Cessna 172M Skyhawk : OO-LNC

C172 OO-LNC
C172-interieur

Aircraft S/N : 17201510 / 1976 

Engine

  • Type Lycoming O-320-E2D
  • Power 150 BHP @ 2700 RPM
  • Static RPM 2300 - 2420 RPM

Fuel

  • Type 100 (green) or 100LL (blue)
  • Total usable 144 l. (38 USGal)
  • FFcruise, 75%BHP 31l/u (8,2 USGal)

Oil

  • Type W80
  • Total Capacity 7,6 l (8.0 qt)
  • min. Required 5,7 l (6.0 qt)

 

Speed max glide range : 65 kts. (Cl/CD)max = 9

Empty weight : 670,3kg.

Max usable load : 372,7 kg. (norm) / 236,9 kg. (util)

MTOW : 1043 kg. (norm) / 907,2 kg. (util)

Max. crosswind component : 15 kts.

ISA MSL T/O run required : 264 m (flaps 0)

ISA MSL T/O distance required over 50 ft : 465 m (flaps 0)

ISA MSL landing ground roll : 159 m (full flaps)

ISA MSL LDR : 381 m (full flaps) over 50 ft.

Significant speeds (kts):

Vs : 47 flaps up/ 41 flaps full      Vx : 59      Vglide : 65 flaps up/ 60 flaps down      Vy : 78 SL/ 74 @ 4000ft      Vfe : 85      Va : 97 @ 1043kg./81 @ 740 kg.      Vno : 128      Vne : 160        

 

Robin DR400-120 : D-EGPG

C172 OO-LNC
Robin-interieur

Aircraft S/N : 2379

Engine

  • Type Lycoming O-235-???
  • Power 112 BHP @ 2600 RPM

Fuel

  • Type 100 (green) or 100LL (blue)
  • Total usable 99l. (of 109 l total) 
  • FFcruise, 75%BHP 22l/u

Oil

  • Type ???
  • Total Capacity 5,6 l (6.0 qt)
  • min. Required 4,2 l (4,5 qt)

 

Speed max glide range : 73 kts. (Cl/CD)max = 10

Empty weight : 575kg.

Max usable load : 325 kg.

MTOW : 900 kg.

Max. crosswind component : 22 kts.

ISA MSL T/O run required : 255 m (flaps 1)

ISA MSL T/O distance required over 50 ft : 535 m (flaps 1)

ISA MSL landing ground roll : 200 m (full flaps)

ISA MSL LDR : 460 m (full flaps) over 50 ft.

Significant speeds (kts):

Vs : 51 flaps up/ 46 flaps full      Vx : 65      Vglide : 73 flaps up      Vy : 75 SL       Vfe : 89      Va : 116 @  900 kg.      Vno : 140  Vne : 166