1. N269AR WEIGHT AND BALANCE SHEET
Date__________ Pilot_____________________ Instructor________________________
Longitudinal W/B Weight(lbs.) Arm Moment
Long. CG with Fuel:
Weight__________ Moment_____________
CG__________________
Long. CG “0” Fuel:
Long. CG Doors OFF:
Weight________ Moment_______________
Lat. CG with Fuel:
Weight_________ Moment______________
Lat. CG with “0” Fuel:
Doors Off Aircraft Empty Weight: 1191 LBs
Basic Empty W/T
Pilot ______________ _______________
Passenger RH ______________ _______________
Fuel ______________ _______________
“0” Fuel LBs 108.5
Totals ______________ _______________
Doors Off
LF Door LBS
RF Door LBS
Total LBS ______
Lateral W/B Weight(LBS) Arm Moment
Basic Empty W/T
Pilot ___________ ________________
Passenger ___________ 13.8 ________________
Fuel ___________ 18.0 ________________
“0” Fuel LBS ________________
Totals: ___________ ________________
Longitudinal Limit: 95.0 to 101.0
Lateral Limits: At to -2.12
At to -2.5
Max Weight 2050

2. N717CN WEIGHT AND BALANCE SHEET
Date__________ Pilot_____________________ Instructor________________________
Longitudinal W/B Weight(lbs.) Arm Moment
Long. CG with Fuel:
Weight__________ Moment_____________
CG__________________
Long. CG “0” Fuel:
Long. CG Doors OFF:
Weight________ Moment_______________
Lat. CG with Fuel:
Weight_________ Moment______________
Lat. CG with “0” Fuel:
Doors Off Aircraft Empty Weight: 1191 LBs
Basic Empty W/T
Pilot ______________ _______________
Passenger RH ______________ _______________
Fuel ______________ _______________
“0” Fuel LBs 107.0
Totals ______________ _______________
Doors Off
LF Door LBS
RF Door LBS
Total LBS ______
Lateral W/B Weight(LBS) Arm Moment
Basic Empty W/T
Pilot ___________ ________________
Passenger ___________ 13.8 ________________
Fuel ___________ 18.0 ________________
“0” Fuel LBS ________________
Totals: ___________ ________________
Longitudinal Limit: 95.0 to 101.0
Lateral Limits: At to -2.12
At to -2.5
Max Weight 2050

3. N269L WEIGHT AND BALANCE SHEET
Date__________ Pilot_____________________ Instructor________________________
Longitudinal W/B Weight(lbs.) Arm Moment
Long. CG with Fuel:
Weight__________ Moment_____________
CG__________________
Long. CG “0” Fuel:
Long. CG Doors OFF:
Weight________ Moment_______________
Lat. CG with Fuel:
Weight_________ Moment______________
Lat. CG with “0” Fuel:
Aircraft Empty Weight Doors Off: 1184 LBs
Basic Empty W/T
Pilot ______________ _______________
Passenger RH ______________ _______________
Fuel ______________ _______________
“0” Fuel LBs 108.5
Totals ______________ _______________
Doors Off
LF Door LBS
RF Door LBS
Total LBS ______
Lateral W/B Weight(LBS) Arm Moment
Basic Empty W/T
Pilot ___________ ________________
Passenger ___________ 13.8 ________________
Fuel ___________ 18.0 ________________
“0” Fuel LBS ________________
Totals: ___________ ________________
Longitudinal Limit: 95.0 to 101.0
Lateral Limits: At to -2.12
At to -2.5
Max Weight 2050

4. N2070J WEIGHT AND BALANCE SHEET
Date__________ Pilot_____________________ Instructor________________________
Long. CG with Fuel:
Weight__________ Moment_____________
CG__________________
Long. CG “0” Fuel:
Long. CG Doors OFF:
Weight________ Moment_______________
Lat. CG with Fuel:
Weight_________ Moment______________
Lat. CG with “0” Fuel:
Aircraft Empty Weight Doors Off:
Longitudinal W/B Weight(lbs.) Arm Moment
Basic Empty W/T
Pilot ______________ _______________
Passenger RH ______________ _______________
Fuel ______________ _______________
“0” Fuel LBs 108.5
Totals ______________ _______________
Doors Off
LF Door LBS
RF Door LBS
Total LBS ______
Lateral W/B Weight(LBS) Arm Moment
Basic Empty W/T
Pilot ___________ ________________
Passenger ___________ 13.8 ________________
Fuel ___________ 18.0 ________________
“0” Fuel LBS ________________
Totals: ___________ ________________
Longitudinal Limit: 95.0 to 101.0
Lateral Limits: At to -2.12
At to -2.5
Max Weight 2050

5. N396CP WEIGHT AND BALANCE SHEET
Date__________ Pilot_____________________ Instructor________________________
Long. CG with Fuel:
Weight__________ Moment_____________
CG__________________
Long. CG “0” Fuel:
Long. CG Doors OFF:
Weight________ Moment_______________
Lat. CG with Fuel:
Weight_________ Moment______________
Lat. CG with “0” Fuel:
Aircraft Empty Weight Doors Off: 1189 LBs
Longitudinal W/B Weight(lbs.) Arm Moment
Basic Empty W/T
Pilot ______________ _______________
Passenger RH ______________ _______________
Fuel ______________ _______________
“0” Fuel LBs 108.5
Totals ______________ _______________
Doors Off
LF Door LBS
RF Door LBS
Total LBS _____
Lateral W/B Weight(LBS) Arm Moment
Basic Empty W/T
Pilot ___________ ________________
Passenger ___________ 13.8 ________________
Fuel ___________ 18.0 ________________
“0” Fuel LBS ________________
Totals: ___________ ________________
Longitudinal Limit: 95.0 to 101.0
Lateral Limits: At to -2.12
At to -2.5
Max Weight 2050

6. N717CN WEIGHT AND BALANCE SHEET
Date__________ Pilot_____________________ Instructor________________________
Long. CG with Fuel:
Weight__________ Moment_____________
CG__________________
Long. CG “0” Fuel:
Long. CG Doors OFF:
Weight________ Moment_______________
Lat. CG with Fuel:
Weight_________ Moment______________
Lat. CG with “0” Fuel:
Aircraft Empty Weight Doors Off: 1144 LBs
Longitudinal W/B Weight(LBs.) Arm Moment
Basic Empty W/T
Pilot ______________ _______________
Passenger RH ______________ _______________
Fuel ______________ _______________
“0” Fuel LBs 108.5
Totals ______________ _______________
Doors Off
LF Door LBS
RF Door LBS
Total LBS ______
Lateral W/B Weight(LBs) Arm Moment
Basic Empty W/T
Pilot ___________ ________________
Passenger ___________ 13.8 ________________
Fuel ___________ 18.0 ________________
“0” Fuel LBS ________________
Totals: ___________ ________________
Longitudinal Limit: 95.0 to 101.0
Lateral Limits: At to -2.12
At to -2.5
Max Weight 2050

8. WEIGHT and BALANCE - DOORS OFF N144TG
Date__________ Pilot______________ Instructor_______________
Longitudinal (From Page 1)
Total Weight_______________ Total Moment__________________
Weight Arm Moment
LF F/W/D LBs___________ ________________
RT F/W/D LBs___________ ________________
LF Aft/D LBs___________ ________________
RT Aft/D LBs___________ ________________
Total W/T Change ___________ Total M/T Change_______________
TOTAL W/T _________________ TOTAL M/T____________________
C/G _____________
Lateral (From Page 1)
Total Weight _______________ Total Moment__________________ Weight Arm Moment
LF F/W/D LBs __________ ________________
RT F/W/D LBs __________ ________________
LF Aft/D LBs __________ ________________
RT Aft/D LBs __________ ________________
Total W/T Change ___________ Total M/T Change________________
TOTAL W/T _________________ TOTAL M/T_____________________

10. WEIGHT and BALANCE - DOORS OFF N155MG
Date__________ Pilot______________ Instructor_______________
Longitudinal (From Page 1)
Total Weight_______________ Total Moment__________________
Weight Arm Moment
LF F/W/D LBs___________ ________________
RT F/W/D LBs___________ ________________
LF Aft/D LBs___________ ________________
RT Aft/D LBs___________ ________________
Total W/T Change ___________ Total M/T Change_______________
TOTAL W/T _________________ TOTAL M/T____________________
C/G _____________
Lateral (From Page 1)
Total Weight _______________ Total Moment__________________ Weight Arm Moment
LF F/W/D LBs __________ ________________
RT F/W/D LBs __________ ________________
LF Aft/D LBs __________ ________________
RT Aft/D LBs __________ ________________
Total W/T Change ___________ Total M/T Change________________
TOTAL W/T _________________ TOTAL M/T_____________________

11. PRESSURE ALTITUDE_________ TEMPERATUR (F)__________
VNE__________________
(Max VNE 95 Knots, 109 mph, Doors Off 89 Knots 102 mph)
Rough Celsius to Fahrenheit Conversion:
________ C x = __________F (+/- 2 to 3 degrees)
Long. _______________ Lateral________________
Long________________ Lateral________________

12. OGE
IGE

14. Density Altitude Chart
DENSITY ALTITUDE FORMULA (estimate)
PRESSURE ALTITUDE
STD Pressure (29.92) – Current pressure________ (+/-)=____________
X 1000 = ____________+ Field Elevation(5016) =_______________(PA)
DENSITY ALTUTUDE
Current Temp. _______ - STD Temp__________ x 120 =____________
+ Pressure Altitude (PA) = __________________