poh factsheet
TRANSCRIPT
-
8/2/2019 Poh Factsheet
1/3
POH FACTSHEET
Max sea level speed: 110ktsMax cruise speed at 8000ft: 107ktsStall speed flaps up: 48 ktsStall speed flaps down: 43kts
Max weight: 1670lbs.Empty weight: 1081lbs (152), 1118lbs (152II)Useful load: 589 lbs (152), 552lbs (152II)Fuel capacity: 26GAL/39GAL (long range)Oil capacity sump: 6QTS.Engine: O-235-L2CEngine: 110BHP at 2550RPM.
Dimensions:Length: 24-1Height: 8-6Tail width: 10-0Wing span: 33-4Prop diameter: 5-9: min 67.5 in, max 69 inGear width: 7-7 1/4
Fuel: AVGAS 100LL/AVGAS 100.Standard tanks: total 26, each tank 13 gal, usable 24.5Long range tanks: total 39 gal, each tank 19.5, usable 37.5Oil:25psi = red line.
60-90psi: green arcMaximum pressures: 100psi.Temperature: green arc: 100-245F (38-118C), max 118C (245F)MIL-L-6082Total capacity: 7 quarts when oil filter is installed. Otherwise: 6 in the sump.Minimum capacity to fly: 4QTS. When flying >3hrs: 6qts.
MTOM: 1670lbs.MLM: 1670lbs.Baggage area 1: 120lbs.Baggage area 2: 40lbs.
Standard empty weight: 1081 lbs (152), 1118 (152II)
Wing loading: 10.5lbs/sq.ft.Power loading: 15.2lbs/hp.
Speed limitationsVne: 145KCAS, 149KIASVno: 108KCAS, 111KIASVa:1670lbs: 101KCAS, 104KIAS1500lbs: 96KCAS, 98KIAS1350lbs: 91KCAS, 93KIASVfe: 87KCAS, 85KIASWindow open speed: 139KCAS, 143KIAS
-
8/2/2019 Poh Factsheet
2/3
Arcs:White: 35-85Green: 40-111Yellow: 111-149Red line: 149.
Minimum oil pressure: 25psiMaximum oil pressure: 100psi.
CofG ranges: 31 inches aft of datum through 36.5 inches aft of datum.
Manoevre entry speed (for all manoevres): 95kts.
Landing without engine power:Flaps up: 65 KIASFlaps down: 60KIAS
Take-off:Climb out speed: 65-75KIASShort field take-off: 54KIASClimbing:Flaps up: 70-80KIASBest ROC (Vy): 67KIAS at MSLBest ROC (Vy): 61KIAS at 10000ft.Best AOC (Vx): 55KIASApproach:
Flaps down approach: 55-65ktsNormal flaps up: 60-70KIASShort field: 54KIASBalked landing: 55KIASCrosswind velocity: 12kts.
RPM green arc range: 1900-2550RPM, max 2550RPM.
Electrics:28V DC system, powered by a 60amp alternator.24volt, 14amphr battery
Vacuum system: provides the suction necessary to operate the attitude indicator anddirectional indicator.
Attitude indicator: 10, 20, 30, 60, 90.
Nose wheel tire pressure: 30psiMain wheel tire pressure: 21psi
Carbheat decrease in rpm: 150-200RPM.
Suction indicator: 4.6-5.4 inches of mercury.
Empty fuel tank: 0.75 remains in each tank.
-
8/2/2019 Poh Factsheet
3/3
Decrease in braking action: release the brake pedals and engage them positively.Minimum fuel amount: 2GAL
Forwards CG:31.0inch aft when 1350lbs32.65inch aft when 1670lbs.
Cessna 152: for utility category
Alternator check: 1700RPMStatic engine RPM: 2280-2380rpm
Minimum turning radius when using nosewheel steering: 248.Acciddental opening of the doors: up to 65kts.