Airplane Flight Manual Supplement

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MT-Propeller Entwicklung GmbH AFMS Doc. No. E-1487 Flugplatzstr.1 DA 20-C1 94348 Atting MT 175 R 150 - 2Ca GERMANY Propeller Installation Airplane Flight Manual Supplement Log of revisions Rev. No. Description Pages Revised Approved by / Date Original Issue - 01 March 2007 Page 2 of 7 MT-Propeller Entwicklung GmbH AFMS Doc. No. E-1487 Flugplatzstr.1 DA 20-C1 Katana 94348 Atting MT 175 R 150 - 2Ca GERMANY Propeller Installation SECTION 1 - GENERAL The information contained in this document, together with the basic Airplane Flight Manual or later approved versions is applicable and must be carried in the airplane. For further information concerning the MT 175 R 150 - 2Ca propeller refer to Section 2 and Section 7. SECTION 2 - LIMITATIONS Engine Limits: No change. Propeller: MT 175 R 150 - 2Ca Note: Static rpm at full throttle, ISA, SL, no wind (carburator heat off and mixture leaned to max. rpm) : 2000 to 2200 rpm Diameter: 175 cm (68.9 in) No cut-off approved. Propeller Pitch: At station 65.6 cm (25.8 in): 150 cm (59.1 in) Tachometer: No change. Placards: Markings and signs concerning other propellers are obsolete. SECTION 3 - EMERGENCY PROCEDURES No change. SECTION 4 - NORMAL PROCEDURES No change. Original Issue - 01 March 2007 Page 3 of 7 MT-Propeller Entwicklung GmbH AFMS Doc. No. E-1487 Flugplatzstr.1 DA 20-C1 94348 Atting MT 175 R 150 - 2Ca GERMANY Propeller Installation SECTION 5 - PERFORMANCE Noise Data: Noise Measurement Method Noise Value Maximum Allowable ICAO Annex 16, Vol. 1, Part 2, Chapter 10 68.0 dBA 75.3 dBA No change to the basic airplane except Cruise Performance. Note: Performance Data is not TCCA Approved. Figure 1: Density Altitude Chart: Example: Pressure Altitude: 6000 ft Outside Air Temperature: 15 °C Density Altitude: 7391 ft Original Issue - 01 March 2007 Page 4 of 7 MT-Propeller Entwicklung GmbH AFMS Doc. No. E-1487 Flugplatzstr.1 DA 20-C1 94348 Atting MT 175 R 150 - 2Ca GERMANY Propeller Installation SECTION 5 - PERFORMANCE Maximum propeller speed: 2800 RPM Note: Performance Data is not TCCA Approved. Figure 2: Power Chart Example: Density Altitude: 6000 ft Desired BHP: 65% Engine RPM: 2440 RPM Original Issue - 01 March 2007 Page 5 of 7 MT-Propeller Entwicklung GmbH AFMS Doc. No. E-1487 Flugplatzstr.1 DA 20-C1 94348 Atting MT 175 R 150 - 2Ca GERMANY Propeller Installation SECTION 5 - PERFORMANCE Figure 3: Speed Power – Cruise Performance Note: Performance Data is not TCCA Approved. Example: Density Altitude: 6000 ft Desired BHP: 65% True Airspeed: 122 knots Note: The cruise performance while not a certification requirement, are based on actual flight tests. The actual performance attained will vary from airplane to airplane depending on age and condition of the airframe and powerplants, aircraft rigging and operator technique. Original Issue - 01 March 2007 Page 6 of 7 MT-Propeller Entwicklung GmbH AFMS Doc. No. E-1487 Flugplatzstr.1 DA 20-C1 94348 Atting MT 175 R 150 - 2Ca GERMANY Propeller Installation SECTION 5 - PERFORMANCE Figure 4: Cruise Performance Table to calculate maximum endurance and range depending on the available fuel. Note: Performance Data is not TCCA Approved. SECTION 6 - WEIGHT AND BALANCE AND EQUIPMENT LIST Refer to the latest revised empty weight and center of gravity data for effect on loading instructions. SECTION 7 - DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS Propeller: The MT 175 R 150 - 2Ca is a 2-blade wood composite fixed pitch propeller. Note: The airplane may be operated without a spinner but in this case the front plate must cover the central bore of the propeller completely. Original Issue - 01 March 2007 Page 7 of 7