# TCDS A3EA: The Jamieson Corporation - Type: Type certificate data sheet - Status: Current - Holder: The Jamieson Corporation - Revision: 0 - Revised: August 15, 1963 - Product: Aircraft, Small Airplane - Certification basis: Part 3 - Data sheet PDF: https://openairdocs.org/files/sha256/53/05/5305d70909ffe9b488cc17f6026a3c5c27b8fab23d60aee1395eb1533ea05a1c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AF342B15754FDF6A852567380060EE43.0001 - Page: https://openairdocs.org/tcds/A3EA ## Models (1) As the data sheet lists them. - J-2-L1b ## 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 3 Rev. No. Reformatted 6/94. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A3EA JAMIESON J-2-L1b August 15, 1963 TYPE CERTIFICATE DATA SHEET NO. A3EA This data sheet which is a part of type certificate No. A3EA prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Civil Air Regulations. Type Certificate Holder The Jamieson Corporation P.O. Box 2482 Deland, Florida I. - Model J-2-L1b, 3 PCLM (Normal Category), Approved July 3, 1963 Engine Lycoming O-235-C1 (Carburetor setting 10-3103) Fuel 80/87 minimum grade aviation gasoline Engine Limits Takeoff ( 1 minute) 2800 rpm (115 hp) Maximum continuous 2600 rpm (108 hp) Propeller and Propeller Limits Sensenich two-position manually controlled, CS-2FM6-1 Hub with PC-276A6-2 Blades Maximum diameter74 inches Minimum diameter 72.5 inches Pitch settings at 27.75-inch station: Low 9.6°, High 16.2° Airspeed Limits MPH KNOTS CAS) Vne Never exceed 173 150 Vno Maximum structural cruising 154 134 Vp Maneuvering 110 96 Vfe Flaps extended 99 86 Vlo Landing gear operating 130 113 Vle Landing gear extended 130 113 C. G. Range (landing gear extended) 1 1 0 0 1 4 1 0 1 6 0 0 2 0 2 1 . 9 2 5 . 7 2 7 . 0 FW D. LIM IT A FT . LIM IT CG--Inc hes A f t of Dat um Moment due to retraction of landing gear +710 in.-lb. (CG moves aft) Empty Weight C.G. Range None A3EA Page 2 Datum Front face of firewall Leveling Means Underside of fuselage, edge of nose-wheel well Maximum Weight 1600 lb. Number of Seats 3 (2 at +24, 1 at +54) Maximum Baggage Glove compartment 20 lb. (+6) Rear compartment 120 lb. (+63) Fuel Capacity 22 gallons (two 10.5-gallon wing tanks at +24 and a 1 gallon header tank at +24) (Usable 21.3 gallons) See NOTE 1 for data on unusable fuel. Oil Capacity 1.5 gallons (-19) Control Surface Wing flaps Down 12° Movements Aileron Up 19° Down 15° Elevator Tab Up 10° Down 30° Elevator Up 19° Down 8° Rudder Left 15° Right 17° Serial Numbers Eligible 2 and up Certification Basis CAR 3 as amended to May 15, 1956 and Amendments 3-1 through 3-5. Type Certificate No. A3EA issued July 3, 1963. Date of Application for Type Certificate October 15, 1960. Production Basis None. Prior to original certification of each aircraft, an FAA representative must perform a detailed inspection for workmanship, materials, and conformity with the approved technical data, and a check of flight characteristics. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. 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. The certificated empty weight and corresponding center-of-gravity location must include unusable fuel of 4 lb. at (+24) with standard wing tanks. NOTE 2. The following placards must be displayed in front of and in clear view of the pilot or at appropriate locations: A. "THIS AIRPLANE IS CERTIFICATED ONLY FOR DAY-VFR OPERATION. NO ACROBATIC MANEUVERS, INCLUDING SPINS, APPROVED. THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS AND MARKINGS." B. "LIMITING AIRSPEEDS (CAS) NEVER EXCEED 173 M.P.H. MAXIMUM STRUCTURAL CRUISING 154 M.P.H. MANEUVERING 110 M.P.H. FLAPS EXTENDED 99 M.P.H. LANDING GEAR EXTENDED 130 M.P.H. C. LOADING SCHEDULE A3EA Page 3 STANDARD 170 LB OCCUPANTS MAXIMUM BAGGAGE FUEL FRONT REAR GLOVE UNDER REAR AFT (GAL.) SEATS SEATS COMPT SEAT COMPARTMENT 22 1 --- 20 ←————120————→ 22 2 --- 20 ←————120————→ 22 2 Values to be entered to be determined from actual weight and balance of each airplane. D. At propeller control: "PROPELLER: PUSH TO INCREASE R.P.M." E. On fuel tank caps: "FUEL 880/87 OCTANE, 10.7 GAL." F. At fuel gage selector switch: FU EL GA GE SW IT CH LEFT T A N K RIGH T T A N K PU SH FOR LEFT T A N K. FU EL LEV EL IS A V ERA GE OF LEFT & RIGH T REA D IN GS. G. At emergency fuel pump: "EMERGENCY FUEL PUMP: PULL & RELEASE RAPIDLY" H. On flap handle: "FLAPS, PULL TO EXTEND" I. On flap control quadrant cover: "FLAP POSITION: LANDING, 1ST NOTCH 12°" J. Near handle for emergency landing gear extension: "EMERGENCY LANDING GEAR EXTENSION: MOVE DOWN & UP ABOUT 150 TIMES" K On baggage compartment: "COMPARTMENT CAPACITY 120 POUNDS" L. On glove compartment: "COMPARTMENT 20 LBS." ....END.... ``` ## ADs None name its models. ## Registered aircraft by registry model (OpenAirDocs) - [Jamieson J-2-L1B](https://openairdocs.org/model/jamieson-j-2-l1b): 0 aircraft (registry code 4651004) ## STCs approved under this data sheet (7) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc - [STC SA2683NM](https://openairdocs.org/stc/SA2683NM): Installation of Precise Flight, Inc. stand-by vacuum system (SVS). Precise Flight Inc - [STC SA489EA](https://openairdocs.org/stc/SA489EA): Installation of ARP Inc. carburetor ice detection system. Aircraft & Rotorcraft Products (ARP) Inc - [STC SA5159NM](https://openairdocs.org/stc/SA5159NM): Installation of chip detector system.. Northwest Aircraft Inc --- 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.