TCDS E-310

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION E-310 Revision 12 (Small Engine Div) Gipsy Queen 70-4 70 MK2 70 MK3 March 22, 2007 TYPE CERTIFICATE DATA SHEET NO. E-310 Engines of models described herein conforming with this data sheet (which is a part of type certificate No. 310) and other approved data on file with the Federal Aviation Administration meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Civil Air Regulations provided they are installed, operated and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. Type Certificate Holder Rolls-Royce Ltd. (Small Engine Division) Leavesden, Hartfordshire, England Model Gipsy Queen 70-4 70 MK2 70 MK3 Type 6LIA Ratings Max. cont., hp., rpm, in.Hg. at: Rated pressure alt. (ft.) Sea level pressure alt. (ft.) Takeoff (5 min.), hp., rpm, in.Hg. at: 330-2600-40.0-5000 315-2600-40.0-S.L. 340-2800-42.0-S.L. 355-2700-42.0-4250 342-2700-42.0-S.L. 380-3000-45.0-S.L. 361-2800-42.0-5250 346-2800-42.0-S.L. 400-3000-47.0-S.L. Fuel (min. grade aviation gasoline) 100/130 - - - - Lubricating oil D.Eng. RD 2472 A/O, B/O; D.E.D. 2479/0; Canadian Government Specification Board 3-GP-55A. DeHavilland DNE 227 Aeroshell W.80, W.100 or W.120 - - - - Bore and stroke, in. 4.725 X 5.905 - - - - Displacement, cu. in. 621.0 - - - - Supercharging (drive gear ratio) 11.206:1 - - - - Compression ratio 6.5:1 - - - - Weight (dry), lb. 690 698 - - C.G. location (dry) Aft of front mounting trunnion, in. Below crankshaft C.L., in. 6.15 4.35 6.20 5.35 - - - - Propeller shaft SBAC No. 2 - - - - Carburetion Hobson injection type DH/G1 or DH/G4 when Mod. 1360 embodied or DH/G6 when Mod. 1773 embodied. Hobson injection type DH/G.7 or DH/G.8 when Mod. G.2025 embodied. Hobson injection type DH/G.8 Ignition, dual magnetos B.T.H. type C.G.D. or C.G.D/1 B.T.H. C.G.D., C.G.D/1 or C.G.D/C B.T.H. type C.G. D/C.1 Timing, °B.T.C. 30 - - 28° Spark plugs K.L.G. type K.A. 1, K.H.1, R.C. 5/4 or R.C. 9/2R or Lodge type L.H.1, R.S.9/1R orR.S.5/7R or Champion REL37B (see Note 5) or AC Type SR74P (see Note 6) - - K.L.G. type K.A.1 or Lodge type R.S. 9/1R or Champion REL37B (see Note 5) or AC Type SR74P (see Note 6) Lubrication Dry sump - - - - "- -" indicates "same as preceding model." Page No. 1 2 Rev. No. 12 12 E-310 2 Certification basis CAR 10. Type Certificate No. 310, issued September 21, 1959; reissued to Bristol Siddeley October 25, 1962. Date of Application for Type Certificate October 28, 1948. The aviation authority for the United Kingdom, the UK Civil Aviation Authority (CAA), originally type certificated this engine. The FAA validated this product under U.S. Type Certificate Number E-310. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of the UK. Import requirements To be considered eligible for installation on U.S. registered airc raft, each new engine to be exported to the United States with UK CAA or EASA airwor thiness approval shall have a Joint Aviation Authorities (JAA) or EASA Form 1, Authorized Re lease Certificate. The JAA or EASA Form 1 should state that the engine conforms to the type design approved under the U.S. Type Certificate E- 310, is in a condition for safe operation and has undergone a final operational check. NOTE 1. Maximum permissible cylinder head temperatures (measured with shoe type thermocouple, Weston 11A): 500°F with DED 2479/0 or Canadian Govern ment Specification Board 3-GP-55A oil 554° with D.Eng. R.D. 2472 A/O, B/O; deHavilland D.H.E. 227, Aeroshell W.80, W.100 or W.120 oil Maximum permissible oil inlet temperature: D.E.D. 2470/0 or C. G.S.B. 3-GP-55A 167°F D.Eng. R.D. 2472 A/O 195°F D.Eng. R.D. 2472 B/O 212°F DeHavilland DHE 227 220°F NOTE 2. Pressure limits - normal operation: Max. Min. Fuel pressure, psi 29 25 Oil pressure, psi 70-4 engine 60 40 70 MK2, 70 MK3 engines 55 40 NOTE 3. The following accessories are approved for use with the engine: Direction of Max. Torque (in.-lb.) Maximum Overhang Moment Accessory Rotation* Speed** Cont. Static (in.-lb.) Starter (and Feathering Pump), Rotax C4602 CC 1:1 — 5640 93 Generator, Rotax 750 Watt B2001, or Rotax 100 Watt B2003, or Newton 1200 Watt RX2 CC 2.096:1 60 500 65 Vacuum pump, Plessey B3X MK. II C 1.294:1 33 320 17 Air compressor, Hymatic Type 3H6/7C or hydraulic pump, Lockheed MK. V or MK. VI C 0.549:1 112 750 8 Tachometer flexible drive C 0.250:1 1:5 245 — Constant speed unit CC 0.902:1 57 1380 Mounted vertically *C - Clockwise; CC - Counter Clockwise, facing engine pad. **Speed - times crankshaft rpm NOTE 4. Deleted March 1, 1961. NOTE 5. To accommodate British thread size on ignition harness, special conversion elbow and grommet (Cooperative Industries, Inc. Part Nos. 54190 and 7269, respectively, with Champion sleeve Part No. AS681, or equivalents, are required to accomplish thread conversion for use of Champion type REL37B spark plugs. NOTE 6. To accommodate British thread size on igniti on harness, special conversion elbow and grommet (Cooperative Industries, Inc. Part Nos. 54190 and 7269, respectively, with AC Spark Plug sleeve Part No. AVT-CS or equivalents) are required to accomplish thread conversion for use of AC Type SR47P spark plugs. NOTE 7. Each of the documents listed be low must state that it is approved by the European Aviation Safety Agency (EASA) or, for approvals made before September 28, 2003 by the United Kingdom Civil Aviation Authority. Any such documents including those approved under a de legated authority, are accepted by the FAA and are considered FAA approved. • Service bulletins, • Structural repair manuals, • Vendor manuals, • Aircraft flight manuals, and • Overhaul and maintenance manuals. • Technical Variances These approvals pertain to the type design only. .....END.....