N269AR WEIGHT AND BALANCE SHEET

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Presentation transcript:

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 1203.0 101.54 121852.2 Pilot ______________ 83.2 _______________ Passenger RH ______________ 83.2 _______________ Fuel ______________ 108.5 _______________ “0” Fuel 6 LBs 108.5 Totals ______________ _______________ Doors Off LF Door -6 LBS 74.0 -444 RF Door -6 LBS 74.0 -444 Total -12 LBS -888 ______ Lateral W/B Weight(LBS) Arm Moment Basic Empty W/T 1203.0 .039 228.4 Pilot ___________ -13.8 ________________ Passenger ___________ 13.8 ________________ Fuel ___________ 18.0 ________________ “0” Fuel 6 LBS 18.0 ________________ Totals: ___________ ________________ Longitudinal Limit: 95.0 to 101.0 Lateral Limits: At 99.5 +4 to -2.12 At 101.0 +2 to -2.5 Max Weight 2050

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 1157.0 100.82 116648.74 Pilot ______________ 83.2 _______________ Passenger RH ______________ 83.2 _______________ Fuel ______________ 107.0 _______________ “0” Fuel 6 LBs 107.0 Totals ______________ _______________ Doors Off LF Door -6 LBS 74.0 -444 RF Door -6 LBS 74.0 -444 Total -12 LBS -888 ______ Lateral W/B Weight(LBS) Arm Moment Basic Empty W/T 1157.0 .024 277.48 Pilot ___________ -13.8 ________________ Passenger ___________ 13.8 ________________ Fuel ___________ 18.0 ________________ “0” Fuel 6 LBS 18.0 ________________ Totals: ___________ ________________ Longitudinal Limit: 95.0 to 101.0 Lateral Limits: At 99.5 +4 to -2.12 At 101.0 +2 to -2.5 Max Weight 2050

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 1196.0 101.8 121745.6 Pilot ______________ 83.2 _______________ Passenger RH ______________ 83.2 _______________ Fuel ______________ 108.5 _______________ “0” Fuel 6 LBs 108.5 Totals ______________ _______________ Doors Off LF Door -6 LBS 74.0 -444 RF Door -6 LBS 74.0 -444 Total -12 LBS -888 ______ Lateral W/B Weight(LBS) Arm Moment Basic Empty W/T 1196.0 .20 248 Pilot ___________ -13.8 ________________ Passenger ___________ 13.8 ________________ Fuel ___________ 18.0 ________________ “0” Fuel 6 LBS 18.0 ________________ Totals: ___________ ________________ Longitudinal Limit: 95.0 to 101.0 Lateral Limits: At 99.5 +4 to -2.12 At 101.0 +2 to -2.5 Max Weight 2050

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: 1232.16 Longitudinal W/B Weight(lbs.) Arm Moment Basic Empty W/T 1244.16 99.59 123905.89 Pilot ______________ 83.2 _______________ Passenger RH ______________ 83.2 _______________ Fuel ______________ 108.5 _______________ “0” Fuel 6 LBs 108.5 Totals ______________ _______________ Doors Off LF Door -6 LBS 74.0 -444 RF Door -6 LBS 74.0 -444 Total -12 LBS -888 ______ Lateral W/B Weight(LBS) Arm Moment Basic Empty W/T 1244.16 -0.26 -323.48 Pilot ___________ -13.8 ________________ Passenger ___________ 13.8 ________________ Fuel ___________ 18.0 ________________ “0” Fuel 6 LBS 18.0 ________________ Totals: ___________ ________________ Longitudinal Limit: 95.0 to 101.0 Lateral Limits: At 99.5 +4 to -2.12 At 101.0 +2 to -2.5 Max Weight 2050

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 1203.2 100.25 120620.8 Pilot ______________ 83.2 _______________ Passenger RH ______________ 83.2 _______________ Fuel ______________ 108.5 _______________ “0” Fuel 6 LBs 108.5 Totals ______________ _______________ Doors Off LF Door -7.2LBS 74.0 -532.8 RF Door -7.2 LBS 74.0 -532.8 Total -14.2 LBS -1065.6 _____ Lateral W/B Weight(LBS) Arm Moment Basic Empty W/T 1203.2 .060 721.92 Pilot ___________ -13.8 ________________ Passenger ___________ 13.8 ________________ Fuel ___________ 18.0 ________________ “0” Fuel 6 LBS 18.0 ________________ Totals: ___________ ________________ Longitudinal Limit: 95.0 to 101.0 Lateral Limits: At 99.5 +4 to -2.12 At 101.0 +2 to -2.5 Max Weight 2050

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 1157.0 100.82 116648.74 Pilot ______________ 83.2 _______________ Passenger RH ______________ 83.2 _______________ Fuel ______________ 108.5 _______________ “0” Fuel 6 LBs 108.5 Totals ______________ _______________ Doors Off LF Door -6 LBS 74.0 -444 RF Door -6 LBS 74.0 -444 Total -12 LBS -888 ______ Lateral W/B Weight(LBs) Arm Moment Basic Empty W/T 1157.0 .24 277.48 Pilot ___________ -13.8 ________________ Passenger ___________ 13.8 ________________ Fuel ___________ 18.0 ________________ “0” Fuel 6 LBS 18.0 ________________ Totals: ___________ ________________ Longitudinal Limit: 95.0 to 101.0 Lateral Limits: At 99.5 +4 to -2.12 At 101.0 +2 to -2.5 Max Weight 2050

WEIGHT and BALANCE - DOORS OFF N144TG Date__________ Pilot______________ Instructor_______________ Longitudinal (From Page 1) Total Weight_______________ Total Moment__________________ Weight Arm Moment LF F/W/D - 7.5 LBs___________ 49.4 -369.00 ________________ RT F/W/D -7.5 LBs___________ 49.4 -369.00 ________________ LF Aft/D -7.0 LBs___________ 75.4 -527.80 ________________ RT Aft/D -7.0 LBs___________ 75.4 -527.80 ________________ 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 - 7.5 LBs __________ -24.0 -180.00________________ RT F/W/D -7.5 LBs __________ +24.0 +180.00________________ LF Aft/D -7.0 LBs __________ -23.0 -161.00________________ RT Aft/D -7.0 LBs __________ +23.0 +161.00________________ Total W/T Change ___________ Total M/T Change________________ TOTAL W/T _________________ TOTAL M/T_____________________

WEIGHT and BALANCE - DOORS OFF N155MG Date__________ Pilot______________ Instructor_______________ Longitudinal (From Page 1) Total Weight_______________ Total Moment__________________ Weight Arm Moment LF F/W/D - 7.5 LBs___________ 49.4 -369.00 ________________ RT F/W/D -7.5 LBs___________ 49.4 -369.00 ________________ LF Aft/D -7.0 LBs___________ 75.4 -527.80 ________________ RT Aft/D -7.0 LBs___________ 75.4 -527.80 ________________ 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 - 7.5 LBs __________ -24.0 -180.00________________ RT F/W/D -7.5 LBs __________ +24.0 +180.00________________ LF Aft/D -7.0 LBs __________ -23.0 -161.00________________ RT Aft/D -7.0 LBs __________ +23.0 +161.00________________ Total W/T Change ___________ Total M/T Change________________ TOTAL W/T _________________ TOTAL M/T_____________________

PRESSURE ALTITUDE_________ TEMPERATUR (F)__________ VNE__________________ (Max VNE 95 Knots, 109 mph, Doors Off 89 Knots 102 mph) Rough Celsius to Fahrenheit Conversion: ________ C x 2 + 30 = __________F (+/- 2 to 3 degrees) Long. _______________ Lateral________________ Long________________ Lateral________________

OGE IGE

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) = __________________