WPCh 2sB#Jm Z|xTimes New Roman (TT)Symbol (TT)C\  P6QPa\  P[AP2|?tzphoenix#C\  P6QP# Jon Steiger2Default Paragraph FoDefault Paragraph Font11#XP\  P6QXP##C\  P6QP#  APPENDIX 4. SAMPLE DOCUMENTATION OF TECHNICAL STANDARDS COMMITTEE FINDINGS  (INSTRUCTIONS: Complete all blanks; Insert N/A in blanks not applicable to this particular review; check off other applicable items () as provided.) ISSUED TO: _______________________ ULTRALIGHT MAKE/MODEL: ______________________ ADDRESS: _______________________ SERIAL NUMBER: ______________________ _______________________ REGISTRATION NUMBER: ______________________ ENGINE MAKE/MODEL: ____________ PROPELLER MAKE/MODEL: _______________________ ENGINE MANUFACTURER'S PROPELLER DIAMETER: _______________________ RATED HORSEPOWER: ____________ PROPELLER PITCH: _______________________ FUEL CAPACITY: fuselage tank ________ wing tank _______ other _______ TOTAL: _________ GROSS EMPTY WEIGHT ........................................88888888888888....... _________ Exclusion for parachute system weight .....888888....... ________ ( ) handdeployed ( ) ballistically deployed ( ) installed and operational ( ) standard allowance weight given ( ) parachute system weighed separately Exclusion for floats .....................8888888888...... ________ ( ) weighed in landplane configuration only ( ) weighed in floatplane configuration only ( ) standard allowance for floatsonly given ( ) standard allowance for amphib floats given ( ) standard allowance for amphib fuselage given ( ) standard allowance for outrigger floats given ( ) all floats weighed separately FLOAT MAKE/MODEL: ________________________ Fuel on board at weighing ..................88888888...... ________ TOTAL WEIGHT ALLOWANCES .....................8888...... ________ NET EMPTY WEIGHT (minus weight allowances) ......888888888888.........8.. ________ MAXIMUM FULLPOWER LEVEL FLIGHT SPEED (calculated by AC 1037, Appendix 1). ________ ( ) engine manufacturer maximum rated horsepower used ( ) derated horsepower of engine = ________. per engine manufacturer's specs DEMONSTRATED MAXIMUM FULLPOWER LEVEL FLIGHT SPEED 888................. ________ ( ) timed (average of a series of three level runs in both directions) ( ) radar gun (average series of level runs per timed instructions) ( ) speed adjusted to sea level conditions ( ) artificial restriction ( ) power ( ) propeller ( ) aerodynamic DESCRIPTION OF RESTRICTION (should be included on the back of this form in sufficient written and graphic detail for an FAA inspector or other qualified person to ascertain that the restriction is in place and operational) MAXIMUM POWEROFF STALL SPEED (calculated by AC 1037, Appendix 2) .8888.. ________ operating weight used = ________ maximum coefficient of lift used = ________ DEMONSTRATED POWEROFF STALL SPEED .........................888888888....... ________ ( ) average of six or more stalls (in level flight, with an airspeed reduction of approximately one knot per second until stall occurs) ( ) high lift devices installed ( ) flaps ( ) slots ( ) other CONFIGURATION: ( ) provisions for one occupant only ( ) seat width 22 inches or less (inside measurement) ( ) single seatbelt/shoulder harness ( ) single controls located logically for a person sitting in the center of the seat ( ) no equipment is installed which could logically be construed as for a purpose other than sport/recreation of the operator, such as: ( ) towing hitches ( ) agricultural equipment ( ) advertisement on the wings AIRWORTHINESS CERTIFICATION: ( ) no U.S. or foreign airworthiness certificate is currently Issued to this particular ultralight unit ( ) this ultralight has not been registered with the U.S. federal government. LIST OF INSTALLED INSTRUMENTS AND EQUIPMENT: OTHER: ISSUED BY: ( ) A & P Mechanic; Name ______________________________ Certificate Number ________________ ( ) Technical Standards Committee: Names: _________________________________________________ __________________________________________________ __________________________________________________ ( ) National pilot organization recognizing this committee: ______________________________________ DATE OF ISSUANCE OF THIS DOCUMENT: ________________________