FEDERAL AVIATION AGENCY

TYPE CERTIFICATE DATA SHEET NO. G6EU	G6EU
Revision 1
AER-PEGASO
M-100 S
                August 23, 1966	

This data sheet which is a part of type certificate No. G6EU prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Civil Air Regulations.

Type Certificate Holder		Aer-Pegaso S.p.A.
				Torino, Italy

Model "M-100 S" approved February 18, 1965

Airspeed limits (IAS) 		Glide or dive 		119 kts. 	(still air)
				" 	" 		70   " 	(rough air)
				Airbrakes extended 	108 " 	(still air)
				" 	" 		70   " 	(rough air)
				Airplane tow 		81   "
				Auto-winch tow 		55   "

C.G. Range 			from (+11.3) to (+16.5)

Datum 				Wing leading edge

Leveling means 			Fuselage upper contour just in front of the dorsal fin at 4° down with
				respect to horizontal reference.

Maximum weight 		693 lbs.

No. seats 			1 at (-19.7)

Baggage 			(+7.88) Max. permissible baggage: 100 lbs.

Control surfaces 			Elevator 	Up 	28° ± 2° 	Down 	20° ± 2°
				Rudder 		Right 	28° ± 2° 	Left 	28° ± 2°
				Ailerons 	Up 	28° ± 2° 	Down 	28° ± 2°

Serial Nos. eligible 		An Italian Certificate of Airworthiness for Export endorsed as noted under
				"Import Requirements" must be submitted for each individual glider
				for which application for certification is made.

Certification basis 		CAR 10 Type Certificate G6EU. CAR 5 dated February 5, 1956 (Basic Glider
				Criteria, revised 1962)
				Date of Application for Type Certificate May 7, 1963.

Import Requirements 		An U.S. Airworthiness Certificate may be issued on the basis of a
				Certificate of Airworthiness for Export signed by a representative
				for the R.A.I., containing the following statement: "The glider covered
				by this Certificate has been examined and found to comply with
				CAR 5 dated February 15, 1956 (Basic Glider Criteria, revised 1962),
				Type Certificate G6EU and is airworthy.

Equipment 			Non cloud flying and Acrobatic: safety harness, airspeed indicator, altimeter.
				Cloud flying: above items plus: turn and bank indicator, compass, variometer.

NOTE 1. 	Current weight and balance report, including list of equipment included in certified empty weight,
		and loading instructions when necessary, must be in the glider at the time of original certification
		and at all times thereafter.

NOTE 2. 	The following placards must be installed in full view of the pilot:

		Max. speed (Vne) still air 					119 kts.
		" 	" 	with airbrakes extended, still air 		108  "
		" 	" 	rough air (airbrakes extended or closed) 	70    "
		" 	" 	aero tow 				81    "
		" 	" 	auto-winch tow 				55    "

		Permitted aerobatics:
			Looping: entry speed 				78 kts.
			chandelle: " 	" 				70  "
			spin:  	   " 	" 				32  "
			tight turns till 3.5g.
			All other acrobatics are prohibited."

		"Night flying is prohibited"

		"Auto-Winch tow is permitted for towing mechanism located near the C.G."

		The following placard must be installed in the baggage compartment:

			"Max. permissible baggage: 100 lbs."

						...END...