CESSNA 182P SKYLANE OWNER'S MANUAL
CESSNA 182P SKYLANE · Performance Data
Overview
This document serves as the performance data manual for the Cessna 182P Skylane, detailing critical specifications, operational limitations, and performance metrics essential for pilots and aviation enthusiasts. It outlines the aircraft's capabilities under various conditions, including weight, altitude, and fuel configurations. The manual is designed to assist pilots in understanding the performance characteristics of the Cessna 182P, ensuring safe and efficient operation. It includes detailed tables and charts that provide information on takeoff and landing distances, climb rates, stall speeds, and fuel consumption, making it a vital resource for flight planning and operational decision-making.
- Gross weight: 2950 lbs
- Top speed: 168 mph
- Cruise speed at 6500 ft: 160 mph
- Takeoff distance to clear 50 ft obstacle: 1350 ft
- Stall speed (flaps up): 64 mph
- Empty weight: 1645 lbs
- Fuel capacity: 60 gallons (standard)
Document
Source
Originally published by seahorse-hibiscus-e399.squarespace.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Performance Data
- Year
- 1974
- Pages
- 15
- File size
- 2.4 MB
- Publisher
- seahorse-hibiscus-e399.squarespace.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 690
- Engine (hp)
- 230
- Propeller
- Constant Speed, Diameter
- Engine model
- Continental Engine
- Max speed (kt)
- 138
- Cruise speed (kt)
- 139
- Empty weight (lb)
- 1,645
- Fuel capacity (gal)
- 60
- Rate of climb (fpm)
- 890
- Service ceiling (ft)
- 17,700
- Max takeoff weight (lb)
- 2,950
Performance
- Landing over 50ft
- 1,350
- Takeoff over 50ft
- 1,025
- Landing distance (ft)
- 590
- Takeoff distance (ft)
- 1,350
- Stall speed clean (kt)
- 64
- Stall speed landing (kt)
- 57
V-speeds
- VNE
- 198
- VNO
- 160
- VS1
- 64
- VSO
- 57
Weight & balance
- Useful load (lb)
- 1,305
- Baggage allowance (lb)
- 120
- Basic empty weight (lb)
- 1,645
- Max takeoff weight (lb)
- 2,950
Common. Rarer than 1% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA 182P SKYLANE.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Performance Specifications
The Cessna 182P Skylane has a gross weight of 2950 lbs and a top speed of 168 mph at sea level. The cruise speed at 75% power at 6500 ft is 160 mph, with a range of 690 nautical miles using 60 gallons of fuel without reserve. The rate of climb at sea level is 890 feet per minute, and the service ceiling is 17,700 ft.
Takeoff and Landing Data
Takeoff distances vary based on weight and altitude. For a gross weight of 2950 lbs, the ground run is 705 ft, and the total distance to clear a 50-foot obstacle is 1350 ft at sea level. Landing distances with 40° flaps at the same weight are 590 ft ground roll and 1350 ft total distance to clear a 50-foot obstacle.
Stall Speeds
Stall speeds for the Cessna 182P are 64 mph with flaps up and 57 mph with flaps down, both under power-off conditions.
Weight and Balance
The empty weight of the Cessna 182P is approximately 1645 lbs, with a useful load of 1305 lbs. The baggage allowance is 120 lbs, and the center of gravity range is specified in inches.
Fuel and Oil Capacity
The total fuel capacity is 60 gallons for standard tanks and 79 gallons for optional long-range tanks. The oil capacity is 12 quarts.
Safety notes
- Always operate within FAA-approved markings and placards.
- Ensure weight and balance calculations are accurate before flight.
Full document text
CESSNA M OR E P E OP LE B U Y AND FLY C ES S NA A IR P LA NE S THAN A N Y O TH ER MAKE 1974 W ORL D ' S LA RG EST P RO - D U C E R O F GE NE RA L .A. VI A T I O N A I R C R A F T S I N C E 1 956 MODEL 162 SKY LANE OWNER'S M i\ _NUAL PERFORMANCE - SPECIFICATIONS GROSS WEIGHT . . . . . . . . SPEED : Top Speed at Sea Level . . . Cruise , 75% Power at 6500 ft RANGE: Cruise, 75% Power at 6500 ft 60 Gallons , No Reserve Cruise , 75% Power at 6500 ft 79 Gallons, No Res e rv e Maximwn Range at 10, 000 lt 60 Gallons, No Res erve Maximwn Range a t 10 , 000 ft 79 Gallons, No Reserv e RATE OF CLIMB AT SEA LEVEL SERVICE CEILING . . . . . . TAKE-OFF : Ground Run ....... . Total Di stance Ov er 50 - F oot Ob s tacle LANDING: Ground Roll .. .. . .. ... . . Total Distance Over 50-F oot Obstacle STAL L SPEEDS : Flaps Up, Power Off . . . . Flaps Down, Power Off EMPTY WEIGHT : (Approximate} Skylan e .. Model 182 . USEFUL LOAD : Sky la ne Model 182 BAGGAGE : F o rward Ar ea "A" (Sta tion 82 to 108) Aft Area "B" (Station 108 to 124) . WING LOADING : Pound s / Sq Fo ot POWER LOADING : Pound s / HP FUEL CAPACITY : Total Standard Tanks Optional Lon g Range Tank s OIL CAPACITY : Total PROPELLER : Constant Speed, Diameter . ENGINE : Contin e ntal Engine 230 r ated BHP at 2600 RPM NOTE: P e rforman ce data is shown for the Skylane whic h is 2 to 3 mph faster than a stand.a.rd-equipped Model 182 (with o ut speed fairings}. Ther e ~s a corresponding difference in range, while all other per forman ce figures are the same for the 182 as s hown for th e Skyl.ane. Skyla ne * 29 50 l bs 168 mph 160 mph 690 mi 4. 3 hrs 160 mph 910 mi 5. 7 hrs 160 mph 885 mi 7. 7 hrs ll 5 mp h 11 60 mi 10 . 1 hrs 11 5 mph 890 f pm 17 . 700 ft 7 05 It 13 50 ft 590 ft 1350 ft 64 mph 57 mph 1 645 l bs 159 5 lbs 1305 lb s 1355 lb s 12 0 lbs 80 lb s 16. 9 12.8 65 gal . 84 gal . 12 qts 82 in ches 0 -4 70-R *This manual covers operation of the Model 182 / Skylane which is certificated as Model !82P under FAA Type Certificate No . 3Al3. 0 1 02 1 · 13 - RA ND - 2000 - 1 175 Section If 111c================:::::::__·,,,~~~~:=--------------~Dn' ......._ OPERATING LIMITATIONS OPERATIONS AUTHORIZED. Your Cessna exceeds the requirements for airworthiness as set forth by the United States Government, and is certificated under FAA Type Cer- tificate No. 3Al3 as Cessna Model No. 182P. The airplane may be equipped for day, night, VFR, or IFR operation. Your Cessna Dealer will be happy to assist you in selecting equipment best suited to your needs. Your airplane must be operated in accordance with all FAA-approved markings and placards in the airplane. If there is any information in this section which contradicts the FAA-approved markings and placards, it is to be disregarded . MANEUVERS-NORMAL CATEGORY. The airplane is certificated in the normal category. The normal category is applicable to airplanes intended for non-aerobatic operations. These include any maneuvers incidental to normal flying, stalls (except whip stalls) and turns in which the angle of bank is not more than 60°. In connection with the foregoing, the following gross weight and flight load factors apply: Gross Weight Flight Load Factor: *Flaps Up .. *Flaps Down . . +3 . 8 +2. 0 2950 lbs -1. 52 *The design load factors are 150% of the above, and in all cases, the structure meets or exceeds design loads. 4-1 AIRSPEED LIMITATIONS (CAS). The following is a list of the certificated calibrated airspeed (CAS) limitations for the airplane. Never Exceed Speed (glide or dive, smooth air) . Maximum Structural Cruising Speed Maximum Speed, Flaps Extended Flaps 10° . . . . . . ... Flaps 10° - 40° . . . . . . *Maneuvering Speed . . . . . . *The maximum speed at which you may use abrupt control travel. . 198 MPH . 160MPH . 160 MPH . 110 MPH . 126 MPH AIRSPEED INDICATOR MARKINGS. The following is a list of the certificated calibrated airspeed markings (CAS) for the airplane. Never Exceed (glide or dive, smooth air). Caution Range . . . . . Normal Operating Range Flap Operating Range . ENGINE OPERATION LIMITATIONS. . . . 198 MPH (red line) 160-198 MPH (yellow arc) 68-160 MPH (green arc) . 63-110 MPH (white arc) Power and Speed . . . . . . . . . . . . . . 230 BHP at 2600 RPM ENGINE INSTRUMENT MARKINGS. OIL TEMPERATURE GAGE. 4-2 Normal Operating Range Do Not Exceed . . . Green Arc 225 ° F (red line) OIL PRESSURE GAGE. Idling Pressure . Normal Operating Range Maximum Pressure FUEL QUANTITY INDICATORS. . . 10 psi (red line) 30-60 psi (green arc) . 100 psi {red line) Empty ...................... E (red line) (2. 5 gallons unusable each tank in normal flight maneuvers with fuel selector valve on "BarH. ") CYLINDER HEAD TEMPERATURE GAGE. Normal Operating Range Do Not Exceed . . . . . TACHOMETER . Normal Operating Range ..... Do Not Exceed (Engine rated speed) MANIFOLD PRESSURE GAGE. Normal Operating Range 200 -460 ° F (green arc) ... 460 ° F (red line) 2200-2450 RPM (green arc) .2600 RPM (red line) . .. 15-23 in. Hg (green arc) CARBURETOR AIR TEMPERATURE GAGE (OPT). Icing Range . . . . . . . . . -15° to 5°C (yellow arc) SUCTION GAGE (GYRO SYSTEM). Normal Operating Range .... 4.6-5.4 in. Hg (green arc) WEIGHT AND BALANCE. Th e following information will enable you to operate your Cessna within the pre scribed weight and center of gravity limitations. To figure weight and balance, use the Sample Loading Problem, Loading Graph, and Center of Gravity Moment Envelope as follows: Take the licensed empty weight and moment from appropriate weight and balance records carried in your airplane, and write them down in the column titled "YOUR AIRPLANE" on the Sample Loading Problem. NOTE The licensed empty weight and moment are recorded on the Weight and Balance and Installed Equipment Data sheet, or 4-3 Section fl OPERATIONAL DATA The operational data charts on the following pages are presented for two purposes; first, so that you may know what to expect from your air-
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plane under various conditions, and second, to enable you to plan your flights in detail and with reasonable accuracy. The data in the charts has been compiled from actual flight tests with the airplane and engine in good condition and using average piloting tech- niques. Note also that the range charts make no allowances for wind, nav- igational errors, warm-up, take-off, climb, etc. You must estimate these variables for yourself and make allowances accordingly. Speeds shown in the Cruise Performance charts reflect performance of the Skylane con- figuration; these speeds are 2 to 3 MPH faster than the Model 182 , Remember that the charts contained herein are based on standard day conditions. For more precise power, fuel consumption, and endur- ance information, consult the Power Computer supplied with your air- craft. With the Power Computer you can easily take into account tem- perature variations from standard at any flight altitude. AIRSPEED CORRECTION TABLE FLAPS IAS 60 80 100 120 140 160 180 --- UP CAS 68 83 101 119 139 158 177 --- FLAPS DOWN IAS 40 50 60 70 BO 90 100 110 20 °- 40 ° CAS 55 60 66 74 83 92 102 111 Figure 6-1. 6-1 STALL SPEEDS - MPH CAS ANGLE OF BANK !CONDITION oo I 30° I 60° FLAPS UP 64 69 91 2950 LBS. GROSS FLAPS 20° 59 63 83 WEIGHT FLAPS 40° 57 61 81 POWER OFF - AFT CG Figure 6-2. 6-2 (j) I w TAKE-OFF DATA TAKE- O FF DI STA N CE W IT H 2 0° FLA PS FROM HAR D SURFACE RUNWAY GROSS !AS HEAD AT SEA LEVEL & 59°F. AT 2500 IT. & 50 " F. AT 5000 FT. & 41°F. AT 7500 FT. & 32° F. WEIGHT @50 ' WIND GROUND TOTAL TO GROUND TOTAL TO GROUND TOTAL TO GROUND TOTAL TO LBS. MPH KNOTS RUN CLEAR 50' OBS RUN CLEAR 50' OBS RUN lcLEAR 50' "''" RUN CLEAR 50' OBS 0 705 1350 845 1625 1015 1990 1240 2585 2950 60 10 490 1025 595 1245 725 1550 900 2040 20 310 740 385 910 480 1150 610 1545 0 485 965 575 1120 690 1330 840 1630 2500 55 10 325 710 395 840 475 1005 590 1255 20 195 490 245 590 300 720 380 915 0 295 655 350 745 415 855 500 1005 2000 50 10 185 460 225 530 275 620 335 740 20 105 305 130 355 160 425 205 515 NOTES: 1. Increase distances t0%for each 25°F above etanda.rd temperature for particular altitude. 2. For operation on a dry, grass runway, increase dlatances (both "ground run" and "total to clear 50 ft. obstacle") by 7% o( the "total to clear 50 ft. obstacle" figure . MAXIMUM RATE-OF-CLIMB DATA AT SEA LEVEL & 59°F. AT 5000 IT. & 4l " F. AT 10,000 FT . & 23°F. AT 15, 000 FT. & 5°F. AT 20, 000 FT. & -12"F. GROSS !AS RATE GAL. !AS RATE !FromSL !AS RATE FromSL !AS RATE IFromSL !AS RATE From SL WE!GJIT MPH OF OF MPH OF FUEL MPH OF FU EL MPH OF FUEL MPH OF FUEL LBS. CLIMB FUEL CLIMB USED CLIMB USED CLIMB USED CLIMB USED FT/ MIN USED FT/MIN IT/MIN FT/ MIN FT / MIN 2950 89 890 1. 5 87 665 3. 8 85 445 6.8 83 220 11. 5 -- -- -- 2500 87 1210 I. 5 85 935 3.2 83 655 5. 2 BO 380 8. 2 78 105 14. 9 2000 84 1710 I. 5 82 1350 2. 7 79 995 4.1 76 640 5. 9 74 280 9. 2 NOTES: 1. Fla.pa up, full throttle, 2600 RPM, mixture leaned for smooth operation above 5000 ft. 2. Fuel used includes warm - up and take-off allowance. . 3. For hot weather, decrease rate of climb 30 !t. / min. for each 10°F above standard day temperature for particular altitude . Figure 6- 3. UISE PERFORMANC EXTENDED RANGE MIXTURE Standard Conditions ~Zero Wind ~Gross Weight- 2950 Pounds 2500 FEET 60 GAL( NO RESERVE) 79 GAL(NO RESERVE) 3 TAS GAL/ ENDR. RANGE ENDR . RANGE RPM MP BHP MPH HOUR HOURS MILES HOURS MILES 2450 23 76 156 14. 2 4.2 660 5.6 870 22 72 15 .3 13. 4 4. 5 685 5. 9 900 21 68 149 12. 7 4. 7 705 6.2 925 20 63 144 12.0 5. 0 720 6, 6 950 2300 23 71 151 13. l 4. 6 690 6. 0 910 22 67 148 12.2 4. 9 730 6, 5 960 21 62 143 11. 5 5. 2 745 6. 9 980 20 59 140 11. 0 5. 5 765 7. 2 1005 2200 23 67 148 12. 1 5.0 735 6. 5 965 22 63 144 11. 4 5. 3 760 6. 9 1000 21 59 140 10.8 5. 6 780 7. 3 1025 20 55 135 10. 2 5. 9 795 7.7 1045 •2000 20 47 123 8. 7 6. 9 850 9.1 1115 19 43 117 8.2 7. 3 855 9. 6 1125 18 39 110 7.5 8. 0 880 10, 5 1160 17 35 101 7. 0 8. 6 865 11. 3 1140 •P ow er s ett ings· in this block r e pres ent m aximum rang e settings. Figure 6-4 (Sheet 1 of 5). 6-4 CRUISE PERFORMANC EXTENDED RANGE MIXTURE Standard Conditions~ Zero Wind~ Gross Weight- 2950 Pounds 5000 FEET 60 GAL( NO RESERVE) 79 GAL(NO RESERVE) % TAS GAL/ ENDR . RANGE ENDR . RANGE RPM MP BHP MPH HOUR HOURS MILES HOURS MILES 2450 23 78 160 14. 5 4.1 660 5. 4 870 22 73 157 13.6 4.4 695 5.8 910 21 70 153 13. 0 4. 6 705 6. 1 930 20 65 149 12.2 4.9 735 6. 5 965 2300 23 73 157 13. 4 4. 5 705 5.9 925 22 69 152 12. 6 4.8 725 6. 3 955 21 64 148 11. 9 5. 0 745 6.6 985 20 60 144 11. 2 5. 4 770 7.1 1015 2200 23 68 151 12.4 4. 8 730 6. 4 960 22 64 148 11. 7 5. 1 760 6.8 1000 21 60 144 11. 0 5.5 785 7.2 1035 20 57 139 10. 5 5. 7 795 7.5 1045 •2000 20 48 128 9.0 6. 7 855 8.8 1125 19 45 121 8. 5 7. 1 855 9.3 1125 18 41 114 7.9 7. 6 865 10.0 1140 17 37 105 7. 3 8. 2 865 10. 8 1135 *Power settings in this block represent maximum range settings. Figure 6-4 (Sheet 2 of 5). 6-5 SE PERFORMANC EXTENDED RANGE MIXTURE Standard Conditions~ Zero Wind~ Gross Weight- 2950 Pounds 7500 FEET 60 GAL(NO RESERVE) 79 GAL(NO RESERVE) 3 TAS GAL/ ENDR. RANGE ENDR. RANGE RPM MP BHP MPH HOUR HOURS MILES HOURS MILES 2450 21 71 157 13. 1 4. 6 720 6.0 945 20 67 154 12, 4 4.8 745 6. 4 980 19 62 149 11. 7 5. 1 765 6. 8 1005 18 58 144 11.0 5. 5 785 7.2 1035 2300 21 66 153 12. 2 4.9 750 6.5 990 20 62 149 ll. 6 5. 2 770 6. 8 1015 19 58 144 11. 0 5. 5 785 7.2 1035 18 54 139 10. 5 5.7 795 7. 5 1045 2200 21 62 149 11. 4 5. 3 785 6.9 1035 20 58 144 10. 7 5. $. 805 7.4 1065 19 54 139 10. 2 5.9 820 7. 7 1075 18 51 133 9.7 6. 2 825 8.1 1085 •2000 20 50 132 9. 2 6. 5 860 0. 6 1135 19 47 126 8. 7 6.9 870 9.1 1145 18 43 118 8. l 7. 4 875 9.8 1150 17 39 110 7. 6 7.9 870 10.4 1145 I •Power settings in this block represent maximum range settings. Figure 6-4 (Sheet 3 of 5). 6-6 UISE PERFORMANC EXTENDED RANGE MIXTURE Standard Conditions~ Zero Wind~ Gross Weight- 2950 Pounds 10,000 FEET 60 GAL( NO RESERVE) 79 GAL(NO RESERVE) 3 TAS GAL/ ENDR . RANGE ENDR . RANGE RPM MP BHP MPH HOUR HOURS MILES HOURS MILES 2450 19 63 154 11. 9 5. 0 775 6. 6 1020 18 60 149 11. 2 5. 4 800 7.1 1050 17 55 143 10. 6 5. 7 810 7. 5 1065 16 51 137 10.0 6 .0 820 7.9 1080 2300 19 60 149 11. 1 5. 4 805 7. 1 1060 18 56 144 10. 5 5. 7 825 7.5 1085 17 51 137 9.8 6. 1 840 8. 1 1105 16 47 130 9. 2 6. 5 850 8.6 1115 2200 19 56 144 10. 4 5. 8 830 7.6 1095 18 52 138 9. 8 6. 1 845 8. 1 1110 17 49 132 9. 3 6. 5 850 8. 5 1120 16 45 124 8. 7 6. 9 855 9.1 1125 *2000 19 48 130 8. 9 6. 7 875 8. 9 1155 18 44 123 8. 4 7. I 880 9.4 1155 17 40 115 7. 8 7. 7 885 10.1 1165 16 38 101 7. 4 8. 1 820 10. 7 1080 •Power settings i n this block r e present maximum ra nge settings, Figure 6-4 (Sheet 4 of 5). 6-7 CRUISE PERFORMANCE EXTENDED RANGE MIXTURE Standard Conditions~ Zero Wind~ Gron Weight- 2950 Pounds 15,000 FEET 60 GAL( NO RESERVE) 79 GAL(NO RESERVE) % TAS GAL/ ENDR. RANGE ENDR. RANGE RPM MP BHP MPH HOUR HOURS MILES HOURS MILES 2450 2300 2200 2000 6-8 16 15 14 16 15 14 16 15 14 16 15 54 50 46 50 47 42 47 44 40 40 37 145 10. 4 139 126 139 131 113 131 120 106 106 97 9. 8 9. 2 9.6 9 .1 8. 5 9. 1 8. 6 8.0 7. 8 7. 3 5. 8 6.1 6 .5 6.2 6.6 7.1 6. 6 7.0 7. 5 7. 7 8. 2 835 850 820 870 865 800 865 835 795 815 795 Figure 6-4 (Sheet 5 of 5). 7. 6 8. 1 8. 6 8. 2 8. 7 9. 3 8. 7 9. 2 9.9 10.1 10. 8 1100 1120 1080 114 5 1135 1050 1135 1100 1045 1075 1050 a> I <.D LANDING DISTANCE TABLE LANDING DISTANCE WITH 40° FLAPS ON HARD SURFACED RUNWAY @SEA LEVEL & 59" F @ 2500 FEET & 50 ° F @ 5000 FEET & 41 ° F @ 7500 FEET & 32° F GROSS APPROACH WEIGHT IAS GROUND TOTAL GROUND TOTAL GROUND TOTAL GROUND TOTAL POUNDS MPH ROLL TO CLEAR ROLL TO CLEAR ROLL TO CLEAR ROLL TO CLEAR 50 FT. OBS. 50 FT. OBS. 50 FT. OBS. 50 FT. OBS. 2950 69 590 1350 640 1430 680 1505 740 1595 NOTES: 1. Di stances s hown are based on ze r o wind, power o ff and h eavy braking. 2. Reduce landing distances 10% for each 5 k nots headwind . 3. For opera tion on a dry, grass runway, in crease distanceR (both "ground r oll" a nd "tota l to c l ear 50 ft. obstacle") by 20 % of the "tota l to clear 50 ft. obstacle" fi gure . Figure 6-5. MAXIMUM GLIDE e SPEED 80 MPH (IAS) -- e PROPELLER WINDMILLING e FLAPS UP e ZERO WIND ~ 16,000J---+----+----+---+---1-------:m~ .......- 14,00 0 t-----+----t----+----+.,----,-.t'""= z < 12,000 1-----+----+----+----+=rw a: ffi l 0, 000 t-----+----t----t---.rr'i"""+----ir---+----1 I- .... 8000 > 0 cg 6000 < I- 4000 :I: C> .... 2000 :I: 5 10 15 20 25 30 35 GROUND DISTANCE (STATUTE MILES) Figure 6-6. 6-10
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