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Input data for an ultralight aircraft
COMPANY DETAILS:
1.1 Full company name:

1.2 Trading name:

1.3 Telephone number:

1.4 Email address:

1.5 Web site URL:

1.6 Factory/warehouse location:

1.7 Airfield name:

1.8 Sales Manager: Name (+ optional phone & email)

1.9 Dealer(s): Name: State: (+ optional phone & email)
AIRCRAFT CATEGORY DETAILS:
2.1 CAO95.55 para 1.2 approved?:

2.2 CAO95.55 para 1.3 approved?:

2.3 CAO95.55 para 1.4 approved?:

2.4 CAO95.55 para 1.5 approved?:

2.5 CAO95.55 para 1.6 approved?:

2.6 JAR-VLA certification?:

2.7 Other international type certification?:
ENGINE & PROP OPTIONS:
3.1



OTHER OPTIONS AVAILABLE:
4.1



AIRCRAFT PERFORMANCE [Standard ultralight version]:
5.1 Aircraft type & model & engine:

5.2 Performance figures are for weight =         kg

5.3 Performance cruise - 75% power (@         rpm):     knots TAS (@        feet altitude)

5.4 Cruise - 65% power (@        rpm):     knots TAS (@        feet)

5.5 Economy cruise - 55% power (@         rpm):     knots TAS (@        feet)

5.6 Range (at 75% power with 30 mins fuel reserve):        nm

5.7 Endurance (at economy cruise with 30 mins fuel reserve):        hours

5.8 Fuel consumption (performance cruise):     l/hr

5.9 Fuel consumption (65% power):     l/hr

5.10 Fuel consumption (economy cruise):     l/hr

5.11 Vne:     knots

5.12 Va:     knots

5.14 Vx:     knots

5.15 Vy:     knots

5.16 Glide ratio - MTOW, propeller stopped:

5.17 Rate of climb (at sea level):     ft/min

5.18 Service ceiling:     feet

5.19 Take-off ground roll (short, dry grass):        m

5.20 Take-off distance over 15 m screen (still air from rest):        m

5.21 Demonstrated maximum crosswind capability:     knots

5.22 Stall - Vso:     knots CAS

5.23 Stall - Vsi:     knots CAS

5.24 Landing ground roll (short, dry grass):     m

5.25 Landing distance to full stop over 15 m screen (still air):     m
AIRCRAFT DIMENSIONS [Standard ultralight version]:
6.1 Aircraft type & model:

6.2 Engine:

6.3 Propeller:

6.4 Overall height:     m

6.5 Length:     m

6.6 Wing span:     m

6.7 Wing area:     m²

6.8 Aspect ratio:

6.9 Cabin width - shoulder height:     m

6.10 Empty weight :     kg

6.11 Maximum take-off weight (AUF accepted):     kg

6.12 Maximum load with full fuel:     kg [use fuel weight=0.71 kg/l]

6.14 Wing loading:     kg/m² mtow

6.15 Design load limit: +     g / -     g

6.17 Fuel capacity:     litres - usable:     litres

6.18 VHF radio fitted:

6.19 Standard instrumentation fitted:

6.20 Tyre size (mains):

6.21 Tyre size (tail/nose):

6.22 Wheel track:     m
PRICE & DELIVERY DATA
7.1





COMPLETING THE FORM
The easiest way to complete the form in a PC is to click "edit' on the menu bar, 'select all', 'copy' (Ctrl+C) and then 'paste' (Ctrl+V) it into an ASCII text editor e.g. Notepad, Wordpad - enter the details, copy and paste the completed form into an email, or attach the text file to an email. [Contact information] 		¤ Buyers
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