Weight & Balance Sheet
ADVERTISEMENT
1CESSNA 152 WEIGHT & BALANCE SHEET
AIRPLANE C.G. LOCATION-MILLIMETERS AFT OF DATUM (STA. 0.0)
800
800
775
775
775
775
825
825
850
850
875
875
925
925
900
900
800
800
775
775
1700
1700
750
750
725
725
1600
1600
700
700
1500
1500
650
650
675
675
1400
1400
625
625
CENTER OF
CENTER OF
600
600
GRAVITY
GRAVITY
1300
1300
575
575
LIMITS
LIMITS
550
550
1200
1200
525
525
1100
1100
500
500
475
475
1000
1000
30
30
31
31
32
32
33
33
34
34
35
35
36
36
37
37
AIRPLANE C.G. LOCATION-INCHES AFT OF DATUM (STA. 0.0)
Figure 6-9. Center Of Gravity Limits
Item
Weight / Lbs
Arm / Ins
Moments lbs-ins
Basic Empty Weight
1224
(From Flight Manual)
×
31.5
Pilot + Pax
×
39.0
Baggage Area 1
×
64.0
Baggage Area 2
×
84.0
×
42.2
Useable Fuel
Max
22.5 US gall
Take Off Weight
Max
Fuel Burn Of US Gall
×
42.2
Landing Weight
1. Take Off
CG = Take Off Moments ÷ Take Off Weight = ____________ ins AFT
2. Landing
CG = Landing Moments ÷ Landing Weight = ____________ ins AFT
Locate Take Off CG & Landing CG on CG Envelope (Fig 6-9)
I certify that the aircraft is loaded in accordance with the AFM and is within its certified weights and
CG limits for Take Off and Landing.
Note :
Aircraft Registration : 9M - __________
Fuel 1 US Gal = 6 lbs
Fuel 1 US Gal = 3.785 Liters
1 kg = 2.2 lbs
1 lbs = 0.453 kg
___________________
________________
1 Nm = 1.852 km / 1 km = 0.539
Completed By (Name)
Sign
1 Feet = 0.304 m / 1 m = 3.280 Feet
1 Knots = 1.852 Km/h / 1 Km/h = 0.53 Knots
________________
Date / Time
ADVERTISEMENT
0 votes
Related Articles
Related forms
Related Categories
Parent category: Business