Penerbangan bersama MASwings Fokker F50

MASwings hadir melayani penerbangan baik domestik maupun international dengan dukungan armada Fokker F50 dan jenis armada lainnya.

MASwings (nama resmi: MASwings Sdn. Berhad) merupakan sebuah maskapai penerbangan regional yang berbasis di Malaysia. Ia fokus kota-kota dan daerah pedalaman Malaysia Timur. Maswings mulai beroperasi pada 1 Oktober 2007. Pangkalan utamanya terletak di Bandar Udara Miri, Sarawak, Malaysia. Ia dimiliki sepenuhnya oleh Malaysia Airlines.

Destinasi Rute penerbangan domestik MASwings.
Malaysia
Wilayah Persekutuan
    Labuan (Bandar Udara Labuan)

Sabah
    Kota Kinabalu (Bandar Udara Internasional Kota Kinabalu) Hub sekunder
    Kudat (Bandar Udara Kudat)
    Lahad Datu (Bandar Udara Lahad Datu)
    Sandakan (Bandar Udara Sandakan)
    Tawau (Bandar Udara Tawau)

Sarawak
    Ba'kelalan (Bandar Udara Bakelalan)
    Bario (Bandar Udara Bario)
    Bintulu (Bandar Udara Bintulu)
    Kuching (Bandar Udara Internasional Kuching) Hub sekunder
    Lawas (Bandar Udara Lawas)
    Limbang (Bandar Udara Limbang)
    Long Akah (Bandar Udara Long Akah)
    Long Banga (Bandar Udara Long Banga)
    Long Lellang (Bandar Udara Long Lellang)
    Long Seridan (Bandar Udara Long Seridan)
    Marudi (Bandar Udara Marudi)
    Miri (Bandar Udara Miri) Hub
    Mukah (Bandar Udara Mukah)
    Mulu (Bandar Udara Mulu)
    Sibu (Bandar Udara Sibu)
    Sarikei (Bandar Udara Tanjung Manis)

Rute penerbangan international MASwings
Brunei
    Bandar Seri Begawan (Bandar Udara Internasional Brunei)

Indonesia

    Pontianak (Bandar Udara Supadio)
    Tarakan (Bandar Udara Juwata)
Harga Tiket MASwings, promo tiket MASwings, penerbangan MASwings

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Fokker F27 Friendship

The Fokker F27 Friendship is a turboprop airliner designed and built by the defunct Dutch aircraft manufacturer Fokker.

Fokker had produced some excellent airliners during the 'between wars' years, and with the end of World War II lost little time in formulating the design of a new medium-range aircraft in this category. The company's design study of 1950 was for a 32-seat transport to be powered by two Rolls-Royce Dart turboprop engines. Known as the P.275 project, it was enlarged slightly and modified to incorporate a circular-section pressurised fuselage by 1952, when Dutch government backing was sought for its construction and development. The type was then designated Fokker F27, and the first of two prototypes made its maiden flight on 24 November 1955, powered by two Dart 507 turboprops. Of high-wing monoplane configuration, the F27 has a pressurised fuselage, retractable tricycle landing gear and accommodation for 28 passengers. The second prototype, with Dart Mk 511 engines and its fuselage lengthened by 0.91m to seat 32 passengers, was flown on 31 January 1957. Between the initial flights of these two prototypes, Fokker concluded an agreement with the Fairchild Engine and Airplane Corporation for the latter to manufacture and market the F27 in North America, where it was known as the Fairchild F-27. Fokker's first F27 Friendship entered service with Aer Lingus in December 1958, but Fairchild had been a little quicker off the mark, its F-27 entering service with West Coast Airlines three months earlier. The American company had modified the interior layout to seat 40, increased the fuel capacity and made provision for weather radar in a lengthened nose; Fokker adopted similar improvements at a later date. The initial Dutch production version was designated F27 Mk 100 (Fairchild F-27), and was powered by two 1279kW Rolls-Royce Dart RDa.6 Mk 514-7 turboprops. It was followed by the similar F27 Mk 200 (Fairchild F-27A) with 1529kW Dart RDa.7 Mk 532-7 engines. Both airliners had standard accommodation for 40 passengers, but a high-density arrangement made it possible to seat 52. An executive version of the Mk 200 was available with the interior design to customer requirements. Subsequent versions include the F27 Mk 300 Combiplane (Fairchild F-27B), a passenger/cargo aircraft with Mk 100 powerplant, a reinforced cabin floor, cargo tie-down rings and a large cargo door forward of the wing on the port side. A similar Combiplane version of the Mk 200 had the designation F27 Mk 400, but no equivalent version was produced by Fairchild in America. Fokker next developed a lengthened fuselage (by 1.50m) variant of the Mk 200. Designated F27 Mk 500, this failed to appeal initially to airline operators, but 15 were acquired by the French government for service with the nation's Postale de Nuit. Friendship Mk 500s now in service with airlines have standard accommodation for 52 passengers, with high-density seating for 60. Fairchild in America produced its own stretched variant, the FH-227. The last production version was the F27 Mk 600, combining the Mk 200 fuselage without the reinforced cabin floor but with the cargo door of the Mk 300/400 Combiplanes. The F27 Mk 600 introduced an optional roller-track quick-change interior so that the type could be used for passenger/cargo services. Other versions included the F27 Mk 400M and F27 Mk 500M military aircraft, an F27 Mk 400M aerial-survey version and an F27 Maritime suitable for coastal patrol, fishery protection, and search and rescue. Late production aircraft had an updated flight deck and cabin interior. Manufacture was shared by Dassault-Breguet (France), MBB (Germany) and SABCA (Belgium). When production was terminated in 1986 in favour of the Fokker 50, the company had sold 581 F27s alongside 205 Fairchild-built F-27/FH-227 variants. In mid-1991 Fokker stated that around 450 F27s were still in service and that the highest-time aircraft had made some 80,000 flights.

3-View

A three-view drawing (752 x 964)

Specification

MODEL	Fokker F27 Mk 200
ENGINE	2 x Rolls-Royce Dart Mk 536-7R turboprops, 1730kW
WEIGHTS
Take-off weight	20410 kg	44997 lb
Loaded weight	12148 kg	26782 lb
DIMENSIONS
Wingspan	29.0 m	95 ft 2 in
Length	23.56 m	77 ft 4 in
Height	8.5 m	28 ft 11 in
Wing area	70.0 m2	753.47 sq ft
PERFORMANCE
Cruise speed	480 km/h	298 mph
Ceiling	8990 m	29500 ft
Range	1926 km	1197 miles

Seatmap

Powerplants

Mk 200/500/600 - Two 1730kW (2320ehp) RollsRoyce Dart Mk 5367R turboprops driving four blade Dowty Rotol propellers. FH-227E - Two 1715kW (2300shp) Dart 5327Ls.

Performance

Mk 500 - Normal cruising speed 480km/h (260kt). Service ceiling 29,500ft. Range with 52 passengers and reserves 1315km (710nm). FH-227 - Max cruising speed 473km/h (255kt), economical cruising speed 435km/h (236kt). Range with max payload 1055km (570nm), range with max fuel 2660km (1440nm).

Weights

Mk 500 - Empty 12,243kg (26,992lb), operating empty 12,684kg (27,964lb), max takeoff 20,410kg (44,996lb). FH-227 - Operating empty 10,398kg (22,923lb), max takeoff 20,639kg (45,500lb).

Dimensions

Mk 500 - Wing span 29.00m (95ft 2in), length 23.06m (82ft 3in), height 8.71m (28ft 7in). Wing area 70.0m2 (753.5sq ft). FH-227 - Same except length 25.50m (83ft 8in), height 8.41m (27ft 7in).

Capacity

Flightcrew of two. Seating for 44 at four abreast and 76cm (30in) pitch in original fuselage length versions (Mks 100, 200, 300, 400, 600 & F-27). Standard seating for 52 and max seating for 60 at 72cm (28.5in) pitch in Mk 500. FH-227 seats 52 at 79cm (31in) pitch, or a maximum of 56.

Production

581 F-27s, 128 F-27s and 78 FH-227s built. Fokker production comprised 85 Mk 100s, 138 Mk 200s, 13 Mk 300s, 218 Mk 400 & 600s, 112 Mk 500s and six F-27MPA Maritimes. 290 Fokker built and 25 Fairchild aircraft in service in late 1998. Additionally, approx 25 used as corporate transports.

Type

Regional airliners

Schematics

 

History

Probably the closest to being the fabled DC-3 replacement, the Fokker F-27 Friendship, including the Fairchild built F-27 and FH-227, was built in greater numbers than any other western turboprop airliner.
The Fokker F-27 began life as a 1950 design study known as the P275, a 32 seater powered by two RollsRoyce Dart turboprops. With the aid of Dutch government funding the P275 evolved into the F-27, which first flew on November 24 1955. This original prototype was powered by Dart 507s and would have seated 28, by the time the second prototype had flown (in January 1957) the fuselage length grew to allow seating for 32.
By this stage Fokker had signed an agreement that would see Fairchild build Friendships in the USA. The first aircraft to enter service was in fact a Fairchild built F-27, in September 1958.
Fairchild F-27s differed from the initial Fokker F-27 Mk 100s in having basic seating for 40, a lengthened nose capable of housing a weather radar, and additional fuel capacity.
Developments included the Mk 200/F-27A with more powerful engines, Mk 300/F-27B and primarily military Mk 400 Combi versions, the Mk 500 with a 1.50m (4ft 11in) fuselage stretch taking seating to 52, and Mk 600 quick change freight/pax aircraft.

Fairchild independently developed the stretched FH-227, which appeared almost two years earlier than the Mk 500. The FH-227 featured a 1.83m (6ft 0in) stretch over standard length F-27/F-27s, taking standard seating to 52.

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Fokker F28 Fellowship

The Fokker F28 Fellowship is a short range jet airliner designed and built by Dutch aircraft manufacturer Fokker.

Announced by Fokker in April 1962, production was a collaboration between a number of European companies, namely Fokker, MBB of West Germany, Fokker-VFW (also of Germany), and Short Brothers of Northern Ireland. There was also government money invested in the project, with the Dutch government providing 50% of Fokker's stake and the West German government having 60% of the 35% German stake. Projected at first to transport 50 passengers to 1,650 km (1,025 mi), the plane was later designed to have 60-65 seats. On the design sheet, the F28 was originally to mount Bristol Siddeley BS.75 turbofans, but the prototype flew with the lighter Rolls-Royce "Spey Junior", a simplified version of the Rolls-Royce Spey. The F28 was similar in design to the British Aircraft Corporation BAC One-Eleven and Douglas DC-9, as it had a T-tail and engines mounted at the rear of the fuselage. The aircraft had wings with a slight crescent angle of sweep with ailerons at the tip, simple flaps, and five-section liftdumper only operated after landing to dump the lift. These were employed rather than reverse thrust as the designers felt that the adding of reverse thrust systems to the engines not only reduced weight, but maintenance also. Having no reverser's also meant that on unpaved airstrips there was less chance of the engines ingesting debris. The leading edge was fixed (although one experimental model had leading edge slats and these were offered as an option)and was anti-iced by bleed air from the engines. The tail cone could split and be hydraulically opened to the sides to act as a variable air brake - also used on the contemporaneous Blackburn Buccaneer. This design was also copied and used on the HS-146, which became the BAe-146. The design is unique in that it not only slows the aircraft down rapidly, it can aid in rapid descents from economic cruising altitudes and also allowed the engines to be set at higher RPM which helped eliminate 'lag time'. This means the engines respond faster if needed for sudden speed increases or go-arounds on the approach to landing. The Fellowship had a retractable tricycle landing gear which used large low pressure tyres enabling the use of unpaved airstrips. Large wheel brakes also helped in shortening the landing run. In terms of responsibility for production, Fokker designed and built the nose section, centre fuselage and inner wing; MBB/Fokker-VFW constructed the forward fuselage, rear fuselage and tail assembly; and Shorts designed and built the outer wings. Final assembly of the Fokker F28 was at Schiphol Airport in the Netherlands. The F28-1000 prototype, registered PH-JHG, first flew on May 9, 1967 (exactly one month later than the famous Boeing 737). German certification was achieved on February 24, 1969. The first order was from German airline LTU, but the first revenue-earning flight was by Braathens on March 28, 1969 who operated five F28s. The F28 with an extended fuselage was named F28-2000 and could seat up to 79 passengers instead of the 65 seats on the F28-1000. The prototype for this model was a converted F28-1000 prototype, and first flew on April 28, 1971. The models F28-6000 and F28-5000 were modified F28-2000 and F28-1000 respectively, with slats, greater wingspan, and more powerful and quieter engines as the main features. The F28-6000 and F28-5000 were not a commercial success; only two F28-6000 and no F28-5000 were built. After being used by Fokker for a time, the F28-6000 were sold to Air Mauritanie, but not before they were converted to F28-2000s. The most successful F28 was the F28-4000, which debuted on October 20, 1976 with one of the world's largest Fokker operators, Linjeflyg. This version was powered by quieter Spey 555-15H engines, and had an increased seating capacity (up to 85 passengers), a larger wingspan with reinforced wings, a new cockpit and a new "wide-look" interior featuring enclosed overhead lockers and a less 'tubular' look. The F28-3000, the successor to the F28-1000, featured the same improvements as the F28-4000. F28s of Ansett Transport Industries' Western Australian intrastate airline, MacRobertson Miller Airlines of Western Australia, flew the longest non-stop F28 route in the world, from Perth to Kununurra, in Western Australia - a distance of about 2,240 km (1,392 mi). This was also the worlds longest twin-jet route at the time. MMA'a F28's also had the highest utilisation rates at the time, flying over 8 hours per day. By the time production ended in 1987, 241 airframes had been built

Seatmap

Powerplants

Mk 3000 & 4000 - Two 44.0kN (9900lb) RollsRoyce RB1832 Spey Mk 55515P turbofans.

Performance

3000 - Max cruising speed 843km/h (455kt), economical cruising speed 678km/h (366kt). Range at high speed cruise with 65 passengers 2743km (1480nm), at long range cruise with 65 passengers 3170km (1710nm). 4000 - Speeds same. Range at high speed cruise with 85 passengers 1900km (1025nm), at long range cruising speed with 85 passengers 2085km (1125nm).

Weights

3000 - Operating empty 16,965kg (37,400lb), max takeoff 33,110kg (73,000lb). 4000 - Operating empty 17,645kg (38,900lb), max takeoff 33,110kg (73,000lb).

Dimensions

3000 - Wing span 25.07m (82ft 3in), length 27.40m (89ft 11in), height 8.47m (27ft 10in). Wing area 79.0m2 (850sq ft). 4000 - Same except for length 29.61m (97ft 2in).

Capacity

Flightcrew of two. Max seating for 85 at five abreast and 74cm (29in) pitch in Mk 4000, or 65 in Mk 3000. Mk 3000 offered with a 15 seat executive interior.

Production

Total F28 sales of 241, including some military customers. As at late 1998 approx 160 remained in commercial service. Further 10 used as corporate jets.

Type

Regional jet airliner

Schematics

 

 

History

The F28 Fellowship jet was developed to complement Fokker's highly successful F-27 Friendship turboprop.
Fokker began development of the F28 in 1960 after perceiving a market for a higher performance (ie jet engined) and greater capacity airliner in comparison with the F-27. First details of the F28 were made public in April 1962, and production of the first development aircraft began in 1964. The first of three prototypes flew for the first time on May 9 1967, with certification and first customer delivery both occurring on February 24 1969.
The F28 was developed into a range of models. Initial production was of the Mk 1000, which could typically seat between 55 and 65, and was powered by 43.8kN (9850lb) Spey Mk 55515 turbofans. The Mk 2000 was essentially similar but featured a 2.21m (7ft 3in) fuselage stretch, increasing maximum seating to 79.
The Mks 5000 and 6000 were based on the 1000 and 2000 respectively, but introduced a longer span wing (by 1.49m/4ft 11in) and wing leading edge slats. Neither version attracted serious sales interest, and no 5000s and just two 6000s were built. Another version that did not come to fruition was the Mk 6600, which would have been stretched by a further 2.21m (7ft 3in), allowing for seating for 100 in a high density layout. It was aimed at Japanese airlines.
The final production models were the 3000 and 4000, again based on the 1000 and 2000 respectively. Both introduced a number of improvements, while the addition of two extra above wing emergency exits on the 4000 increased maximum seating to 85. Freight door equipped convertible versions of each model were offered, and are identified by a C suffix

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Fokker 100

Fokker 100 regional jet

The Fokker 100 ís a regional jet in service with over 40 operators worldwide. The Fokker 100 was manufactured during 1988 through to 1996 and a total of 278 were built.

Prevailing market conditions have made a number of Fokker 100 aircraft available at affordable prices or monthly lease rentals. Favorable operating expenses and substantial revenue potential combine to make the economics of the Fokker 100 very compelling. The Fokker 100 is the natural successor of the F-28 Fellowship and is formally certified as the F-28 Mk0100. 

Go directly to the Fokker 100 specifications:

• Basics
• Interior
• Performance
• Environment
• Avionics
• Operation
• Availability

FLYFokker for economic sense

The operation of the Fokker 100 is supported by FLYFokker, our full-service Life Cycle Support program. FLYFokker comprises a package of four solutions: Take Off, Take Care, Take Over and Take Next.
Start-up operators can Take Off with their operation in six weeks instead of typically six months. For mature Fokker operators Take Care is a complete solution to increase Technical Dispatch Reliability (TDR), reduce Direct Operating Cost (DOC) and improve passenger comfort. Operators moving to other aircraft types are supported by Fokker Services in the Take Over of the continued competitive operation of their Fokker fleet. The fourth solution is a package for the mean and lean transfer of aircraft to the next operator, entitled Take Next.
Choosing Fokker makes economic sense. This is what existing and start-up operators are saying. Over 200 airlines and operators fly Fokker aircraft. Fokker Services continuously invests in supporting over 600 flying Fokker aircraft across the world for decades to come. For Continued Competitive Operation.

Fokker 100 Basics

 

(click to enlarge)

Dimensions and areas
Overall length	35.53 m	116.7 ft
Overall height	8.51 m	27.1 ft
Fuselage length	32.50 m	106.8 ft
Fuselage external diameter	3.30 m	10.10 ft
Wing area	93.50 m2	1006.46 ft2
Wing span	28.08 m	92.1 ft
Gear track	5.04 m	16.6 ft
Main entry door, integral stairs	1.92  x0.86 m	6.4 x 2.9 ft
Main entry door, forward opening	1.86 x 0.86 m	6.1 x 2.8 ft
Forward Service door	1.30 x 0.63 m	4.3 x 2.1 ft
Cargo hold doors, upward opening	1.45 x 1.40 m	4.9 x 4.7 ft
Cargo hold doors, downward opening	0.90 x 0.95 m	2.9 x 3.1 ft
Cargo holds' volume, large doors	17.72 m3	591 ft3
Cargo holds' volume, small doors	17.08 m3	603 ft3

The Fokker 100 offers a choice of 2 MTOWs, and even lower MTOWs are available to take advantage of reduced weight-related costs, such as landing and navigation charges.

Weights
MTOW	45,810 kg*	101,000 lb
	44,450 kg	98,000 lb
MLW	39,915 kg	88,000 lb
MZFW	36,740 kg	81,000 lb
Fuel capacity	10,731 kg **	23,660 lb**
	10,293 kg	22,690 lb

*  Most aircraft from MSN 11444
** From MSN 11442

Fokker 100 Interior

The Fokker 100 offers flexibility from an all-economy 5-abreast 109 seater at 32 inch pitch to a partially 4-abreast business seating at 40 inch seat pitch. Many alternative and mixed-class seating arrangements are possible. Any arrangement offers a revenue potential unequalled by smaller regional jets.

Fokker 100s formally operated by US Airways have upper deck avionics compartments on both sides of the passenger entry door, increasing forward belly cargo hold space by 3 m³ (100 ft³).

The Fokker 100 is equipped with either a forward-opening passenger door or a downward-opening door with integral stairs. Both are jetway compatible.

Full economy seating, 109 pax @ 31/32 inch seat pitch

Partially business seating, 12 pax @ 40 inch seat pitch and 85 pax @ 32 inch seat pitch

Legend
A	Galley
C	Flight attendant seat
H/I	Jetway adaptor / Integral stairway
T	Toilet
W	Wardrobe

The passenger cabin is spacious and offers over 2m standing height in the aisle. The cabin is also very quiet due to the aft fuselage engine position, Tay low noise characteristics and clever noise attenuating features. Innovative LED lighting is an optional cabin feature.

Fokker 100 Aircraft Performance

The Fokker 100 is powered by two fuel-efficient and reliable Rolls-Royce Tay 620, or Tay 650 turbofan engines. Fuel burn of the Fokker 100 is low due to the fuel efficient engines and advanced aerodynamic design. The combination of low weight, very good low speed capability and high performance engines results in good short field performance.

Design speeds and ceiling
Cruise speed	M.74	800 KPH
Maximum speed	M.77	856 KPH
Minimum approach speed @ MLW	120 KTS	222 KPH
Ceiling	35,000 ft	10,668 m

Landing field length @ MLW
ISA, Sea Level	1345 m
ISA +10°C, 2000 ft	1405 m

Fokker 100 Environment

The Fokker 100 complies with ICAO Chapter 3 / FAA Stage 3 noise regulations with wide margins, enabling it to meet Chapter 4 as well. The Fokker 100 also complies with the CAEP 4 emission level requirements.

Fokker 100 Avionics

The Fokker 100 comes with a ‘glass cockpit’ equipped with a dual Flight Management System and a fully-integrated automatic flight control system which, as standard, has full flight envelope protection and enables Cat IIIA autoland. Cat IIIB with roll-out guidance is also available.
Full EU-OPS1 requirements are installed on many Fokker 100s or can be made available as approved Service Bulletins.
The Fokker 100 can optionally be equipped with Required Navigation Performance (RNP 0.3) which is coupled to the existing FMC. RNP 0.3 enables shorter routes and optimized approach routings, allowing for shorter approaches and lower decision heights.
RNP reduces weather-related diversions and yields lower block times and fuel, contributing to the environmental friendliness of the Fokker 100.

1	Cockpit voice recorder	8	Fire panels
2	Electrical system	9	Air conditioning
3	Hydraulic system	10	Fuel panel
4	Anti-ice	11	Engine start
5	Lighting	12	Pressurization
6	EFIS control	13	APU
7	Auto pilot system	14	Landing gear

15	Primary flight display	23	Flight management system
16	Navigation display	24	Printer
17	Multi-fuction display	25	Flap selector
18	Speed brake lever	26	Throttles
19	IRS	27	Fuel control
20	Parking brake lever	28	Communication
21	Thrust rating panel	29	Navigation
22	ACARS	30	Trim

Fokker 100 Operation

The Fokker 100 offers the possibility of operating a highly reliable and mature aircraft on short to medium haul routes. The accumulated service experience amounts to more almost 10 million flight hours and landings. Fleet leaders have flown more than 50,000 flying hours. Continuous product improvements are made by Fokker Services based on operator experience and any new regulations. With a design life of 90,000 flying hours or landings the average age is only around 35,000 flying hours or 30,000 landings.
Full scale structural testing of at least 180,000 landings has been carried out with the findings solved early on during production, ensuring very few structure-related ADs in the future.
Based on favorable in-service experience, 6 years and 12 years task intervals are currently in the process of being escalated by 30% for reduced maintenance costs.
Overall, the Fokker 100 is a very mature and reliable aircraft and optimized for high cycle operations.

Fokker 100 aircraft availability

At this moment, various Fokker 100 aircraft are available for sale and/or lease at competitive terms and conditions.
Please contact the Remarketing Support Center for an overview of available aircraft.

Contact
We like to invite you to contact the Remarketing Support Center of Fokker Services on non-committal basis for more detailed information on:

• the Fokker 50, 70 or 100 aircraft
• aircraft availability;
• performance calculations;
• route analysis;
• Direct Operating Cost calculations;
• Aircraft comparisons;
• Aircraft Lease intelligence;
• Aircraft values;
  

Mr. Peter van OostrumDirector Aircraft Remarketing
e-Mail: peter.vanoostrum@fokker.com
Phone: +31 (0)88 6280 477
Mob.:   +31 (0)6 2652 6420
Hoeksteen 40
2132 MS  Hoofddorp
The Netherlands

Mr. Ton van RooijenDirector Remarketing Support Center
e-Mail: ton.vanrooijen@fokker.com
Phone: +31 (0)88 6280 557
Mob.:   +31 (0)6 5340 7709
Hoeksteen 40
2132 MS  Hoofddorp
The Netherlands

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FOKER 70

Fokker 70 passenger jet

The Fokker 70 is basically a shorter fuselage version of a late-production Fokker 100. It has more than 95% commonality in terms of line-removable units (LRUs). The size of the Fokker 70 is similar to its predecessor, the F-28 Fellowship.
The Fokker 70 allows the same type rating as the Fokker 100 enabling optimum use of flight crews at a minimum cost as well as maximum flexibility in matching seat supply with passenger demand.

47 Fokker 70s were manufactured in the 1994-1997 period. The Fokker 70 is being used by nine operators world-wide adding to the more than thirty operators currently flying the larger Fokker 100.

Go directly to the Fokker 70 specifications:

• Basics
• Interior
• Performance
• Environment
• Avionics
• Operation
• Availability

FLYFokker for economic sense

The operation of the Fokker 70 is supported by FLYFokker, our full-service Life Cycle Support program. FLYFokker comprises a package of four solutions: Take Off, Take Care, Take Over and Take Next.
Start-up operators can Take Off with their operation in six weeks instead of typically six months. For mature Fokker operators Take Care is a complete solution to increase Technical Dispatch Reliability (TDR), reduce Direct Operating Cost (DOC) and improve passenger comfort. Operators moving to other aircraft types are supported by Fokker Services in the Take Over of the continued competitive operation of their Fokker fleet. The fourth solution is a package for the mean and lean transfer of aircraft to the next operator, entitled Take Next.
Choosing Fokker makes economic sense. This is what existing and start-up operators are saying. Over 200 airlines and operators fly Fokker aircraft. Fokker Services continuously invests in supporting over 600 flying Fokker aircraft across the world for decades to come. For Continued Competitive Operation.

Fokker 70 Basics

Dimensions and areas
Overall length	30.91 m	101.5 ft
Overall height	8.51 m	27.11 ft
Fuselage length	27.88 m	91.6 ft
Fuselage external diameter	3.30 m	10.10 ft
Wing area	93.50 m2	1006.46 ft2
Wing span	28.08 m	92.1 ft
Gear track	5.04 m	16.6 ft
Main entrance door (h x w)	1.92 x 0.86 m	6.4 x 2.9 ft
Forward cargo door (h x w)	1.45 x 1.40 m	4.9 x 4.7 ft
Forward compartment volume	8.15 m3	288 ft3
Aft cargo door (h x w)	1.22 x 0.97 m	4.0 x 3.2 ft
Aft compartment volume	4.63 m3	163 ft3
Service/emergency door	1.30 x 0.63 m	4.3 x 2.1 ft

The Fokker 70 is available with four MTOWs, allowing a maximum range with a full passenger payload of approximately 1800 NM. The lower MTOWs enable the operator to take advantage of lower weight-related navigation fees and landing charges.

Weights
MTOW	41,730 kg	92,000 lb
MLW	36,740 kg	81,000 lb
MZFW	33,565 kg	74,000 lb
Fuel capacity	10,731 kg	23,660 lb

Note: Lower MTOW options are available

Fokker 70 Interior

The Fokker 70's maximum capacity is 80 seats at 31/32 in pitch. Many alternative seating arrangements are possible, e.g. a mixed class configuration with 12 First and 60 Economy class seats with full hot galleys.

The Fokker 70 is equipped with a downward opening door with integral stairs that are fully jetway compatible, thus enabling maximum operation flexibility.

Full economy seating, 79 pax @ 31/32 inch seat pitch

 

Legend
A	Galley
AV	Avionics rack
C	Flight attendant seat
J	Stowage
T	Toilet
W	Wardrobe

The passenger cabin is spacious and offers over 2 meters standing height in the aisle. The 5-abreast seating, at typical load factors, offers a wide choice of seating arrangements not encountererd on most regional jets. The cabin can optionally be equipped with LED lighting.

Fokker 70 performance

The Fokker 70 is exclusively powered by reliable Rolls-Royce Tay 620 engines, which provide it with excellent field and climb performance and good overall fuel burn.
The Fokker 70 can optionally be modified for steep approach capability, which enables it to operate from/to London City Airport.

Design speeds and ceiling
Cruise speed	M.74	800 KPH
Maximum speed	M.77	856 KPH
Minimum approach speed @ MLW	120 KTS	222 KPH
Ceiling	35,000 ft	10,668 m

Landing field length @ MLW
ISA, Sea Level	1270 m
ISA +10°C, 2000 ft	1360 m

Fokker 70 Environment

The Fokker 70 complies with ICAO Chapter 3 / FAA Stage 3 noise regulations with very wide margins, enabling it to also meet Chapter 4 with a good margin. The aircraft additionally complies with CAEP 4 emission level requirements.

Fokker 70 Avionics

The Fokker 70 comes with a ‘glass cockpit’ equipped with a dual Flight Management System and a fully-integrated automatic flight control system which, as standard, has full flight envelope protection and enables Cat IIIA autoland. Cat IIIB with roll-out guidance is also available.
Full EU-OPS1 requirements are installed on most Fokker 70s or can be made available as approved Service Bulletins.
The Fokker 70 can optionally be equipped with Required Navigation Performance (RNP 0.3) which is coupled to the existing FMC. RNP 0.3 enables shorter routes and optimized approach routings, allowing for shorter approaches and lower decision heights.
RNP reduces weather-related diversions and yields lower block times and fuel, contributing to the environmental friendliness of the Fokker 70.

1	Cockpit voice recorder	8	Fire panels
2	Electrical system	9	Air conditioning
3	Hydraulic system	10	Fuel panel
4	Anti-ice	11	Engine start
5	Lighting	12	Pressurization
6	EFIS control	13	APU
7	Auto pilot system	14	Landing gear

15	Primary flight display	23	Flight management system
16	Navigation display	24	Printer
17	Multi-fuction display	25	Flap selector
18	Speed brake lever	26	Throttles
19	IRS	27	Fuel control
20	Parking brake lever	28	Communication
21	Thrust rating panel	29	Navigation
22	ACARS	30	Trim

Fokker 70 Operation

The Fokker 70 is a very mature and reliable aircraft and it is optimized for high cycle operations. The total accumulated service experience for the Fokker 70 and Fokker 100 fleets is close to 10 million flight hours and landings. Initial operator experience on the Fokker 100 was incorporated in the design of the Fokker 70.

Fokker Services make continuous product improvements based on more recent operator feedback and any new regulations. Typically, most Fokker 70s have flown between 25,000 and 30,000 flight hours and landings, which is only a third of the 90,000 flight hours or desgn life cycles.
The structure is basically the same as that of the Fokker 100, which has been tested for at least 180,000 landings, ensuring very few structure-related inspection tasks and ADs in the future.
Based on favorable in-service experience many maintenance task intervals are currently in the process of being escalated for reduced maintenance costs.

Fokker 70 sale or lease

Several Fokker 70s are available for sale or lease. Please contact the Remarkting Support Center for the Fokker 70 aircraft specifications.

Contact
We like to invite you to contact the Remarketing Support Center of Fokker Services on non-committal basis for more detailed information on:

• the Fokker 50, 70 or 100 aircraft
• aircraft availability;
• performance calculations;
• route analysis;
• Direct Operating Cost calculations;
• Aircraft comparisons;
• Aircraft Lease intelligence;
• Aircraft values;
  

Mr. Peter van OostrumDirector Aircraft Remarketing
e-Mail: peter.vanoostrum@fokker.com
Phone: +31 (0)88 6280 477
Mob.:   +31 (0)6 2652 6420
Hoeksteen 40
2132 MS  Hoofddorp
The Netherlands

Mr. Ton van RooijenDirector Remarketing Support Center
e-Mail: ton.vanrooijen@fokker.com
Phone: +31 (0)88 6280 557
Mob.:   +31 (0)6 5340 7709
Hoeksteen 40
2132 MS  Hoofddorp
The Netherlands

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