国内精品♨️_亲子乱aⅴ一区二区三区的_.手.动.输.入.网.址.联.系.客.服.人.员.lanan_shell
MODEL 510 SECTION IV - PERFORMANCE STANDARD CHARTS FAA APPROVED Configuration U.S. TAKEOFF / GO-AROUND THRUST SETTINGS ANTI-ICE OFF (TO DETENT) Figure 4-13 510FM-00 AA 4-27 SECTION IV - PERFORMANCE MODEL 510 STANDARD CHARTS FAA APPROVED U.S. Configuration TAKEOFF / GO-AROUND THRUST SETTINGS ANTI-ICE ON (TO DETENT) Figure 4-14 4-28 AA 510FM-00 MODEL 510 SECTION IV - PERFORMANCE STANDARD CHARTS FAA APPROVED Configuration U.S. MAXIMUM CONTINUOUS THRUST SETTING EXAMPLES EXAMPLE 1: (SINGLE-ENGINE CLIMB) Anti-Ice = OFF a. Indicated RAT = -15°C b. Pressure Altitude = 30,000 FEET c. N1 = 90.4% RPM (Refer to Figure 4-15) EXAMPLE 2: (SINGLE-ENGINE CLIMB) Anti-Ice = ON a. Indicated RAT = -40°C b. Pressure Altitude = SEA LEVEL c. N1 = 81.4% RPM (Refer to Figure 4-16) EXAMPLE 3: (MULTI-ENGINE) Anti-Ice = OFF a. Indicated RAT = -10°C b. Pressure Altitude = 30,000 FEET c. N1 = 88.8% RPM (Refer to Figure 4-17) EXAMPLE 4: (MULTI-ENGINE) Anti-Ice = ON a. Indicated RAT = -30°C b. Pressure Altitude = 10,000 FEET c. N1 = 90.4% RPM (Refer to Figure 4-18) 510FM-00 AA 4-29 SECTION IV - PERFORMANCE MODEL 510 STANDARD CHARTS FAA APPROVED U.S. Configuration MAXIMUM CONTINUOUS THRUST SETTINGS SINGLE-ENGINE (CLB DETENT) ANTI-ICE OFF Figure 4-15 4-30 AA 510FM-00 MODEL 510 SECTION IV - PERFORMANCE STANDARD CHARTS FAA APPROVED Configuration U.S. MAXIMUM CONTINUOUS THRUST SETTINGS SINGLE-ENGINE (CLB DETENT) ANTI-ICE ON Figure 4-16 510FM-00 AA 4-31 SECTION IV - PERFORMANCE MODEL 510 STANDARD CHARTS FAA APPROVED U.S. Configuration MAXIMUM CONTINUOUS THRUST SETTINGS MULTI-ENGINE (CLB DETENT) ANTI-ICE OFF Figure 4-17 4-32 AA 510FM-00 MODEL 510 SECTION IV - PERFORMANCE STANDARD CHARTS FAA APPROVED Configuration U.S. MAXIMUM CONTINUOUS THRUST SETTINGS MULTI-ENGINE (CLB DETENT) ANTI-ICE ON Figure 4-18 510FM-00 AA 4-33 SECTION IV - PERFORMANCE MODEL 510 STANDARD CHARTS FAA APPROVED U.S. Configuration BUFFET ONSET / AIRSPEED - KIAS Figure 4-19 LOW HIGH EXAMPLE: EXAMPLE: Indicated Mach = 0.25 Indicated Mach = 0.40 Pressure Altitude = 20,000 FEET Pressure Altitude = 30,000 FEET Weight = 8,000 POUNDS Weight = 8,000 POUNDS Buffet Onset Buffet Onset Load Factor = 1.35 G’S Load Factor = 2.07 G’S Bank Angle = GREATER THAN 42° Bank Angle = 61° 4-34 AA 510FM-00 MODEL 510 SECTION IV - PERFORMANCE STANDARD CHARTS FAA APPROVED Configuration U.S. CROSSWIND COMPONENT Figure 4-20 EXAMPLE: WIND VELOCITY = 30 KNOTS ANGLE BETWEEN WIND DIRECTION AND RUNWAY = 30° CROSSWIND COMPONENT = 15 KNOTS WIND COMPONENT PARALLEL TO RUNWAY = 26 KNOTS 510FM-00 AA 4-35/4-36
MODEL 510 SECTION IV - PERFORMANCE TAKEOFF FAA APPROVED Configuration U.S. TAKEOFF TABLE OF CONTENTS PAGE Takeoff Performance Simplified Criteria . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-39 Procedures for Use of Takeoff Performance Tables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-40 Maximum Takeoff Weight - Pounds Permitted by Climb Requirements, Flaps UP (Anti-Ice OFF) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-41 Maximum Takeoff Weight - Pounds Permitted by Climb Requirements, Flaps UP (Anti-Ice ON) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-42 Maximum Takeoff Weight - Pounds Permitted by Climb Requirements, Flaps 15° (Anti-Ice OFF) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-43 Maximum Takeoff Weight - Pounds Permitted by Climb Requirements, Flaps 15° (Anti-Ice ON). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-44 Takeoff Field Length - Feet, Flaps UP (Anti-Ice OFF). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-45 Takeoff Field Length - Feet, Flaps UP (Anti-Ice ON). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-61 Takeoff Field Length - Feet, Flaps 15° (Anti-Ice OFF) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-77 Takeoff Field Length - Feet, Flaps 15° (Anti-Ice ON) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-93 Single-Engine Takeoff Flight Path - Flaps UP (First and Second Segments) . . . . . . . . . . . . . . . 4-109 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：Citation Mustang airplane flight manual 2
