A
B
C
D
SCN N°
ST
MN01.00.010
AC
1
2
3
4
A321-200
5
6
STANDARD SPECIFICATION :
E.000.02000 ISSUE 3
7
8
9
RFC
TITLE
10
ATA 01 General description
11
Introduction of A321-200 standard
specification at issue 3
12
ATA 02 Certification
13
DKN02E001B
14
DKN02E002B
15
DKN02E003B
16
DKN02E004B
17
DKN02E005B
18
DKN02E006B
19
20
21
DKN02E4010101S2B OP
DKN02E1010701S1B AC
DKN02E1012002S1B AC
DKN02E4010737S1B AC
DKN02E1210201S1B AC
DKN02E1211705S1B AC
DKN02E1010403B Certification of dynamically tested
passenger seats Y/C
DKN02E1010403S1B AC
15 knots tail wind certification at
DKN02E1012001B take-off
DKN02E1012001S1B AC
A321-200 ETOPS (EASA/JAA 120 min) DKN02E1024021B IAE V2530-A5
DKN02E1024021S1B AC
ATA 03 General aircraft design
criteria
22
23
External livery (drawing)
High altitude certification up to
12000 ft
15 knots tail wind certification at
landing
External livery - Apply colour on
passenger door 1 and 4 surround
Registration numbers on wings (L/H
lower surface)
Compliance status for FAR 121
A321-232 increased design weights MTOW 89 t unchanged, MLW to 77.8 t,
DKN03E2063202B
MZFW to 73.8 t (wv 002)
DKN03E2063202S1B AC
ATA 11 Placards and markings
24
25
DKN11E001B
26
DKN11E002B
27
DKN11E003A
28
DKN11E004B
Engine danger area decals - IAE
engines - specific (owner)
Exterior markings - Ram air turbine
caution markings
Nose landing gear steering (+/70°) and MAX TOW BAR ANGLE markings
Fuel cap locked position red
marking
DKN11E2010510S1B AC
DKN11E2011502S1B AC
DKN11E2011912S1B AC
DKN11E2012884S1B AC
Specifications and descriptions are provided as introductory information.
Accordingly you should rely on your own inspection of the aircraft
29
30
31
32
33
34
35
MSN number and design weight
placard in the cockpit
Seat row numbering placards - white
DKN11E006B
numbering on blue background
Bilingual passenger placards and
DKN11E007B
lighted signs
Bilingual EEPMS exit identifier English below (vertical) and second
DKN11E008B
language (horiz.) - AIRSIGNA
Bilingual English - lavatory
DKN11E009B
placards
Installation of customized placards
DKN11E012B
(owner)
Installation of leasing
identification plates on engines,
DKN11E0012401B LH door frame and lav A partition
DKN11E005B
DKN11E3110415S1B AC
DKN11E3010313S1B AC
DKN11E3011043S1B AC
DKN11E3011136S1B AC
DKN11E3012701S1B AC
DKN11E3012798S1B AC
DKN11E0012401S1B AC
DKN11E2110101S1B AC
37
DKN11E2110101B Emergency cut out markings
US and metric units for cargo
DKN11E3013601B compartment height placards
38
DKN11E3310101B Oxygen supply system label change
DKN11E3310101S1B AC
36
DKN11E3013601S1B AC
ATA 21 Air conditioning
39
40
Cabin air recirulation filter
cartridge equipment selection - Le
DKN21E2010806B Bozec
41
ATA 22 Auto flight
DKN21E2010806S1B AC
DKN22D001A
42
43
FM KITS/MCDUS ALTERNATE EQUIPMENT REV 2+ - THALES AVIONICS/SMITHS
ASSOCIATED WITH IAE ENGINES
Inhibition of the expedite push
AC
DKN22E8114301B button
DKN22E8114301S1B
ATA 23 Communications
44
45
DKN23E002I
46
DKN23E003B
47
DKN23E004B
CVR bulk erase facility
deactivation
Boomsets alternate equipment SENNHEISER - HME46-C
Installation of headset for fourth
occupant - SENNHEISER, model HD46K1
48
DKN23E005B
ENTERTAINMENT SYSTEM
DKN23E3600100G1B AC
49
DKN23E006B
CIDS CHANGES
Installation of single HF system DKN23E007B
HONEYWELL
Automatic programmable ELT with
prog. dongle associated with remote
DKN23E0013235B control panel in cockpit - THALES
VHF data radio alternate equipment,
capable VDL-Mode 2 - Honeywell (SFE
DKN23E1213013B 064-50000-2051)
Instal. of a third RMP with turbo
tuning of VHF channels and HF data
DKN23E1310106B activ. capability - THALES AVIONICS
DKN23E7300100G1B AC
50
51
52
53
DKN23E7117402S1B AC
DKN23E5113630S1B AC
DKN23E5013512S1B AC
DKN23E1111510S1B AC
DKN23E0013235S1B AC
DKN23E1213013S1B AC
DKN23E1310106S1B AC
Specifications and descriptions are provided as introductory information.
Accordingly you should rely on your own inspection of the aircraft
54
55
Installation of a Cockpit Door
DKN23E7011002B Survey System
SSCVR alternate equipment DKN23E7110310B HONEYWELL
DKN23E7011002S1B AC
DKN23E7110310S1B AC
ATA 25 Equipment / Furnishing
56
57
DKN25E001B
Cargo hold definition
DKN25E5000100G1B AC
58
DKN25E002B
Interior color scheme definition
DKN25E2350001S1B AC
59
DKN25E004B
CABIN LAYOUT DEFINITION
DKN25E2000100G1B AC
60
DKN25E005B
61
DKN25E006B
62
DKN25E007B
63
DKN25E008B
CABIN EMERGENCY EQUIPMENT
DKN25E0000100G2B
Installation of electrical galley
catering equipment
DKN25E3513010S1B
Installation of non-electrical
galley catering equipment
DKN25E3513110S1B
Installation of BFE stowage in LH &
RH of forward door 3
DKN25E2717023S1B
64
DKN25E009B
65
DKN25E010B
66
DKN25E011B
67
DKN25E012B
68
DKN25E013B
69
DKN25E014B
70
DKN25E015B
71
DKN25E016B
72
DKN25E017B
73
74
75
76
77
78
AC
AC
AC
AC
Installation of curtain rails
Installation of doghouses fwd of
lavatory D and E
Installation and storage of
auxiliary working table on aft wall
of lavatory E
Installation of plastic mirrors in
Lavatories
Installation of life raft (32
persons) - EASTERN AERO MARINE T32,
PN R1700-103
Space provisions for Philips
defibrillator
Installation of three first aid
kits in cabin - AEROMEDIC
INNOVATIONS, P/N 52001-25
Installation of emergency medical
kit in cabin - AEROMEDIC
INNOVATIONS, PN 520001-37
DKN25E2612920S1B AC
NTF installation in all lavatories
Installation of NTF Gerflor AVR 160
Batiflex, London Solo in Exit areas
DKN25E018B
and Galleys
Installation of seat belts outside
of emergency equipment
DKN25E020B
configuration guide
Non-installation of protective
cover for slide arming levers on
fwd & aft LH/RH emergency exit
DKN25E021B
doors
Installation of spare safety belt)
DKN25E022B
- AMSAFE, PN 2090-1-1-022-0585
Installation of fourth occupant
DKN25E1120803B seat in cockpit - Sogerma/Socea
Installation of double-sided
DKN25E2810302B adhesive tape for carpet
DKN25E2822453S1B AC
DKN25E2762106S1B AC
DKN25E4010102S1B AC
DKN25E4521004S1B AC
DKN25E6210621S1B AC
DKN25E6401214S1B AC
DKN25E6460041S1B AC
DKN25E6461022S1B AC
DKN25E2822471S1B AC
DKN25E6519770S1B AC
DKN25E6518404S1B AC
DKN25E6050013S1B OP
DKN25E1120803S1B AC
DKN25E2810302S1B AC
Specifications and descriptions are provided as introductory information.
Accordingly you should rely on your own inspection of the aircraft
79
DKN25E2812606B Welding of NTF joints
DKN25E2812606S1B AC
80
DKN25E2812607B NTF sealing for all cabin monuments
Installation of slide rafts at fwd
and aft pax/crew/service doors DKN25E6210203B AIR CRUISERS (A321)
Cockpit flashlights alternate
equipment) - DME CORPORATION, PN
DKN25E6500209B P2-07-0001-214
Installation of medical outlets in
aft RH PSU channel (115V/400Hz &
DKN25E6700101B 28V DC/360 W)
DKN25E2812607S1B AC
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
DKN25E6210203S1B AC
DKN25E6500209S1B AC
DKN25E6700101S1B AC
ATA 26 Fire protection
APU fire extinguisher alternate
DKN26E2010301B equipment - WALTER KIDDE
Engine fire extinguishers alternate
DKN26E2110401B equipment - WALTER KIDDE
Cargo holds fire extinguisher
extended duration for ETOPS 120 min
DKN26E2311104B (A321)
Cockpit portable fire extinguisher
alternate equipment - TOTAL
DKN26E2411103B FEUERSCHUTZ, PN 74-20
DKN26E2010301S1B AC
DKN26E2110401S1B AC
DKN26E2311104S1B AC
DKN26E2411103S1B AC
ATA 29 Hydraulic Systems
Hydraulic EDPs alternate equipment
DKN29E1011012B - EATON AEROSPACE, PN 3031863-001
Electropumps alternate equipment DKN29E2110407B EATON AEROSPACE
DKN29E1011012S1B AC
DKN29E2110407S1B AC
ATA 31 Indicating/Recording
FDIMU (-01-01) - FDIU S/W (-8802),
DKN31E3305105B DMU S/W (IA04) for IAE - TELEDYNE
SSFDR alternate equipment HONEYWELL (256 w/s capable) (SFE
DKN31E3320014B 980-4700-042)
DKN31E3305105S1B AC
DKN31E3320014S1B AC
ATA 32 Landing Gear
Wheel and brakes alternate
DKN32E4011330B equipment - MESSIER/BF GOODRICH
MLG tires alternate equipment MICHELIN (1270x455-R22 radial
DKN32E4111123B retreadable tires)
NLG tires selection - MICHELIN
DKN32E4112005B (30X8.8-R15 radial tires)
Installation of universal brake
cooling fans on Messier/BF Goodrich
DKN32E4820014B wheels and brakes
DKN32E4011330S1B AC
DKN32E4111123S1B AC
DKN32E4112005S1B AC
DKN32E4820014S1B AC
ATA 33 Lights
Installation of floor-mounted EEPMS
- LUFTHANSA T. -400 (with cover) /
DKN33E001B
Exit identifier - AIRSIGNA
DKN33E5011041S1B AC
Installation of brighter LED pilot
DKN33E1210902B chart holder and map reading lights DKN33E1210902S1B AC
103 DKN33E4300005B Alternate runway turn-off light
EC DKN33E4300005S1B AC
Specifications and descriptions are provided as introductory information.
Accordingly you should rely on your own inspection of the aircraft
104 DKN33E4600004B Alternate taxi and take-off lights
DKN33E4600004S1B AC
ATA 34 Navigation
105
106
DKN34E001B
107
DKN34E002B
108 DKN34E1011718B
109 DKN34E2020206B
110 DKN34E2020304B
111 DKN34E4131001B
112 DKN34E4210111B
113 DKN34E4320007B
Wiring provisions for T²CAS
DKN34E4324001S1B
Non installation of second ADF
antenna
DKN34E5312302S1B
ADIRS 4MCU - HONEYWELL , PN
HG2030AE23
DKN34E1011718S1B
Installation of ISIS - THALES
AVIONICS, PN C16221VA01
DKN34E2020206S1B
ISIS optional function - altitude
in meter
DKN34E2020304S1B
Dual WXR (ARINC 708A) with PWS
activation - HONEYWELL
DKN34E4131001S1B
Radio altimeters alternate
equipment - HONEYWELL, PN 06650007-0222
DKN34E4210111S1B
TCAS change 7 - HONEYWELL TPA 100 /
ATC ELS, EHS - HONEYWELL (-1402)
DKN34E4320007S1B
AC
AC
AC
AC
AC
AC
AC
AC
114 DKN34E5010409B DDRMI VOR/ADF/DME - THALES AVIONICS DKN34E5010409S1B AC
DME interrogators alternate
115 DKN34E5110109B equipment - HONEYWELL
119 DKN34E5831321B
Full provision for second ADF
system
ADF system alternate equipment HONEYWELL (066-50014-0202)
VOR/MARKER receivers alternate
equipment - HONEYWELL
MMR alternate equipment providing
ILS (FM immunity) and GPS C1
functions - HONEYWELL
120
ATA 35 Oxygen
116 DKN34E5310901B
117 DKN34E5311103B
118 DKN34E5510210B
121
122
123
124
Installation of Protective
Breathing Equipment (PBE) in cabin
Cockpit oxygen cylinder alternate
equipment 115cuft (composite) DKN35E1120104B EROS
Installation of four oxygen masks
DKN35E2001001B per box
Cockpit PBE alternate equipment DKN35E3110818B B/E Aerospace
DKN35E001B
125
ATA 38 Water / Waste
126 DKN38E1010402B
Installation of water conditioner
in potable water system (A318,
A319, A321)
127
ATA 46 Information systems
128
129
ATSU alternate equipment (h/w -070
s/w CSB4.1) - ARINC 615A data load
DKN46E2100007B - VDL mode 2 & FANS A+
Activation of VDL mode 2 for ACARS
DKN46E2111102B in ATSU (CSB4.1)
DKN34E5110109S1B AC
DKN34E5310901S1B AC
DKN34E5311103S1B AC
DKN34E5510210S1B AC
DKN34E5831321S1B AC
DKN35E3212042S1B AC
DKN35E1120104S1B AC
DKN35E2001001S1B AC
DKN35E3110818S1B AC
DKN38E1010402S1B AC
DKN46E2100007S1B AC
DKN46E2111102S1B AC
Specifications and descriptions are provided as introductory information.
Accordingly you should rely on your own inspection of the aircraft
ATA 49 APU
130
APU alternate equipment -
131 DKN49E0010506B HONEYWELL, GTCP131-9A
DKN49E0010506S1B AC
ATA 51 Structure
132
133
DKN51E001B
134
DKN51E002B
135
DKN51E003B
136
DKN51E004B
137
DKN51E005B
Application of adhesive decorative
films (decal) with a red edge on
vertical stabilizer
Application of adhesive decorative
films (decal) with a red edge on
nacelles
External low VOC paint system
(nacelles) - ANAC
DKN51E2226037S1B AC
DKN51E2226038S1B AC
DKN51E2241014S1B AC
Additional clear coat
ANAC (CF primer, strippable) on
fuselage & vertical stabilizer
DKN51E2241016S1B AC
KFR51E2271003S1B AC
ATA 52 Doors
138
installation of deadbolt on
139 DKN52E5110603B reinforced cockpit door
DKN52E5110603S1B AC
ATA 53 Fuselage
140
Erosion prevention on belly fairing
141 DKN53E3005001B panels - additional extrusion
DKN53E3005001S1B AC
Ram air inlet leading edge
142 DKN53E3510002B protection (aluminum)
ATA 55 Stabilizers
143
144
DKN53E3510002S1B AC
Installation of erosion protection
on vertical stabilizer leading edge
DKN55E3010101B - stainless steel
DKN55E3010101S1B AC
145
ATA 56 Windows
146 DKN56E1010211B Alternate lateral windows
147
DKN56E1010211S1B AC
ATA 72 Engines
IAE engines - V2530-A5 at 30000 lbf
148 DKN72E0012131B nominal thrust (A321-232)
DKN72E0012131S1B AC
Avionics summary
Multi-Mode Receiver
Honeywell
2
Radio Altimeter Transceiver
Honeywell
2
Weather Radar Transceiver
Honeywell
1
Enhanced GPWS
Honeywell
1
ATC Transponder
Honeywell
2
TCAS II Computer
Honeywell
1
ATSU
Aerospatiale
Specifications and descriptions are provided as introductory information.
Accordingly you should rely on your own inspection of the aircraft
FMGC
Thales
2
Flight Augmentation Computer
Thales
2
HF Com Transceiver
Honeywell
1
VHF Com Transceiver
Honeywell
3
Fixed ELT
Thales
1
Pre-recorded Ann. & Music
Matshushita
1
Cockpit Voice Recorder
Honeywell
1
Flight Data Recorder (SSFDR)
Honeywell
1
Flight Data Unit
Sagem
1
Air Data/Inertial Reference Unit
Honeywell
Integrated Standby Inst. System
Thales
1
VOR Receiver
Honeywell
2
ADF Receiver
Honeywell
1
DME Interrogator
Honeywell
2
DDRMI (VOR/ADF/DME)
Thales
Specifications and descriptions are provided as introductory information.
Accordingly you should rely on your own inspection of the aircraft