History of Aircraft - History of JAS
History of Aircraft
(JAS) 1954-2004
Introducing the history of aircraft of JAS (Japan Air System Co., Ltd.
1954-1973
January
DH-114-1B-TAW
In service from January 25, 1954 to June 13, 1973.
Open
| Aircraft versions | DH-114-TAW(TAWRON) |
|---|---|
| Manufacture | De Havilland Aircraft Company |
| Engine Model | Continental IO-470-D |
| Maximum Take off Thrust× Number of Engines Installed |
260hp×4 |
| Overall Length(m)/Wing Span(m)/ Overall Heigth(m) |
14.8m/21.8m/4.8m |
| Cruising Speed(km/hr) | 280km/h |
| Maximum Range(km) | 1,930km (MAX) |
| Fuel Tank Capacity (Volume/Weight) |
384US gal |
| Seatting Capacity | 16 |
1965-2006
April
YS-11
In service from April 10, 1965 to December 20, 2006.
Open
| Aircraft versions | YS-11 |
|---|---|
| Manufacture | Nippon Aeroplane Manufacturing company |
| Engine Model | Rolls Royce DART MK542-10J/K |
| Maximum Take off hrust× Number of Engines Installed |
3,060HP×2 |
| Overall Length(m)/Wing Span(m)/ Overall Heigth(m) |
26.3m/32.0m/9.0m |
| Cruising Speed(km/hr) | 444km/h |
| Maximum Takeoff(Landing) Weight(t) |
25t (25t) |
| Maximum Range(km) | 1,110km |
| Fuel Tank Capacity (Volume/Weight) |
4,928l/3,957kg |
| Seatting Capacity | 64 |
| Flight Crew | 2 |
1972-1975
Boeing 727-100
In service from 1972 to 1975.
Open
| Aircraft versions | Boeing 727-100 |
|---|---|
| Manufacture | Boeing Company |
| Engine Model | Pratt & Whitney PWJT8D-9 |
| Maximum Take off Thrust× Number of Engines Installed |
6,580kg×3 |
| Overall Length(m)/Wing Span(m)/ Overall Heigth(m) |
46.7m/32.9m/10.5m |
| Cruising Speed(km/hr) | 880km/h |
| Maximum Range(km) | 2,170km |
| Fuel Tank Capacity (Volume/Weight) |
29140l |
| Seatting Capacity | 178 |
| Flight Crew | 3 |
1973-1997
September
CV-240
In service from September 11, 1973 to January 31, 1997.
Open
| Aircraft versions | DC9-31/DC9-41 |
|---|---|
| Manufacture | McDonnell Douglas Corporation (Boeing) |
| Engine Model | Pratt & Whitney JT8D-15 |
| Maximum Take off Thrust× Number of Engines Installed |
15,000 lbs×2 |
| Overall Length(m)/Wing Span(m)/ Overall Heigth(m) |
38.3m/28.4m/8.5m |
| Cruising Speed(km/hr) | 815km/h |
| Maximum Takeoff(Landing) Weight(t) |
52t (46t) |
| Maximum Range(km) | 2,420km |
| Fuel Tank Capacity (Volume/Weight) |
16,120l/12,943kg |
| Seatting Capacity | 128 |
| Flight Crew | 2 |
1980-2006
June
A300-B2(A300-B4)
In service from June 26, 1980 to June 13, 2006.
Open
| Aircraft versions | A300-B2 [A300-B4] |
|---|---|
| Manufacture | Airbus industrie |
| Engine Model | General Electric CF6-50C 2R |
| Maximum Take off Thrust× Number of Engines Installed |
51,000 lbs×2 |
| Overall Length(m)/Wing Span(m)/ Overall Heigth(m) |
53.6m/44.8m/16.5m |
| Cruising Speed(km/hr) | 848km/h |
| Maximum Takeoff(Landing) Weight(t) |
137t (130t) [150t (134t)] |
| Maximum Range(km) | 2,820km [3,480km] |
| Fuel Tank Capacity (Volume/Weight) |
43,993 l/35,322kg |
| Seatting Capacity | 298 |
| Flight Crew | 3 |
1981-1999
January
DC9-81/MD-81
In service from January 26, 1981 to September 27, 1999.
Open
| Aircraft versions | DC9-81/MD-81 |
|---|---|
| Manufacture | McDonnell Douglas Corporation (Boeing) |
| Engine Model | Pratt & Whitney JT8D-217A/C |
| Maximum Take off Thrust× Number of Engines Installed |
20,000 lbs×2 |
| Overall Length(m)/Wing Span(m)/ Overall Heigth(m) |
45.1m/32.9m/9.0m |
| Cruising Speed(km/hr) | 815km/h |
| Maximum Takeoff(Landing) Weight(t) |
64t (58t) |
| Maximum Range(km) | 2,740km |
| Fuel Tank Capacity (Volume/Weight) |
22,104 l/17,748kg |
| Seatting Capacity | 163 |
| Flight Crew | 2 |
1988-2008
June
MD-87
In service from June 3, 1988 to May 19, 2008.
Open
| Aircraft versions | MD-87 |
|---|---|
| Manufacture | McDonnell Douglas Corporation (Boeing) |
| Engine Model | Pratt & Whitney JT8D-217A/C |
| Maximum Take off Thrust× Number of Engines Installed |
20,000 lbs×2 |
| Overall Length(m)/Wing Span(m)/ Overall Heigth(m) |
39.8m/32.9m/9.3m |
| Cruising Speed(km/hr) | 815km/h |
| Maximum Takeoff(Landing) Weight(t) |
57t (54t) |
| Maximum Range(km) | 2,370km |
| Fuel Tank Capacity (Volume/Weight) |
22,104 l/17,748kg |
| Seatting Capacity | 134 |
| Flight Crew | 2 |
1988-2000
April
DC-10-30
In service from April 1, 1988 to April 20, 2000.
Open
| Aircraft versions | DC-10-30[International] |
|---|---|
| Manufacture | McDonnell Douglas Corporation(Boeing) |
| Engine Model | General Electric CF6-50C2 |
| Maximum Take off Thrust× Number of Engines Installed |
51,800 lbs×3 |
| Overall Length(m)/Wing Span(m)/ Overall Heigth(m) |
55.3m/50.4m/17.6m |
| Cruising Speed(km/hr) | 891km/h |
| Maximum Takeoff(Landing) Weight(t) |
193t (186t) [268t (186t)] |
| Maximum Range(km) | 9,700km [10,460km] |
| Fuel Tank Capacity (Volume/Weight) |
151,300 l/121,467kg |
| Seatting Capacity | 295 [276] |
| Flight Crew | 3 |
1991-2011
April
A300-600R
In service from April 28, 1991 to September 16, 2011.
Open
| Aircraft versions | A300-600R [International] |
|---|---|
| Manufacture | Airbus industrie |
| Engine Model | Pratt & Whitney PW4158 |
| Maximum Take off Thrust× Number of Engines Installed |
58,000 lbs×2 |
| Overall Length(m)/Wing Span(m)/ Overall Heigth(m) |
54.1m/44.8m/16.5m |
| Cruising Speed(km/hr) | 848km/h |
| Maximum Takeoff(Landing) Weight(t) |
144t (140t) [172t (140t)] |
| Maximum Range(km) | 3,890km [6,760km] |
| Fuel Tank Capacity (Volume/Weight) |
68,150 l/54,720kg |
| Seatting Capacity | 292 [239] |
| Flight Crew | 2 |
1995-2013
January
MD-90
In service from July 3, 1995 to May 21, 2013.
Open
| Aircraft versions | MD-90 |
|---|---|
| Manufacture | McDonnell Douglas Corporation(Boeing) |
| Engine Model | International AeroEngines V2525-D5 |
| Maximum Take off Thrust× Number of Engines Installed |
25,000 lbs×2 |
| Overall Length(m)/Wing Span(m)/ Overall Heigth(m) |
46.5m/32.9m/9.4m |
| Cruising Speed(km/hr) | 815km/h |
| Maximum Takeoff(Landing) Weight(t) |
66t (64t) |
| Maximum Range(km) | 2,330km |
| Fuel Tank Capacity (Volume/Weight) |
22,104 l/17,748kg |
| Seatting Capacity | 166 |
| Flight Crew | 2 |
1997
April
Boeing 777-200
Introduced on April 1997.
Open
| Aircraft versions | Boeing 777-200 |
|---|---|
| Manufacture | Boeing Company |
| Engine Model | Pratt & Whitney PW4074 |
| Maximum Take off Thrust× Number of Engines Installed |
74,500 lbs×2 |
| Overall Length(m)/Wing Span(m)/ Overall Heigth(m) |
63.7m/60.9m/18.5m |
| Cruising Speed(km/hr) | 893km/h |
| Maximum Takeoff(Landing) Weight(t) |
208t (202t) |
| Maximum Range(km) | 5,000km |
| Fuel Tank Capacity (Volume/Weight) |
117,300 l/94,184kg |
| Seatting Capacity | 380 |
| Flight Crew | 2 |
2001-2004
A300-600R