TCDS G5EA

Page No. 1 2 Rev. No. 2 2 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION G5EA Revision 2 K & L Soaring, LLC SGS 1-36 November 29, 2010 GLIDER DATA SHEET NO. G5EA This data sheet which is a part of type certificate No. G5EA prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder K & L Soaring, LLC 5996 State Route 224 Cayuta, New York 14824 Type Certificate Holder Record Schweizer Aircraft Corporation County Airport P.O. Box 147 Elmira, New York 14902 I - Model SGS 1-36, 1 PCLM, Approved October 15, 1980 Type Class I, High Performance Airspeed limits Va (Mane uvering) 65 m.p.h. (57 knots) (CAS) Vne (Glide or Dive) 123 m.p.h. (107 knots) Vc (Max. cruising) 110 m.p.h. (96 knots) Vta (Airplane tow) 100 m.p.h. (87 knots) Vtaw (Auto-Winch Tow) 78 m.p.h. (68 knots) Vdb (Glide or Dive) 123 m.p.h. (107 knots) (Dive Brake Open) Center of Gravity Weight Forward C.G. Aft. C.G. (C.G. Range) 710 lb. F.S. 76.96 (25%) F.S. 82.71 (40%) or less Inches Aft. of Datum (+13.347) (+19.095) Straight line variation between points given. Mean Aerodynamic Chord 38.32 inches (Leading edge of M. A.C. at Fuselage Sta. 67.832, +3.767 inches aft. of datum) Control Surface Movements Elevator 21° up (+3° or -0°) 18° down (+3° or -0°) Rudder 27° left 27° right Aileron 30 1/2° up (+3° or -0°) 10° down (+3° or -0°) Dive Brakes upper 87° up (+10° or -0°) lower 68° down (+10° or -0°) Data Pertinent to All Models Datum Wing leading edge at root (Fuselage Sta. 63.615) Levelling Means See Aircraft Weight a nd Balance data in Aircraft Log Book G5EA 2 _________________________________________________________________________________________________ Certification Basis FAR 21, effective February 1, 1965 including Amendments 21-1 through 21-38 FAR 23 effective February 1, 1965 including Amendments 23-1 through 23-12 Basic Glider Criteria Handbook dated 1962 Glider Type Certificate No. G5EA dated October 15, 1980 Date of application for Type Certificate June 28, 1979 Production Basis None Equipment The basic equipment as prescrib ed in the applicable Airworthiness Regulations (see Certification Basis) must be installed in the glider for certification. NOTE 1. A suitable placard to cover the maximum and minimum pilot weights must be installed in full view of the pilot as determined from the manufact urer's weight and balance report. NOTE 2. The following placard must be in stalled in full view of the pilot. FLIGHT LIMITS MODEL SGS 1-36 SER NO. MAX. GLIDE OR DIVE 121 MPH MAX. AERO TOW 98 MPH MAX. AUTO OR WINCH TOW 78 MPH MAX. DIVE BRAKE OPER. 121 MPH MAX. GROSS WT. 710 LBS. MAX. WT PILOT LBS. MIN. WT PILOT LBS. INSTRUMENT FLIGHT PROHIBITED NORMAL OPERATING SPEEDS CALM CONDITIONS AT GROSS WT. AERO TOW 60-70 mph/52-61 knots AUTO/WINCH TOW 55-60 mph/48-52 knots LANDING APPROACH 55 mph/48 knots STALL (BRAKES CLOSED) 35 mph/30 knots BEST GLIDE 53 mph/46 knots MIN SINK 42 mph/37 knots MANEUVERING 64 mph/56 knots APPROVED AEROBATIC MANEUVERS NORMAL ENTRY SPEED SPINS NORMAL STALL ENTRY LOOPS 90 mph/78 knots WINGOVERS 90 mph/78 knots FOR OTHER CONDITIONS SEE PILOTS OEPRATING MANUAL NOTE 3. An approved safety belt and shoul der harness is required for occupant. ...END...