Takeoff... Landing...

Transcription

1 CESSNA NORMAL SECTION 4. PROCEDURES INTRODUCTION Section 4 provides checklist and amplified procedures for the conduct of normal operation. Normal procedures associated ith Optional Systems can be found in Section 9. SPEEDS FOR NORMAL OPERATION Unless otherise noted, the folloing speeds are based on a maximum eight of 2950 pounds and may be used for any lesser eight. Hoever, to achieve the performance specified in Section 5 for takeoff distance, the! speed appropriate to the particular eight must be used. Takeoff: Normal Climb Out Maximum Performance Takeoff, Speed at 50 Feet... Enroute Climb, Flaps Up: Normal, SeaLevel Normal, 10,000Feet Best Rateof Climb, SeaLevel Best Rateof Climb, 10,000Feet BestAngleof Climb, SeaLevel BestAngleof Climb, 10,000Feet Landing Approach: Normal Approach, Flaps Up,. Normal Approach, Flaps Short Field Approach, Flaps Balked Landing: During Transition to Maximum Poer, Flaps Maximum Recommended Turbulent Air Penetration Speed: 2950 Lbs Lbs Lbs Maximum Demonstrated Crossind Velocity: Takeoff Landing KIAS 57 KIAS 95 KIAS 85 KIAS 80 KIAS 73 KIAS 59 KIAS 63 KIAS KIAS KIAS 60 KIAS 70 KIAS 110 KIAS 100 KIAS 89 KIAS 20 KNOTS 15 KNOTS 4-3

2 " SECTION 5 CESSNA AIRSPEED CALIBRATION NORMAL STATIC SOURCE FLAPS UP KIAS KCAS FLAPS 20. KIAS KCAS FLAPS 40 KIAS KCAS " Figure 5-1. Airspeed Calibration (Sheet 1 of 2) \ 5-8

3 CESSNA SECTION 5 AIRSPEED CALIBRATION ALTERNATE STATIC SOURCE FLAPS UP HEATERVENTS AND WINDOWSCLOSED NORMAL KIAS ALTERNATE KIAS FLAPS 20 NORMAL KIAS ALTERNATE KIAS FLAPS 40. NORMAL KIAS ALTERNATE KIAS FLAPS UP HEATERVENTS OPENAND WINDOWSCLOSED NORMAL KIAS ALTERNATE KIAS FLAPS 20 NORMAL KIAS ALTERNATE KIAS FLAPS 40 NORMAL KIAS ALTERNATE KIAS FLAPS UP WINDOWS OPEN NORMAL KIAS ALTERNATE KIAS FLAPS 20 NORMAL KIAS ALTERNATE KIAS FLAPS 40 NORMAL KIAS ALTERNATEKIAS Figure 5-1. Airspeed Calibration (Sheet 2 of 2) 5-9

4 SECTION 5 CESSNA TEMPERATURE CONVERSION CHART 120 \ t: I Z a:: I ;;: 40 (f) a:: <.:J DEGREES - CELSIUS Figure 5-2. Temperature Conversion Chart 5-10

5 CESSNA SECTION 5 51 ALL SPEEDS Poer Off NOTES: 1. Maximumaltitude loss during a stall recovery is approximately 160 feet. 2. KIAS values are approximate. MOST REARW ARD CENTER OF GRAVITY ANGLE OF BANK WEIGHT LBS FLAP DEFLECTION KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS UP MOST FOR WARD CENTER OF GRAVITY WEIGHT LBS FLAP DEFLECTION ANGLE OF BANK KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS UP Figure 5-3. Stall Speeds 5-11

6 <:J1 I... ~ Flaps RPMand Full Throttle Prior to Brake Release Col Flaps Open Paved, Level, Dry Runay Zero Wind TAKEOFF DISTANCE MAXIMUM WEIGHT 2950 LBS NOTES: 1. Maximum performance technique as specified in Section Prior to takeoff from fields above 5000 feet elevation, the mixture should be leaned to give maximum poer in a full throttle, static runup. 3. Decreasedistances10for each9 knots headind, For operation ith tailinds up to 10 knots, increase distances by 10 for each 2 knots. 4. Where distance value has been deleted, climb performance after lift-off is lessthan 150 fpm at takeoff speed. 5. For operation on a dry, grass runay, increase distances by 15 of the "ground roll" figure. ~C) I::!jl::!j ::tjo ~j ::tj@ ~<:J1 ~I::!j " TAKEOFF OOC 1QoC 20 C 30 C 40 C SPEED PRESS WEIGHT KIAS ALT TOTAL LBS TOTAL TOTAL TOTAL TOTAL FT LIFT AT GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR OFF 50FT ROLL 50 FT OBS ROLL 50 FT OBS ROLL 50 FT OBS ROLL 50 FT OBS ROLL 50 FT OBS S.L Q Figure 5-4. Takeoff Distance (Sheet 1 of 2) ~ t:1 I::!jO t"'1::!j C) coc) ~~

7 TAKEOFF DISTANCE 2700 LBS AND 2400 LBS REFER TO SHEET 1 FOR APPROPRIATE CONDITIONS AND NOTES. s;:o 8~ trj~ t"':j> c.:> "d \. TAKEOFF OOC 10 C 20 C 30 C 40 C SPEED WEIGHT PRESS KIAS AlT lbs TOTAL TOTAL TOTAL TOTAL TOTAL LIFT AT FT GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR OFF 50 FT ROll 50 FT OBS ROll 50 FT OBS ROll 50 FT OBS ROll 50 FT OBS ROll 50 FT OBS S.L S.L , "d trj ~ >"<j OtlJ ~trj CJ1 I... C,.) Figure 5-4. Takeoff Distance (Sheet 2 of 2) ~g 02: trj CJ1.

8 SECTION 5 CESSNA RATE OF CLIMB Flaps Up 2600 RPM Full Throttle Col F laps Open NOTE: Mixture leaned above 5000 feet for maximum poer. WE!GHT LBS PRESS CLIMB RATE OF CLIMB - FPM ALT SPEED FT KIAS -20 C OOC 20 C 40 C 2950 S.L , , Figure 5-5. Rate of Climb 5-14

9 CESSNA SECTION 5 TIME, FUEL, AND DISTANCE TO CLIMB MAXIMUM RATE OF CLIMB Flaps Up 2600 RPM Full Throttle Col FlapsOpen StandardTemperature NOTES: 1..Add 1.8 gallonsof fuel for enginestart, taxi and takeoff alloance. 2. Mixture leanedabove5000 feet for maximum poer. 3. Increasetime, fuel and distanceby 10for each 1O0Cabovestandardtemperature. 4. Distancesshon arebasedon zero ind. WEIGHT LBS 2950 PRESSURE CLIMB RATE OF FROM SEA LEVEL TEMP ALTITUDE SPEED CLIMB c TIME FUEL USED DISTANCE FT KIAS FPM. MIN GALLONS NM S.L , , , Figure 5-6. Time, Fuel, and Distance to Climb (Sheet 1 of 2) 5-15

10 SECTION 5 CESSNA TIME, FUEL, AND DISTANCE TO CLIMB NORMAL CLIMB - 90 KIAS '- Flaps Up 2450 RPM 23 Inches MP or Full Throttle Col Flaps Open Standard Temperature " NOTES:. 1. Add 1.8 gallons of fuel for engine start, taxi and takeoff alloance. 2. Mixture leaned above 5000 feet for best poer. 3. Increase time, fuel and distance by 10 for each looc above standard temperature. 4. Distances shon are based on zero ind. PRESSURE RATE OF FROM SEA LEVEL WEIGHT TEMP ALTITUDE CLIMB LBS c FT FPM TIME FUEL USED DISTANCE MIN GALLONS NM 2950 S.L , , , Figure 5-6. Time, Fuel, and Distance to Climb (Sheet 2 of 2) 5-16

11 CESSNA SECTION 5 CRUISE PRESSURE ALTITUDE 2000 FEET Recommended Lean Mixture 2950 Pounds Col Flaps Closed RPM MP 20 C BELOW STANDARD 20 C ABOVE STANDARD TEMP TEMPERATURE STANDARD TEMP -9 C 11 C 31 C BHP BHP BHP Figure 5-7. Cruise Performance (Sheet 1 of 6) 5-17

12 SECTION 5 CESSNA CRUISE PRESSURE ALTITUDE 4000 FEET Recommended Lean Mixture 2950 Pounds Col Flaps Closed RPM MP 20 C BELOW STANDARD 20 C ABOVE STANDARD TEMP TEMPERATURE STANDARD TEMP -13 C 7 C 27 C BHP BHP BHP KTAS GPH Figure 5-7. Cruise Performance (Sheet 2 of 6) 5-18

13 CESSNA SECTION 5 CRUISE PRESSURE ALTITUDE 6000 FEET Recommended Lean Mixture 2950 Pounds Col Flaps Closed RPM. 20 C BELOW STANDARD 20 C ABOVE STANDARD TEMP TEMPERATURE STANDARD TEMP -17 C 3 C 23 C MP BHP BHP BHP KTAS GPH Figure 5-7. Cruise Performance (Sheet 3 of 6) 5-19

14 SECTION 5 CESSNA CRUISE PRESSURE ALTITUDE 8000 FEET " Recommended Lean Mixture 2950 Pounds. Col Flaps Closed RPM MP. 20 C BELOW STANDARD 20 C ABOVE STANDARD TEMP TEMPERATURE STANDARD TEMP -21 C -1 C 19 C BHP BHP BHP KTAS GPH Figure 5-7. Cruise Performance (Sheet 4 of 6) 5-20

15 CESSNA SECTION 5 CRUISE PRESSURE ALTITUDE 10,000 FEET Recommended Lean Mixture 2950 Pounds Col Flaps Closed 20 C BELOW STANDARD 20 C ABOVE. STANDARD TEMP TEMPERATURE STANDARD TEMP -25 C -5 C 15 C RPM MP BHP BHP BHP KTAS GPH Figure 5-7. Cruise Performance (Sheet 5 of 6). 5-21

16 SECTION 5 CESSNA CRUISE PRESSURE ALTITUDE12,000 FEET " Recommended Lean Mixture 2950 Pounds Col Flaps Closed RPM MP 20 C BELOW STANDARD 20 C ABOVE STANDARD TEMP TEMPERATURE STANDARD TEMP -29 C -9 C 11 C BHP BHP BHP KTAS GPH \ Figure 5-7. Cruise Performance (Sheet 6 of 6) 5-22

17 CESSNA SECTION Pounds Recommended Lean Mixture for Cruise Standard Temperature Zero Wind RANGE PROFILE 45 MINUTES RESERVE 56 GALLONS USABLE FUEL NOTES: 1..This chart allos for the fuel used for engine start, taxi, takeoff and climb, and the distance during a normal climb as shon in figure5-6 (sheet 2). 2. Reserve fuel is based on 45 minutes at 45 BHP and is 6.5 gallons. 12,000 10, f- u., D 6000 => f- i= --1 <! KTAStJ i::' I 'j!" 141 ::f KTAS,,f Q: ir 133KTAS::123 mtm109.a: a:..;: ;: ;: 3: i 0 Q. 0 Q. 0 0 Q. Q. * * * * I!) I!) I!) LD,... <C I!) I qo '3DKTAS KTAS S.L KTAS 129 KTASJ120 KTAS 107KTAS RANGE - NAUTICAL MILES 650 Figure 5-8, Range Profile (Sheet 1 of 2) 5-23

18 SECTION 5 CESSNA RANGE 2950 Pounds Recommended Lean Mixture for Cruise Standard Temperature Zero Wind PROFILE 45 MINUTES RESER V E 75 GALLO NS U SABLE FUEL NOTES: 1. This chart allos for the fuel used for engine start, taxi, takeoff and climb, and the distance during a normal climb as shon in figure 5-6 (sheet 2). 2. Reserve fuel is based on 45 minutes at 45 BHP and is 6.5 gallons. I- u. 12,000 10, ::> I- i=...j <:( S.L. 600 ~. ~ $' IV. <:1..~J ~v). «., 144 KTAS «; "LV,.,c- "~J ;c.,~j(tj41 KTAS v' 141KTAS'::j:: 133KTAS 112KTAS KTAS 138 KTAS 127 inl1 KTAS:!I:!KTAS a: a: a: a: UJ UJ UJ KTAS KTAS S S S $ c.. c.. a.. a.. * * * ;j! " co 10 "'" KTAS 120KTAS KTAS RANGE - NAUTICAL MILES Figure 5-8. Range Profile (Sheet 2 of 2) 5-24

19 CESSNA SECTION 5 ENDURANCE 2950 Pounds Recommended Lean Mixture for Cruise Standard Temperature PROFILE 45 MINUTES RESERV E 56 GALLONS USABLE FUEL NOTES: 1. This chart allos for the fuel used for engine start, taxi, takeoff and climb, and the time during a normal climb as shon in figure 5-6 (sheet 2). 2. Reserve fuel is based on 45 minutes at 45 BHP and is 6.5 gallons. r- u.. Q ::> r- i= -I <t: 12,000 10, LLJ "j:!',t;j Q:" i!:l -J 5J Ll.. i Q:" & ~J :;: :;::;: :;: Q.. Q.. Q.. Q.. "#. "#."#. "#. I!) I!) I!) I!) r-- (I) I!).q &III S.L ENDURANCE- HOURS 6 7 Figure 5-9. Endurance Profile (Sheet 1 of 2) 5-25

20 SECTION 5 CESSNA ENDURANCE PROFILE 45 MINUTES RESERVE 75 GALLO NS U SABLE FUEL 2950 Pounds Recommended Lean Mixture for Cruise Standard Temperature NOTES: 1. This cl;jart allos for the fuel used for engine start, taxi, takeoff and climb, and the time during a normal climb as shon in figure 5-6 (sheet 2). 2. Reserve fuel is based on 45 minutes at 45 BHP and is 6.5 gallons. 12,000 10, I- u.. CI 6000 ::> I- I-..J « rlj.j ;::!J t;, Q::-, ;; -.,J -.,J,.:::;, 4.. i Q::- oj!t) ~j S S S S II.' * * * * S.L ENDURANCE- HOURS 5-26 Figure 5-9. Endurance Profile (Sheet 2 of 2)

21 Flaps 40 Poer Off Maximum Braking Paved, Level, Dry Runay Zero Wind LANDING DISTANCE ;S:C1 8~ t:<j~ t""> I-' 00 N ~ NOTES: 1. Maximum performance technique as specified in Section Decrease distances 10 for each 9 knots headind. For operation ith tailinds up to 10 knots, increase distances by 10 for each 2 knots. 3. For operation on a dry, grass runay, increase distances by 40 of the "ground roll" figure. WEIGHT LBS SPEED OOC 1QoC 20 C 30 C 40 C AT PRESS ALT 50 FT TOTAL TOTAL TOTAL TOTAL TOTAL FT KIAS GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR ROLL 50 FT OBS ROLL 50 FT OBS ROLL 50 FT OBS ROLL 50 FT OBS ROLL 50 FT OBS 'v1 IṈ.;J "- '@ IN 00 c" ( S.L Figure Landing Distance ~ :;tj >'j am :;tjt:<j ~ ~@ t:<j1:]1