JEROEN VOGELAAR: Aviation Photographs

passenger

Focke-Wulf A 16

Focke-Wulf A.16 D437 Bremen

The Focke-Wulf A.16 was a German three/four passenger light transport monoplane.

  • Role: Light passenger transport
  • National origin: Germany
  • Manufacturer: Focke-Wulf Flugzeugbau AG
  • Designed by: Heinrich Focke and Georg Wulf
  • First flight: 1924
  • Number built: 20+

Focke-Wulf A.16 D437 Bremen

Specifications (A.16c)

General characteristics

  • Crew: 1
  • Capacity: 3–4
  • Length: 8.5 m (27 ft 1034 in)
  • Wingspan: 13.90 m (45 ft 714 in)
  • Height: 2.30 m (7 ft 612 in)
  • Wing area: 27.1 m2 (291 ft2)
  • Empty weight: 570 kg (1256 lb)
  • Gross weight: 970 kg (2138 lb)
  • Powerplant: 1 × Siemens-Halske Sh 11 7-cylinder radial piston engine, 56 kW (75 hp)

Performance

  • Maximum speed: 135 km/h (84 mph)
  • Range: 550 km (342 miles)
  • Service ceiling: 2500 m (8200 ft)

Junkers Ju 52

Junkers Ju-523mg4e HB-HOS Ju-Air

The Junkers Ju 52 (nicknamed Tante Ju (“Aunt Ju”) and Iron Annie) was a German trimotor transport aircraft manufactured from 1931 to 1952. It saw both civilian and military service during the 1930s and 1940s.

  • Role: Transport aircraft
  • National origin: Germany
  • Manufacturer: Junkers
  • First flight: 13 October 1930 (Ju 52/1m); 7 March 1932 (Ju 52/3m)
  • Introduction: 1931
  • Status: retired
  • Produced: 1931–1945 (Germany) Junkers, 1945–1947 (France) Amiot AAC 1 Toucan, 1945–1952 (Spain) CASA 352 and 352L
  • Number built: 4,845

Military Junkers Ju 52 Fact-sheet

Junkers Ju-523mg4e HB-HOS Ju-Air

Specifications (Junkers Ju 52/3m ce)

General characteristics

  • Crew: two
  • Capacity: 17 passengers
  • Length: 18.90 m ()
  • Wingspan: 29.25 m ()
  • Height: 6.10 m ()
  • Wing area: 110.5 m² ()
  • Empty weight: 5,970 kg (13,180 lb)
  • Max. takeoff weight: 9,210 kg (20,330 lb)
  • Powerplant: 3 × BMW Hornet A2, 386 kW (525 PS) each

Performance

  • Maximum speed: 271 km/h (168 mph) at 900 m
  • Cruise speed: 222 km/h (138 mph)
  • Range: 950 km (590 mi)
  • Service ceiling: 5,200 m (17,050 ft)
  • Rate of climb: 3.90 m/s ()
  • Wing loading: 83.35 kg/m² ()
  • Power/mass: 7.95 kg/kW (5.85 kg/PS)

Junkers (CASA) 352A-3 (Ju-52) HB-HOY Ju-Air

Pilatus PC-12

Pilatus PC-12.47E HB-FVY Pilatus Aircraft Factory

  • Role: Passenger and cargo aircraft
  • National origin: Switzerland
  • Manufacturer: Pilatus Aircraft
  • First flight: 31 May 1991
  • Introduction: 1994
  • Status: Active service, in production

Pilatus PC-12 HB-FVJ Privat

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)