TCDS TA5CH

Page No. 1 2 3 Rev. No. 8 9 5 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TA5CH Revision 9 Zenair CH2000 October 21, 2011 TYPE CERTIFICATE DATA SHEET NO. TA5CH This data sheet, which is part of Type Certificate No. TA5CH, 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: Zenair Ltd. P.O. Box 235 Midland, Ontario Canada L4R 4K8 I - Model CH2000 (Utility Category) Approved July 25, 1995; (Normal Category) Approved January 29, 2003 Engine Lycoming O-235-N2C with Slick magnetos, MA-3PA carburetor, and Sky-Tec Starter Fuel 100/100LL aviation grade Oil SAE grades 15W50 or 20W50 (Refer to Lycoming Service Instruction 1014) Engine Limits Maximum Takeoff Power 2800 r.p.m. (116 hp) Maximum Continuous Power 2800 r.p.m. (116 hp) Propeller and Propeller Limits Sensenich 72-CK-0-46 or 72-CK-0-48 Diameter: Maximum: 72 in (183 cm) Minimum: 70 in (178 cm) No further reduction permitted. No. of Blades: Two Pitch: 46" - 48" Maximum Static at Full Throttle 2750 r.p.m. Minimum Static at Full Throttle 2550 r.p.m. Airspeed Limits Vne Never Exceed Speed 139 KCAS Vno Maximum Structural Cruising Speed 104 KCAS V A Maneuvering Speed 104 KCAS V fe Maximum Flap Extended Speed 99 KCAS C.G. Range Utility Category: +13.8 in to +17.1 in (+350 mm to +435 mm) at 1608 lbs (730 kg) +12.6 in to +17.1 in (+320 mm to +435 mm) at 1475 lbs (670 kg) or less Straight line variation between points given Normal Category: +14.5 in to +17.1 in (+368 mm to +435 mm) at 1692 lbs (768 kg) +12.6 in to +17.1 in (+320 mm to +435 mm) at 1475 lbs (670 kg) or less Straight line variation between points given Empty Weight C.G. Range None Reference Datum Wing Leading Edge at Rib number 4. Levelling Means Upper Fuselage Longeron. Maximum Weight Utility Category: Takeoff and Landing: 1608 lbs (730 kg) Empty Weight: 1175 lbs (535 kg) Normal Category: Takeoff: 1692 lbs (768 kg) Landing: 1608 lbs (730 kg) Empty Weight: 1175 lbs (535 kg) Minimum Crew One (1) Pilot. No. of Seats Two at +16 in (+400 mm) TA5CH 2 of 3 Maximum Baggage 40 lbs (18g) at +50 in (+1,250 mm). Fuel Capacity 28 gal (106 lite rs) at +39.4 in (+1,000 mm) Usable: 27.5 gal (104 liters) (See Note 1) Oil Capacity 6 qt (5.7 liters) at -36 in (-914 mm) (See Note 1) Control Surface Movements AILERON 15 o ± 1o UP 15 o ± 1o DOWN STABILATOR 12 o ± 0.5o T.E. UP 9.5 o ± 0.5o T.E. DOWN FLAP 50 o ± 2o DOWN RUDDER 21.5 o ± 1.5o left 21.5 o ± 1.5o right Manufacturer's Serial Nos. Those aircraft shown to comply with Canadian DOT Aircraft Type Approval A-185. The Canadian Department of Transport Certificate of Airworthiness for Export endorsed as noted under "Import Requirements" must be submitted for each individual aircraft for which application for certification is made. Serial Numbers 20-0002 thru 20-0043 and 20-0063 thru 20-0065 inclusive, and Serial Numbers 20- 0069 and subsequent are manufactured by Zenair Ltd. Serial Numbers 20-0044 thru 20-0062 and 20-0066 thru 20-0068, and 20-1001 thru 20-1065 were manufactured by Aircraft Manufacturing & Development Co. Import Requirements A U.S. Airworthiness Certificate may be issued on the basis of the Canadian Department of Transport "Certificate of Airworthiness for Export" signed by or for the Minister of Transport, containing the following statement: "The aircraft covered by this certificate has been examined and found to comply with the data forming the basis for DOT Approval No. A-185, (FAA Type Certificate No. TA5CH)". Certification Basis FAR 21.29 and FAR 23 effective Februa ry 1, 1965, as amended by 23-1 through 23-42. JAR-VLA effective April 26, 1990, through Amendment VLA/92/1 effective January 1, 1992, used as a safety equivalence to FAR 23, as provided by AC 23-11. FAR 36 dated December 1, 1969, as amended by current amendment as of the date of type Certification. Production Basis Aircraft Manufactur ing & Development Co. Production Certificate 339CE for Serial Numbers 20-0044 thru 20-0062, 20-0066 thru 20-0068, and 20-1001 thru 20-1065. Equipment The basic required equipment as prescrib ed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. In addition, the following equipment is also required: FAA Approved CH2000 Trainer with Lycoming O-235-N2C Airplane Flight Manual dated July 25, 1995 or later approved revision. Current empty weight and balance report to include a list of installed equipment. Maintenance and Inspection Maintenance and Inspection of this ai rcraft must be carried out according to the most recent publication of the Zenair Ltd. CH2000 Trainer with Lycoming O-235-N2C Service Manual. NOTE 1 A current weight and balance report including list of equipment included in certificated empty weight must be provided with each aircraft at the time of original certification. The certificated empty weight and corresponding center of gravity location must include full oil (2.21 lbs at -36 in.), and unusable fuel of 3.31 lbs (1.5 kg) at +39.4 in. NOTE 2 All placards specified in the FAA Approved Airplane Flight Manual must be displayed in the airplane in the appropriate locations. NOTE 3 Components which are life limited are listed in Service Manual, Section IIIA. Revisions to the Airworthiness Limitations must be FAA approved. 3 of 3 TA5CH NOTE 4 The following are approved options: 1) IFR configuration Night flying lights Wheel fairings Propeller Spinner Vacuum system plus gyros Wing fuel tank Fuel Capacity: Total: 2 x 14.3 ga l (2 x 54 liters) at +33 in (+850 mm) Usable: 2 x 13.2 gal (2 x 50 liters) Alternate fuselage fuel tank Fuel Capacity: Total: 34.3 gal (130 liters) at +39.4 in (+1,000 mm) Usable: 33.8 gal (128 liters) 2) Base airplane as defined in IP L #B is an approved configuration. NOTE 5 Nose Wheel Travel, right or left 14 degrees ± 1 degree. NOTE 6 Serial number 20-0022 and subsequent are appr oved for spins as manufactured. Serial number 20-0002 through 20-0021 inclusive are approved for spins when modified by Zenair in accordance with Inspection Parts List (IPL) #RS. -- END --