MODEL172R SECTON 6 WEGHT & BALANCE EQUPMENT LST 2500 1100 '{j)2300 c z 5 2200 a. -... S2100 [j ~ 2000 z :5 8: 1900 «ffi 1800 0 ~ 1700 1600 700 1500 illl m 111111'~11111l1!nT U 1111111111111111111 50 60 70 80 90 100 110 120 ~ LOADED ARPLANE MOMENT/1000 (POUND-NCHES) 1050 '10008 52-..J 950 - :r: 0 W 900 3: w 850 ~ a: < 0 800 w ~ 750..J. Figure 6-7. Center of Gravity Moment Envelope 0585C1007 Feb 28/00 6-15
SECTON 6 WEGHT & BALANCE / EQUPMENT LST LOAD MOMENT/1000 (KLOGRAM. MLLMETERS) 0 50 100 150 200 250 300 350 400 U"",,1'"1'"1 d t""1 t.,...", 400 ~ 5 350 ~ ~300, e!) W 250 3:..., 175 ~ ~ 150 e!) 9 S2-125!i: e!) jjj 100 3:, 150. - 100. 50 NOTE: LNE REPRESENTNG ADJUSTABLE SEATS SHOWS THE PLOT OR PASSENGER CENTER OF GRAVTY ON ADJUSTABLE SEATS POSTONED FOR AN AVERAGE OCCUPANT. REFER TO THE LOADNG ARRANGEMENTS DAGRAM FOR FORWARD AND AFT LMTS OF OCCUPANT C.G. RANGE. Figure 6-6. Loading Graph 0585C1006, 6-14 Nov 3/97
SECTON 5 STALL SPEEDS AT 2450 POUNDS Conditions: Power Off FLAP SETTN' MOST REARWARD CENTER OF GRAVTY KAS ANGLE OF BANK 00 300 450 600 KCAS KJAS KCAS KJAS KCAS KAS KCAS UP 44 51 48 55 53 61 63 73 100 35 48 38 52 42 58 50 69 300 33 47 36 50 40 56 47 66 FLAP SETTNr.! MOST FORWARD CENTER OF GRAVTY ANGLE OF BANK 00 300 450 600, KJAS KCAS KAS KCAS KAS KCAS KfAS KCAS UP 44 52 48 56 53 62 63 74 100 37 50 40 53 44 59 53 70 300 33 47 36 50 40 56 47 66 NOTES: 1. Altitudeloss during a stall recovery may be as much as 230 feet. 2. KASvalues are approximate. Figure 5-3. Stall Speeds 5-12 Dee 2/96
SECTON 5 PERFQRMANCE CONDTONS: SHORT FELD TAKEOFF DSTANCE AT 2450.POUNDS Flaps10 FullThrottlePriorto BrakeRelease Paved,level,dryrunway ZeroWind Lift Off: 51 KAS Speedat 50 Ft: 57 KAS NOTES: O C 10 C 20 C 30 C. 40 C Press Grnd Total Grnd Total "Gmd rrotal Grnd Total Grnd Total Alt Roll FtTo Roll FtTo Roll FtTo Roll FtTo' Roll FtTo Ft Clear Ft Clear Ft Clear Ft Clear Ft Clear n 50 Ft 50 Ft 50 Ft 50 Ft 50 Ft Feet Obst Obst Obst Obst Obst S.L. 845 1510 910 1625 980 1745 1055 1875 1135 2015 1000 925 1660 1000 1790, :1075 1925 1160 2070 1245 2220 2000 1015 1830 1095 1970 1185 2125 1275 2290 1365 2455 3000 1115 2020 1205 2185 130, 236f) 1400 2540 1505 2730 4000 1230 245 1330 2430 1435 2630 1545 2830' 1655.3045 5000 1355 2500 1470 2715 1585 2945 1705 3175 1830 3430 6000 1500 2805 1625 3060 1750 3315 1880 3590 2020 3895 7000 1660 3170 1795 3470 1935 3770 2085 4105 2240 4485 8000 1840 3620 1995 3975 2150 4345 2315 4775 --.... 1. Short field technique as specified in Section 4. 2. Prior to takeoff from fields above 3000 feet elevation, the mixture should be leaned to give maximum RPM in a fullthrottle, static runup. 3. Decrease distances 10% for each 9 knots headwind. For operation with tallwinds up to 10 knots. increase distances by 100/0for each 2 knots. 4. For' operation on dry, grass runway, increase distances by 15% of the "ground roll"figure. 5. Where distance value has been deleted. climb performance s minimal. Figure5.5. Short FieldTakeoffDistance 5.14 Original ssue
SECTON 5 CRUSE CONDTONS:.2450 Pounds Recommended Lean Mixture At All Altitudes (Refer to Section 4, Cruise) 20 0BELOW STANDARD 20 0ABOVE PRESS STANDARDTEMP TEMPERATURE STANDARDTEMP ALT RPM FT % % % BHP KTAS GPH BHP KTAS GPH BHP KTAS GPH 8000 2400 -- --- ---. 80 122 9.2 76 121 8.7 2350 81 120 9.3 76 119 8.7 71 118 8.2 2300 76 117 8.7 71 116 8.2 68 115 7.8 2200 68 111 7.7 64 110 7.3 61 107 7.0 2100 60 104 6.9 57 102 6.6 55 99 6.4 2000 54 96 6.2 52 94 6.0 51 91 5.9 10,0002350 76 119 8.8 72 118 8.2 68 117 7.8.2300 72 116 '8.3 68 115 7.8 65 113 7.4 2250 68 113 7.8 65 112 7.4 61 109 7.1 NOTE: 2200 65 110 7.4 61 108 7.0 59 105 6.7 2100 58 102 6.6 55 100 6.4 54 97 6.2 2000 52 94 6.1 51 91 5.9 50 88 5.8 12,0002350. 73 119 8.3 69 117 7.9 65 115 7.5 2300 69 115 7.9 65 113 7.5 62 111 7.1 2250 65 112 7.5 62 109 7.1 59 107 6.8 2200 62 108 7.1 59 105 6.8 57 103 6.6 2100 56 100 6.4 54 97 6.2 53 94 6.1 1. Cruise speeds are shown for tin airplane equipped with speed fairings. Without speed fairings, decrease speeds shown by 2 knots. Figure 5-8. Cruise Performance (Sheet 2 of 2) 5-18 Dee 2196
SECTlbN 5 '. MAXMUM RATE-OF-CLMB AT 2450 POUNDS CONDTONS: Flaps Up FullThrottle PRESS CLMB RATE OF CLMB. FPM ALT SPEED FT KAS -20 C QOC 20 C 40 C S.L. 79 830 770 705 640 2000 77 720 655 595 535 4000 76 645 585 525 4.5 ; 6000 74 530 475 415 360 '" 8000 72 420 365 310 250 10,000 71 310 255 200 145 12,000 69,.aQO " 145 -.--.-. NOTE: 1. Mixtureleaned above3000 feet for maximum RPM. Figure 5~6. Maximum Rate of Climb' Dee 2/96 5.15
SECTON 5 MODEL172R ENDURANCEPROFLE 45 MNUTESRESERVE 53 GALLONSUSABLEFUEL CONDTONS: 2450 Pounds Recommended Lean Mixturefor Cruise At AnAltitudes Standard Temperature 12,000 j- -...-...-! 10,000 ti: 8000 w c ::::) - 3 6000 <C 4000 ':tt:[o. ~ t-~..,:t]:~' '...1..""..1..' '.."".'.'-1.'.,..j..,, +:r.llrh:.f!':~'.f::llmw:t:"",-.",,. a:ff1m:13~~ "i..t'1~i ~~ ~""""""""""""'" 2000,, t'1"'" 1-4 '-"'-"""'" "",,-,..,,,- SL.::tt::t::.t:t:.tfUt.t.t..tt.t1:tt..tt.:t:tt::t::tttt::t:t..t:,. 4 5 6 7 ENDURANCE. HRS NOTE: 1. Thischart allowsfor the fuel used for engine start. taxi, takeoff and climb,and the timeduringclimb...., Figure 5-10. Endurance Profile 8 "5-20 Feb 28/97
SECTON5 ) CONDTONS: Flaps30 PowerOff MaximumBraking Paved,level,dry runway ZeroWind Speedat 50 Ft: 62 KAS SHORT FELD LANDNG DSTANCE AT 2450 POUNDS ) O C 10 C 20 C 30 C 40 C Grnd Total Grnd Total Grnd Total Grnd Total Grnd Total Press Roll FtTo Roll FtTo Roll FtTo Roll FtTo Roll FtTo Alt Ft Clear Ft Clear Ft Clear Ft Clear Ft Clear 50Ft 50Ft 50Ft 50Ft 50Ft n Obst Obst Obst Obst Obst Feet S.L. 525 1250 540 1280 560 110 580 1340 600 1370 1000 545 1280 560 1310 580 1345 600 ;1375 620 1405 2000 565 1310 585 1345 605 1375 625 1410 645 1440 3000 585 1345 605 1380 625 1415 650 1445 670 1480 4000 605 1380 630 1415 650 1450 670 1485 695 1520 5000 630 1415 650 1455 675 1490 700 1525 720 1560 6000 655 1455 675 1490 700 1530 725 1565 750 1605 7000 680 1495 705 1535 730 1570 755 1610 775 1650 8000 705 1535 730 1575 755 1615 780 1655 810 1695 NOTES:' ) 1. Shortfieldtechniqueas specifiedin Section4. 2. Decreasedistances 10% for each 9 knots headwind. For operation with tail winds up to 10 knots, increasedistancesby 10%for each 2 knots. 3. For operation on dry, grass runway, increase distances by 45% of the "groundroll"figure. 4. f landingwith flaps up, increasethe approachspeed by 7 KAS and allowfor 35%longerdistances. Figure 5-11. Short Field Landing Dist,ance Revision8 5-21/5-22
MODEL 172A SECTON5 ) CONDTONS: SHORT FELD LANDNG DSTANCE AT 2450 POUNDS Flaps30 PowerOff MaximumBraking Paved,level,dry runway ZeroWind Speedat 50 Ft: 62 KAS ) O C 10 C 20 C 30 C 40 C Grnd Total Grnd Total Grnd Total Grnd Total Grnd Total Press Roll FtTo Roll FHa Roll FtTo Roll FtTo Roll FtTo Alt Ft Clear Ft Clear Ft Clear Ft Clear Ft Clear 50Ft 50Ft 50Ft 50Ft 50Ft 'n Obst Obst Obst Obst Obst Feet S.L. 525 1250 540 1280 560 110 580 1340 600 1370 1000 545 1280 560 1310 580 1345 600 ;1375 620 1405 2000 565 1310 585 1345 605 1375 625 1410 645 1440 3000 585 1345 605 1380 625 1415 650 1445 670 1480 4000 605 1380 630 1415 650 1450 670 1485 695 1520 5000 630 1415 650 1455 675 1490 700 1525 720 1560 6000 655 1455 675 1490 700 1530 725 1565 750 1605 7000 680 1495 705 1535 730 1570 755 1610 775 1650 8000 705 1535 730 1575 755 1615 780 1655 810 1695 NOTES:. ) 1. Shortfieldtechniqueas specifiedin Section4. 2. Decreasedistances 10% for each 9 knots headwind. For operation with tail winds up to 10 knots, increasedistancesby 10%for each 2 knots. 3. For operation on dry, grass runway, increase distances by 45% of the "groundroll"figure. 4. f landingwith flaps up, increasethe approachspeed by 7 KAS and allowfor 35%longerdistances. Figure 5-11. Short FieldLandingDist~nce Revision8 5-21/5-22
SECTON 5 CRUSE CONDTONS:. 2450 Pounds Recommended Lean Mixture At All Altitudes (Refer to Section 4, Cruise) 20.C BELOW STANDARD 20.C ABOVE PRESS STANDARDTEMP TEMPERATURE STANDARDTEMP ALT RPM FT % % % BHP KTAS GPH BHP KTAS GPH BHP KTAS GPH 8000 2400 -- --- -- 80.122 9.2 76 121 8.7 2350 81 120 9.3 76 119 8.7 71 118 8.2 2300 76 117 8.7 71 116 8.2 68 115 7.8 2200 68 111 7.7 64 110 7.3 61 107 7.0 2100 60 104 6.9 57 102 6.6 55 99 6.4 2000 54 96 6.2 52 94 6.0 51 91 5.9 10,000 2350 76 119 8.8 72 118 8.2 68 117 7.8.2300 72 116 '8.3 68 115 7.8 65 113 7.4 2250 68 113 7.8 65 112 7.4 61 109 7.1 2200 65 110 7.4 61 108 7.0 59 105 6.7 2100 58 102 6.6 55 100 6.4 54 97 6.2 2000 52 94 6.1 51 91 5.9 50 88 5.8 12,000 2350, 73 119 8.3 69 117 7.9 65 115 7.5 2300 69 115 7.9 65 113 7.5 62 111 7.1 2250 65 112 7.5 62 109 7.1 59 107 6.8 2200 62 108 7.1 59 105 6.8 57 103 6.6 2100 56 100 6.4 54 97 6.2 53 94 6.1 NOTE: 1. Cruise speeds are shown for an airptiine equipped with speed fairings. Without speed fairings, decrease speeds shown by 2 knots. Figure 5-8. Cruise Performance (Sheet 2 of 2) " 5-18 Dee 2/96
MODEL172R SECTON 5 RANGEPROFLE 45 MNUTES RESERVE 53 GALLONS USABLE FUEL CONDTONS: 2450 Pounds Recommended Lean Mixturefor Cruise At AllAltitudes Standard Temperature Zero Wind 12,000 10,000 t1: 8000 i'~}++' w. g 6000 f- ~«4000 w"""""'~"'"~-'"-""" 2000 -.+!- L, SL 550 Hi.113 KTAS.108 KTAS' 600 650 700 RANGE - NAUTCAL MLES 750 NOTES: 1. This chart allows for the. fuel used for engine start, taxi, takeoff and climb,and the distance duringclimb. 2. Performance is shown for an airplane equipped with speed fairings. which increase the cruise speeds by approximatelytwo knols. Figure 5.9. Range Profile Feb28/97 5-19
SECTON 6 WEGHT & BALANCE/ EQUPMENT LST, WEGHTAND MOMENT TABt)LATON SAMPLE YOUR TEM DESCRPTON ARPLANE ARPLANE Weight Moment Weight Moment (bs.) (Lbwlns. /1000) (fbs.) (Lbwln». /1000 1. Basic EmptyWeight (Use the data pertainin to your airplane as t s r,resently ncludes unusable equipped. fuel and full 011) 1639 64.4 2. Usable Fuel (At 6 Lbs.lGal.) 53 Gallons Maximum 35 Gallons (To reduced fuel ndicator tab) 210 10.1 3. Pilot and Front Passenger (Station 34 to 46) 340 12.6 4. RearPassengers 220 16.0 5. *Baggage Area 1 (Station 82 to 108; 120 Lbs. Max.) 48 3.4 6. *Baggage Area 2 (Station 108 to 142;50 Lbs. Max.) 7. RAM WEGHT AND MOMENT (add columns) 2457 106.5 8. Fuel allowance for engine start, taxi and runup w7.0-0.3 9. TAKEOFF WEGHT AND 1105' MOMENT 8 from Step()btract 7 Step 2450 106.2 10. Locate this point (2450 at 106.2 on the Center of Gravity Moment Envelope, and slnoe th s point falls within the * envelope, the loading s accetable. The maximum allowabfecom ned weight oapaclty for baggage areas 1 and 2 s 120 pounds. Figure 6-5. Sample Loading Problem (Sheet 1 of 2) j \ \:\ or '. 6w12 Feb 28/00
, (.- WEGHT & BALANCE AND NSTALLED EQUPMENT DATA CEBSmARCRAFT COMPANY ~ SNGLEENGNEDM8ON Ce8iii -. - -.. REGlllTRA1OH -.T -- ARM milt 172t18l' 1'- \lol (lltl...-, ( 8T- EllPn'W!Of1' 1.858.7 40.666 87,187 NJTA.U!D ""---- ALTMETERwml20 FT MAR<NG,DW. WNDOW,2l1OOOFT 0.0 0.000 a lable:adc81tem6. USEDWNBT NAVCOM-- 0..0. 0.000 a CS PM.!XCWCE 0.2 1UOa 3 DGYRO!XCWCE 0.5 14.000 7 DUAL AXS ATOPLO\' 18.7 111.200 1,7117 DUALPUW,-1)tVEN V- SYSTEM 0.0. 0.000 a - LDCATCRTRANNTCR NSTL 0.0 a.doo a!ngn, l Yc:oNG 0.0. 0..000 a GYRO NSTALLATDN 0.0 0.000 a K.H 114GPS NSTALLATON 4.8 15.000 72 1OA2'81ACON1NTl. 0..0 0.000 a KT78C MOD!C TRAN&PONC!RNSTL 0..0. 0..000 a 1011511ANAVCOM#1NSTALLATON-NOGoS 0..0. a.doo a KX15ANAVCOMP2NSTALLATONWJG.e. 8.8 17.300 118 '41.:/310P81NAV&iJiCTCR.,,. - G.2 1.!OO 3 -. 3f CONTRCt. WH!!L. - 0..2 211.000 5 0.0 0.000 a Wll'UFAeRC 85A18 0..0. 0.000 a WHE&L PARNG NBTALLATON 18.5 411.100 1111 t'r0p!uer-.ccau\.&y, FXEDPTCH,1C23M.FA78'ro ===::=:==~=: Weighed: 4Zt.ZOO3-6f7f1.OO3.1 -"" --"'-.....,-...----..."'--- --...- to -, "...- - """'-"-' "",",*-_'101 BA8lCMPTY- -- U8!'.UW) oo,li3 MAXMUMTAMoO'r- -... ;...