P/N 135A FAA Approved: 5/14/2007 Section 9 Initial Release Page 1 of 10

Transcription

1 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR MT PROPELLER INSTALLATION Serial No: Registration No: When the MT Propeller is installed on the Liberty Aerospace XL2, this supplement is applicable and must be inserted in the Supplements Section (Section 9) of the Liberty Aerospace XL2 Airplane Flight Manual. The information contained herein supplements the FAA approved Airplane Flight Manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this document, consult the basic XL2 FAA Approved Airplane Flight Manual. FAA Approved: Date: Melvin D Taylor, Manager Atlanta Aircraft Certification Office Federal Aviation Administration P/N 135A FAA Approved: 5/14/2007 Section 9 Initial Release Page 1 of 10

2 MT Propeller Log of Revisions Rev. To Pages Description FAA Approval Signature and Date A Pages 2, 4, 8, 9, 10 Section 5 added Dawley Exhaust and Formatting Melvin D Taylor, Manager Atlanta Aircraft Certification Office Federal Aviation Administration Atlanta, GA Date: B Page 2, 8 Section 5 added information to the second paragraph For: Melvin D Taylor, Manager Atlanta Aircraft Certification Office Federal Aviation Administration Atlanta, GA Date: C Page 2, 8 Part 36 Amendment citations updated and level corrected For: Melvin D Taylor, Manager Atlanta Aircraft Certification Office Federal Aviation Administration Atlanta, GA Date: D Page 2, 8, 9 Added Table 1 to indicate the different noise levels for the different configurations For: Melvin D Taylor, Manager Atlanta Aircraft Certification Office Federal Aviation Administration Atlanta, GA Date: Section 9 FAA Approved: 5/14/2007 P/N 135A Page 2 of 10 Revision D: 10/28/2009

3 SECTION 1 - GENERAL No change SECTION 2 - LIMITATIONS No change SECTION 3 EMERGENCY PROCEDURES No change SECTION 4 NORMAL PROCEDURES No change P/N 135A FAA Approved: 5/14/2007 Section 9 Initial Release Page 3 of 10

4 SECTION 5 - PERFORMANCE Title, chart changes, and additional noise characteristics data. TAKEOFF RATE OF CLIMB Conditions: Weight LBS Flaps...20 Power...Full Throttle (WOT annunciator ON) Indicated Airspeed...65 KIAS (V y ) For operation in air colder than this table provides, use coldest data shown. For operation in air warmer than this table provides, use extreme caution. Rate of climb data of less than 100 ft/min are not published. Data was derived from actual flight testing and does not include data for any altitude where the temperature is below ISA -20 or above ISA +30. Maximum Climb Gradient FT/NM Press Temperature C Alt FT ISA SL Section 9 FAA Approved: 5/14/2007 P/N 135A Page 4 of 10 Revision A: 4/18/2008

5 TAKEOFF CLIMB GRADIENT Conditions: Weight LBS Flaps...20 Power... Full Throttle (WOT annunciator ON) Indicated Airspeed KIAS (V y ) For operation in air colder than this table provides, use coldest data shown. For operation in air warmer than this table provides, use extreme caution. Climb gradient data of less than 100 ft/nm are not published. Data was derived from actual flight testing and does not include data for any altitude where the temperature is below ISA -20 or above ISA +30. Maximum Climb Gradient % Press Temperature C Alt FT ISA SL P/N 135A FAA Approved: 5/14/2007 Section 9 Initial Release Page 5 of 10

6 BALKED LANDING RATE OF CLIMB Conditions: Weight LBS Flaps...30 Power...Full Throttle (WOT annunciator ON) Indicated Airspeed...65 KIAS For operation in air colder than this table provides, use coldest data shown. For operation in air warmer than this table provides, use extreme caution. Rate of climb data of less than 100 ft/min are not published. Data was derived from actual flight testing and does not include data for any altitude where the temperature is below ISA -20 or above ISA +30 Maximum Climb Gradient FT/NM Press Temperature C Alt FT ISA SL Section 9 FAA Approved: 5/14/2007 P/N 135A Page 6 of 10 Initial Release

7 BALKED LANDING CLIMB GRADIENT Conditions: Weight LBS Flaps...30 Power... Full Throttle (WOT annunciator ON) Indicated Airspeed KIAS For operation in air colder than this table provides, use coldest data shown. For operation in air warmer than this table provides, use extreme caution. Climb gradient data of less than 100 ft/nm are not published. Data was derived from actual flight testing and does not include data for any altitude where the temperature is below ISA -20 or above ISA +30 Maximum Climb Gradient % Press Temperature C Alt FT ISA SL P/N 135A FAA Approved: 5/14/2007 Section 9 Initial Release Page 7 of 10

8 NOISE CHARACTERISTICS The table below shows the certificated noise level for various configurations of the Liberty XL-2 airplane. Propeller Dawley Exhaust Type and Part Number Gross Weight (lbs) FAR 36 Appendix G Amendment Noise Level (db) A Weighted MT MT Standard DEL Quiet DEL Table 1 Noise Figures The baffle P/N DEL inside the muffler tailpipe and the two oblong openings in the pipe can identify the reduced sound Dawley Exhaust, P/N DEL If there is no baffle and no oblong openings in pipe, then the exhaust system is the Dawley Exhaust, P/N DEL Figure 5-1 No determination has been made by the Federal Aviation Administration that the noise levels of this airplane are or should be acceptable or unacceptable for operation at, into, or out of, any airport. Section 9 FAA Approved: 5/14/2007 P/N 135A Page 8 of 10 Revision D: 10/28/2009

9 SECTION 6 WEIGHT AND BALANCE See current weight and balance. SECTION 7 AIRPLANE AND SYSTEM DESCRIPTION The MT Propeller Installation consists of a two-blade, fixed pitch, wood composite propeller. The Spinner Assembly includes spacer and supporting hardware (P-1026). The model is MT175R127-2Ca and manufactured by MT-Propeller Entwicklung GmbH. SECTION 8 HANDLING, SERVICE, AND MAINTENANCE No change P/N 135A FAA Approved: 5/14/2007 Section 9 Revision D: 10/28/2009 Page 9 of 10

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