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A319 Model -131 A320 Model -231
A319 Model -132 A320 Model -232
A320 Model -233
A321 Model -111
A321 Model -112
A321 Model -131
A321 Model -211
A321 Model -231
September 18, 2002
TYPE CERTIFICATION DATA SHEET A28NM
This Data Sheet which is part of Type Certificate No. A28NM prescribes conditions and limitations under which the product for
which the Type Certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations.
Type Certificate Holder: Airbus
1, Rond-Point Maurice Bellonte
31707 Blagnac, France
Type Certificate Holder Record Name change from Airbus Industrie to Airbus January 2002
I. Type A319-100 Series Transport Category Airplanes
Model A319-112, Approved August 30, 1996;
Model A319-111, Approved June 20, 1997;
Model A319-113, Approved June 20, 1997;
Model A319-114, Approved June 20, 1997;
Model A319-131, Approved June 20, 1997;
Model A319-132, Approved June 20, 1997;
Engines:
Model A319-111, Two CFMI Model CFM56-5B5 or CFM56-5B5/P jet engines;
Model A319-112, Two CFMI Model CFM56-5B6 or CFM56-5B6/P or CFM56-5B6/2P jet engines;
Model A319-113, Two CFMI Model CFM56-5A4 jet engines;
Model A319-114, Two CFMI Model CFM56-5A5 jet engines;
Model A319-131, Two IAE Model V2522-A5 jet engines;
Model A319-132, Two IAE Model V2524-A5 jet engines;
Fuel:
See Installation Manual - Documents CFM 2026 or IAE-0043
SPECIFICATION
NOMENCLATURE FRANCE U.S.A U.K.
Kerosene MIL-T83133A (JP8)
Air 3405C ASTM D1655 (Jet Al) (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," CMF TPOI-13 or IAE V2500 “Installation and Operating Manual”
IAE-0043, 4. The above mentioned fuels and additives are also suitable for the APU.
A28NM Page 2 of 22
Engine Limits:
CFMI CFM56-5B5 or -
5B5/P
CFMI CFM56-5B6 or -
5B6/P or -5B6/2P
CFMI CFM56-5A4
Engine FAA Data Sheets FAA Data Sheets FAA Data Sheet
Limitation E37NE E38NE E37NE E38NE E28NE
Static Thrust at Sea Level
- Take-off (5 min)** 9 786 daN (22,000 lb) 10 453 daN (23,500 lb) 9 786 daN (22,000 lb)
(Flat rated 30°C)
Maximum Continuous 9 008 daN (20,250 1b) 9 008 daN (20,250 1b) 9 195 daN (20,670 1b)
(Flat rated 25°C)
Maximum Engine Speed
- N1 rpm (%) 5,200 (104) 5,200 (104) 5,100 (102)
- N2 rpm (%) 15,183 (105) 15,183 (105) 15,183 (105)
Max Gas Temperature (°C) Eng. Limit/ ECAM
- Take-off (5 min)** 950 950 915/890
- Max Continuous 915 915 880/855
- Starting * 725 725 725/725
Max Oil Temperature
(supply pump inlet; °C)
- Take-off, Stabilized 140 140 140
- Transient (15 min max) 155 155 155
Min. Press. (PSI) 13 13 13
Approved Oils See SB See SB See SB
CFMI 79-001-0X CFMI 79-001-0X CFMI 79-001-0X
CFMI CFM56-5A5 IAE V2522-A5 IAE V2524-A5
Engine Limitation Data Sheets Data Sheets Data Sheets
E28NE (FAA) E40NE (FAA) E40NE (FAA)
Static Thrust at Sea Level
- Take-off (5 min)** 10 453 daN (23,500 lb) 10 249 daN (23,040 lb) 10 889 daN (24,480 lb)
(Flat rated 30°C)
Maximum Continuous 9 195 daN (20,670 1b) 8 540 daN (19,200 1b) 8 540 daN (19,200 1b)
(Flat rated 25°C)
Maximum Engine Speed
- N1 rpm (%) 5,100 (102) 5,650 (100) 5,650 (100)
- N2 rpm (%) 15,183 (105) 14,950 (100) 14,950 (100)
Max Gas Temperature (°C) Eng. Limit/ ECAM
- Take-off (5 min)** 915/890 645 645
- Max Continuous 880/855 610 610
- Starting * 725/725 650 650
Max Oil Temperature
(supply pump inlet; °C)
- Take-off, Stabilized 140 155 155
- Transient (15 min max) 155 165 165
Min. Press. (PSI) 13 60 60
Approved Oils See SB See Doc IAE 0043 Sec 4.9 See Doc IAE 0043 Sec 4.9
CFMI 79-001-0X (MIL-L-23699) (MIL-L-23699)
* 4 consecutive cycles of 2 minutes each.
** 10 minutes at take-off thrust allowed in case of engine failure (at take off and during go around).
A28NM Page 3 of 22
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 27/40 177 Landing
* Auto flap retraction at 210 kt in Take-off configuration.
　
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