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(KG)
(LBS)
Max. Ramp
Weight
73900
162949
68400
150822
75900
167360
77400
170667
73900
162950
75900
167360
77400
170667
75900
167360
77400
170667
71900
158512
73900
162949
Max. Takeoff
Weight
73500
162068
68000
149940
75500
166478
77000
169785
73500
162068
75500
166478
77000
169785
75500
166478
77000
169785
71500
157631
73500
162068
Max.
Landing
Weight
64500
142223
64500
142223
64500
142223
64500
142223
64500
142223
64500
142223
64500
142223
66000
145505
66000
145505
64500
142223
64500
142223
Max. Zero
Fuel
Weight
60500
133403
60500
133403
60500
133403
60500
133403
61000
134505
61000
134505
61000
134505
62500
137789
62500
137789
61000
134505
61500
135584
Minimum Weight:
A320-100:
VARIANT 000
(BASIC)
(KG) (LBS)
Minimum Weight 36,750 81,030
A320-200:
VARIANT All
(KG) (LBS)
Minimum Weight 37,230 82,080
Minimum Crew:
2 Pilots
Maximum Passengers:
179
Maximum Baggage:
CARGO COMPARTMENT MAXIMUM LOAD
(KG) (LBS)
Forward 3,402 7,500
Aft 4,536 10,000
Rear (Bulk) 1,497 3,300
For the positions and the loading conditions authorized in each position (references of containers, pallets, and associated
weights), see Weight and Balance Manual, ref. 00D080A0001/C1S Chapter 1.10.
A28NM Page 11 of 22
Fuel Capacity (0.8 kg/liter):
A320-100:
2-Tank Airplane
Tank Usable Fuel Unusable Fuel
Liters (kgs) Gallons (lbs) Liters (Kgs) Gallons (lbs)
Wing 15,843 4,185 57.3 15.1
(12,674) (27,946) (45.8) (101.0)
Total 15,843 4,185 57.3 15.1
(12,674) (27,946) (45.8) (101.0)
3-Tank Airplane
Tank Usable Fuel Unusable Fuel
Liters (kgs) Gallons (lbs) Liters (Kgs) Gallons (lbs)
Wing 15,843 4,185 58.9 15.6
(12,674) (27,946) (47.1) (103.9)
Center 8,250 2,179 23.2 6.1
(6,600) (14,484) (19.6) (43.2)
TOTAL 24,093 6,364 82.1 21.7
(19,274) (42,430) (65.7) (147.1)
A320-200:
Tank Usable Fuel Unusable Fuel
Liters (kgs) Gallons (lbs) Liters (Kgs) Gallons (lbs)
Wing 15,609 4,124 58.9 15.6
(12,487) (27,534) (47.1) (103.9)
Center 8,250 2,179 23.2 6.5
(6,600) (14,484) (19.6) (41.0)
TOTAL 23,859 6,304 82.1 20.8
(19,087) (42,087) (65.7) (144.9)
Oil Capacity:
CFMI CFM56-5A/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:
- 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.
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 modification applicable to it.
Refer to Type Certification Standard Equipment List 00D000A0101/C1S.
Refer Note 4 for list of A320 airplane model FAA Type Definitions.
Serial Numbers Eligible:
A320 aircraft, all series, all models, are produced in Blagnac (France) under approval P09 or F.G.035 issued by DGAC to
Airbus.
A French "Certificat de Navigabilite pour Exportation," endorsed as noted under "Import Requirement," must be submitted for
each individual aircraft for which application for U.S. certification is made.
A28NM Page 12 of 22
Import Requirements:
A FAA Standard Airworthiness Certificate may be issued on the basis of a French "Certificat de Navigabilite pour Exportation,"
signed by a representative of the Direction Generale de 1'Aviation Civile (DGAC) of France, 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
　
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