*****AIRCRAFT “Mooney - Bravo M20P”*****

REFERENCE INFORMATION (by Aircraft performance database)

 

*****Aircraft Features*****

Wing position: Low wing

Engine position: Nose mounted

Tail configuration: Regular tail, high set

Landing gear: Tricycle retractable

Wing Span: 11.1 m

Length: 8.15 m

Height: 2.5 m

Power plant: 20C: 1 x 180 HP Lycoming O-360-A1D piston engine with 2 blade propeller. 20E: 1 x 200 HP Lycoming IO-360-A1A piston engine with 2 blade propeller. 20R: 1 x 280 HP Continental IO-550G piston engine with 2 blade propeller.

Accommodation: One pilot and 3 passengers.

Notes: Light aircraft. In service since the mid 50s (M-20E since 1963). Developed in many versions. From the mid 60s all models with a small fin fillet and a large squared rear cabin window. From 1970 to 1972 MOONEY was known as the AEROSTAR. The M-20C Ranger was designed as AEROSTAR 200, the M-20E Chaparral as AEROSTAR 201 and M-20F Executive as AEROSTAR 220. Production ceased in 1972. MOONEYS new owner Republic Steel Company placed the M-20 family back into production in 1973 with new models. Production halted in 2008.
Alternative names:
220 (AEROSTAR), AEROSTAR (1) 200,201,202,220, Allegro, ATS, Chaparral, Executive, M-20, M-20 Mark 21,Ranger,Master, M-20 Statesman,Ovation,Allegro
M-20 Super 21,Chaparral,Executive, M-201,205,ATS,MSE,PFM, M-205,ATS,MSE,PFM
M-20A/B/C/D/E/F/G/J/L/R/S, Mark 21, Master, MOONEY M-20 Mark 21,Ranger,Master
MOONEY M-20 Statesman,Ovation,Allegro, MOONEY M-20 Super 21,Chaparral,Executive, MOONEY M-20,M-20A/B/C/D/E/F/G/J/L/R/S, MOONEY M-201,205,ATS,MSE,PFM, MSE, Ovation, PFM, Ranger (M-20) , Statesman, Super 21
M-20A/B/C/D/E/F/G/J/L/R
.

 

*****Total Flight Simulator aircraft weight with full fuel*****  

000,000 lbs - 1.170 kg

VMO - Maximum Operating Speed 237 KIAS

MMO - Maximum Operating Speed Mach  nd Mach

Turbulent Air Penetration Speed   000 KIAS/.00 Mach

VLO - Maximum Gear Operating Speed   000 KIAS

VLE - Maximum Landing Gear Extension Speed   000 KIAS/.00 Mach

 

*****Maximum Flap Placard Speeds*****

Flaps degrees KIAS

1                      000

2                      000

5                      000

10                    000

15                    000

25                    000

30                    000

40                    000

 

*****Take-off*****

WTC:               L

Distance:         450 mt

V2 (IAS):         70 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:                 100 kt

ROC:               1240 ft/min

-(to FL150)

IAS:                 150 kt

ROC:               1000 ft/min

-(to FL240)

IAS:                 150 kt

ROC:               500 ft/min

-(mach)

mach:              nd

ROC:               nd ft/min

*****Cruise*****

TAS:                237 kt

MACh:             nd data

Ceiling:            FL250

Range:            1445 NM

 

*****Descent *****

- (to FL240)

mach:              nd

ROD:               nd ft/min

- (to FL100)

IAS:                 150 kt

ROD:               500 ft/min

 

*****Approach*****

IAS:                 150 kt

MCS:               66 kt

ROD:               500 ft/min

 

*****Landing*****

Vht (IAS):        60 kt

APC:                A

Distance:         250 mt