-... S2100 ~ LOADED AIRPLANE MOMENT/1000 (POUND-INCHES) ~ z :5 8: 1900 CESSNA MODEL172R. '{j)2300 c z 1050I. 950 I- :r: W 900 3: w.

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1 MODEL172R SECTON 6 WEGHT & BALANCE EQUPMENT LST '{j)2300 c z a S2100 [j ~ 2000 z :5 8: 1900 «ffi ~ illl m '~11111l1!nT U ~ LOADED ARPLANE MOMENT/1000 (POUND-NCHES) 1050 ' J :r: 0 W 900 3: w 850 ~ a: < w ~ 750..J. Figure 6-7. Center of Gravity Moment Envelope 0585C1007 Feb 28/

2 SECTON 6 WEGHT & BALANCE / EQUPMENT LST LOAD MOMENT/1000 (KLOGRAM. MLLMETERS) U"",,1'"1'"1 d t""1 t.,...", 400 ~ ~ ~300, e!) W 250 3:..., 175 ~ ~ 150 e!) 9 S2-125!i: e!) jjj 100 3:, 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

3 SECTON 5 STALL SPEEDS AT 2450 POUNDS Conditions: Power Off FLAP SETTN' MOST REARWARD CENTER OF GRAVTY KAS ANGLE OF BANK KCAS KJAS KCAS KJAS KCAS KAS KCAS UP FLAP SETTNr.! MOST FORWARD CENTER OF GRAVTY ANGLE OF BANK , KJAS KCAS KAS KCAS KAS KCAS KfAS KCAS UP 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

4 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 , : , 236f) ' Short field technique as specified in Section 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

5 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 , ' NOTE: , 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

6 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 ; '" , ,000 69,.aQO " NOTE: 1. Mixtureleaned above3000 feet for maximum RPM. Figure 5~6. Maximum Rate of Climb' Dee 2/

7 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 ::::) <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:, ENDURANCE. HRS NOTE: 1. Thischart allowsfor the fuel used for engine start. taxi, takeoff and climb,and the timeduringclimb...., Figure Endurance Profile 8 "5-20 Feb 28/97

8 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 ; 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 Short Field Landing Dist,ance Revision8 5-21/5-22

9 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 ; 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 Short FieldLandingDist~nce Revision8 5-21/5-22

10 SECTON 5 CRUSE CONDTONS: 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 , ' , , 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

11 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"""""'~"'"~-'"-""" !- L, SL 550 Hi.113 KTAS.108 KTAS' 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/

12 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». / Basic EmptyWeight (Use the data pertainin to your airplane as t s r,resently ncludes unusable equipped. fuel and full 011) Usable Fuel (At 6 Lbs.lGal.) 53 Gallons Maximum 35 Gallons (To reduced fuel ndicator tab) Pilot and Front Passenger (Station 34 to 46) RearPassengers *Baggage Area 1 (Station 82 to 108; 120 Lbs. Max.) *Baggage Area 2 (Station 108 to 142;50 Lbs. Max.) 7. RAM WEGHT AND MOMENT (add columns) Fuel allowance for engine start, taxi and runup w TAKEOFF WEGHT AND 1105' MOMENT 8 from Step()btract 7 Step Locate this point (2450 at 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

13 , (.- WEGHT & BALANCE AND NSTALLED EQUPMENT DATA CEBSmARCRAFT COMPANY ~ SNGLEENGNEDM8ON Ce8iii REGlllTRA1OH -.T -- ARM milt 172t18l' 1'- \lol (lltl...-, ( 8T- EllPn'W!Of1' ,187 NJTA.U!D ""---- ALTMETERwml20 FT MAR<NG,DW. WNDOW,2l1OOOFT a lable:adc81tem6. USEDWNBT NAVCOM a CS PM.!XCWCE 0.2 1UOa 3 DGYRO!XCWCE DUAL AXS ATOPLO\' ,7117 DUALPUW,-1)tVEN V- SYSTEM a - LDCATCRTRANNTCR NSTL 0.0 a.doo a!ngn, l Yc:oNG a GYRO NSTALLATDN a K.H 114GPS NSTALLATON OA2'81ACON1NTl a KT78C MOD!C TRAN&PONC!RNSTL a ANAVCOM#1NSTALLATON-NOGoS a.doo a KX15ANAVCOMP2NSTALLATONWJG.e '41.:/310P81NAV&iJiCTCR.,,. - G.2 1.!OO f CONTRCt. WH!!L a Wll'UFAeRC 85A a WHE&L PARNG NBTALLATON t'r0p!uer-.ccau\.&y, FXEDPTCH,1C23M.FA78'ro ===::=:==~=: Weighed: 4Zt.ZOO3-6f7f1.OO3.1 -"" --"'-....., "' to -, " """'-"-' "",",*-_'101 BA8lCMPTY- -- U8!'.UW) oo,li3 MAXMUMTAMoO'r ;...