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Airbus A319 / ACJ

 

airbusa319
A319-113


The 124-145 seat A319 followed the A321, in June 1993. A shortened fuselage (by 3.77 m) version of the A320 with a standard two-class cabin configuration and a range of up to 6500km with payload.


Essentially a seven-frame shrink of the A320 (it was originally designated the A320M-7), the A319 retains the wing of the A320, but the inboard spoilers are deleted. The cockpit and flight characteristics are identical to the A320 and its stretched derivative, the A321, which allows for Cross Crew Qualification.


The A319 was launched officially in June 1993, although International Lease Finance Corp (ILFC) had already announced an order for six (plus two options) during the previous December. Two of these were placed with Swissair, which, in March 1994, became the first airline to place a firm order for the A319.


The A319, assembled by Daimler-Benz Aerospace Airbus at Hamburg-Finkenwerder, was first flown on August 25, 1995, and was certificated by the European Joint Airworthiness Authorities (JAA) on April 10, 1996.


96 of the first 120 A319s ordered were to be powered by the CFM International CFM56-5. Flight certification tests of the international Aero Engines V2500-powered A319, which will be delivered to United, started on May 22 1996.

 

Airbus-319-2
A319-115CJ 9H-SNA

 

Based on the A319, the ACJ (Airbus Corporate Jet) differs mainly in having up to six extra fuel tanks in its cargo hold as well as a higher ceiling of 41,000 ft.

Engines: CFM56-5A4, 22,000 lb st / 97.9 kN
Wing span: 34.10m / 111ft 10in
Length: 33.84m / 111ft
Height: 11.76m / 38ft 7in
Fuselage width: 3.95m / 12ft 11in
Max landing: 61,000 kg /134,500 lb
Max zero fuel: 57,000 kg /125,700 lb
Operating empty: 40,100 kg / 88,500 lb
Max payload: 16,900 kg / 37,200 lb
Max fuel cap: 23,860 lt /6,300 USG
Max seats: 145
Max takeoff (basic): 64,000 kg /141,100 lb
Under floor cap: (basic): 27.64 sq.m / 976 cu ft
Cruising speed: Mach 0.78-0.80
Max cruising altitude: 39,000ft / 12,000m
Wing area: 123 sq.m / 1323.96 sq ft
Crew: 2
Max payload range (FAR domestic reserves, 200nm alternate)
Basic MGTOW    680 nm /1,260 km
(68t option MGTOW):     1,475 nm /2,730 km
(70t option MGTOW):     1,800 nm /3,330 km
Max range (124 passengers + bags)
(FAR domestic reserves, 200nm alternate)
Basic MGTOW:    1,900 nm /3,510 km
(68t option MGTOW):   2,650 nm /4,900 km
(70t option MGTOW):   3,000 nm /5,550 km

Engines: CFM56-5A5, 23,500 lb st / 104.5 kN
Wing span: 34.10m / 111ft 10in
Length: 33.84m / 111ft
Height: 11.76m / 38ft 7in
Fuselage width: 3.95m / 12ft 11in
Max landing: 61,000 kg /134,500 lb
Max zero fuel: 57,000 kg /125,700 lb
Operating empty: 40,100 kg / 88,500 lb
Max payload: 16,900 kg / 37,200 lb
Max fuel cap: 23,860 lt /6,300 USG
Max seats: 145
Max takeoff  (option): 70,000 kg /154,300 lb
Under floor cap: (basic): 27.64 sq.m / 976 cu ft
Cruising speed: Mach 0.78-0.80
Max cruising altitude: 39,000ft / 12,000m
Wing area: 123 sq.m / 1323.96 sq ft
Crew: 2
Max payload range (FAR domestic reserves, 200nm alternate)
Basic MGTOW    680 nm /1,260 km
(68t option MGTOW):     1,475 nm /2,730 km
(70t option MGTOW):     1,800 nm /3,330 km
Max range (124 passengers + bags)
(FAR domestic reserves, 200nm alternate)
Basic MGTOW:    1,900 nm /3,510 km
(68t option MGTOW):   2,650 nm /4,900 km
(70t option MGTOW):   3,000 nm /5,550 km

Engines: CFM56-5B5, 22,000 lb st / 97.9 kN
Wing span: 34.10m / 111ft 10in
Length: 33.84m / 111ft
Height: 11.76m / 38ft 7in
Fuselage width: 3.95m / 12ft 11in
Max landing: 61,000 kg /134,500 lb
Max zero fuel: 57,000 kg /125,700 lb
Operating empty: 40,100 kg / 88,500 lb
Max payload: 16,900 kg / 37,200 lb
Max fuel cap: 23,860 lt /6,300 USG
Max seats: 145
Max takeoff  (option): 68,000 kg /149,900 lb
Under floor cap: (basic): 27.64 sq.m / 976 cu ft
Cruising speed: Mach 0.78-0.80
Max cruising altitude: 39,000ft / 12,000m
Wing area: 123 sq.m / 1323.96 sq ft
Crew: 2
Max payload range (FAR domestic reserves, 200nm alternate)
Basic MGTOW    680 nm /1,260 km
(68t option MGTOW):     1,475 nm /2,730 km
(70t option MGTOW):     1,800 nm /3,330 km
Max range (124 passengers + bags)
(FAR domestic reserves, 200nm alternate)
Basic MGTOW:    1,900 nm /3,510 km
(68t option MGTOW):   2,650 nm /4,900 km
(70t option MGTOW):   3,000 nm /5,550 km

Engines: CFM56-5B6, 23,500/ 104.5 kN
Wing span: 34.10m / 111ft 10in
Length: 33.84m / 111ft
Height: 11.76m / 38ft 7in
Fuselage width: 3.95m / 12ft 11in
Max landing: 61,000 kg /134,500 lb
Max zero fuel: 57,000 kg /125,700 lb
Operating empty: 40,100 kg / 88,500 lb
Max payload: 16,900 kg / 37,200 lb
Max fuel cap: 23,860 lt /6,300 USG
Max seats: 145
Max takeoff  (option): 70,000 kg /154,300 lb
Under floor cap: (basic): 27.64 sq.m / 976 cu ft
Cruising speed: Mach 0.78-0.80
Max cruising altitude: 39,000ft / 12,000m
Wing area: 123 sq.m / 1323.96 sq ft
Crew: 2
Max payload range (FAR domestic reserves, 200nm alternate)
Basic MGTOW    680 nm /1,260 km
(68t option MGTOW):     1,475 nm /2,730 km
(70t option MGTOW):     1,800 nm /3,330 km
Max range (124 passengers + bags)
(FAR domestic reserves, 200nm alternate)
Basic MGTOW:    1,900 nm /3,510 km
(68t option MGTOW):   2,650 nm /4,900 km
(70t option MGTOW):   3,000 nm /5,550 km

Engines: IAE V2522-A5, 22,000 lb st / 97.9 kN
Wing span: 34.10m / 111ft 10in
Length: 33.84m / 111ft
Height: 11.76m / 38ft 7in
Fuselage width: 3.95m / 12ft 11in
Max landing: 61,000 kg /134,500 lb
Max zero fuel: 57,000 kg /125,700 lb
Operating empty: 40,100 kg / 88,500 lb
Max payload: 16,900 kg / 37,200 lb
Max fuel cap: 23,860 lt /6,300 USG
Max seats: 145
Max takeoff (basic): 64,000 kg /141,100 lb
Under floor cap: (basic): 27.64 sq.m / 976 cu ft
Cruising speed: Mach 0.78-0.80
Max cruising altitude: 39,000ft / 12,000m
Wing area: 123 sq.m / 1323.96 sq ft
Crew: 2
Max payload range (FAR domestic reserves, 200nm alternate)
Basic MGTOW    680 nm /1,260 km
(68t option MGTOW):     1,475 nm /2,730 km
(70t option MGTOW):     1,800 nm /3,330 km
Max range (124 passengers + bags)
(FAR domestic reserves, 200nm alternate)
Basic MGTOW:    1,900 nm /3,510 km
(68t option MGTOW):   2,650 nm /4,900 km
(70t option MGTOW):   3,000 nm /5,550 km

Engines: IAE V2524-A5, 23,500 lb st / 104.5 kN
Wing span: 34.10m / 111ft 10in
Length: 33.84m / 111ft
Height: 11.76m / 38ft 7in
Fuselage width: 3.95m / 12ft 11in
Max landing: 61,000 kg /134,500 lb
Max zero fuel: 57,000 kg /125,700 lb
Operating empty: 40,100 kg / 88,500 lb
Max payload: 16,900 kg / 37,200 lb
Max fuel cap: 23,860 lt /6,300 USG
Max seats: 145
Max takeoff  (option): 70,000 kg /154,300 lb
Under floor cap: (basic): 27.64 sq.m / 976 cu ft
Cruising speed: Mach 0.78-0.80
Max cruising altitude: 39,000ft / 12,000m
Wing area: 123 sq.m / 1323.96 sq ft
Crew: 2
Max payload range (FAR domestic reserves, 200nm alternate)
Basic MGTOW    680 nm /1,260 km
(68t option MGTOW):     1,475 nm /2,730 km
(70t option MGTOW):     1,800 nm /3,330 km
Max range (124 passengers + bags)
(FAR domestic reserves, 200nm alternate)
Basic MGTOW:    1,900 nm /3,510 km
(68t option MGTOW):   2,650 nm /4,900 km
(70t option MGTOW):   3,000 nm /5,550 km

319-113

Engines: CFM56-5A4
Wing span: 34.10m / 111ft 10in
Length: 33.84m / 111ft
Height: 11.76m / 38ft 7in
Fuselage width: 3.95m / 12ft 11in

319-114
Engines: CFM56-5A5
Wing span: 34.10m / 111ft 10in
Length: 33.84m / 111ft
Height: 11.76m / 38ft 7in
Fuselage width: 3.95m / 12ft 11in

ACJ
Wing span: 34.10m / 111ft 10in
Length: 33.84m / 111ft
Height: 11.76m / 38ft 7in
Fuselage width: 3.95m / 12ft 11in
Pax cap: 50
Range: 10,000 km

 

 


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