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Model A320-214, Approved December 12, 1996.
Engines:
Model A320-111, Two CFMI Model CFM-56-5A1 jet engines;
Model A320-211, Two CFMI Model CFM-56-5A1 jet engines;
Model A320-212, Two CFMI Model CFM56-5A3 jet engines;
Model A320-214, Two CFMI Model CFM56-5B4 or CFM56-5B4/P or CFM56-5B4/2P jet engines;
Model A320-231, Two IAE Model V2500-A1 jet engines;
Model A320-232, Two IAE Model V2527–A5 jet engines;
Model A320-233, Two IAE Model V2527E–A5 jet engines;
Fuel:
See Installation Manual - Documents CFM 2026 or IAE-0043
SPECIFICATION
NOMENCLATURE FRANCE U.S.A U.K.
Kerosene Air 3405C ASTM D 1655 (JET A1) (JET A) DERD 2494
Wide Cut Air 3407 ASTM D 1655 (JET B) DERD 2454
Air 3407 (TR4) MIL-T 5624 (JP4) DERD 2454
High Flash Point Air 3404 MIL-T 5624 (JP5) DERD 2452
Additives: See CFMI “Specific Operating Instructions”, CFM TPOI-13 or IAE V2500 “Installation and Operation Manual”
IAE-0043, 4.5. The above mentioned fuels and additives are also suitable for the APU.
Engine Limits:
CFMI CFM56-
5A1
CFMI CFM56-
5A3
CFMI CFM56-
5B4 or -5B4/P or
–5B4/2P
IAE V2500-A1 IAE V2527-A5
or V2527E-A5
Engine Limitation Data Sheets Data Sheets Data Sheets Data Sheets Data Sheets
E28NE (FAA) E28NE (FAA) E37NE E38NE FAA E31NE (FAA) E40NE (FAA)
Static Thrust at Sea
Level
- Take-off (5 min)**
(Flat rated 30°C)
11 120 daN
(25,000 lb)
11 787 daN
(26,500 lb)
12 010 daN
(27,000 lb)
11 030 daN
(24,800 lb)
11 030 daN
(24,800 lb)
- Maximum Continuous
(Flat rated 25°C)
10 542 daN
(23,600 lb)
10 542 daN
(23,600 lb)
10 840daN
(24,370 lb)
9 890 daN
(22,240lb)
9 890 daN
(22,240lb)
Maximum Engine
Speed
- N1 rpm (%) 5,100 (102) 5,100 (102) 5,200 (104) 5,465 (100) 5,650 (100)
- N2 rpm (%) 15,183(105) 15,183(105) 15,183(105) 14,915(100) 14,950(100)
Eng. limit/
Max Gas Temp.(°C) ECAM
- Take-off (5 min)** 890 915/890 950 635 645
- Max Continuous 855 880/855 915 610 610
- Starting* 725 725/725 725 635 650
A28NM Page 9 of 22
Maximum Oil Temp.
(Supply Pump Inlet; °C)
-Takeoff, Stabilized 140 140 140 155 155
-Transient
(15 min max)
155 155 155 165 165
Min. Press. (PSI) 13 13 13 60 60
Approved oils See SB See SB See SB See doc IAE See doc IAE
CFMI 79-001-
0X
CFMI 79-001-
0X
CFMI 79-001-0X 0043 (MIL-L
23699)
0043 (MIL-L
23699)
* 4 consecutive cycles of 2 minutes each.
** 10 minute at take-off thrust allowed in case of engine failure (at take-off and during go-around)
Airspeed Limits (Indicated Airspeed - IAS - Unless otherwise Stated:
- Maximum Operating Mach - MMO: 0.82
- Maximum Operating Speed - VMO: 350 kt
- Maneuvering Speed VA: - See Chapter 2.0 of the DGAC-approved Flight Manual
- Extended Flaps/Slats Speed - VFE
Configuration Slats/Flaps VFE (Kt)
1 18/0 230 Intermediate
Approach
*18/10 215 Take-off
2 22/15 200 Take-off and
Approach
3 22/20 185 Take-off,
Approach, and
Landing
Full 27/35 177 Landing
* Auto flap retraction at 210 kt in Take-off configuration.
Landing Gear:
- VLE - Extended 280 Kt/Mach 0.67
- VLO - Extension 250 kt
- Retraction 220 kt
Tire Limit Speed (Ground Speed) = 195.5 kt (225 mph)
Minimum Control Speed:
A320-100:
- VMCA (Air): 105 kt
- VMCG (Ground): 102 kt (all config.)
A320-200:
- VMCA (Air) and VMCG (Ground): See TAB program issue M or N with associated A/C performances module
Maximum Weights:
A320-100:
000
VARIANT (BASIC)
(KG) (LBS)
Max. Ramp Weight 68,400 150,820
Max. Take-off Weight 68,000 149,940
Max. Landing Weight 63,000 138,915
Max. Zero Fuel Weight 59,000 130,100
A28NM Page 10 of 22
A320-200:
FAA Approved
Weight Variants
000
BASIC
001 003 007 008 009 010 011 012 013 014
A320-211 YES YES YES YES YES YES YES YES YES
A320-212 YES YES YES YES YES YES YES YES YES YES
A320-214 YES YES YES YES YES YES YES YES YES YES
A320-231 YES YES YES YES YES YES YES YES YES
A320-232 YES YES YES YES YES YES YES YES YES YES
A320-233 YES YES YES YES YES YES YES YES YES YES
VARIANT 000
BASIC
001 003 007 008 009 010 011 012 013 014
(KG)
(LBS)
(KG)
(LBS)
(KG)
(LBS)
(KG)
(LBS)
(KG)
(LBS)
(KG)
(LBS)
(KG)
(LBS)
(KG)
(LBS)
(KG)
(LBS)
(KG)
(LBS)
　
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