TCDS E00008SE

Page No. 1 2 Rev. No. 0 0 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TC E00008SE Revision Original Merlyn Products IO-540-MX1 Original Issue Date: April 30, 2008 TYPE CERTIFICATE DATA SHEET E00008SE This data sheet, which is part of Type Certificate No. E00008SE, 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: Merlyn Products Inc. 7500 West Park Drive Spokane, WA 99224 I – Engine Model IO-540-MX1 Type: 6HOA Direct Drive Rating: Takeoff and Maximum 250 @ 2425 Continuous hp, rpm, Full throttle at Sea level pressure altitude Fuel (Minimum grade aviation Gasoline) 100/100LL Injection Lycoming Type FM250 Pump Drive See Note 3 Oil Lubrication Oil, SAE Number, Above 80 deg F 60 Above 60 deg F 50 30 deg F to 90 deg F 40 0 deg F to 70 deg F 20 Below 10 deg F 20 Oil Sump Capacity, Quarts 12 Ignition, dual Magneto drive 1.500:1 – clockwise viewed from propeller end Magnetos (2) Unison Slick Aircraft Products 6363 (Left) 6360 (Right) Optional Magnetos (2) TCM Bendix S6LN-1208 (Left) S6LN-1209 (Right) Timing (deg BTDC) 20 Spark Plugs Champion RHB37E Champion RHB32E Champion RHB-36S Champion RHB-32S E00008SE 2 Compression Bore and Stroke, in 5.125 x 4.375 Displacement, cu. in. 541.5 Compression Ratio 7.3:1 Weight (dry), lb 479 lb C.G. Location See Note 5 Propeller Shaft – Specification Type 2, Flange Modified A.S. 127 Crankshaft dampers (torsional) One fi fth order and one sixth order damper. Certification Basis: FAR 33, Effective June 10, 1964 including amendments through amendment 21 NOTE 1. Temperature Limits (Maximum permissible) Cylinder head (well type thermocouple) 500 deg F Oil Inlet 245 deg F Air inlet to injector 400 deg F Note 2. Pressure Limits Fuel 45 psi max, -2 psi min at inlet to fuel pump. Pressure at inlet to fuel injector Maximum 45 psi Minimum 18 psi Minimum Idle 12 psi Max Injector in 65 psi Idle cutoff Note 3. Accessory Drive Provisions: Maximum Torque (in-lb) Accessory Rotation Facing Drive Pad Speed Ratio to Crankshaft Continuous Static Maximum Overhung Moment (in-lb) Starter CC 16.556:1 N/A 450 150 Alternator C 3.250:1 60 120 175 Vacuum Pump CC 1.300:1 70 450 25 Hydraulic Pump C 1.385:1 100 800 40 Tachometer C 0.500:1 7 50 5 Prop Governor C 0.947:1 125 2200 25 Fuel Pump CC 1.000:1 25 450 25 “C” Clockwise, “CC” Counter-Clockwise (viewed from anti-propeller end) NOTE 4, Accessories and Equipment Starters, generators and alternators approved for use on this engine are listed in the latest revision to Merlyn Products Specification No. MX1 NOTE 5. The engine center of gravity is located 18.25 inches from the front face of the propeller mounting flange, and 0.88 inches below and 0.16 inches to the right of the propeller center line. NOTE 6. This engine incorporates provisions for absorbing propeller thrust in both tractor and pusher type installations. NOTE 7. Refer to Merlyn Products document MX1-01A, Section 1.4.3.6 for applicable inspection procedures for engines which have been operated above the specified maximum continuous RPM rating (except momentary overspeed as defined in this document). -END-.