Airbus A310 Seats

Airbus A310 has a maximum seat capacity of 200 seats. SEATMAESTRO has actually in data base seat maps for 3 aircrafts and for 5 among which Adria Airways. Choosing the best seat on Airbus A310 will also depend on the airlines configuration of seats and different the class offered onboard. We recommend once using our general information for best aircraft seats on Airbus A310 that you also consider taking notice of the seat maps of the airline by aircraft.

Class	Pitch	Seats	Recline
Business Class	n/a	19	n/a
Economy Class	n/a	200	n/a
Economy Class	n/a	176	n/a

Seats
2-5 A,K : This seat has all the pros and perks of a standard Business class seat as well as good views (weather and flight time depending).
2-5 A,K : This seat has all the pros and perks of a standard Business class seat and it is easy to get out of if you are in a rush to get off the plane or to go to the loo.
7,8 A,K : Good views (weather and flight time depending). No one will be climbing past you to get in and out of their seat.
7,8 B,D,G, : Easy to get out of if you are in a rush to get off the plane or to go to the loo!
7,8 E,F : No view but then no bumps from trolleys.
6 A,K : Good views (weather and flight time depending). No one will be climbing past you to get in and out of their seat. You will get extra legroom.
6 B,D,G,H : Easy to get out of if you are in a rush to get off the plane or to go to the loo! You will get extra legroom.
6 E,F : No view but then no bumps from trolleys. You will get extra legroom.

BAe 146-300 / AVRO RJ100

BAe 146-300 / AVRO RJ100

Regional Airliner

The British Aerospace BAe 146-300 / AVRO RJ100 is a four-engined regional airliner with a capacity of maximum 128 passengers produced by the British manufacturer British Aerospace (today BAE Systems). It is part of the BAe 146 / AVRO RJ family of regional airliner.

Crew	2
Passengers	100-116, max. 128
Propulsion	4 Turbofan Engines
Engine Model	Lycoming / Honeywell ALF 502R-5 (LF507-1F)
Engine Power (each)	31 (31,1) kN	6970 (7000)lbf
Speed	780 km/h	421 kts 484 mph
Mmo (max. Mach)	Mach 0.73
Service Ceiling	9.449 (10.668) m	31.000 (35.000) ft
Range	2.815 (2.759) km	1.520 (1.490) NM 1.749 (1.715) mi.
Empty Weight	24.880 (25.600) kg	54.850 (56.440) lbs
max. Takeoff Weight	45.132 (46.040) kg	99.500 (101.500) lbs
max. Landing Weight	39.236 (40.143) kg	86.500 (88.500) lbs
Wing Span	26,34 m	86,4 ft
Wing Area	77,3 m²	832 ft²
Length	30,99 m	101,7 ft
Height	8,59 m	28,2 ft
First Flight	01.05.1987 (13.05.1992)
Production Status	out of production
Production Range	1987-2003
Total Production	71 (71), Total 142
Developed from	BAe 146-100
ICAO Code	B463, RJ1H
FAA TCDS	A49EU
EASA TCDS	A.182
other TCDS	CAA UK BA16
Data for (Version)	BAe 146-300 (RJ100)
Variants	BAe 146-300, AVRO RJ100, BAe 146-300QC, BAe 146-300QT

Remarks
The BAe 146 was developed by Hawker Siddeley as the HS.146. The BAe 146-300 is a stretched variant of the BAe 146-100 (+4,81m / 15ft 8in). The AVRO RJ100 is a modernized variant which was introduced in 1992.

BAe 146-200 / AVRO RJ85

BAe 146-200 / AVRO RJ85
Regional Airliner
The British Aerospace BAe 146-200 / AVRO RJ85 is a four-engined regional airliner with a capacity of maximum 112 passengers produced by the British manufacturer British Aerospace (today BAE Systems). It is part of the BAe 146 / AVRO RJ family of regional airliner.

Crew	2
Passengers	85-112
Propulsion	4 Turbofan Engines
Engine Model	Lycoming / Honeywell ALF 502R-5 (LF507-1F)
Engine Power (each)	31 (31,1)kN	6970 (7000)lbf
Speed	780 km/h	421 kts 484 mph
Mmo (max. Mach)	Mach 0.73
Service Ceiling	9.449 (10.668) m	31.000 (35.000)ft
Range	2.908 (2.963) km	1.570 (1.600) NM 1.807 (1.841) mi.
Empty Weight	23.882 (24.603) kg	52.650 (54.240) lbs
max. Takeoff Weight	42.184 (43.998) kg	93.000 (97.000) lbs
max. Landing Weight	36.741 (38.555) kg	81.000 (85.000) lbs
Wing Span	26,34 m	86,4 ft
Wing Area	77,3 m²	832 ft²
Length	28,55 m	93,7 ft
Height	8,61 m	28,2 ft
First Flight	01.08.1982 (23.03.1992)
Production Status	out of production
Production Range	1983-2003
Total Production	116 (87), Total 203
Developed from	BAe 146-100
ICAO Code	B462, RJ85
FAA TCDS	A49EU
EASA TCDS	A.182
other TCDS	CAA UK BA16
Data for (Version)	BAe 146-200 (RJ85)
Variants	BAe 146-200, AVRO RJ85, BAe 146-200QC, BAe 146-200QT

RemarksThe BAe 146 was developed by Hawker Siddeley as the HS.146. The BAe 146-200 is a stretched variant of the BAe 146-100 (+2,36m / 7ft 9in).The AVRO RJ85 is a modernized variant which was introduced in 1992.

BAe 146-100 / AVRO RJ70

BAe 146-100 / AVRO RJ70

Regional Airliner

The British Aerospace BAe 146-100 / AVRO RJ70 is a four-engined regional airliner with a capacity of maximum 94 passengers produced by the British manufacturer British Aerospace (today BAE Systems). It is part of the BAe 146 / AVRO RJ family of regional airliner.

Crew	2
Passengers	70-94
Propulsion	4 Turbofan Engines
Engine Model	Lycoming / Honeywell ALF 502R-5 (LF507-1F)
Engine Power (each)	31 (31,1)kN	6970 (7000)lbf
Speed	780 km/h	421 kts 484 mph
Mmo (max. Mach)	Mach 0.73
Service Ceiling	9.449 (10.668) m	31.000 (35.000) ft
Range	3.000 (3.074) km	1.620 (1.660) NM 1.864 (1.910) mi.
Empty Weight	23.288 (23.900) kg	51.341 (52.690)lbs
max. Takeoff Weight	38.102 (43.091) kg	84.000 (95.000)lbs
max. Landing Weight	35.153 (37.875) kg	77.500 (83.500) lbs
Wing Span	26,34 m	86,4 ft
Wing Area	77,3 m²	832 ft²
Length	26,16 m	85,8 ft
Height	8,61 m	28,2 ft
First Flight	03.09.1981 (23.06.1992)
Production Status	out of production
Production Range	1983-2003
Total Production	35 (12), Total 47
ICAO Code	B461, RJ70
FAA TCDS	A49EU
EASA TCDS	A.182
other TCDS	CAA UK BA16
Data for (Version)	BAe 146-100A (RJ70)
Variants	BAe 146-100, AVRO RJ70, BAe 146-100QC, BAe 146-100QT, BAe 146 Statesman

Remarks
The BAe 146 was developed by Hawker Siddeley as the HS.146. The AVRO RJ70 is a modernized variant which was introduced in 1992.

BAe 125-1000 / Hawker 1000

 

The BAe 125-1000 / Hawker 1000 is a twin-engined long-range corporate travel jet aircraft for max. 15 passengers produced by the British manufacturer BAe, British Aerospace and later by the US-American manufacturer Raytheon, today Hawker Beechcraft.

Crew	2
Passengers	15
Propulsion	2 Turbofan Engines
Engine Model	Pratt & Whitney Canada PW305
Engine Power (each)	23,2kN	5222lbf
Speed	867 km/h	468kts 539 mph
Service Ceiling	13.106 m	43.000ft
Range	6.375 km	3.442 NM 3.961 mi.
Empty Weight	7.629 kg	16.819lbs
max. Takeoff Weight	14.061 kg	31.000lbs
Wing Span	15,66 m	51,4ft
Wing Area	34,8 m²	375ft²
Length	16,42 m	53,9ft
Height	5,21 m	17,1ft
First Flight	16.06.1990
Production Status	out of production
Total Production	52
EASA TCDS	A.085
Data for (Version)	BAe 125-1000

Remarks
The BAe 125-1000 is a stretched long-range development of the BAe 125-800.

BAe 125-800 / Hawker 800

The BAe 125-800 / Hawker 800 is a series of twin-engined corporate jet aircraft for max. 15 passengers produced by the British manufacturer BAe, British Aerospace and later by the US-American manufacturer Raytheon, today Hawker Beechcraft. The BAe 125-800 series include the BAe 125-800 / Hawker 800 (BAe.125 Series 800A & Series 800B), the Hawker Beechcraft Hawker 800XP, Hawker 850XP, Hawker 900XP and the Hawker 750. The Hawker U-125A is a search and rescue (SAR) variant for the Japan Air Self Defense Force.

Crew	2
Passengers	8-14
Propulsion	2 Turbofan Engines
Engine Model	AlliedSignal TFE-731-5BR1H
Engine Power (each)	20,7kN	4654lbf
Speed	845 km/h	456kts 525 mph
Mmo (max.Mach)	Mach 0.80
Service Ceiling	12.497 m	41.000ft
Range	4.430 km	2.392 NM 2.753mi.
Empty Weight	7.075 kg	15.598lbs
max. Takeoff Weight	12.700 kg	28.000lbs
Wing Span	15,66 m	51,4ft
Wing Area	34,8 m²	375ft²
Length	15,60 m	51,2ft
Height	5,36 m	17,6ft
First Flight	26.05.1983 (HS 125-800)
Production Status	in production
Developed from	Hawker-Siddeley / BAe HS-125, DeHavilland D.H.125
FAA TCDS	A3EU
EASA TCDS	A.085
Data for (Version)	Hawker 800XP
Variants	BAe.125 Series 800A, Series 800B, Hawker 800, Hawker 800XP, Hawker 850XP, Hawker 900XP, Hawker 750, U-125, U-125A

Remarks
The BAe 125-800 is a development of the earlier Hawker Siddeley HS.125 (British Aerospace BAe 125) and is the successor of the BAe 125-700. The BAe 125-800 / Hawker 800 differs from the BAe 125-700 in the following major respects: new Garrett/AlliedSignal TFE 731-5R engines, increased wing span, new avionics including EFIS (Electronic Flight Instrument System), higher certified weights and a higher speed. The Hawker 800XP is equipped with more powerful AlliedSignal TFE 731-5BR engines. The Hawker 850XP differs from the Hawker 800XP by addition of winglets on the outboard wings. The Hawker 900XP is equipped with Honeywell TFE731-50R engines and new avionics equipment and offers a longer range. The Hawker 750 differs from the Hawker 800XP by having an external baggage unit in place of the aft ventral fuel tank. The range and MTOW is less than that of the Hawker 800XP as a result of the decrease in available fuel. Current (2010) production models are the Hawker 750 and the Hawker 900XP.

BAe ATP

The BAe ATP is a twin-engined turboprop regional airliner with a capacity of maximum 72 passengers produced by the British manufacturer BAe, British Aerospace (today BAE Systems).

Crew	2
Passengers	max. 72
Propulsion	2 Turboprop Engines
Engine Model	Pratt & Whitney Canada PW126A
Engine Power (each)	1978 kW	2653 shp
Speed	493 km/h	266kts 306mph
Service Ceiling	7.620 m	25.000ft
Range	1.824 km	985 NM 1.134mi.
Empty Weight	14.193 kg	31.290lbs
max. Takeoff Weight	22.930 kg	50.552lbs
Wing Span	30,63 m	100,5 ft
Wing Area	78,3 m²	843 ft²
Length	26,00 m	85,3 ft
Height	7,14 m	23,4 ft
First Flight	01.04.1984
Production Status	out of production
Total Production	64
Developed from	Hawker Siddeley HS 748
Data for (Version)	BAe ATP

Remarks
The ATP -(A)dvanced (T)urbo (P)rop- is a development of the Hawker Siddeley HS 748.