AopnplicBaatsioisn redpis ÚRAD PRO CIVILNÍ LETECTVí CIVIL AVIATION AUTHORlTY CESKÁ REPUBLIKA CZECH REPUBLIC , v 'ti , TYPOVE OSVEDCENI TYPE CERTIFICATE C. / No: 9 O - O 1 Tímto dokumentem se osvedcuje, že uvedený typ letadla, leteckého motoru nebo vrtule, pokud je udržován a provozován podle príslušn)'ch predpisu s príslušnými provozními omezeními uvedenými v Príloze k tomuto osvedceni, je uznán letove zpusobilým. This document certifies that the type of the mentioned aircraft, aircraft engine or propeller when maintained and operated in accordance with the pertinent regulations and operating limitations, specified in the Type Certificate Data Sheet, is recognised as airworthy. Výrobek Discus CS -PJSSAacriRhldpe-ul2mba2nipcepk-áHirth 638 výr'oba letadel spol. s r.o. Ž56a5date0l1 Chocelí Datmn podáni .žádosti Toto osvedcení a jeho Príloha zusl<Ívaji v platnosti, dokud se jich žadatel nevzdá nebo dokud jejich platnost Úrad pro civilní letectví Ceské republiky nepozastaví, nezruší ci nestanoví ukoncení platnosti jinak. This Type Certificate and the Type Certificate Data Sheet shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Cívil Aviation Authority ofthe Czech Republic. 23-04-2004 Datum vydání - Date of issue (dd-mm-rrrr) - (dd-mm-yyyy) CMIF,T/-O/ /-2/97 /t~ Pódpis -Signature / CIVIL AVlATION AUTHORlTY OF THE CZECH REPUBLIC 90-01 Change 3 Schempp-Hirth výroba letadel spol. sr. o. Discus CS 23.04.2004 TYPE CERTIFICATE DATA SHEET No. 90-01 This data sheet which is a part ofType Certificate No. 90-01 prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Czech Republic .. Model Discus es Application Date Certification Date 19.08.1990 Page No. Rev. No. Change 3 12345 33333 1/5 90-01 Model Discus CS 1. General 1. Data Sheet No.: 2. Model: 3. ~orthiness category: 4. Type Certificate Holder: 5. Manufacturer: 6. Application Date: 7. Certificate Date: 90-01 Discus CS Utility Schempp-Hirth výroba letadel spol. s r.o. Pardubická 638 565 01 Chocen SIN 001 CS through 008 CS Orlican n.p. Chocen SIN 008 CS through 224 CS Orlican a.s Chocen SIN 225 CS and up Schempp-Hirth výroba letadel spol. s r.o. Chocen 19.08.1990 n. Certification Basis 1. Certification Basis: 2. Specia1 Conditions: 3. Exemptions: 4. Equiva1ent Safety Findings: Joint Aviation Requirements JAR 22, Change 3, 13.9.1982 Preliminary Directives for Strengtb Ana1ysis of Components for Sailplanes and Powered Sailplane constructed from Glass and Carbon Fiber Reinforced Plastic, edition of January 1981. None None Change 3 2/5 90-01 m. Technical Characteristics and Operationa! Limitations 1. Type Design Definition: 2. Description: 3. Equipment: 4. Dimensions: 5. Towhook: 6. Air Speeds: 7. Load factors: List of drawings for the Discus CS sailplane, type data sheet No. L-360, state to date ofMay 1990. Single-seat mid-wing sailplane from glass and carbon composite, two-piece wing, airbrakes on the upper surface, water tanks in wing and :fin. Glass composite fuselage with retractable main wheel with damping and brake. T-tail empennage with stabiliser and elevator. Minimum equipment: 1 Airspeed indicator, range up to 300 km/h. 1 Altimeter 1 Four-point safety harnesses (symmetrical) 1 Back cushions (thickness approx. 8 cm compressed) unless parachute used. Span: Length: Height: Wing Area: Aspect Ratio: 15,0 m 6,58 m 1,0 m 10,58 m2 21,3 Nose tow hook "E72", LBA approved - No.:60.230/1 or Nose tow hook" E75", LBA approved - No.:60.230/1 or Nose tow hook " E85", LBA approved - No.:60.230/1 Safety C.G. tow hook" Europa G 72", LBA approvedNo.:60.230/2 or Safety C.G. tow hook " Europa G 73", LBA approvedNo.:60.230/2 ... or Safety C.G. tow hook" Europa G 88", LBA approvedNo.:60.230/2 .. Never exceed speed Manoeuvring speed Maximum speed on aerotow Maximum winch launch speed Rough air speed At VA = 200 km/h At VNE = 250 km/h VNE 250 km/h VA 200 km/h Vr 180 km/h Vw 150 km/h V RA 200 km/h n = +5,3 n = -2,65 n = +4,0 n = -1,5 Change 3 3/5 90-01 8. Weights: 9. Centre of Gra~ty Range: Maximum pennitted take-off mass Maximum pennitted mass of all non-lifting parts Empty mass From 260 to 400 mm behind the datum. 525 kg 240 kg 233 kg 10. Datum: Leading edge ofthe wing root rib. 11. Mean Aerodynamic Cord (MAC): 0,762 m with origin 63 mm behind datum. 12. Leveling Means: 13. Weak links: Wedge 100:4 on the rear top fuselage, horizontal. Winch launch an aerotow max. 680 daN 14. Minimum Flight Crew: . 15. Numberofseats 1 1 16. Control surface deflections: Aileron up down Measuring point distance from aileron axis of rotation Elevator up down Measuring point distance from elevator axis of rotation Rudder to both sides Measuring point distance from rudder axis of rotation 65mm±5mm 35mm±5mm 162 mm 47mm±4mm 47mm±4mm 157 mm 160 mm±20mm 340 mm 17. Wheels and Tyres:: 18. Other Limitations: 4" braked wheel Kobold 103-Tech. spec. No. 32.240/5TS Tyre 4.00-4 - Fabrication permitted at Schempp-Hirth výroba letadel spol. s r.o., Chocen. - AU sailplanes outside surfaces exposed to sunlight must be white painted apart from registration Number and anti-collision marking. - The sai1plane is approved for Day VFR flight. Change 3 4/5 90-01 IV. Operating and Service lnstructions 1. Letová prírucka, vydáni cerven 1990, schváleno SL!. 2. Flight manual, Issue June 1990 3. Flughandbuch fiir das Segelflugzeug Discus es, Ausgabe 1990 4. Prírucka pro údržbu, vydání cerven 1990. 5. Maintenance manual, Issue 1990 6. Wartungshandbuch filr das Segelflugzeug Discus es, Ausgabe 1990 7. Betriebshandbuch filr die Schleppkuplung, Baureihe: Bugkupplung E85, Ausgabe Marz 1989, Revision 4 Mm 2001 8. Betriebshandbuch fiir die Schleppkuplung/Sicherheitskupplung, Baureihe: Sicherheitskupplung Evropa G 88, Ausgabe Februar 1989, Revision 3 Mm-z 2001 v. Notes es1. The Discus is a license production ot the German sailplane Discus b. The developing company and holder ot the design is Schempp-Hirth Flugzeugbau GmbH, KrebenstraBe 25, D-73230 KirchheimlTeck, Germany Change 3 5/5 90-01