Literature,Specs
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Home for Falcon Aircraft Falcon Ultralight Falcon XP Used Falcons Falcon Parts  and Tedlar 

  Falcon OEM Literature  and Specs

The following are scanned images of original Falcon Literature  and spec sheets from the early eighties. This is probably the best source for specs and performance figures and hard to find documents. If some are difficult to read on the screen, try printing them.

 

   OEM Lit p1.jpg (178838 bytes)   OEM Lit p2.jpg (1325508 bytes)   OEM Lit p3.jpg (1088157 bytes)   Oem Lit p4.jpg (268484 bytes)

Original Factory Literature on UL and XP

This was a two page, two sided piece, color pages outside, white inside

 

xpspecs1.jpg (1048888 bytes)    xpspecs2.jpg (334402 bytes)    xpspecs3.jpg (317576 bytes)    xp 3 view.jpg (1330509 bytes)

Factory XP Specs and 3 view drawing

Model Makers: this is probably the only source of a 3 view drawing of the XP. Notice however the early style tip rudders which need to be changed to the later fixed fins and movable rudders on top. See pictures elsewhere. The UL has the same size wing and canard, however less sweep and a smaller fuselage.  

 

OEM UL Lit p1.jpg (1938498 bytes)       OEM UL Lit p2.jpg (2122431 bytes)

UL Literature

UL W&B1.jpg (1189806 bytes)    UL W&B2.jpg (1857331 bytes)

UL W&B Specs

UL Specs p1.jpg (1271899 bytes)     UL Specs p2.jpg (1379692 bytes)    UL tech standards1 .jpg (2121918 bytes)    UL tech standards2.jpg (1206426 bytes)

UL Specs and Tech Standards Committee Application

XP weight and balance 

Weight and balance
Aircraft: Typical XP Date:
Note: Falcon XP: Maximum design limits are 86 to 115 in flight mode with MGW at 1000 pounds

 

Empty ( actual readings) No pilot, no fuel                
                 
    Station   x weight   =moment    
Front wheel   14   9   126    
Right wheel   118   256   30208    
Left wheel   118   256   30208    
Pilot   59   0   0    
Passenger   98   0   0    
Fuel   120   0   0    
    Total   521   60542 CG is 116.2035
                 
Pilot only, minimum fuel ( calculated )                
                 
    Station   x weight   =moment    
Front wheel   14   9   126    
Right wheel   118   256   30208    
Left wheel   118   256   30208    
Pilot   59   200   11800    
Passenger   98   0   0    
Fuel   120   14   1680    
    Total   735   74022 CG is 100.7102
                 
                 
Pilot only, full fuel (calculated)                
                 
    Station   x weight   =moment    
Front wheel   14   9   126    
Right wheel   118   256   30208    
Left wheel   118   256   30208    
Pilot   59   200   11800    
Passenger   98   200   19600    
Fuel   120   90   10800    
    Total   1011   102742 CG is 101.6241
                 
Pilot, passenger, minimum fuel (calculated )                
                 
    Station   x weight   =moment    
Front wheel   14   9   126    
Right wheel   118   256   30208    
Left wheel   118   256   30208    
Pilot   59   200   11800    
Passenger   98   200   19600    
Fuel   120   14   1680    
    Total   935   93622 CG is 100.1305
                 
Pilot, passenger, full fuel, ( calculated )                
                 
    Station   x weight   =moment    
Front wheel   14   9   126    
Right wheel   118   256   30208    
Left wheel   118   256   30208    
Pilot   59   200   11800    
Passenger   98   200   19600    
Fuel   120   90   10800    
    Total   1011   102742 CG is 101.6241
Note MGW is limited to 1000 pounds

Weight and balance Template for working purposes- copy and print
Aircraft: Date:
Note: Falcon XP: Maximum design limits are 86 to 115
Empty ( actual readings) No pilot, no fuel                
                 
  Range Station   x weight   =moment    
Front wheel   14       0    
Right wheel   118       0    
Left wheel   118       0    
Pilot   59       0    
Passenger   98       0    
Fuel   120       0    
    Total   0   0 CG is
                 
Pilot only, minimum fuel ( calculated )                
                 
  Range Station   x weight   =moment    
Front wheel   14       0    
Right wheel   118       0    
Left wheel   118       0    
Pilot 130-200 59       0    
Passenger   98       0    
Fuel 3 gal 120       0    
    Total   0   0 CG is
                 
                 
Pilot only, full fuel (calculated)                
                 
  Range Station   x weight   =moment    
Front wheel   14       0    
Right wheel   118       0    
Left wheel   118       0    
Pilot 130-200 59       0    
Passenger   98       0    
Fuel 15 gal 120       0    
    Total   0   0 CG is
                 
Pilot, passenger, minimum fuel (calculated )                
                 
  Range Station   x weight   =moment    
Front wheel   14       0    
Right wheel   118       0    
Left wheel   118       0    
Pilot 130-200 59       0    
Passenger 210max 98       0    
Fuel 3 gal 120       0    
    Total   0   0 CG is
                 
Pilot, passenger, full fuel, ( calculated )       See note        
                 
  Range Station   x weight   =moment    
Front wheel   14       0    
Right wheel   118       0    
Left wheel   118       0    
Pilot 130-200 59       0    
Passenger 210 max 98       0    
Fuel 15 gal 120       0    
    Total   0   0 CG is
                 
Note MGW is limited to 1000 pounds                
                 

 

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