VULCAN AIR  / PATRENAVIA P68B

 

 
Partenavia P68B
 

S/N 023

Year 1974
Aeromeccanica SA
Tel: +41 (0) 91 745 66 89
 

Total time: 4007 Location: Switzerland Lyco IO-360-A1B6 200hp TSOH: 226 Overh 10/00. Hartzell HC-C2YK-2CUF TSO: 101 Overh by Publiaerfoto, 12/01 KMA24 Audio w MB and Intcom KY155 COM NAV 760 Chan, FM Immune KR87 ADF KI227-01ADF/RMI KN64 DME KI525 HSI KT76 XPDR Skymap III Moving Map Century IIIB 3 ax Ap KI NAV 2 Indic w g s ELT Cop Altime Elect Trim Copi Attit Indic and Airspeed Indic White w red black stripes 08/10 Gray leather w Bordeaux redone in 99 08/10 deice, Prop. elec deice, Windsh alcohol Euro 155k VAT Incl

 

 

 

Wipline 3450 Series Floats

P.68B Max Takeoff 4321lb, Empty 2645 #  
Floats 3450 643 lbs.  (Exchange 480 #) (100%) 3600 lbs. -- (80%) 4000 lbs.
Amphibious Maximum aircraft gross weight with 80% reserve buoyancy (2 floats) as per TSO-C27.

Aerocet 3400 Amphibious Floats are designed to handle airplanes with gross weights up to 3775 lb.  $65,500

BERIEV Aircraft Company

Standard Empty C-Model Amphibious Wipline 6100 Float Specifications    
Engine:   IO 360 A1 B6 (200 HP)
Max Ramp Weight:   4630 lb
Max Take Off Weight:   4594 lb
Max Landing Weight:   4365 lb
Max Useful Load Wheels:   1720 lb
Max Useful Load Amphibian:     760 lb  180k US
Max Useful Load Floats:   1234 lb  105k US
Fuel Capacity184 USG:   1242 lb
Number of Seats:   6
Luggage Capacity:   20 cubic ft
   
     

 

 

Specifications :

Targeted TBO : 3,000 hours
Consumption : 39 l/h at 200 hp = 10.5 US Gal/h
Max Operating Altitude : 12 500 ft
Critical Altitude: 10 000 ft
Max Cylinder Heads Temp : 181°C / 358°F
Max Oil Temp : 110°C / 230°F
Oil Pressure at 2,200 rpm : 4,2 bar abs
Max Input Fuel Temp : 65°C
Input Pressure at Fuel Pump : 600 mbar
Max Input Air Temp : 65°C / 149°F
Manifold Air Pressure at take-off power : 2,9 bar = 86 in Hg
Max Inlet Temp : 715°C
Turbo Speed at Cruise Power : 125 500 rpm

Power : 230 hp
Fuel : Jet A 1
Displacement : 5 liters / 305 cubic inches
Oil : AeroShell Oil Diesel 10w40
Glow Plugs : Preheat for starts
Propeller speed : 2,200 rpm
Dry weight : 192 kg / 423 lbs
Dimensions : - Length: 820 mm or 32 in
  - Width: 930 mm or 36.3 in
  - Height: 730 mm or 28.5 in
 

 

Sandrine VACHER

+33 01 60 95 07 87

sandrine.vacher@smasr.com

 

Olivier DUQUESNE

+33 01 57 60 63 37

Olivier.O.Duquesne@OPE.shell.com

 
Advantages and performance
1 - Improved performance
- Take-off power : 230hp
- Maxi continuous power until 10.000 feet : 200hp
2 - Reduced consumption by 30 to 40%
- 47 l/h (12,41 US Gal) at 230 hp
- 39 l/h (10,30 US Gal) at 200 hp
- 34 l/h (8,99 US Gal) at 85% of  mct
- 25 l/h (6,61 US Gal) at 65% of  mct
3 Targeted TBO 3000 hours thanks to :
- Diesel technology
- Aeronautical design of the engine
- Materials chosen
- Reduced engine speed
4 - Easier maintenance
- First visit every 100 hours
- More than 70% fewer parts
- Easier access to all components
- Direct injection
 
5 - User friendly
- Single lever
- Reduced noise level in the cabin
- Immediate cold start up -20°C
6 - Increased safety and reliability
- Fuel less volatile
- Integrated electronic engine monitoring
- No magneto or spark plugs
- No detonation or risk of back fire
- Manual emergency mode
 
7 - Respect for environment
- Noise level reduced by 5 to 7 Db
- Significant reduction in air pollution
8 - Compatibility
- Suitable for most of the 180-250 hp light aircraft in the market
 
 

Performance

Larger C-Model

 

Partenavia P 68

Luxurious interior

State of the art instruments