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Posted on Sep 10, 2024

use this chart. thank you 41. Using the Turbo Lance information in figure 2-27. determine the take-off distance required for a zero-flap take-off under the

use this chart. thank you image text in transcribed

41. Using the Turbo Lance information in figure 2-27. determine the take-off distance required for a zero-flap take-off under the following conditions. Aerodrome elevation 1.000 Ft Tornperature - 18 ONH 1013 hPa Surface short, dry grass Slope 3% down Wind component 15 kt head Planned take off weight 1,500 kg 42. Using the take off chart in figure 2-28. determine the maximum permissible take- off weight for the following conditions. Aerodrome elevation 2.430 Temperature ONH 995 hPa Propeller 60 TODA 300 m Surface short, wet grass Stop 1% down Wind component 5 kt head 42. Using the take-off chart in figure 2-28, determine the take off distance required for the following conditions. Aerodrome elevation 2.210 ft Temperature .30- 1020 hPa Propeller 50 Surface short, dry Grass Siope Wind component 5 kt head Planned take-off weight 1.040 kg 4. Using the information for the Turbo Lance in figure 2-29, determine the maximum permissible take-off weight with a 25 flap setting for the following conditions. Aerodrome elevation 500 Ft Temperature +05 ONH 1013 hPa TODA Surface level 5 kt head 13 Up 10 m long. wet grass Slope Wind component achieve a .....% climb gradient in 40. Using the Turbo Lance information in figure 2-27. determine the per- missible take-off weight with a zero flap setting for the following conditions. Aerodrome elevation 2.000 ft Temperature +30 ONH 1013 hPa TODA 1.230 m Surface short, dry grass Slope 1% Up Wind component 10 kt head 41. Using the Turbo Lance information in figure 2-27, determine the take-off distance required for a zero-flap take-off under the following conditions. Aerodrome elevation 1.000 ft Temperature +18 1013 hPa Surface short, dry grass Slope 3% down Wind component 15 kt head Planned take off weight 1.500 kg 42. Using the take-off chart in figure 2-28. determine the maximum permissible take- off weight for the following conditions. Aerodrome elevation 2.430 ft Temperature +35 995 hPa Propeller 60" TODA 800 m Surface short, wet grass Slop 1% down Wind component 5 kt head 43. Using the take-off chart in figure 2-28. determine the take-off distance required for the following conditions. Aerodrome elevation 2.210 ft Temperature +30 ONH 1020 hPa Propeller 58" Surface short, dry grass Slope 1% up Wind component 5 kt head Planned take-off weight 44. Using the information for the Turbo Lance in figure 2-29. determine the maximum 1.040 kg permissible take-off weight with a 25 flap setting for the following conditions. Aerodrome elevation 500 ft Temperature +05 ONH 1013 hPa TODA Surface level 910 m long. wet grass Slope Wind component 5 kt head FUEL, TIME, AND DISTANCE TO CLIMB 20,000 Disi, un vis 10,000 16,000 14,000 17.000 GEAR UP FLAPS UP 3600 LBS MAXIMUM CONTINUOUS POWER 95 KUS, ZERO WINO 10.000 Zigg. Antallet 40 30 -20 -10 10 20 0 10 20 30 40 50 60 OUTSIDE AR TEP. C FUEL TIME AND DISTANCE TO CUMB BEST POWER CRUISE PERFORMANCE BEST ECONOMY APPROX % POWER BEAR UP. FLAPS UP, 1633 kg GROSS WEST APPROX. POWER FUEL FLOW FUEL FLOW COM FUPS CLOSED!!! 24 GPH 17-4 GPH BEST POWER MOTURE LENED TO 150F RICH OF 75 21-9 GPX 65 PEAK E.G.T. (1650F MAX. ALLOWABLE !!! 15-7 GPH 19-3GPH BEST ECONOMY MIXTURE LEARNED TO SO'F RICH OF 35 13-8 GPH 16.8 GPM PEAK E.G.T. 11650F MAX. ALLOWABLE] BEST POWER BEST ECONOMY 75 81 65 55 75 81% PM 14.000 12.000 Press AR FI ,000 4,000 NOTE SEE LEARING KSTRUCTIONS SECTION 2 72.000 Sea Leal -10 0 10 20 30 40 120 180 30 20 20 140 160 THE USE YOTE 41. Using the Turbo Lance information in figure 2-27. determine the take-off distance required for a zero-flap take-off under the following conditions. Aerodrome elevation 1.000 Ft Tornperature - 18 ONH 1013 hPa Surface short, dry grass Slope 3% down Wind component 15 kt head Planned take off weight 1,500 kg 42. Using the take off chart in figure 2-28. determine the maximum permissible take- off weight for the following conditions. Aerodrome elevation 2.430 Temperature ONH 995 hPa Propeller 60 TODA 300 m Surface short, wet grass Stop 1% down Wind component 5 kt head 42. Using the take-off chart in figure 2-28, determine the take off distance required for the following conditions. Aerodrome elevation 2.210 ft Temperature .30- 1020 hPa Propeller 50 Surface short, dry Grass Siope Wind component 5 kt head Planned take-off weight 1.040 kg 4. Using the information for the Turbo Lance in figure 2-29, determine the maximum permissible take-off weight with a 25 flap setting for the following conditions. Aerodrome elevation 500 Ft Temperature +05 ONH 1013 hPa TODA Surface level 5 kt head 13 Up 10 m long. wet grass Slope Wind component achieve a .....% climb gradient in 40. Using the Turbo Lance information in figure 2-27. determine the per- missible take-off weight with a zero flap setting for the following conditions. Aerodrome elevation 2.000 ft Temperature +30 ONH 1013 hPa TODA 1.230 m Surface short, dry grass Slope 1% Up Wind component 10 kt head 41. Using the Turbo Lance information in figure 2-27, determine the take-off distance required for a zero-flap take-off under the following conditions. Aerodrome elevation 1.000 ft Temperature +18 1013 hPa Surface short, dry grass Slope 3% down Wind component 15 kt head Planned take off weight 1.500 kg 42. Using the take-off chart in figure 2-28. determine the maximum permissible take- off weight for the following conditions. Aerodrome elevation 2.430 ft Temperature +35 995 hPa Propeller 60" TODA 800 m Surface short, wet grass Slop 1% down Wind component 5 kt head 43. Using the take-off chart in figure 2-28. determine the take-off distance required for the following conditions. Aerodrome elevation 2.210 ft Temperature +30 ONH 1020 hPa Propeller 58" Surface short, dry grass Slope 1% up Wind component 5 kt head Planned take-off weight 44. Using the information for the Turbo Lance in figure 2-29. determine the maximum 1.040 kg permissible take-off weight with a 25 flap setting for the following conditions. Aerodrome elevation 500 ft Temperature +05 ONH 1013 hPa TODA Surface level 910 m long. wet grass Slope Wind component 5 kt head FUEL, TIME, AND DISTANCE TO CLIMB 20,000 Disi, un vis 10,000 16,000 14,000 17.000 GEAR UP FLAPS UP 3600 LBS MAXIMUM CONTINUOUS POWER 95 KUS, ZERO WINO 10.000 Zigg. Antallet 40 30 -20 -10 10 20 0 10 20 30 40 50 60 OUTSIDE AR TEP. C FUEL TIME AND DISTANCE TO CUMB BEST POWER CRUISE PERFORMANCE BEST ECONOMY APPROX % POWER BEAR UP. FLAPS UP, 1633 kg GROSS WEST APPROX. POWER FUEL FLOW FUEL FLOW COM FUPS CLOSED!!! 24 GPH 17-4 GPH BEST POWER MOTURE LENED TO 150F RICH OF 75 21-9 GPX 65 PEAK E.G.T. (1650F MAX. ALLOWABLE !!! 15-7 GPH 19-3GPH BEST ECONOMY MIXTURE LEARNED TO SO'F RICH OF 35 13-8 GPH 16.8 GPM PEAK E.G.T. 11650F MAX. ALLOWABLE] BEST POWER BEST ECONOMY 75 81 65 55 75 81% PM 14.000 12.000 Press AR FI ,000 4,000 NOTE SEE LEARING KSTRUCTIONS SECTION 2 72.000 Sea Leal -10 0 10 20 30 40 120 180 30 20 20 140 160 THE USE YOTE