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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.

Original Factory Literature on UL and XP

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

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.

UL Literature

UL W&B Specs

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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