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 N90341 a

FAA Database: Link

Technische Daten:

Immatrikulation: N90341
Hersteller:  Globe 
 Typ: GC-1B
 Baujahr: 1946
 S/N 355
Motor: 6 Zylinder, Continental IO-360-K, 195 PS.
Spannweite: 8.94 m
Länge: 6.35 m
Flügelfläche: 12.3 m2
Leergewicht: 621 kg
Max. Fluggewicht:   776 kg (1710 lb)
Ausrüstung: voll IFR tauglich, Autopilot

I Brett 

 

Checkliste Seite 1

Checkliste Seite 2

 

Performance

Maximum speed: 130 mph (208 km/h)
Range: 480 miles (768 km)
Service ceiling: ft ( m)
Rate of climb: ft/min ( m/min)
Wing loading: lb/ft² ( kg/m²)

Specifications

Original base price: $3,750 to $4,000
Engine make/model: Continental IO-360-D (modified)
Horsepower for takeoff: x210 (modified)
TBO hours: 1800
Fuel type: 100LL
Propeller make/type: McCauley two-bladed
Landing gear type: Conv./Ret.

Weights

Max ramp weight (lbs):1975
Gross weight (lbs):1975
Max landing weight (lbs): 1975
Empty weight (lbs):1370
Usable fuel (gals): 49 gal.
Oil capacity (qts): 0 qts.

Dimensions

Wingspan: 29 ft. 4 in
Overall length: 20 ft. 10 in.
Height: 6 ft. 2 in.
Wing loading; (lbs/sq. ft.): 15
Power loading; (lbs/hp): 9.4
Wheel track: 10 ft. 6 in.
Seating capacity: x2
Cabin width: 3 ft. 4 in.
Cabin height: 3 ft. 10 in.
Baggage capacity: (lbs): 100

Performance; (knots):

75% power: *173 to 180
65% power: *160
55% power: *150

Max range (with reserve) (nm):

75% power: *1000

Fuel consumption (gph):

75% power: *9
Estimated endurance (65% power w/1 hr reserve) (hrs) : 4.5

Stall speed (flaps up) (knots): *63
Best rate of climb (fpm): *1500
Service ceiling (ft.): *18,000+
Takeoff ground roll (ft.): *400
Landing ground roll (ft.): *800