SPECIFICATIONS
Overall Dimensions
Imperial |
Metric |
Series |
|
Wing span |
88ft 6in 93ft 6in |
26.98m 28.50m |
200/300/400 475/500 |
Wing chord at root
|
16ft 5in 16ft 9.5in |
5.01m 5.11m |
All versions except 475/500 (late prod) |
Wing chord at tip |
5ft 3.5in 5ft 5in |
1.61m 1.65m |
All versions except 475/500 (late prod) |
Wing aspect ratio |
8.0 8.5 8.65 |
|
200/300/400 500 (early prod) 475/500 (late prod) |
Sweepback at quarter chord |
20 degrees |
|
All versions |
Overall length |
93ft 6in 107ft 0in |
28.50m 32.61m |
200/300/400/475 500 |
Fuselage length |
83ft 10in 97ft 4in |
25.55m 29.67m |
200/300/400/475 500 |
Max fuselage width/depth |
11ft 2in |
3.40m |
All versions |
Overall height |
24ft 6in |
7.47m |
All versions |
Tailplane span |
29ft 6in |
8.99m |
All versions |
Ground clearance to fuselage |
2ft 7.5in |
0.80m |
All versions |
Wheel track |
14ft 3in |
4.34m |
All versions |
Wheel base |
33ft 1in 33ft 0in 41ft 4in |
10.08m 10.06m 12.60m |
200/300/400 475 500 |
Overall turning radius measured to outer wing tip |
51ft 6in 56ft 0in |
15.70m 17.07m |
200/300/400/475 500 |
Forward passenger doorHeight Width Height to sill |
5ft 8in 2ft 8in 7ft 0in |
1.73m 0.82m 2.13m |
All versions All versions All versions |
Ventral entranceHeight Width Height to sill |
6ft 0in 2ft 4in 7ft 0in |
1.83m 0.71m 2.13m |
All versions All versions All versions |
Galley service doorHeight Width Height to sill |
4ft 0in 2ft 3in 7ft 0in |
1.22m 0.69m 2.13m |
All versions All versions All versions |
Overwing emergency exitsHeight Width |
3ft 0in 1ft 8in |
0.91m 0.51m |
All versions All versions |
Main deck freight doorHeight Width Height to sill |
6ft 1in 10ft 0in 7ft 0in |
1.85m 3.05m 2.13m |
400/475 400/475 400/475 |
Underfloor frt door (Fwd)Height (projected) Width Height to sill |
2ft 7in 3ft 0in 3ft 7in |
0.79m 0.91m 1.09m |
All versions All versions All versions |
Underfloor frt door (Rear)Height (projected) Width Height to sill |
2ft 2in 3ft 0in 4ft 3in |
0.66m 0.91m 1.30m |
All versions All versions All versions |
Internal Dimensions
|
Imperial |
Metric |
Series |
Cabin length (including flight deck) |
56ft 10in 70ft 4in |
17.31m 21.44m |
200/300/400/475 500 |
Max cabin width |
10ft 4in |
3.16m |
All versions |
Max cabin height |
6ft 6in |
1.98m |
All versions |
Max floor width |
9ft 6in |
2.98m |
All versions |
Floor area (approx)
|
506ft² 665ft² |
47.00m² 61.78m² |
200/300/400/475 500 |
Forward freight holdHeight Width Length
Volume |
3ft 0in 7ft 5in 17ft 11in 22ft 10in 354ft³ 451ft³ |
0.91m 2.26m 2.46m 6.96m 10.02m³ 12.77m³ |
All versions All versions 200/300/400/475 500 200/300/400/475 500 |
Rear freight holdHeight Width Length
Volume |
3ft 0in 7ft 5in 11ft 6in 10ft 0in 15ft 0in 180ft³ 156ft³ 236ft³ |
0.91m 2.26m 3.51m 3.06m 4.59m 5.09m³ 4.42m³ 6.68m³ |
All versions All versions 200/300/400 475 500 200/300/400 475 500 |
External Areas
|
Imperial |
Metric |
Series |
Gross wing area
|
980ft² 1031ft² |
91.04m² 95.78m² |
200/300/400 475/500 |
Ailerons (total) |
30.8ft² |
2.86m² |
All versions |
Flaps (total) |
175.6ft² |
16.30m² |
All versions |
Spoilers (total) |
24.8ft² |
2.30m² |
300/400/475/500 |
Vertical tail surface (total) |
117.4ft² |
10.90m² |
All versions |
Rudder (including tab) |
32.8ft² |
3.05m² |
All versions |
Horizontal tail surface (total) |
257ft² |
23.9m² |
All versions |
Elevators (including tab) |
70.4ft² |
6.55m² |
All versions |
Weights & Loadings
|
Imperial |
Metric |
Series |
Typical Operating Weight Empty (varies with customer fit) |
46,405lb 48,722lb 50,822lb 51,822lb 51,731lb 54,582lb |
21,049kg 22,098kg 23,050kg 23,505kg 23,464kg 24,758kg |
200 300 400 NAL 400 475 500 |
Maximum Payload |
17,595lb 20,025lb 21,269lb 26,418lb |
7,981kg 9,083kg 9,647kg 11,983kg |
200 300/400 475 500 |
Maximum Take-off Weight |
79,000lb 88,500lb 98,500lb 104,500lb |
35,833kg 40,142kg 44,678kg 47,400kg |
200 300/400 475 500 |
Maximum Landing Weight
|
71,000lb 78,000lb 87,000lb |
32,204kg 35,380kg 39,462kg |
200 300/400 475/500 |
Maximum Zero Fuel Weight (varies between customers – typical figure shown) |
64,000lb 71,000lb 68,500lb 73,000lb 81,000lb |
29,030kg 32,204kg 31,070kg 33,112kg 36,741kg |
200 300/400 NAL 400 475 500 |
Maximum Wing Loading |
78.3lb/ft² 88.8lb/ft² 89.2lb/ft² 96.7lb/ft² |
382.0kg/m² 433.6kg/m² 435.5kg/m² 472.0kg/m² |
200 300/400 475 500 |
Maximum Power Loading |
3.82lb/lb st 3.96lb/lb st 4.16lb/lb st |
390.1kg/kN 400.3kg/kN 424.7kg/kN |
300/400 475 500 |
The Maximum Ramp Weight figure for each model is 500lb (226.8kg) greater than the quoted MTOW figure shown above.
Performance
|
|
Series |
Max level cruising speed at 21,000ft (6,400) TAS |
548mph (475kt, 882km/h) 541mph (470kt, 871km/h) |
200/300/400 475/500 |
Fuel economical cruising speed at 25,000ft (7,620m) TAS |
507mph (440kt, 815km/h) 461mph (400kt, 742km/h) |
200/300/400 475/500 |
Max never exceed diving speed (structural) EAS at sea level |
460mph (399kt, 740km/h) 472mph (410kt, 760km/h) |
200 300/400/475/500 |
Stalling speed (take-off flap setting) EAS |
125mph (109kt, 201km/h) 131mph (114kt, 211km/h) 114mph (99kt, 184km/h) 121mph (105kt, 195km/h) |
200 300/400 475 500 |
Rate of climb at sea level at 345mph (300kt, 555km/h) EAS |
2,500ft/min (762m/min) 2,580ft/min (786m/min) 2,480ft/min (756m/min) 2,280ft/min (695m/min) |
200 300/400 475 500 |
Maximum cruise altitude |
35,000ft (10,670m) 37,000ft (11,285m) 40,000ft (12,200m) |
200 300/400/475/500 NAL 400 |
Still air range with max Fuel, ISA, with reserves for 230 miles (200nm, 370km) diversion and 45 minutes hold |
2,130 miles (3,430km) 2,250 miles (3,620km) 2,300 miles (3,700km) 2,165 miles (3,484km) |
200* 300/400 475 500 |
Still air range with capacity payload, ISA, reserves as above |
875 miles (1,140km) 1,430 miles (2,300km) 1,865 miles (3,000km) 1,705 miles (2,744km) |
200 300/400 475 500
|
Ferry range with zero payload, ISA, reserves as above |
2,617 miles (4,215km) 2,477 miles (3,988km) 2,430 miles (3,912km) 2,339 miles (3,766km) 2,206 miles (3,552km) 3,950 miles (6,357km) |
200* 300 400 475 500 NAL 400 |
Still air range with max standard fuel, ten passengers and 45 minutes reserve |
3,753 miles (6,040km) |
NAL 400 |
Still air range with max optional fuel, eight passengers and 45 minutes reserve |
3,950 miles (6,357km) |
NAL 400 |
Take-off run at sea level, ISA |
6,500ft (1,981m) 7,500ft (2,286m) 7,450ft (2,270m) 5,500ft (1,676m) 6,500ft (1,981m) |
200 300 400 475 500 |
Balanced take-off to 35ft (10.70m) at sea level, ISA |
6,850ft (2,088m) 8,000ft (2,438m) 7,800ft (2,377m) 5,900ft (1,798m) 7,300ft (2,225m) |
200 300 400 475 500 |
Landing distance (BCAR) at sea level, ISA, at max landing weight |
4,720ft (1,439m) |
475 |
Flap operating speedsTake-off setting |
253mph,(220kt, 408km/h) 276mph,(240kt, 445km/h) |
200 300/400/500 |
Approach setting |
207mph,(180kt, 334km/h) 220mph,(191kt, 354km/h) 222mph,(193kt, 358km/h) |
200 300/400/475 500 |
Landing setting |
190mph,(165kt, 306km/h) 207mph,(180kt, 334km/h) 211mph,(183kt, 339km/h) |
200 300/400 475/500 |
Landing gear operating speedsApproach setting |
253mph,(220kt, 408km/h) 265mph,(230kt, 427km/h) |
200 All other |
* With optional centre tank
One-Eleven Series 200
The initial production version was the Series 200, powered by 46.3 KN Rolls-Royce RB163 Spey 506-14 turbofans. The aircraft (G-ASHG cn 004) first flew from Hurn on the 20 August 1963. First delivery went to Braniff Airways (N1543 cn 017) on 11 March 1965, while British United Airways received their first aircraft (G-ASJJ cn 014) on 6 April 1965. Other customers for this version were Braniff Airways, Mohawk Airlines, Aer Lingus, and Aloha Airlines. Three aircraft were also supplied new as corporate jets to Helmut Horten GmbH and Tenneco Inc, while two others were delivered to the Royal Australian Air Force. The last aircraft (N503T cn 183) was delivered to Tenneco on the 8 July 1969. A total of 58 Series 200 aircraft were built.
One-Eleven Series 300
In May 1963 BAC announced two new versions of the One-Eleven; the Series 300 and Series 400, both of which offered more powerful Spey 511-14s of 50.7 kN thrust, fitted into lengthened nacelles. Although dimensions were the same as the Series 200, the Series 300 offered longer range by virtue of an additional centre section fuel tank and a higher maximum take-off weight. The aircraft (G-ATPJ cn 033) first flew from Weybridge on the 20 May 1966. First delivery went to British Eagle International Airways (G-ATPJ cn 033) on 8 June 1966 while Laker Airways received their first aircraft on the 25 February 1967. The Series 300 was only ordered by three customers, British Eagle, Laker and Kuwait Airways who cancelled their order. The last aircraft was delivered to Laker (G-AVYZ cn 133) on the 11 April 1968. A total of 9 Series 300 aircraft were built.
One-Eleven Series 400
The Series 400 was originally configured with a maximum take-off weight of 36060 kgs, which was lower than the Series 300’s 40000 kgs due to US restrictions on the gross weight for two-crew operation. With the easing of the restrictions, the maximum take-off weights of US-operated Series 400s were brought into line with those of the Series 300 through adoption of 300’s additional centre-section fuel tank and the two models became effectively indistinguishable. The aircraft (G-ASYD cn 053) first flew from Hurn on the 13 July 1965. First delivery went to American Airlines (N5015 cn 055) on 23 December 1965. Other Series 400 customers included Austral, Autair, Bahamas Airways, Bavaria Flug, Channel Airways, Lacsa, Philippine Airlines, Quebecair, Tarom and VASP. One aircraft was supplied new as a corporate jet to Engelhard Industries, and two were delivered as transports to the Brazilian Air Force. The last Series 400 was delivered to Bavaria Flug (D-ANNO cn 160) on the 22 December 1970. A total of 70 Series 400 aircraft were built. Many former airline aircraft were subsequently converted to executive configuration and in particular 16 former American Airlines aircraft were converted by the Dee Howard Company at San Antonio for National Aircraft Leasing Inc. it is these aircraft that make up the great majority of the still active Series 400 fleet.
One-Eleven Series 475
The Series 475 was the last UK-built version of the One-Eleven, conceived to bring improved field performance to the One-Eleven range, in addition to the capability to operate from unprepared runways. These goals were achieved by combining the standard length fuselage of the Series 400 with the increased wingspan and more powerful engines of the Series 500 and a new undercarriage fitted with larger low pressure tyres. The Series 475’s maximum take-off weight was 44678 kg. The Aircraft (G-ASYD cn 053) first flew from Hurn on the 27 August 1970. The first delivery went to Faucett of Peru (OB-R-953 cn 239) on 23 July 1971. Further airline orders for the Series 475 came from Air Malawi, Air Pacific and Tarom. Three were fitted out as corporate jets and three more were supplied to the Air Force of the Sultanate of Oman, all of which were eventually fitted with a large cargo door (3.05m x 1.85m) on the port forward fuselage. The last two Series 475 (G-BLHD cn 260 and G-BLDH cn 262) were delivered to McAlpine Aviation on the 9 July 1984 A total of 13 Series 475 aircraft were built.
One-Eleven Series 500
The Series 500 was launched on the strength of an order placed on the 27th January 1967 by British European Airways. This version had the fuselage extended by 13ft 6in (4.11m) by the insertion of two plugs. This allowed for four more seat rows to be installed and therefore increased passenger capacity by twenty. Overwing emergency exits had to be doubled to four. Underfloor hold volume was increased. Various structural changes were also required and higher rated Speys were fitted. This gave the aircraft a maximum take-off weight of 47400 kg. The aircraft (G-ASYD cn 053) first flew from Hurn on the 30 June 1967. First delivery (G-AVMJ cn 138) went to British European Airways on the 29 August 1968. Other Series 500 customers included British United Airways, Caledonian Airways, Panair / Paninternational, Aviateca, Bahamas Airways, Court Line, Sadia / Transbrasil, ALA / Austral, British Midland Airways, Germanair, Tarom, Philippine Airlines, Bavaria, Phoenix Airways, Lacsa, Cyprus Airways and Britsh Airways. The last delivery went to Tarom (YR-BCO cn 272) on the 12 Mar 1982 and was the last ever airliner to be constructed at Hurn! A total of 87 Series 500 aircraft were built.
One-Eleven Series 670
A plan to supply a Series 475 derivative, the Series 670, as a YS-11 replacement to Japanese carriers resulted in one aircraft (G-ASYD cn 053) being developed and flown from Hurn on the 13 September 1977 as such, but hopes of a significant sales break through were ultimately frustrated, despite major improvements in performance, due to the Japanese authorities introducing more stringent regulatory requirements.
Rombac One-Eleven Series 560
An agreement for the licenced production of the One-Eleven at the Romanian Government aircraft (IRMA) factory in Baneasa, Romania on was signed 9 June 1979. As the first step towards the transfer of One-Eleven production, BAC produced two Series 525 passenger aircraft and a single windowless freighter Series 485 which were supplied to CNIAR as training models. A further 22 One-Elevens were then to be supplied in kit form from the UK and assembled locally with gradually increasing Romanian content. The first Rombac One-Eleven, (YR-BRA cn 401) a series 561RC was rolled out at Baneasa on 27 August 1982, and flew for the first time on 18 September 1982. Plans for the production of 80 One-Elevens in the country were however curtailed by political and social unrest and in the end only 9 Series 561s were produced between September 1982 and April 1989. The first aircraft was delivered to Tarom on 29 December 1982. The Romanian carrier took delivery of all but two of the aircraft produced, with the remaining two going to Romavia, the last of which (YR-BRI cn 409) was delivered on 1 January 1993. Two further aircraft were partially completed when production was abandoned and scrapped.
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