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Aircraft Performance Database

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Performance

TAKE-OFF CLIMB (to FL 150) CLIMB (to FL 240) MACH CLIMB CRUISE INITIAL DESCENT (to FL 240) DESCENT (to FL 100) APPROACH LANDING INITIAL CLIMB (to 5000 ft) CLIMB (to FL 240) CLIMB (to FL 150) DESCENT (to FL 100)

Select performance graph to see data.

TAKE-OFF MTOW: WTC: RECAT-EU: - Distance: V2 (IAS): - - INITIAL CLIMB (to 5000 ft) IAS: ROC: - - CLIMB (to FL 240) IAS: ROC: - - CLIMB (to FL 150) IAS: ROC: - - MACH CLIMB MACH: ROC: - - CRUISE MACH: Ceiling: - - TAS: - Range: - INITIAL DESCENT (to FL 240) MACH: - ROD: - DESCENT (to FL 100) IAS: - ROD: - APPROACH IAS: - MCS: - ROD: - LANDING Vat (IAS): - APC: - Distance: - - -

Take-off

V2 (IAS) 60 kts

Distance 300 m

WTC L

RECAT-EU Light

MTOW 1050 kg

Initial climb (to 5000ft)

IAS 90 kts

ROC 400 ft/min

Climb (to FL 150)

IAS no data kts

ROC no data ft/min

Climb (to FL 240)

IAS no data kts

ROC no data ft/min

MACH climb

MACH no data

ROC no data ft/min

Cruise

TAS 115 kt

MACH no data

Ceiling FL 130

Range 430 NM

Initial Descent (to FL 240)

MACH no data

ROD no data ft/min

Descent (to FL 100)

IAS 120 kt

ROD 500 ft/min

Approach

IAS 110 kt

ROD 500 ft/min

MCS no data kt

Landing

Vat (IAS) 65 kt

Distance 160 m

APC A

Type of Aircraft

Type

L1P

APC

A

WTC

L

RECAT-EU

Light

Technical

Wing Span

10,9 m

Length

8,2 m

Height

2,7 m

Power plant

1 x 145 HP Continental O-300-A or 1 x 175 HP Continental GO-300-C or 1 x 145 HP Continental O-300-C or 1 x 160 HP Lycoming O-320-H2AD or 1 x 195 HP Continental IO-360-KB piston engine with 2 blade propeller.

Performance Similarity

No data

Recognition

Wing position

High wing (wing struts)

Engine position

Nose mounted

Tail configuration

Regular tail, mid set

Landing gear

Tricycle fixed

Recognition similarity

No data

Supplementary

IATA

no data

Accommodation

One pilot and 3 passengers.

Notes

Light utility aircraft. In service since 1956 (172R since 1996). Exists in many civil and military models. Worldwide about 37.000 aircraft built between 1955 and 1985. Non retractable gear. Last major Skyhawk Model CESSNA 172N. Licence production F172 by REIMS, France. New version 172R and 172SP based on the 172N with quiet engines, GPS/IFR GPS and single axis autopilot were put in production in 1996. US-mil. type: T-41 Mescalero as basic trainer and observation aircraft. Note: Has 2 side windows and rounded rear window.

Alternative names

  • AVIONES COLOMBIA 172

  • CESSNA 172,P172,Skyhawk,Hawk XP

  • CESSNA R172 Cutlass

  • Cutlass

  • F172 Skyhawk

  • FMA P-172

  • FP172 Reims Rocket

  • FR172 Hawk XP

  • Hawk XP

  • P-172

  • P172 Hawk XP

  • R172 Cutlass

  • REIMS F172,FP172, Skyhawk,Reims Rocket

  • REIMS FR172 Hawk XP

  • Reims Rocket

  • Skyhawk (172)

  • CESSNA 172,Skyhawk