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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)
Maximum Weights:
000 001 002
VARIANT BASIC Mod 25328 Mod 27112
(KG) (LBS) (KG) (LBS) (KG) (LBS)
Max. Take-Off Weight 64,000 141,090 70,000 154,322 75,500 166,447
Max. Landing Weight 61,000 134,480 61,000 134,480 62,500 137,787
Max. Zero Fuel Weight 57,000 125.660 57,000 125,660 58,500 128,969
Minimum Weight:
VARIANT All
Minimum Weight
(KG) (LBS)
35,400 78,042
Minimum Crew:
2 Pilots
Maximum Passengers:
145
Maximum Baggage:
CARGO COMPARTMENT MAXIMUM LOAD
(KG) (LBS)
Forward 2,268 5,000
Aft 3,020 6,660
Rear (Bulk) 1,497 3,300
For the positions and the loading conditions authorized in each position (references of containers, pallets, associated weights),
see Weight and Balance Manual, Ref. 00J080A0001/C1S Chapter 1.10.
A28NM Page 4 of 22
Fuel Capacity (0.8 kg/liter)
3-Tank Airplane
Tank Usable Fuel Unusable Fuel
Liters (kgs) Gallons (lbs) Liters (Kgs) Gallons (lbs)
Wing 15,609 4,124 58.9 15.6
(12,487) (27,531) (47.1) (103.9)
Center 8,250 2,179 23.2 6.5
(6,600) (14,551) (18.6) (41.0)
TOTAL 23,859 6,303 82.1 20.8
(19,087) (42,082) (65.7) (144.9)
4 to 9-Tank Airplane
Tank Usable Fuel Unusable Fuel
Liters (kgs) Gallons (lbs) Liters (Kgs) Gallons (lbs)
TOTAL
3-Tank 23,859 6,303 82.1 20.8
Airplane (19,087) (42,082) (65.7) (144.9)
ACT 1 3,121 824 17 4.3
(2,497) (5,505) (13.6) (28.8)
TOTAL
4-Tank 26,980 7,128 99.1 25.1
Airplane (21,584) (47,587) (79.3) (173.7)
ACT 2 3,121 824 17 4.3
(2,497) (5,505) (13.6) (28.8)
TOTAL
5-Tank 30,101 7,952 116.1 29.4
Airplane (24,081) (53,092) (92.9) (202.5)
ACT 3 2,186 577 22 5.6
(1,749) (3,855) (17.6) (37.4)
TOTAL
6-Tank 32,287 8,530 138.1 35.0
Airplane (25,830) (56,947) (110.5) (239.9)
ACT 4 2,186 577 22 5.6
(1,749) (3,855) (17.6) (37.4)
TOTAL
7-Tank 34,473 9,107 160.1 40.6
Airplane (27,579) (60,803) (128.1) (277.3)
ACT 5 3,046 804 12 3.1
(2,437) (5,372) (9.6) (20.6)
TOTAL
8-Tank 37,519 9,912 172.1 43.7
Airplane (30,016) (66,176) (137.7) (297.9)
ACT 6 3,121 824 17 4.3
(2,497) (5,505) (13.6) (28.8)
TOTAL
9-Tank 40,640 10,737 189.1 48.0
Airplane (32,513) (71,681) (151.3) (326.7)
Oil Capacity
CFMI CFM56-5B - Engine Oil Capacity, 10 quarts/engine (9.46 liters).
IAE V2500-A5 - Engine Oil Capacity, 7 quarts/engine (6.6 liters)
Maximum Operating Altitude:
- 41,000 feet (12,600 m) clean if modification 28162 is embodied.
- 39,800 feet (12,200 m) clean if modification 30748 is embodied.
- 39,100 feet (12,000 m) clean.
- 20,000 feet (6,500 m) Slats/Flaps extended.
A28NM Page 5 of 22
Equipment:
The basic equipment as prescribed in the airworthiness regulations (see certification basis) must be installed in the aircraft for
certification.
Equipment approved for installation are listed in the definition of the reference model and the modifications applicable to it.
Refer to Type Certification Standard Equipment Lists:
-00J000A0012/C0S for A319-111 Model
-00J000A0004/C0S for A319-112 Model
-00J000A0113/C0S for A319-113 Model
-00J000A0114/C0S for A319-114 Model
-00J000A0131/C0S for A319-131 Model
-00J000A0132/C0S for A319-132 Model
Refer to Note 4 for list of A319 airplane model FAA Type Definitions.
Serial Numbers Eligible:
A319 aircraft, all series, all models, are produced in Hamburg (Germany) under approval LBA.G.0009 or I-A9 issued by LBA to
Airbus.
A German Export Certificate of Airworthiness endorsed as noted under “Import Requirement,” must be submitted for each
individual aircraft for which application for U.S. certification is made.
Import Requirements:
A FAA Standard Airworthiness Certificate may be issued on the basis of a German Export Certificate of Airworthiness, signed
by a representative of the Luftfahrt-Bundesamt (LBA) of Germany, containing the following statement: “The Airplane covered
by this certificate has been examined, tested, and found to conform to the Type Design approved under Type Certificate No.
A28NM and to be in condition for safe operation.”
The U.S. airworthiness certification basis for aircraft type certificated under FAR Section 21.29 and exported by the country of
manufacture is FAR Sections 21.183(c) or 21.185(c). The U.S. airworthiness certification basis for aircraft type certificated
under FAR Section 21.29 exported from countries other than the country manufacture (e.g., third party country) is FAR Sections
　
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