យន្តហោះធុន Pilatus PC-6 Porter មានច្រើនសេរី ផលិតនៅប្រទេសស្វីស សម្រាប់បម្រើគ្រប់បេសកកម្ម ដូចជា ចារកម្ម វាយហារ វាយគាំទ្រ ទំលាក់គ្រាប់បែក សង្រ្គោះ រុករក មន្ទីរពេទ្យចល័ត ...កងទ័ពអាកាសភូមិន្ទថៃ បំពាក់យន្តហោះធុន Pilatus PC-6 Porter ចំនួន ១៥គ្រឿងសម្រាប់បេសកកម្មចារកម្មក្រៅប្រទេស និង ២២ គ្រឿងផ្សេងទៀតសម្រាប់ ហ្វឹកហ្វឺន។
The PC-6/A turboporter is the first aircraft in the Pilatus fleet to be powered by Turbomeca Astazou IIE or an IIG turboprop engine. The variant’s engine can generate 320kW of power.
Pilatus PC-6 variants: The Pilatus PC-6 has 15 variants namely PC-6/350, PC-6/A, PC-6/A1, PC-6/A2, PC-6/B, PC-6/B1, PC-6B2-H2, PC-6/C, PC-6/C1, PC-6/C2-H2, PC-6/D-H3, AU-23A Peacemaker, OV-12, UV-20A Chiricahua, and PC-8 Twin Porter. The PC-6/350 is an enhanced version of the original PC-6 model. It is powered by a single Avco Lycoming IGO-540-A1A piston engine. This engine can produce 261kW of output power. The PC-6/A turboporter is the first aircraft in the Pilatus fleet to be powered by Turbomeca Astazou IIE or an IIG turboprop engine. The variant’s engine can generate 320kW of power.
ចំណុចបច្ចេកទេស General characteristics
✈ តម្លៃ Unit Cost: $1,900,000 (2010)
✈ អាកាសយានិក Crew: 1
✈ ទម្ងន់ផ្ទុក Capacity: up to 10 pax / 1,130 kg
✈ ប្រវែងបណ្តោយ Length: 11 m
✈ ទទឹងចុងស្លាបសងខាង Wingspan: 15.87 m (52 ft 1 in)
✈ កម្ពស់ Height: 3.2 m (10 ft 6 in)
✈ ផ្ទៃសំចត Wing area: 30.15 m2 (324.5 sq ft)
✈ ទម្ងន់សំបកយន្តហោះ Empty weight: 1,270 kg (2,800 lb)
✈ Max takeoff weight: 2,800 kg (6,173 lb)
✈ ល្បឿន Maximum speed: 232 km/h
✈ ល្បឿន Cruise speed: 213 km/h (132 mph, 115 kn)
✈ ល្បឿន Stall speed: 96 km/h (60 mph, 52 kn)
✈ ល្បឿន Never exceed speed: 280 km/h
✈ ចម្ងាយ Range: 730 km
✈ ចម្ងាយ Ferry range: 1,612 km
✈ កម្ពស់ Service ceiling: 8,197 m
✈ Average fuel consumption: 148 litres/h (39 US gal/h)
✈ Fuel internal: 645 (+490) lt
- ✈ Capacity: 10 pax.
- ✈ Design diving speed (VD): 167 kt
- ✈ Never exceed speed (VNE): 151 kt
- ✈ Design cruising speed (VC): 119 kt
- ✈ Max. flap extended speed (VFE): 95 kt
- ✈ Stall speed (idle power) flaps up (VS): 58 kt
- ✈ Stall (idle power) flaps dn (VSO): 52 kt
- ✈ Max. operating altitude: 25,000 ft
- ✈ Service ceiling (at max. weight): 20,500 ft
- ✈ Max. rate of climb at sea level: 1,010 ft/min
- ✈ Max. rate of climb at 5,000 ft: 935 ft/min
- ✈ Take-off ground roll at sea level: 197 m / 646 ft
- ✈ Take-off dist to 15 m (50 ft): 475 m / 1,558 ft
- ✈ Landing ground roll at sea level: 127 m / 417 ft
- ✈ Landing distance from 15 m (50 ft): 315 m / 1,033 ft
- ✈ Take-off ground roll at sea level: 197 m / 646 ft
- ✈ Take-off distance to 15 m (50 ft): 440 m / 1,443 ft
- ✈ Max. Range at opt. speed, no reserves, at 10,000 ft: 500 nm
- ✈ Endurance at opt. speed, no reserves: 4 h 20 min
- ✈ Max range with underwing tanks: 870 nm
- ✈ រយៈពេលហោះ Endurance with underwing tanks: 7 h 35 min
- ✈ សាំង/ម៉ោង Average fuel consumption: 148 litres/h (39 US gal/h)
Other Source
- ✈ PC-6/B2-H2
- ✈ Engine: P&WAC PT6A-27, 550 hp / 507kW
- ✈ Wingspan: 15.87 m / 52 ft 1 in
- ✈ Length: 10.9 m / 36 ft 9 in
- ✈ Height: 3.2 m / 11 ft 6 in
- ✈ Wing area: 30.15 sq.m / 324.53 sq ft
- ✈ Wing loading: 15.57 lb/sq.ft
- ✈ loading: 8.8 lb/hp.
- ✈ Gross wt: 4850 lb
- ✈ Empty wt: 2680 lb.
- ✈ Equipped useful load: 1973 lb
- ✈ Payload max fuel: 851 lb.
- ✈ Range max fuel/cruise: 388 nm/2.9 hr
- ✈ Range max fuel / range: 461 nm/ 3.6 hr.
- ✈ Service ceiling: 30,000 ft
- ✈ Max cruise: 135 kt.
- ✈ Max range cruise: 130 kt
- ✈ Stall: 44-50 kt.
- ✈ 1.3 Vso: 57 kt
- ✈ ROC: 1270 fpm.
- ✈ Min field length: 770 ft
- ✈ Fuel cap: 1122 lb. (580 Kg= 580 liters)
- ✈ Seats: 11.
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