.
n for A320-200 in the aircraft manuals (Aircraft Flight Man-ght & Balance Manual, Flight Crew Opera-ual, ) tion of the CG diagram in all performance related manuals and soft-dapt to the new maximum weights (MTOW, ) ent of labels bonded to the NLG/MLG main icating MTOW and tire pressure
, changes of the brakes, wheels and tires cessary
possible limitweights (for exturns).
Note for A320-2If the Tire Pressstalled, the TPISmodified accordin
EPAC selection Individual
-
General aircraft design criteria 03
Issue 6 Revision 1, January 2012 03.20.500
A320 Family
[ 03-11]
Figure 03-7 - Design weight options (A320)WeightVariant
A320-214CFM 56-5B4/3
A320-215CFM 56-5B5/3
A320-216CFM 56-5B6/3
A320-232IAE V2527-A5
A320-233IAE V2527E-A5
CN03.20.514 CN03.20.515 CN03.20.516 CN03.20.532 CN03.20.533 TDU
008MTOWMLWMZFW
73.564.561
Basic Basic Basic Basic Basic 08 Certified = SCG item (no lead-time constraint)
009MTOWMLWMZFW
75.564.561
Certified Certified Certified Certified Certified 09
010MTOWMLWMZFW
7764.561
Certified N/A N/A Certified Certified 10
011MTOWMLWMZFW
75.566
62.5Certified Certified Certified Certified Certified 11
012MTOWMLWMZFW
7766
62.5Certified N/A N/A Certified Certified 12
013MTOWMLWMZFW
71.564.561
Certified Certified Certified Certified Certified 13
014MTOWMLWMZFW
73.564.561.5
Certified Certified Certified Certified Certified 14
015MTOWMLWMZFW
7864.561
Certified N/A N/A Certified Certified 15
016MTOWMLWMZFW
73.566
62.5Certified Certified Certified Certified Certified 16
017MTOWMLWMZFW
7866
62.5Certified N/A N/A Certified Certified 17
018MTOWMLWMZFW
71.566
62.5Certified Certified Certified Certified Certified 18
N/A = Not Applicable
Design weights(tons)
Page 49
-
03 General aircraft design criteria A320 Family
Issue 6 Revision 1, January 2012 03.20.500
[ 03-12]
Figure 03-8 - Basic CG limits diagram (A320)
25 27 29 31 332321191715
35
40
45
50
55
60
65
70
75
80
85
90
35
40
45
50
55
60
65
70
75
80
85
9035 37 39 41% RC
Aircraft weight (kg x 1 000) Aircraft weight (kg x 1 000)
11090705 13 15 17 19 21 23 25 %RC27 29 31 33 35 37 39 41 43 45
47.5
69.5
MTOW 73 500kg
MLW 64 500kg
MZFW 61 000kg
Take-offTake-off/landing
FlightFlight
Landing
Page 50
-
General aircraft design criteria 03
Issue 6 Revision 1, January 2012 03.20.500
A320 Family
[ 03-13]
Figure 03-9 - CG limits diagram with max. optional MTOW (A320)
Page 51
-
03 General aircraft design criteria A320 Family
Is [ 03-14]
0
OTsiae
BTa
D
00ure Indication System (TPIS) is in-
computer pin programming has to be gly.
mode
Page 52sue 6 Revisio
3.20.60
bjective fo allow thegn weightble weightngines/air
asic aircrhe aircrafre as follo
MaximumMaximumMaximumMaximum
escriptiochangesual, Weition Manmodificachangesware to aMLW, replacemfitting indpossiblywhen nen 1, January 2012 03.20.600
0 - Design weights (A321)or A321-200 customer to select predefined alternate de-
variants as shown in following table (select- variants associated with basic and optional craft models).
aft for A321-200t basic design weights (weight variant 000) ws:
Taxi Weight (MTW) 89.4 t Take-Off Weight (MTOW) 89.0 t Landing Weight (MLW) 75.5 t Zero Fuel Weight (MZFW) 71.5 t.
n for A321-200 in the aircraft manuals (Aircraft Flight Man-ght & Balance Manual, Flight Crew Opera-ual, ) tion of the CG diagram in all performance related manuals and soft-dapt to the new maximum weights (MTOW, ) ent of labels bonded to the NLG/MLG main icating MTOW and tire pressure
, changes of the brakes, wheels and tires cessary.
Note for A321-2If the Tire Pressstalled, the TPISmodified accordin
EPAC selection Individual
-
General aircraft design criteria 03
Issue 6 Revision 1, January 2012 03.20.600
A320 Family
[ 03-15]
Figure 03-10 - Design weight options (A321)Weight variant A3
21-21
1CF
M 56
-5B3/3
A321
-212
CFM5
6-5B1
/3
A321
-213
CFM5
6-5B2
/3
A321
-231
IAE
V253
3-A5
A321
-232
IAE
V253
0-A5
Design weights (t)
CN03.20.611 CN03.20.612 CN03.20.613 CN03.20.631 CN03.20.632 TDU
000MTOW 89MLW 75.5 Basic Basic Basic Basic Basic 20MZFW 71.5
001MTOW 93MLW 77.8 Certified Certified Certified Certified Certified
Certified
01MZFW 73.8
002MTOW 89MLW 77.8 Certified Certified Certified Certified 02MZFW 73.8
004MTOW 87MLW 75.5 04MZFW 71.5
005MTOW 85MLW 75.5 Certified Certified Certified Certified Certified
Certified Certified Certified Certified Certified
Certified Certified Certified
Certified Certified Certified
Certified Certified Certified
Certified Certified Certified
Certified Certified Certified Certified Certified
05MZFW 71.5
006MTOW 83MLW 75.5 06MZFW 71.5
007MTOW 83MLW 73.5 Not yetcertified
Not yetcertified 07
MZFW 69.5
008MTOW 80MLW 73.5 Not yet
certifiedNot yetcertified 08
MZFW 69.5
MZFW 69.5
009MTOW 78MLW 73.5 Not yetcertified
Not yetcertified 09
Not yetcertified
Not yetcertified 10
Certified = SCG item (no lead-time constraint)
Not yet certified = certification possible on specific customer request (lead-time constraint)
010MTOW 85MLW 77.8MZFW 73.8
Certified Certified Certified Certified Certified 11011MTOW 93.5MLW 77.8MZFW 73.8
Page 53
-
03 General aircraft design criteria A320 Family
Issue 6 Revision 1, January 2012 03.20.600
[ 03-16]
Figure 03-11 - Basic CG limits diagram (A321)
35
40
45
50
55
60
65
70
75
80
85
90
95
35
40
45
50
55
60
65
70
75
80
85
95
90
25 27 29 31 33232119171513 35 37 39 41% RCAircraft weight (kg x 1 000) Aircraft weight (kg x 1 000)
11090705 13 15 17 19 21 23 25 %RC27 29 31 33 35 37 39 41 43 45
MTOW 89 000kg
MLW 75 500kg
MZFW 71 500kg
Take-off
Take-off/landingFlight
FlightLanding
81.8
4
0
.
1
Page 54
-
General aircraft design criteria 03
Issue 6 Revision 1, January 2012 03.20.600
A320 Family
[ 03-17]
Figure 03-12 - CG limits diagram with max. optional MTOW (A321)25232119171513 27 29 31 33 35 37 4139
15 17 1911090705 13 21 23 25 27 29 31 33 35 4537 39 41 43 35
40
45
50
55
60
65
70
75
80
85
90
95
35
40
45
50
55
60
65
70
75
80
85
90
95
%RC
%RCAircraft weight (kg x 1000) Aircraft weight (kg x 1000)
E23_011_232A
Take-off42.9
MTOW 93 500 kg
MLW 77 800 kg
MZFW 73 800 kg
80.3
75.5
79.2
4
0
.
6
Take-off/landing
Flight
Flight
Landing
89.0
91.5
17.515.3
3
9.5
15.5
19.6
5
17
21.6
5
36.8
837
.83
39.1
6
Page 55
-
03 General aircraft design criteria A320 Family
Intentionally left blank
Issue 6 Revision 1, January 2012
03.20.600 [ 03-18]Page 56
-
Issue 6 Revision 1, January 2012
[ 11-1]
A320 Family Placards and markings 11
Reference Title11.00.124 Installation of leasing identification plates11.20.100 Second language for door operation external placards and markings11.20.110 Second language for selected external placards and markings11.20.119 Nose Landing Gear (NLG) permanent steering markers11.20.135 Second language for residual cabin & cargo pressure exterior door warning placards11.21.101 Emergency cut-out markings11.22.100 Landing gear placards11.30.100 Installation of additional access placards in forward and aft cargo holds11.30.121 Second language for cargo compartment placards11.30.136 US and metric units for cargo compartment height placards11.33.101 Placard for flight crew oxygen system
Page 57
-
11 Placards and markings A320 Family
Is [ 11-2]
1
OTo
BMfrAe
DLpcoe
NTcob
EIn
Page 58sue 6 Revisio
1.00.12
bjectiveo install sn the aircr
asic aircranufacturame of the SELCAL l.
escriptioeasing plaer frame ockpit side
r requirem
otehe wordinntracts a
efore the s
PAC seledividualn 1, January 2012 11.00.124
4 - Installation of leasing identification plates
upplementary (leasing) identification plates aft.
after and owner plates are installed on the forward RH passenger/crew/service door.
plate is installed on the main instrument pan-
ntes are installed on each engine, on the up-f the forward LH passenger door and on the of lavatory A partition according to custom-ents.
g of the plates shall be provided to AIRBUS s soon as possible or at the latest one week tart of the ground check.
ction mode
-
Placards and markings 11
Issue 6 Revision 1, January 2012 11.00.124
A320 Family
[ 11-3]
Table 11-1 - Technical solutions descriptionTDU Title (Remarks) Appl. Weight (kg)
MWE/OWE/APLEquipmentreference
Equipmentsupplier
EquipmentPN
QTY STS
01 Installation of leasing identifi-cation plates on engines, LH door frame and Lav A partition
A318-100A319-100A320-200A321-200
Negl./Negl./Negl.Negl./Negl./Negl.Negl./Negl./Negl.Negl./Negl./Negl.
02 Installation of leasing identifi-cation plates on engines
A318-100A319-100A320-200A321-200
Negl./Negl./Negl.Negl./Negl./Negl.Negl./Negl./Negl.Negl./Negl./Negl.
03 Installation of leasing identifi-cation plates on LH door frame
A318-100A319-100A320-200A321-200
Negl./Negl./Negl.Negl./Negl./Negl.Negl./Negl./Negl.Negl./Negl./Negl.
04 Installation of leasing identifi-cation plates on Lavatory A partition
A318-100A319-100A320-200A321-200
Negl./Negl./Negl.Negl./Negl./Negl.Negl./Negl./Negl.Negl./Negl./Negl.
Page 59
-
11 Placards and markings A320 Family
Is [ 11-4]
1 l placards and markings
OTdg
BE
DTo
(Ta
N
mode
Page 60sue 6 Revisio
1.20.10
bjectiveo provideoor operauage) inst
asic aircrxterior pla
escriptiohe followinperation, s
passengcargo dohese ma
ge).
otethe transcustomeessary, sity scalean indivilanguagebookletsn 1, January 2012 11.20.100
0 - Second language for door operation externa
exterior placards and markings related to tion in bilingual (English and a second lan-ead of English only.
aftcards and markings are in English.
ng exterior placards and markings, related to hall be bilingual:er/crew doors and emergency exits ors. rkings are considered as one single pack-
lation of the basic English wording into the rs nominated language and a graphic, if nec-hall be provided by the customer (high qual-
one printout and/or floppy disk)dual RFC has to be issued with the second identification (refer to external markings
).
EPAC selection Individual
-
Placards and markings 11
Issue 6 Revision 1, January 2012 11.20.100
A320 Family
[ 11-5]
Table 11-2 - Technical solutions descriptionTDU Title (Remarks) Appl. Weight (kg)
MWE/OWE/APLEquipmentreference
Equipmentsupplier
EquipmentPN
QTY STS
01 Second language for door operation external placards and markings
A318-100A319-100A320-200A321-200
Negl./Negl./Negl.Negl./Negl./Negl.Negl./Negl./Negl.Negl./Negl./Negl.
Second language TBD TBD SFE
Page 61
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11 Placards and markings A320 Family
Is [ 11-6]
1 rds and markings
OTbE
BE
DIncasim
N
EIn
Page 62sue 6 Revisio
1.20.11
bjectiveo provide ilingual (English onl
asic aircrxternal pla
escriptio addition tbin press
ble to selearkings a
otethe transcustomeessary, san indiviguage idplacardsbooklets
PAC seledividualn 1, January 2012 11.20.110
0 - Second language for selected external placa
selected external placards and markings in nglish and a second language) instead of y.
aftcards and markings are in English.
no the external placards dedicated to residual ure warnings and doors operation, it is pos-ct some of the others external placards and
s bilingual ones.
lation of the basic English wording into the rs nominated language and a graphic, if nec-hall be provided by the customerdual RFC has to be issued for second lan-entification and the selection of concerned and markings (refer to external markings ). ction mode
-
Placards and markings 11
Issue 6 Revision 1, January 2012 11.20.110
A320 Family
[ 11-7]
Table 11-3 - Technical solutions descriptionTDU Title (Remarks) Appl. Weight (kg)
MWE/OWE/APLEquipmentreference
Equipmentsupplier
EquipmentPN
QTY STS
01 Second language for selected external placards and mark-ings (A319)
A319-100 Negl./Negl./Negl. Second language TBD TBD SFE
02 Second language for selected external placards and mark-ings (A320)
A320-200 Negl./Negl./Negl. Second language TBD TBD SFE
03 Second language for selected external placards and mark-ings (A321)
A321-200 Negl./Negl./Negl. Second language TBD TBD SFE
04 Second language for selected external placards and mark-ings (A318)
A318-100 Negl./Negl./Negl. Second language TBD TBD SFE