Civilian aviation
Fokker 100
- Role: Narrow-body Regional jet airliner
- National origin: Netherlands
- Manufacturer: Fokker
- First flight: 30 November 1986
- Introduction: April 5, 1988 with Swissair
- Status: Out of production, in service
- Produced: 1986-1997
- Number built: 283
- Developed from: Fokker F28 Fellowship
- Variants: Fokker 70
Specifications
General characteristics
- Cockpit crew: Two
- Seating capacity: 122 (1-class, maximum)
- Overall length: 35.53 metres (116 ft 7 in)
- Wingspan: 28.08 metres (92 ft 2 in)
- Wing area: 93.5 square metres (1,006 sq ft)
- Overall height: 8.50 metres (27 ft 11 in)
- Fuselage width: 3.30 m (10 ft 10 in)
Fokker 100 with Rolls-Royce Tay Mk 620-15
- Operating empty weight: 24,375 kilograms (53,738 lb)
- Maximum payload weight: 11,242 kilograms (24,784 lb)
- Maximum take-off weight: 43,090 kilograms (95,000 lb)
- Engine (× 2): Rolls-Royce Tay Mk 620-15, thrust 13,850 lbf (61.6 kN)
Performance
- Service ceiling: 35,000 ft (11,000 m)
- Cruising speed: 845 km/h (525 mph, 456 kn), Mach 0.77
- Range fully loaded: 1,323 nautical miles (2,450 km; 1,522 mi)
Fokker 100 with Rolls-Royce Tay Mk 650-15
- Operating empty weight: 24,541 kilograms (54,104 lb)
- Maximum payload weight: 11,993 kilograms (26,440 lb)
- Maximum take-off weight: 45,810 kilograms (100,990 lb)
- Engine (× 2): Rolls-Royce Tay Mk 650-15 thrust 15,100 lbf (67.2 kN)
Performance
- Service ceiling: 35,000 ft (11,000 m)
- Cruising speed: 845 km/h (525 mph, 456 kn), Mach 0.77
- Range fully loaded: 1,710 nautical miles (3,170 km; 1,970 mi)
Airbus A320
Airbus A320 is the basis for a whole family of airliners, now including the A318, A319 and A321.The A320 was the first narrow body airliner from Airbus.
- Role: Narrow-body jet airliner
- National origin: European Multi-national
- Manufacturer: EADS/Airbus
- Production line: Toulouse – Blagnac, France
- First flight: 22 February 1987 F-WWAI
- Introduction: 18 April 1988 with Air France
- Status: In service
- Produced: 1986–present
- Number built: 3,867 February 2015
Variants A320 family
Specifications
General characteristics
- Cockpit crew: 2
- Seating capacity: – 156 one class
- Overall length: 33.84 m (111 ft 0 in)
- Wingspan: 34.10 m (111 ft 11 in) (35.8 m (117 ft 5 in) with sharklets)
- Overall height: 11.76 m (38 ft 7 in)
- Fuselage width: 3.95 m (13 ft 0 in)
- Fuselage Height: 4.14 m (13 ft 7 in)
- Operating empty weight: 40,800 kg (89,900 lb)
- Maximum landing weight: 62.5 t (138,000 lb)
- Maximum take-off weight: 75.5 t (166,000 lb)
- Engine (× 2):
- – CFM International CFM56-5A1 rated 111.2 kN.
- – CFM International CFM56-5A3 rated 117.88 kN.
- – CFM International CFM56-5B4 rated 117.9 kN.
- – International Aero Engines V2500-A1 rated 111.2 kN.
- – International Aero Engines V2527-A5 rated 117.9 kN.
Performance
- Service ceiling: 12,000 m (39,000 ft)
- Cruising speed: Mach 0.78 (828 km/h/511 mph at 11,000 m/36,000 ft)
- Maximum speed: Mach 0.82 (871 km/h/537 mph at 11,000 m/36,000 ft)
- Range fully loaded: 3,600 nmi (6,700 km; 4,100 mi), 3,700 nmi (6,900 km; 4,300 mi) with sharklets
Boeing 737
Boeing 737 Next Generation (737NG) series includes four variants and can seat between 110 to 210 passengers.
- Role: Narrow-body jet airliner
- National origin: United States
- Manufacturer: Boeing Commercial Airplanes
- First flight: February 9, 1997
- Introduction: 1998 with Southwest Airlines
- Status: In service
- Produced: 1996–present
- Number built: 5,000 as of July 16, 2014
Specifications
Boeing 737-600
- Cockpit crew: 2
- Seating capacity: 149 (1-class, maximum)
- Overall length: 102 ft 6 in (31.2 m)
- Wingspan: 117 ft 5 in (35.7 m)
- Overall height: 41 ft 3 in (12.6 m)
- Fuselage width: 12 ft 4 in (3.76 m)
- Fuselage Height: 13 ft 2 in (4.01 m)
- Operating empty weight: 80,031 lb (36,378 kg)
- Maximum landing weight: 120,500 lb (54,658 kg)
- Maximum take-off weight: 145,500 lb (66,000 kg)
- Service ceiling: 41,000 ft (12,500 m)
- Cruising speed: Mach 0.785 (447 kn, 514 mph, 828 km/h)
- Maximum speed: Mach 0.82 (475 kn, 544 mph, 876 km/h)
- Range fully loaded: 3,050 nmi (5,648 km)
- Engine (× 2): CFM 56-7B20
Boeing 737-700
- Cockpit crew: 2
- Seating capacity: 149 (1-class, dense)
- Overall length: 110 ft 4 in (33.6 m)
- Wingspan: 117 ft 5 in (35.7 m)
- Overall height: 41 ft 3 in (12.6 m)
- Fuselage width: 12 ft 4 in (3.76 m)
- Fuselage Height: 13 ft 2 in (4.01 m)
- Operating empty weight: 84,100 lb (38,147 kg)
- Maximum landing weight: 134,000 lb (60,781 kg)
- Maximum take-off weight: 154,500 lb (70,080 kg)
- Service ceiling: 41,000 ft (12,500 m)
- Cruising speed: Mach 0.785 (447 kn, 514 mph, 828 km/h)
- Maximum speed: Mach 0.82 (475 kn, 544 mph, 876 km/h)
- Range fully loaded: 3,365 nmi (6,230 km)
- Engine (× 2): CFM 56-7B26
Boeing 737-800
- Cockpit crew: 2
- Seating capacity: 189 (1-class, dense)
- Overall length: 129 ft 6 in (39.5 m)
- Wingspan: 117 ft 5 in (35.7 m)
- Overall height: 41 ft 3 in (12.6 m)
- Fuselage width: 12 ft 4 in (3.76 m)
- Fuselage Height: 13 ft 2 in (4.01 m)
- Operating empty weight: 91,108 lb (41,413 kg)
- Maximum landing weight: 146,300 lb (66,361 kg)
- Maximum take-off weight: 174,200 lb (79,010 kg)
- Service ceiling: 41,000 ft (12,500 m)
- Cruising speed: Mach 0.785 (447 kn, 514 mph, 828 km/h)
- Maximum speed: Mach 0.82 (475 kn, 544 mph, 876 km/h)
- Range fully loaded: 3,060 nmi (5,665 km)
- Engine (× 2): CFM 56-7B27
Boeing 737-900
- Cockpit crew: 2
- Seating capacity: 220 (1-class high density, maximum certificated)
- Overall length: 138 ft 2 in (42.1 m)
- Wingspan: 117 ft 5 in (35.7 m)
- Overall height: 41 ft 3 in (12.6 m)
- Fuselage width: 12 ft 4 in (3.76 m)
- Fuselage Height: 13 ft 2 in (4.01 m)
- Operating empty weight: 98,495 lb (44,676 kg)
- Maximum landing weight: 157,300 lb (71,350 kg)
- Maximum take-off weight: 187,700 lb (85,130 kg)
- Service ceiling: 41,000 ft (12,500 m)
- Cruising speed: Mach 0.785 (447 kn, 514 mph, 828 km/h)
- Maximum speed: Mach 0.82 (475 kn, 544 mph, 876 km/h)
- Range fully loaded: ,265 NM (6,045 km) in 2 class layout
- Engine (× 2): CFM 56-7B27
AgustaWestland AW109
- Role: SAR/utility helicopter
- Manufacturer: Anglo-Italian manufacturer AgustaWestland
- First flight: 4 August 1971
- Introduction: 1976
- Status: Active service In production
- Produced: 1971-present
Specifications (AW109 Power with PW206C)
General characteristics
- Crew: 1 or 2
- Capacity: 6 or 7 passengers
- Length: 11.448 m (37 ft 7 in) fuselage
- Width: 2.88 m (9 ft 5 in)
- Height: 3.50 m (11 ft 6 in)
- Empty weight: 1,590 kg (3,505 lb)
- Max takeoff weight: 2,850 kg (6,283 lb)
- Powerplant: 2 × Pratt & Whitney Canada PW206C Turboshaft engine, 418 kW (561 hp) each
- Main rotor diameter: 11.00 m (36 ft 1 in)
Performance
- Maximum speed: 285 km/h (177 mph; 154 kn)
- Ferry range: 932 km (579 mi; 503 nmi)
- Rate of climb: 9.8 m/s (1,930 ft/min)
Pilatus PC-12
- Role: Passenger and cargo aircraft
- National origin: Switzerland
- Manufacturer: Pilatus Aircraft
- First flight: 31 May 1991
- Introduction: 1994
- Status: Active service, in production
Specifications
General characteristics
- Crew: one or two pilots
- Capacity: 9 passengers standard, 6-8 executive
- Payload: 1,500 kg (3,502 lb)
- Length: 14.40 m (47 ft 3 in)
- Wingspan: 16.23 m (53 ft 3 in)
- Height: 4.26 m (14 ft 0 in)
- Wing area: 25.81 m² (277.8 ft²)
- Empty weight: 2,761 kg (5,867 lb)
- Loaded weight: 4,700 kg (10,450 lb)
- Max. takeoff weight: 4,740 kg (10,450 lb)
- Powerplant: 1 × Pratt & Whitney Canada PT6A-67B or -67P turboprop, 895 kW (1,200 shp)
- Maximum landing: 4,500 kg (9,921 lb)
- Maximum payload full fuel: 539 kg (1,189 lb)
- Tail wingspan: 5.20 m (17 ft 1 in)
- Propeller: Hartzell HC – E4A – 3D/E10477K – 4 blade aluminum
- Propeller diameter: 2.67 m (8 ft 9 in)
- Propeller RPM: 1,700 rpm
Performance
- Cruise speed: 500 km/h (312.5 mph/270 KTAS/280 KTAS @ 20000 ft (PC-12NG))
- Stall speed: 120 km/h (74.8 mph/ 65 KCAS/66 KCAS (PC-12NG))
- Service ceiling: 9,150 m (30,000 ft)
- Rate of climb: 512 m/min at sea level (1,680 ft/min)
- Wing loading: 174.3 kg/m² (35.7 lb/ft²)
- Power/mass: 3.7 kg/shp (8.2 lb/shp)
- Range 0 passenger: 3,389 km (1,830 nm)
- Range 9 passenger: 2,804 km (1,753 mi) (1,513 nm)
- Takeoff distance over 15 m (50 ft) obstacle: 701 m (2,300 ft)
- Takeoff distance ground roll: 450 m (1,475 ft)
- Landing distance over 15 m (50 ft) obstacle: 558 m (1,830 ft)
- Landing distance ground roll: 228 m (945 ft)
- Climb to 30,000 ft: 26.5 minutes
- Fuel consumption: 360 pounds per hour (54 gph)
Avionics
Honeywell Primus Apex (PC-12NG)