Pilatus PC-6 Porter/Turbo Porter
November 15, 2008 by R.Vogelaar · Leave a Comment
Pilatus PC-6 Turbo Porter PH-JFD of Icarus Para Club Rotterdam
The Pilatus PC-6 success is due to providing operators with the flexibility of choice or conversion between roles. These include passenger and/or cargo transport, supply and Para dropping, photographic and aerial survey, forward support, agricultural work, search and rescue, ambulance and a variety of other missions. In addition the Pilatus PC-6 is certified to operate with amphibious or normal floats and also with skis.
The Pilatus PC-6 Porter started with a piston engine. The first PC-6/A Turbo-Porter with French Turboméca Astazou II turboprop power, giving vastly improved performance. First deliveries to Air Alps, a Swiss customer and Wien Alaska Airlines got under way in 1962.
The real breakthrough for the aircraft came in 1964, when the PT6A-6A engine was fitted. The current B2-H4-model was introduced in mid 1985, featuring an enlarged dorsal fin, up-rated shock absorbers, new tail-wheel and airframe reinforcement.
Pilatus PC-6 Turbo Porter EC-EMZ
Pilatus PC-6 Turbo Porter N4229S
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Manufacturer/designer: |
Pilatus Aircraft AG. |
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Production line: |
Production at Stans continues at low rates. |
|
Task: |
STOL (short take off and landing) utility transport. |
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First flight: |
- PC-6 Porter May 4, 1959, HB-FAN. - PC-6/A Turbo Porter May 2, 1961, HB-FAD. - PC-6/B Turbo Porter May 2, 1964, N187H. - Fairchild-Hiller PC-6/C Turbo Porter October 1965, N180K. - PC-6/D-H3 Swept tail April 3, 1970, HB-FFW. - PC-8D Twin Porter November 28, 1967, HB-KOA. |
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Pilatus PC-6/B2-H4 Turbo Porter |
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Crew: |
2. |
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Passengers: |
7 – 11. |
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Cabin length: |
2,3 m without cockpit. |
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Cabin width: |
1,16 m. |
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Cabin height: |
1,18 m. |
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Cabin floor area: |
2,67 m². |
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Cabin volume: |
3,30 m³. |
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Wing Span: |
18,57 m. |
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Wing Area: |
30,15 m². |
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Fuselage length: |
11,00 m. |
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Fuselage height: |
3,20 m tail down. |
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Elevator span: |
5,12 m. |
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Wheelbase: |
7,87 m. |
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Wheel track: |
3,00 m. |
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Engines: |
one Pratt & Whitney Canada PT6A-27 turboprop rated 410 kW. |
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Propeller: |
Hartzell HC-B3TN-3D constant speed, diameter 2,56 m. |
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Weight: |
- empty: 1.270 Kg. - max. zero-fuel weight 2.400 kg. - internal fuel: 508 Kg. - external fuel: 392 Kg. - max. payload: 1.130 Kg. |
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Max. take off weight: |
- 2.800 Kg on wheels. - 2.699 Kg on skis. |
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Max. landing weight: |
2.660 Kg. |
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Cruise speed: |
213 km/h at 3.050 m. |
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Max. speed: |
280 km/h at m. |
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Max. ceiling: |
7.620 m. |
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Range: |
- range 926 km without external tanks. - ferry range 1.612 km external tanks. |
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Performance: |
- max. rate of climb at sea level 287 m per minute. - take-off run 197 m at max. take-off weight. - landing run 127 m at max. landing weight. |
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g limits: |
-1.5 / +3.72 |
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Underwing hardpoints: |
two for underwing tanks. |
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Extra: |
skis or amphibious floats. |
Civil Pilatus PC-6 written-off by accidents from the year 2000:
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12-03-2000 |
OO-FWJ |
PC-6/B2-H2 |
Paracentrum Oost Turnhout. |
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08-04-2000 |
HB-FMC |
PC-6/B2-H2 |
Imiginair. |
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13-06-2000 |
D-FDHM |
PC-6/C1-H2 |
Private. |
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26-06-2001 |
F-GUAS |
PC-6/B2-H2 |
Parachutisme 74. |
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01-07-2001 |
D-FALL |
PC-6/B2-H2 |
Pull Out Skydiving. |
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22-01-2002 |
OB-1600 |
PC-6/B2-H2 |
Aero Andino. |
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01-06-2002 |
D-FEAR |
PC-6/B2-H2 |
Private. |
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09-06-2002 |
OO-NAP |
PC-6/B2-H2 |
Namur Air Promotion. |
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15-08-2002 |
F-GLTP |
PC-6/B2-H2 |
SARL Europlane. |
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18-08-2002 |
? |
PC-6 |
Italy? |
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28-08-2003 |
N394R |
PC-6C/H2 |
Ton Bishop (Skydive Texas) ex Air America (CIA). |
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13-11-2003 |
F-GMMA |
PC-6/B2-H2 |
On Top Aviation. |
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16-07-2005 |
N908PL |
PC-6/B2-H2 |
GG Aircraft. |
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03-10-2005 |
N7895J |
PC-6/B2-H2 |
Vertical Air. |
Pilatus PC-6 Porter / Turbo Porter
November 14, 2008 by R.Vogelaar · Leave a Comment
Pilatus PC-6 V-631 of the Swiss Air Force
The Pilatus PC-6 success is due to providing operators with the flexibility of choice or conversion between roles. These include passenger and/or cargo transport, supply and Para dropping, photographic and aerial survey, forward support, agricultural work, search and rescue, ambulance and a variety of other missions. In addition the Pilatus PC-6 is certified to operate with amphibious or normal floats and also with skis.
The Pilatus PC-6 Porter started with a piston engine. The first PC-6/A Turbo-Porter with French Turboméca Astazou II turboprop power, giving vastly improved performance.
The real breakthrough for the aircraft came in 1964, when the PT6A-6A engine was fitted. The current B2-H4-model was introduced in mid 1985, featuring an enlarged dorsal fin, up-rated shock absorbers, new tail-wheel and airframe reinforcement.
Fairchild-Hiller
Thirty-six armed PC-6/C’s were produced for COIN duties in Vietnam as Fairchild-Hiller AU-23A Peacemaker, they flew their missions in the Royal Thai Air Force.
CIA
At least 37 PC-6 Turbo Porters were flying for the CIA by Air America, Continental Air Services, Bird & Sons, ICCS Air Services and Air Asia, Tainan. From the beginning Air America used its Turbo Porters in three theaters of South East Asia: Several were assigned to an Air Force contract for use out of Saigon as liaison aircraft. Several were used to support the CIA’s Hmong program in Laos, and two went to contracts in Thailand, especially to support the Royal Thai Border Police.
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Production line: |
Production at Stans continues at low rates. |
|
Task: |
STOL (short take off and landing) utility transport. |
|
First flight: |
- PC-6 Porter May 4, 1959, HB-FAN. - PC-6/A Turbo Porter May 2, 1961, HB-FAD. - PC-6/B Turbo Porter May 2, 1964, N187H. - Fairchild-Hiller PC-6/C Turbo Porter October 1965, N180K. - PC-6/D-H3 Swept tail April 3, 1970, HB-FFW. - PC-8D Twin Porter November 28, 1967, HB-KOA. |
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Pilatus PC-6/B2-H4 Turbo Porter |
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Crew: |
2. |
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Passengers: |
7 – 11. |
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Cabin length: |
2,3 m without cockpit. |
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Cabin width: |
1,16 m. |
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Cabin height: |
1,18 m. |
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Cabin floor area: |
2,67 m². |
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Cabin volume: |
3,30 m³. |
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Wing Span: |
18,57 m. |
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Wing Area: |
30,15 m². |
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Fuselage length: |
11,00 m. |
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Fuselage height: |
3,20 m tail down. |
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Elevator span: |
5,12 m. |
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Wheelbase: |
7,87 m. |
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Wheel track: |
3,00 m. |
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Engines: |
one Pratt & Whitney Canada PT6A-27 turboprop rated 410 kW. |
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Propeller: |
Hartzell HC-B3TN-3D constant speed, diameter 2,56 m. |
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Weight: |
- empty: 1.270 Kg. - max. zero-fuel weight 2.400 kg. - internal fuel: 508 Kg. - external fuel: 392 Kg. - max. payload: 1.130 Kg. |
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Max. take off weight: |
- 2.800 Kg on wheels. - 2.699 Kg on skis. |
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Max. landing weight: |
2.660 Kg. |
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Cruise speed: |
213 km/h at 3.050 m. |
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Max. speed: |
280 km/h at m. |
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Max. ceiling: |
7.620 m. |
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Range: |
- range 926 km without external tanks. - ferry range 1.612 km external tanks. |
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Performance: |
- max. rate of climb at sea level 287 m per minute. - take-off run 197 m at max. take-off weight. - landing run 127 m at max. landing weight. |
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g limits: |
-1.5 / +3.72 |
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Underwing hardpoints: |
two for underwing tanks. |
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Extra: |
skis or amphibious floats. |
Pilatus PC-6 production:
528 built in all versions, approximately 258 active, stored or under rebuilt 20, written-off 150 and scrapped 100.
Production by Pilatus Aircraft Ltd Switzerland: 436
Production by Fairchild-Hiller Corp. under license: 92
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Pilatus PC-6 built of each variant: |
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64 – PC-6, Lycoming GSO-480-B1A6. |
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1 – PC-6/275, Lycoming GO-480-D1A. |
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8 – PC-6/350, Lycoming IGO-540-A1A. |
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35 – PC-6/A, Turbomeca Astazou IIE / G. |
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6 – PC-6/A1, Turbomeca Astazou XII. |
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1 – PC-6/Ax, Turbomeca Astazou X. |
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1 – PC-6/A2, Turbomeca Astazou XIVE. |
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12 – PC-6/B, Pratt & Whitney PT6A-6A. |
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94 – PC-6/B1, Pratt & Whitney PT6A-20. |
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236 – PC-6/B2, Pratt & Whitney PT6A-27. |
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34 – PC-6/C, Garrett TPE-331-25D. |
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1 – PC-6/C1, Garrett TPE-331-1-100. |
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36 – PC-6/C2*, Garrett TPE-331-1-101F. |
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1 – PC-6/D-H3, Lycoming TIO-720-C1A2. |
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1 – PC-8D, Lycoming IO-540-G1B5. |
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Pilatus PC-6 military operators: |
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Algerian. |
- 2 PC-6/B2-H4. - 1 PC-6. |
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Angola. |
- 6 PC-6. |
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Argentina. |
- 4 PC-6/B1A-H2. - 6 PC-6/B2-H2. |
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Australia. |
- 19 PC-6/B1-H2. |
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Austria. |
- 13 PC-6/B2-H2. - 1 PC-6/B2-H4. |
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Bolivia. |
- 1 PC-6A. - 2 PC-6C-1. - 16 PC-6/B2-H2. |
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Brazil. |
- 5 PC-6. |
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Chad. |
- 2 PC-6. |
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Chile. |
- 1 PC-6. |
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Colombia. |
- 1 PC-6A. - 6 PC-6/B2-H2. |
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Dubai. |
- 2 PC-6/B2-H4. |
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Ecuador. |
- 2 PC-6/B2-H2. - 3 PC-6/B2-H4. |
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France. |
- 5 PC-6/B2-H2. |
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Guatemala. |
- 6 PC-6. |
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Hungary. |
- 4 PC-6/B1/H2. |
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Indonesia. |
- 11 PC-6B. |
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Iran. |
- 15 PC-6/B2-H2. |
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Israel. |
- 1 PC-6. - 1 PC-6/B1-H2. - 1 PC-6A. |
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Malaysia. |
- 7 PC-6/B2-H4. |
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Mexico. |
- 6 PC-6/B2-H4. |
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Myanmar. |
- 7 PC-6/B2-H2. |
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Nepal. |
- 1 PC-6/B1-H2. |
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Oman. |
- 2 PC-6/B1-H2. |
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Peru. |
- 17 PC-6A. - 23 PC-6/B2-H2. |
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Slovenia. |
- 2 PC-6/B2-H4. |
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South-Africa. |
- 9 PC-6/B2-H4. |
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Sudan. |
- 7 PC-6/B1-H2. |
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Sweden. |
- 1 PC-6. |
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Switzerland. |
- 12 PC-6/B2-H2M-1. |
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Thailand. |
- 2 PC-6/B1-H1. - 5 PC-6/B2-H2. - 18 AU-23A. - 3 PC-6C-H2. |
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United States of America. |
|
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US Army. |
- 2 UV-20A. - 1 PC-6/B2-H4. (UV-20A). |
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CIA – Central Intelligence Agency. |
- 7 PC-6A/H2. - 1 PC-6C/H1. - 29 PC-6C/H2. |
Military Pilatus PC-6 written-off by accidents:
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Pilatus PC-7
October 19, 2008 by R.Vogelaar · Leave a Comment
The Pilatus PC-7 Turbo Trainer is based on the piston-powered Pilatus P-3. Since its introduction in 1978, close to 500 aircraft have been sold, with the majority still being in service today. The aircraft’s capability to cover all aspects of basic training including aerobatics, instrument, tactical and night flying, has convinced 20 air forces to select the PC-7 to train professional military pilots.
The Pilatus PC-7 is powered by Pratt & Whitney Canada PT6A-25A turboprop, and a clear-vision mounded bubble canopy for the non-pressurized tandem-cockpit.
The Pilatus PC-7 Mk.II M airframe is based on that of the Pilatus PC-9, but a lower-powered Pratt & Whitney Canada PT6A-25C turboprop engine variant is used. The cockpit of the Pilatus PC-7 Mk.II M is equipped with a comprehensive tandem-capable VFR/IFR day and night avionics package for navigation, communication and identification using state-of-the-art equipment.
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Developing nation: |
Switzerland. |
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Manufacturer/designer: |
Pilatus Aircraft. |
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Production line. |
Stans. |
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Task: |
Turbo trainer. |
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First flight: |
- Pilatus P-3 re-engined April 12, 1966 HB-HON. - Pilatus PC-7 first production aircraft August 18, 1978 HB-HAO. - Pilatus PC-7Mk.II M September 28, 1992. |
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First delivery: |
- Pilatus PC-7 early 1979 to Myanmar Air Force. - Pilatus PC-7Mk.II M November 30, 1994 to South-African Air Force. |
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Pilatus PC-7 |
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Crew: |
2 |
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Ejection seat: |
Martin-Baker CH.Mk.15A. |
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Wing span: |
10,40 m. |
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Wing area: |
16,60 m². |
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Length: |
9,78 m. |
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Height: |
3,21 m. |
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Tail plane span: |
3,40 m. |
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Wheelbase: |
2,32 m. |
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Wheel track: |
2,60 m. |
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Engine: |
One Pratt & Whitney Canada PT6A-25A turboprop rated 485 kW. |
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Propeller: |
Hartzell HC-B3TN-2 three-blade, constant speed. |
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Weight: |
- Empty: 1.330 Kg. - Internal fuel: 474 liters. - External fuel: 2 x 240 liters. - Max. ordnance: 1.040 Kg. |
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Max. take off weight: |
2.700 Kg. |
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Max. landing weight: |
2.565 Kg. |
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Cruise speed: |
412 km/h. |
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Max. speed: |
500 km/h at 6.095 m. |
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Service ceiling: |
10.060 m. |
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Range: |
- range 1.200 km without drop tanks. - ferry range 2.630 km with drop tanks. Max. endurance 4 hours, 22 minutes. |
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Performance: |
- max. rate of climb at sea level 655 m per minute. - climb to 5.000 m in 9 minutes, 0 seconds. - take-off run 780 m at max. take-off weight. - landing run 505 m at max. landing weight. |
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g limits: |
-3 / +6. |
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Underwing hardpoints: |
6. |
|
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Pilatus PC-7 Mk.II M* |
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Ejection seat: |
Martin-Baker Mk.CH11A. |
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Wing span: |
10,19 m. |
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Wing area: |
16,29 m². |
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Length: |
10,13 m. |
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height: |
3,26 m. |
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Engine: |
One Pratt & Whitney Canada PT6A-25C turboprop rated 522 kW. |
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Propeller: |
Hartzell four-blade, diameter 2,44 m. |
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Weight: |
- Empty: 1.670 Kg. - Zero fuel weight 1.900 kg. - Internal fuel: 518 liters. - External fuel: 2 x 240 liters. - Max. ordnance: 1.040 Kg. |
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Max. take off weight: |
2.850 Kg. |
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Max. landing weight: |
2.750 Kg. |
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Cruise speed: |
465 km/h at 3.050 m. |
|
Max. speed: |
555 km/h. |
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Service ceiling: |
9.150 m |
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Range: |
- range 1.200 km without drop tanks. - ferry range 2.935 km with drop tanks. Max. endurance 4 hours, 40 minutes. |
|
Performance: |
- max. rate of climb at sea level 865 m per minute. - climb to 6.095 m in 10 minutes, 55 seconds. - take-off run 259 m at max. take-off weight. - landing run 335 m at max. landing weight. |
|
g limits: |
-3,5 / +7 |
| Pilatus PC-7 operators: | |
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Angola: |
- 25 PC-7. |
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Austria: |
- 16 PC-7. |
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Bolivia: |
- 24 PC-7. |
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Bophuthatswana: |
- 2 PC-7 returned via South-African Air Force to Pilatus Aircraft. |
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Botswana: |
- 7 PC-7. |
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Brunei: |
- 4 PC-7 Mk.II M. |
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Chad: |
- 2 PC-7. |
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Chile: |
- 10 PC-7. |
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France: |
- 6 PC-7. |
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Guatemala: |
- 12 PC-7. |
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Iran: |
- 35 PC-7. |
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Iraq: |
- 52 PC-7. |
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Malaysia: |
- 45 PC-7. - 4 PC-7 Mk.II M. |
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Mexico: |
- 88 PC-7. |
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Myanmar: |
- 17 PC-7. |
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Netherlands: |
- 13 PC-7. |
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South-Africa: |
- 60 PC-7 Mk.II M. |
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Suriname: |
- 2 PC-7, one to civil. |
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Switzerland: |
- 40 PC-7. |
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UAE (Abu-Dhabi): |
- 31 PC-7. |
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Uruguay: |
- 6 PC-7. |
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Civil: |
more than 7 PC-7. |
Fokker F-27 Friendship
October 15, 2008 by Marcel van Leeuwen · Leave a Comment
Fokker F.27-100 Luxair. LX-LGA
The Fokker F-27 is the most successful civilian airplane the fokker factory has ever built.
At the time it was one of the first, and certainly one of the most successful turbo-prop aircraft in the market.
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- WDL Westdeutsche Luftwerbung Fokker F-27 600 D-AELD on Maastricht Aachen Airport
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- East West F-27 at Schiphol Amsterdam
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- Fokker F.27-100 Luxair. LX-LGA
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- Fokker F.27-600 N740FE Federal express
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- Fokker F.27-200 PH-KFG of Fokker friendship association
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- Fokker F27-100 Friendship Fokker Friendship Association
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- F-27 at Maastricht Aachen Airport, CF-JSD
| Developing Nation: | Netherlands |
| First Flight: | F.27-100: March 23rd:1958  H-NIVF.27-200: September 20th 1959F.27-300: May 2nd 1960F.27-300M: August 17th 1960F.27-400: October 6th 1961F.27-400M: April 24th 1965F.27-500: November 15th 1967 : PH-FLMF.27-600: June 22nd 1967F.27-700: December 29th 1969F.27 Maritime: November 23rd 1978 |
| First Delivery: | early 1959 |
| Crew: | 2 |
| Passengers: | F.27-100: 40F.27-500: 52F.27-600: 44 |
| Wing Span: | 29,00 m |
| Wing Area: | 70,00 m² |
| Length: | F.27-100: 23,56 mF.27-500: 25,06 mF.27-600: 23,56 m |
| Height: | F.27-100: 8,50 mF.27-500: 8,71 mF.27-600: 8,50 m |
| Engine(s): | F.27-100: Two Rolls-Royce Dart Da.6 Mk.514-7F.27-500: Two Rolls-Royce Dart DA.7 Mk.536-7RF.27-600: Two Rolls-Royce Dart DA.7 Mk.536-7R |
| Weight: | |
| Max. Take off weight: | F.27-100: 18350 kgF.27-500: 20410 kgF.27-600: 20410 kg |
| Max. Landing weight: | F.27-100: -F.27-500: 19050 kgF.27-600: 18600 kg |
| Cruise Speed: | 415 Kph |
| Max. Speed: | |
| Operating altitude: | 7620 m |
| Max. Range: | F.27-100: 1715 kmF.27-500: 1315 kmF.27-600: 1890 km |
Fokker 27 crashes: |
| June 10th 1960 Trans Australia Airlines VH-TFB, crashed at Mackay, Australia. 29 died |
| September 23rd 1961 Turkish Airlines TC-TAY, crashed at Ankara, Turkey. 28 died |
| February 7th 1966 Indian Airlines PH-SAB, crashed at Srinagar, India. 37 died |
| February 28th 1967 Philippine Airlines PI-C501, crashed at Mactan, Philippines. 12 died |
| March 27th 1967 Fokker Corporation PK-PFB, crashed at Malaybalay, Philippines. 19 died |
| June 7th 1967 Philippine Airlines PI-C527, crashed at Bacolod, Philippines. 21 died |
| March 21st 1969 Indian Airlines VT-DOJ, crashed at Doulatpoor, Pakistan. 44 died |
| August 6th 1970 Pakistan International Airlines AP-ALM, crashed at Islamabad, Pakistan. 30 died |
| August 29th 1970 Indian Airlines VT-DWT, crashed at Silcher, India. 39 died |
| December 6th 1971 Sudan Airways ST-AAY, crashed at Tikaka, Sudan. 10 died |
| March 16th 1972 Aero Transporti Italiani I-ATIP, crashed at Foggia, Italy. 18 died |
| May 21st 1972 DTA Angola CR-LLD, crashed at Lobito, Angola. 21 died |
| October 30th 1972 Aero Transporti Italiani I-ATIR, crashed at Poggiorsini, Italy. 27 died |
| December 8th 1972 Pakistan International Airlines AP-AUS, crashed at Rawalpindi, Pakistan. 26 died |
| September 7th 1974 Garuda Indonesia PK-GFJ, crashed at Tandjung-Karang, Indonesia. 33 died |
| March 16th 1975 Aerolineas Argentinas TC-72, crashed at Barito, Argentina. 55 died |
| November 4th 1976 Bali International Air Service PK-KFR, crashed at Banjarmasin, Indonesia. 29 died |
| March 25th 1978 Burma Airways XY-ADK, crashed at Okaraba, Burma. 48 died |
| July 20th 1981 Somali Airlines 6O-SAY, crashed at Mogadishu, Somalia. 50 died |
| August 5th 1984 Biman Bangladesh S2-ABJ, crashed at Dacca, Bangladesh. 49 died |
| June 10th 1986 Air Sinai SU-GAD, crashed at Cairo, Egypt. 23 died |
| August 16th 1986 Sudan Airways ST-ADY, crashed at Malakal, Sudan. 60 died |
| October 23rd 1986 Pakistan International Airlines AP-AUX, crashed at Peshawar, Pakistan. 13 died |
| June 21st 1987 Burma Airways XY-ADP, crashed at Heho, Burma. 45 died |
| October 11th 1987 Burma Airways XY-AEL, crashed at Pagan, Burma. 49 died |
| December 8th 1987 Servicio Aeronaval de Peru AE-560, crashed at Lima, Peru. 42 died |
| July 10th 1988 Kenya Airways 5Y-BBS, crashed at Kisumu, Kenya. no deaths |
| October 19th 1988 Vayudoot VT-DMC, crashed at Gauhati, India. 34 died |
| February 3rd 1989 Burma Airways XY-AEK, crashed at Rangoon, Myanmar. 26 died |
| June 28th 1989 Somali Airlines 6O-SAZ, crashed at Borana, Somalia. 30 died |
| August 25th 1989 Pakistan International Airlines AP-BBF, crashed at Gilgit, Pakistan. 54 died |
| May 10th 1990 Avicsa F-GHXA, crashed at Tuxtla-Gutierrez, Mexico. 27 died |
| May 9th 1991 Merpati Nusantara Airlines PK-MFD, crashed at Sulawesi, Indonesia. 13 died |
| April 26th 1992 SAHA Airlines, crashed at Saweh, Iran. 39 died |
| June 18th 1994 Merpati Nusantara Airlines PK-MFI, crashed at Multiara, Indonesia. 12 died |
| June 26th 1994 Air Ivorie TU-TIP, crashed at Abidjan, Ivory Coast. 17 died |
| November 9th 1995 Lineas Aereas del Estado TC-72, crashed at Luyaba, Argentina. 53 died |
| July 17th 1997 Sempati Air PK-YPM, crashed at Bandung, Indonesia. 28 died |
| August 24th 1998 Myanmar Airways XY-AEN, crashed at Manibagi, Myanmar. 39 died |
| January 12th 1999 Channel Express G-CHNL, crashed at Channel Islands, United Kingdom. 2 died |
| July 2nd 1999 Myanmar Airways XY-AEO, crashed at Sittway, Myanmar. 8 died |
| June 5th 2000 Ghana Air Link G-524, crashed at Accra, Ghana. 6 died |
| November 11th 2002 Laoag Airlines RP-C6888, crashed at Manila, Philippines. 19 died |
| February 20th 2003 Pakistan Air Force J-10254, crashed at Kohat, Pakistan. 17 died |
Total built: (including US 206 built by Fairchild): 786
Fokker built: 580
Operators-list (PDF by fokkerf27.nl)
