TCDS A10WE

Page No. 1 2 3 4 5 6 Rev. No. 8 6 6 6 6 6 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A10WE Revision 8 WEATHERLY 201 201A 201B 201C November 5, 2014 TYPE CERTIFICATE DATA SHEET NO. A10WE This data sheet which is part of type certificate No. A10WE 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 Weatherly Aircraft Company 2034 W. Potomac Avenue Chicago, Illinois 60622-3152 Type Certificate Ownership Record GBECK, Inc. (D.B.A.) Weatherly Aircraft Company, 5000 Bailey Loop, McClellan, California 95652 transferred ownership of TC A10WE to Weatherly Aircraft Company on October 20, 2000 I - Model 201 (Restricted Category) Approved January 30, 1967 Engine Pratt & Whitney R985-AN1, AN-3, or AN-14B Fuel 80/87 Minimum Grade Aviation Gasoline Engine Limits HP RPM In. Hg. Press Engine Model AN-1 & AN-3 Alt. Takeoff (1 min.) at SL 450 2300 37.5 SL Max. Continuous at SL 290 2000 30.0 SL Max. Continuous 327 2000 30.0 6300 (Rated Press Alt.) HP RPM In. Hg. Press Engine Model AN-14B Alt. Takeoff (1 min.) at SL 450 2300 36.5 SL Max. Continous at SL 310 2000 30.0 SL Maximum Continuous 343 2000 30.0 6500 (Rated Press Alt.) Propeller and Hamilton Standard 2D-30 Hub, 6101A or 6167A blades propeller limits Diameter: Not over 108 ins.; Not under 99 ins. Air Speed limits Vne - Never Exceed 145 mph (126 knots) EAS Vno - Max. Structural 128 mph (111 knots) EAS Vp - Maneuvering 115 mph (100 knots) EAS C.G. range Inches Aft of Datum (+20.8) to (+24.84) at all weights Empty weight C.G. range None Datum Wing Leading Edge Max. weight 3500 Lbs. A10WE Page 2 of 6 Leveling means Leveling lugs on right side of fuselage Aft of Pilot's Seat No. seats 1 (+67.0) Hopper capacity 1000 Lbs. (+15.0) Fuel capacity 48 Gal. Total - 2 wing tanks 24 Gal. Ea. Unusable Fuel - 2 Gal. per tank (+36.0) Oil capacity 7 1/2 Gal. plus 1 Gal. in System (+86.0) Control surface movements Rudder Left 20° ± 1° Right 20° ± 1° Elevator Up 28° ± 1° Down 15° ± 1° Elevator tab Up 7° ± 1° Down 15° ± 1° Aileron Up 27° ± 1° Down 16° ± 1° Serial Nos. eligible 101 thru 109 II - Model 201A (Restricted Category) Approved November 27, 1968 Same as Model 201 except for larger wing fuel tanks, tail wheel gear and minor changes. Engine Pratt & Whitney R985-AN1, AN-3, or AN-14B Fuel 80/87 Minimum Grade Aviation Gasoline Engine Limits HP RPM In. Hg. Press Engine Model AN-1 & AN-3 Alt. Takeoff (1 min.) at SL 450 2300 37.5 SL Max. Continuous at SL 290 2000 30.0 SL Max. Continuous 327 2000 30.0 6300 (Rated Press Alt.) HP RPM In. Hg. Press Engine Model AN-14B Alt. Takeoff (1 min.) at SL 450 2300 36.5 SL Max. Continous at SL 310 2000 30.0 SL Maximum Continuous 343 2000 30.0 6500 (Rated Press Alt.) Propeller and Hamilton Standard 2D-30 Hub, 6101A or 6167A blades propeller limits Diameter: Not over 108 ins.; Not under 98 ins. Pitch Settings at 42" Station: (Two Position) - 15° Low 17° High Static RPM at Max. permissible throttle settings: Not over 2150; not under 2050 (Constant Speed Optional) - 14° Low 23° High Air Speed limits Vne - Never Exceed 145 mph (126 knots) EAS Vno - Max. Structural 128 mph (111 knots) EAS Vp - Maneuvering 115 mph (100 knots) EAS C.G. range Inches Aft of Datum (+20.8) to (+24.84) at all weights Empty weight C.G. range None Datum Wing Leading Edge A10WE Page 3 of 6 Max. weight 3500 Lbs. Leveling means Leveling lugs on right side of fuselage. Aft of Pilot's Seat No. seats 1 (+67) Hopper capacity 1000 Lbs. (+15.0) Fuel capacity 55 Gal. Total - 2 wing tanks 27 1/2 Gal. Each Unusable Fuel - 2 1/2 Gal. per tank (+36.0) Oil capacity 7 1/2 Gal. plus 1 Gal. in System (+86.0) Control surface movements Rudder Left 20° ± 1° Right 20° ± 1° Elevator Up 27° ± 1° Down 15° ± 1° Elevator tab Up 7° ± 1½° Down 15° ± 1½° Aileron Up 25° ± 1° Down 16° ± 1° Serial Nos. eligible 110 thru 601 III - Model 201B (Restricted Category) Approved 2 December 1971 Same as Model 201A except for new leading edge fillet at wing root, wider canopy and other minor changes. Engine Pratt & Whitney R985-AN1, AN-3, or AN-14B Fuel 80/87 Minimum Grade Aviation Gasoline Engine Limits HP RPM In. Hg. Press Engine Model AN-1 & AN-3 Alt. Takeoff (1 min.) at SL 450 2300 37.5 SL Max. Continuous at SL 312 2000 30.0 SL Max. Continuous 340 2000 30.0 6600 (Rated Press Alt.) HP RPM In. Hg. Press Engine Model AN-14B Alt. Takeoff (1 min.) at SL 450 2300 36.5 SL Max. Continous at SL 310 2000 30.0 SL Maximum Continuous 343 2000 30.0 6500 (Rated Press Alt.) Propeller and Hamilton Standard 2D-30 Hub, 6101A or 6167A blades propeller limits Diameter: Not over 108 ins.; Not under 98 ins. Pitch Settings at 42" Station: (Two Position) - 15° Low 17° High Static RPM at Max. permissible throttle settings: Not over 2150; not under 2050 (Constant Speed Optional) - 14° Low 23° High Air Speed limits Vne - Never Exceed 145 mph (126 knots) EAS Vno - Max. Structural 128 mph (111 knots) EAS Vp - Maneuvering 115 mph (100 knots) EAS C.G. range Inches Aft of Datum (+20.8) to (+24.84) at all weights Empty weight C.G. range None Datum Wing Leading Edge outboard of fillet A10WE Page 4 of 6 Max. weight 3500 Lbs. Leveling means Leveling lugs on right side of fuselage. Aft of Pilot's Seat No. seats 1 (+67.0) Hopper capacity 1000 Lbs. (+15.0) Fuel capacity 55 Gal. Total - 2 wing tanks 27 1/2 Gal. Each Unusable Fuel - 2 1/2 Gal. per tank (+36.0) Oil capacity 7 1/2 Gal. plus 1 Gal. in System (+86.0) Control surface movements Rudder Left 20° ± 1° Right 20° ± 1° Elevator Up 27° ± 1° Down 15° ± 1° Elevator tab Up 7° ± 1½° Down 15° ± 1½° Aileron Up 25° ± 1° Down 16° ± 1° Serial Nos. eligible 602 thru 1000 IV - Model 201C (Restricted Category) Approved December 23, 1975 Same as Model 201B except aft fuselage same monocoque and extended 6 inches, engine mount extended 1 inch, changes to cockpit arrangement, added center section fuel tank, relocated oil tank forward in engine compartment, steel beam tail gear instead of shock strut, chemical hopper reshaped, relocated battery, and other minor changes. Engine Pratt & Whitney R985-AN1, AN-3, or AN-1-14B Fuel 80/87 Minimum Grade Aviation Gasoline Engine Limits HP RPM In. Hg. Press Engine Model AN-1 & AN-3 Alt. Takeoff (1 min.) at SL 450 2300 37.5 SL Max. Continuous at SL 290 2000 30.0 SL Max. Continuous 327 2000 30.0 6300 (Rated Press Alt.) HP RPM In. Hg. Press Engine Model AN-14B Alt. Takeoff (1 min.) at SL 450 2300 36.5 SL Max. Continous at SL 310 2000 30.0 SL Maximum Continuous 343 2000 30.0 6500 (Rated Press Alt.) Propeller and Hamilton Standard 2D-30 Hub, 6101A blades propeller limits Diameter: Not over 108 ins.; Not under 102 ins. Pitch Settings at 42" Station: (Constant Speed) - 10.5° Low 17° High Hamilton Standard 2D-30 Hub, with A6-100-4S Blades Diameter: Not over 104 ins.; Not under 102 ins. Pitch Settings at 42" Station: (Constant Speed) - 9.5° Low 17° High A10WE Page 5 of 6 Propeller and Hartzell HC-B3R30-4 Hub with R10152 - 5 1/2 R Blades propeller limits (cont'd) Diameter: Not over 95 1/2 ins., Not under 95 1/2 ins. Pitch Settings at 30" Station: (Constant Speed) 17° Low 25° High Static RPM at maximum throttle setting not over 2300 RPM, Not under 2200 RPM Hartzell HC-B3R30-4 Hub with R10160-6 Blades Diameter: Not over 95 ins., Not under 95 ins. Pitch Settings at 30" Station (Constant Speed) 17° Low 25° High Placard Required See NOTE 2 B. Static RPM at maximum throttle setting not over 2300 RPM; not under 2200 RPM Air Speed limits Vne - Never Exceed 145 mph (126 knots) EAS Vno - Max. Structural 128 mph (111 knots) EAS Vp - Maneuvering 115 mph (100 knots) EAS C.G. range Inches Aft of Datum (+20.8) to (+25.3) at all weights Empty weight C.G. range None Datum Wing Leading Edge outboard of fillet Max. weight 3500 Lbs. Leveling means Leveling lugs on outboard side of right hand fuselage, frame near Pilot's seat. No. seats 1 (+68) Hopper capacity 1000 Lbs. (+15.0) Fuel capacity 72.5 Gal. Total - 1 Right Wing Tank 27 1/2 Gal. with Unusable Fuel 2 1/2 Gal. (+36.0) - 1 Left wing tank (Combined with center tank) 45 Gal. with Unusable 5 Gal. (+36.0) Oil capacity 6.7 Gal. plus 1 Gal. in System (-22.2) Control surface movements Rudder Left 20° ± 1° Right 20° ± 1° Elevator Up 27° ± 1° Down 15° ± 1° Elevator tab Up 7° ± 1° Down 15° ± 1° Aileron Up 26° ± 1° Down 15° ± 1° Serial Nos. eligible 1001 thru 1500 Specifications Pertinent to All Models Certification basis FAR 21.25(a) Effective February 1, 1965 and CAM 8 Appendix B Airworthiness Requirements. Restricted Type Certificate issued January 30, 1967. Application for Type Certificate dated December 20, 1965. Production basis None. Prior to original certification of each model , an FAA representative must perform a detailed inspection for workmanship, materials and conformity with the approved technical data, and perform a check of the flight characteristics. Export eligibility Aircraft will be eligible for issuance of an Export Certificate of Airworthiness subject to compliance with Federal Aviation Regulation Part 21. Subpart L, Sections 21.321 thru 21.339. The applicable procedures are contained in Advisory Circular 21-2. A10WE Page 6 of 6 Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. (Addition required items of equipment are listed in the FAA Approved List No's A-10 for Model 201 and A-101A or A10B for Model 201A; A-10C-1 for Model 201C. NOTE 1. Current weight and balance report including list of equipment included in certificated weight empty, and loading instructions when necessary, must be provided for each aircraft at the time of original certification. The certificated empty weight and corresponding center of gravity must include for Model 201, undrainable system oil of 7.0 lbs. at (+86.0) and unusable fuel 4 gal. (+36.0). For Model 201A , undrainable system oil for 7.0 lbs. at (+86.0) and unusuable fuel 5 gal. (+36.0). For Model 201C undrainable system oil is 2.3 lbs. at (-22.2) and unusable fuel is 7.5 gals. at (+36.0). NOTE 2. (a) In addition to the operating limitations in this data sheet, area, economic, passenger and other appropriate operating limitations in accordance with FAR 21.25 shall be shown on placards or listing accessible to the pilot. (b) The following placards must be displayed in front of and in clear view of the pilot: (1) "This airplane must be operated as a restricted category airplane in compliance with the operating limitations stated in the form of placards, markings, and manuals." (2) "This airplane limited to day VFR operation only." NOTE: When cockpit and navigation lights are installed per Weatherly Aviation Co. Drawing 50261D, night VFR operation is approved and this placard is not required. (3) "Design maneuvering speed 115 mph, demonstrated crosswind velocity 5 mph." (4) "Restricted" displayed at entrance to cockpit. (5) When using Hartzell HC-B3R30 -4 Hub with R10160-6 Blades the following placard must be installed: "AVOID CONTINUOUS OPERATION BETWEEN 1600 and 1800 RPM". (c) Placard adjacent to Hopper compartment filler door: (1) "1000 lbs. Max." ...END...