# TCDS 4A14: Morrisey Aviation Inc. - Type: Type certificate data sheet - Status: Current - Holder: Morrisey Aviation Inc. - Revision: 0 - Revised: February 28, 1956 - Product: Aircraft, Small Airplane - Certification basis: CAR 3 - Registered aircraft: 2, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/8c/20/8c200556fe261826f34787b63407201df492d488a5fb0d8ce71076c91d405406 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2E1A6F517EB8EFF58525673C0062A470.0001 - Page: https://openairdocs.org/tcds/4A14 ## Models (1) As the data sheet lists them. - 2000C ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 Rev. No. - - Reformatted 1/95. DEPARTMENT OF COMMERCE CIVIL AERONAUTICS ADMINISTRATION 4A14 MORRISEY 2000C February 28, 1956 AIRCRAFT SPECIFICATION NO. 4A14 Manufacturer Morrisey Aviation, Inc. Orange County Airport Santa Ana, California I - Model 2000C, 2 PCLM (Normal Category), Approved December 8, 1955 Engine Continental C90-14F equipped with Marvel-Schebler carburetor MA-3SPA Fuel 80/87 min. grade aviation gasoline Engine limits Takeoff (one minute), 2625 rpm ( 95 hp) For all other operations 2475 rpm ( 90 hp) Airspeed limits Maneuvering 108 mph ( 94 knots) True Ind. Design Cruising 124 mph (108 knots) True Ind. Never Exceed 154 mph (134 knots) True Ind. Flap Speed 78 mph ( 68 knots) True Ind. C.G. range (+11.2) to (+18.2) Empty weight C.G. range None Maximum weight 1450 lbs. No. seats 2 (One at +15.5 and one at +45.5) Maximum baggage None Fuel capacity 14.7 gals. total, 12.7 gals. usable (-13.5). See NOTE 2(a)(3) for placard and NOTE 1 for weight and arm of unusable fuel. Oil capacity 5 quarts Control surface movements Elevator 19° Up 9° Down Aileron 12° Up 12° Down Rudder 30° Right 30° Left Flap 30° Down Serial Nos. eligible 1A only Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: Items 1, 101, 102, 201(a), 202(a), 205(a), 206(a), and 401. Specifications Pertinent to All Models Datum Wing leading edge Leveling means Top longitudinal longeron member in cockpit Certification basis Type Certificate No. 4A14 (CAR 3) Production basis Type Certificate only. Export eligibility Eligible for export to all countries subject to the provisions of MOP 2-4 except as follows: (a) Canada landplane, skiplane not eligible Equipment: A plus (+) or minus (-) sign preceding the weight of an item indicates net weight change when that item is installed. Approval for the installation of all items of equipment listed herein has been obtained by the aircraft manufacturer except those items preceded by an asterisk (*). The asterisk denotes that approval has been obtained by other than the aircraft manufacturer. An item marked with an asterisk may not have been manufactured under a CAA monitored or approved quality control system, and therefore attention should be paid to workmanship and conformity with pertinent data called for in this specification. 4A14 2 Propellers and Propeller Accessories The following propellers are eligible at the limits shown for diameter and static rpm at maximum permissible throttle setting, no additional tolerance permitted. 1. Propeller-McCauley "Met-L-Prop" 1A90-CF, fixed pitch metal Static r.p.m.: Not over 2250, not under 2150 Diameter: Not over 71 in., not under 69.5 in. 21 lbs. (-50.5) Engine and Engine Accessories - Fuel and Oil System 101. 2 Heaters and mufflers, "Ryan" 102. Starter, Delco Remy 12v Model 12F 16 lbs. (-26.5) Landing gear 201. Two main wheel-brake assemblies, 6.00-6 14 lbs. (-27) (a) Firestone Model DFA-207-1 Wheel assembly DFA-180-1 Brake assembly CFA252 202. (a) 2 main wheel 4 ply rating tires, 6.00-6 with regular tubes 18 lbs. (-27) 205. One nose wheel, 5.00-5 3 lbs. (-30) (a) Firestone, Model DFA531-1 206. (a) One nose wheel, 4 ply rating tire 5.00-5, with regular tubes 7 lbs. (-30) Electrical equipment 301. Generator, Delco Remy, 20a, 12v, Model 12F10 lbs. (-26.5) 302. Voltage regulator, Delco Remy Model 9041 lbs. (-22) 303. Battery, Willard Model SYW-7-6, 12v15 lbs. (-23) Interior Equipment 401. (a) CAA Approved Airplane Flight Manual dated December 8, 1955 NOTE 1. Current weight and balance report including list of equipment included in certificated empty weight and loading instructions when necessary, must be in each aircraft at the time of original certification and at all times thereafter (except in the case of air carrier operators having an approved weight control system). The certificated weight empty and corresponding center of gravity location must include unusable fuel of 12 lbs. at (-13.5). NOTE 2. The following placards must be displayed: (a) On the instrument panel in full view of the pilot: (1) "Operate in Normal Category in compliance with approved Flight Manual. Acrobatics (including spins) prohibited." (2) "Solo from the front seat only." (3) "Of the 14.7 gals fuel cap., 2 gals. are unusable and unmeasurable." ....END.... ``` ## ADs None name its models. ## Registered aircraft by registry model (OpenAirDocs) - [Morrisey 2000C](https://openairdocs.org/model/morrisey-2000c): 1 aircraft (registry code 5940102) - [Rearwin 2000-C](https://openairdocs.org/model/rearwin-2000-c): 1 aircraft (registry code 2370705) ## STCs approved under this data sheet (10) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA10077SC](https://openairdocs.org/stc/SA10077SC): Installation of push-button starter system.. Hartzell Engine Technologies, LLC - [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC - [STC SA01944CH](https://openairdocs.org/stc/SA01944CH): Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index, per ASTM Specification D-439 or D-4818 of any volatility class, A through E, or 82UL AVGAS per ASTM D-6227.. Experimental Aircraft Association Inc. - [STC SA869GL](https://openairdocs.org/stc/SA869GL): Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 mimimum antiknock index.. EAA Aviation Foundation - [STC SA3333NM](https://openairdocs.org/stc/SA3333NM): The Model 704 VHF Communication Radio, P/N 430-0050-0 ( )-0( ), is installed on the Morrisey Model 2150A airplane, in accordance with II Morrow, Inc. Installation Report No. 55, dated December 30, 1985.. Garmin AT Inc. - [STC SA489EA](https://openairdocs.org/stc/SA489EA): Installation of ARP Inc. carburetor ice detection system. Aircraft & Rotorcraft Products (ARP) Inc - [STC SA798EA](https://openairdocs.org/stc/SA798EA): Installation of Monitair exhaust gas combustion monitor kit.. Rosemount Engineering Co --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.