European Aviation Safety Agency

Transcription

1 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET SZD-24 Foka Type Certificate Holder: Zakład Szybowcowy Jeżów Henryk Mynarski ul. Długa Jeżów Sudecki POLAND EASA TCDS No. A.319 For variants: SZD-24 C Foka Issue 01, 18 February 2010

2 General 0.I. Table of Content SECTION 0: 0.I. 0.II. 0.III. Table of Content List of Effective Pages Change Record SECTION A: SZD-24 C Foka A.I. A.II. A.III. A.IV. A.V. General Certification Basis Technical Characteristics and Operational Limitations Operating and Service Instructions Notes 0.II. List of Effective Pages Page 0-1 A-1 A-2 A-3 A-4 Issue III. Change Record Issue Date Changes Issue February 2010 Transfer from Polish Approvals: 8/TL/61 dated on 29 December /TL/64 dated on 17 July 1964 Page 0-1, Issue 01, 18 February 2010

3 Section A: SZD-24 C Foka A.I. General 1. Data Sheet No.: EASA.A a) Type: b) Variant: SZD-24 Foka SZD-24 C Foka 3. Airworthiness Category: Sailplane, Utility 4. Type Certificate Holder: Zakład Szybowcowy Jeżów Henryk Mynarski ul. Długa Jeżów Sudecki POLAND 5. Manufacturer: Zakłady Sprzętu Lotnictwa Sportowego ul. Cieszyńska Bielsko-Biała POLAND 6. Polish CAA Certification Date 29 December The EASA Type Certificate replaces Polish Approvals: 8/TL/61 dated on 29 December /TL/64 dated on 17 July 1964 A.II. Certification Basis 1. Certification Basis: Defined on Airworthiness Requirements: Polish Civil Aviation Requirements, Section G - Gliders, issued on Requirements elected to comply: None 4. Special Conditions: None 5. Exemptions: None 6. Equivalent Safety Findings: None Page A-1, Issue 01, 18 February 2010

4 A.III. Technical Characteristics and Operational Limitations 1. Type Design Definition: Drawings No. SZD 24 C SZD 24 C SZD 24 C Description: Single seat, standard class sailplane. Cantilever high-wing monoplane with classic tail unit (fixed stabilizer with elevator, swept-back fin and rudder). Mainly wooden structure, with undevelopable parts of fuselage shells made of glass-polyester composite. Bipartite tapered wings with main and auxiliary spars and sandwich structure shells. Fixed undercarriage consists of main wheel equipped with drum brake, long wooden nose skid with shock absorption and steel tailskid. Double-plate airbrakes protruding from upper and lower surface of wings. 3. Equipment: Standard equipment: - airspeed indicator, - altimeter, - compass, - bank-and-turn indicator, - rate-of-climb indicator, - towing hook, - pilot safety belts. 4. Dimensions: Span 14,98 m Wing area 12,16 m² Aspect Ratio 18,5 Length 7,00 m Height 1,40 m 5. Launching Hook: standard: SZD-III also permissible: TOST G 72, G 73, G 88, E 72, E 75, E Weak links: Ultimate Strength: dan ( kg) 7. Air Speeds: Manoeuvring Speed V A 130 km/h Never Exceed Speed V NE 220 km/h Maximum permitted speeds - in rough air V RA 130 km/h - in aero-tow V T 140 km/h - in winch-launch V W 110 km/h 8. Operational Capability VFR Day, High-altitude flying. Page A-2, Issue 01, 18 February 2010

5 9. Masses: Max. Take Off Mass 375 kg Max. Empty Mass 265 kg 10. Centre of Gravity Range: Empty sailplane with standard equipment: Forward Limit: 551 mm aft of datum point (ADP) Rearward Limit: 599 mm aft of datum point (ADP) Centre of Gravity operational limits: Forward Limit: 205 mm (ADP) (23,0% MAC) Rearward Limit: 350 mm (ADP) (39,3% MAC) 11. Seating Capacity: 1 MAC is 890 mm; 0% MAC is on the same coordinates along longitudinal axis as the datum. Datum: Leading edge and wing-fuselage division plane intersection. Levelling means: Levelling marks on fuselage sides. 12. Lifetime limitations: Refer to Service Bulletin No. BE-008/85 Foka-C 13. Other limitations: Bungee launching is prohibited. Cloud or night flying is prohibited. Aerobatics is prohibited. Manoeuvring load factor limits: +6,0/-3,0 14. Deflection of control surfaces: Aileron: - up 34 ± 2 - down 16 ± 1 Elevator: - up 23 ± 1,5 - down 18 ± 1 Elevator trim tab: - up 15 ± 3 - down 40 ± 3 Rudder: - left right 35-3 Page A-3, Issue 01, 18 February 2010

6 A.IV. Operating and Service Instructions 1. Flight Manual: German: Szybowiec wyczynowy SZD-24C Foka, Instrukcja Użytkowania, wydanie I r. Szybowiec SZD-24C Foka, Instrukcja Użytkowania w Locie, wydanie II r. Flughandbuch für das Segelflugzeug SZD-24C Foka, Ausgabe März Maintenance Manual: Opis Techniczny, Instrukcja Obsługi Technicznej, Terminarz prac okresowych, Szybowiec SZD-24C Foka, wydanie I - maj 1965 r. 3. Flight & Maintenance Manual: German: Betriebsanleitung für das Hochleistungs - Segelflugzeug SZD-24C Foka, English: SZD-24C Foka, High Performance Sailplane, Flight & Maintenance Manual approved by Polish Aviation Authority on 3 September Repairs Manual: German: Instrukcja remontu szybowca SZD-24C Foka, część szczegółowa, wydanie I, 1968 rok. Segelflugzeug - Reparaturanweisung (Holzbau) Ausgabe II, Bulletins: BE-005/75 Foka 4 BE-06/4A/80 Foka 4 Introducing the Annex No. 1 to Technical Service Manual concerning the extended range of glider periodic inspections. Change of time between overhauls and further use. BE-008/85 Foka-C Unification and way of periodic inspections for SZD-24C Foka C gliders on base of the bulletin data for SZD-24-4A Foka 4 type. A.V. Notes 1. Serial Numbers: W-136 W-223 Page A-4, Issue 01, 18 February 2010