#	Piper PA-28-235 Cherokee — Eric_Duensing_pa28_235_wb
#	NOT FOR FLIGHT — source fidelity: unreviewed | operational review: none | completeness: full
#	Source: Piper/PA-28-235 Cherokee/Eric_Duensing_pa28_235_wb.txt
#	Rights: licensed
#	Checklist hash: cbd96a36ddb4178466ecd707449bcae23d809111c7119fb137a0e54c8e14c47c
#	Verify against the aircraft's own approved documentation before use.
section_id	phase	criticality	section_title	item_index	item_id	type	tickable	memory_item	indent	text	response	condition	detail
	weight_and_balance	normal	Weight & Balance	0		note	no	no	0	INSTRUCTIONS: FILL OUT ALL NUMBERS IN BLUE. BLACK NUMBERS GIVE YOU THE ANSWER.			
	weight_and_balance	normal	Weight & Balance	1		note	no	no	0	WEIGHT AND BALANCE — DO NOT DELETE THE DATA IN RED			
	weight_and_balance	normal	Weight & Balance	2		subtitle	no	no	0	Item / Weight / Arm / Moment			
	weight_and_balance	normal	Weight & Balance	3		action	yes	no	0	Basic Empty Weight	1530.76 lb, Arm 83.11, Moment 127220		
	weight_and_balance	normal	Weight & Balance	4		action	yes	no	0	Pilot	200 lb, Arm 88.9, Moment 17780		
	weight_and_balance	normal	Weight & Balance	5		action	yes	no	0	Co-Pilot	0 lb, Arm 88.9, Moment 0		
	weight_and_balance	normal	Weight & Balance	6		action	yes	no	0	Rear Seats	0 lb, Arm 118.5, Moment 0		
	weight_and_balance	normal	Weight & Balance	7		action	yes	no	0	Baggage (200 lb max)	0 lb, Arm 142, Moment 0		
	weight_and_balance	normal	Weight & Balance	8		action	yes	no	0	Fuel (in gallons)	84 gal, 504 lb, Arm 95, Moment 47880		
	weight_and_balance	normal	Weight & Balance	9		action	yes	no	0	TAKEOFF	Weight 2234.76 lb, C.G. 86.30904437165512 in, Moment 192880		
	weight_and_balance	normal	Weight & Balance	10		action	yes	no	0	LANDING	Weight 1808.7600000000002 lb, C.G. 84.26214644286692 in, Moment 152410		
	weight_and_balance	normal	Weight & Balance	11		action	yes	no	0	MAX GROSS WEIGHT	2900 lb		
	weight_and_balance	normal	Weight & Balance	12		subtitle	no	no	0	C.G. vs Weight limits			
	weight_and_balance	normal	Weight & Balance	13		challenge	yes	no	0	Takeoff C.G.: 86.30904437165512 in at 2234.76 lb			
	weight_and_balance	normal	Weight & Balance	14		challenge	yes	no	0	Landing C.G.: 84.26214644286692 in at 1808.7600000000002 lb			
	weight_and_balance	normal	Weight & Balance	15		challenge	yes	no	0	Normal: 83 in / 1400 lb, 83 in / 2100 lb, 91.55 in / 2900 lb, 93 in / 2900 lb			
	weight_and_balance	normal	Weight & Balance	16		challenge	yes	no	0	Utility: 83 in / 1400 lb, 83 in / 1950 lb, 83.7 in / 2020 lb, 93 in / 2020 lb, 93 in / 1400 lb			
	weight_and_balance	normal	Weight & Balance	17		action	yes	no	0	Fuel (Taxi, Climb)	1 gal		
	weight_and_balance	normal	Weight & Balance	18		action	yes	no	0	Fuel Burn	14 gal/hr		
	weight_and_balance	normal	Weight & Balance	19		action	yes	no	0	Planned Flight Time	5 hrs		
	weight_and_balance	normal	Weight & Balance	20		action	yes	no	0	Estimated Fuel Used	71 gal		
	weight_and_balance	normal	Weight & Balance	21		action	yes	no	0	Estimated Fuel Remaining	13 gal		
	weight_and_balance	normal	Weight & Balance	22		action	yes	no	0	Estimated Time Remaining	0.9285714285714286 hrs		
	performance	normal	Computations	0		subtitle	no	no	0	TEMPERATURE			
	performance	normal	Computations	1		action	yes	no	0	Enter oC:	29		
	performance	normal	Computations	2		action	yes	no	0	Get oF:	84.2		
	performance	normal	Computations	3		subtitle	no	no	0	DENSITY ALTITUDE			
	performance	normal	Computations	4		action	yes	no	0	Field Elevation — Departure	295		
	performance	normal	Computations	5		action	yes	no	0	Field Elevation — Arrival	295		
	performance	normal	Computations	6		action	yes	no	0	Altimeter Setting — Departure	29.95		
	performance	normal	Computations	7		action	yes	no	0	Altimeter Setting — Arrival	30.21		
	performance	normal	Computations	8		action	yes	no	0	Temp, deg F — Departure	86		
	performance	normal	Computations	9		action	yes	no	0	Temp, deg F — Arrival	86		
	performance	normal	Computations	10		action	yes	no	0	Std Temp at Field — Departure	56		
	performance	normal	Computations	11		action	yes	no	0	Std Temp at Field — Arrival	40.268		
	performance	normal	Computations	12		action	yes	no	0	Pressure Altitude — Departure	324.9999999999976		
	performance	normal	Computations	13		action	yes	no	0	Pressure Altitude — Arrival	584.9999999999991		
	performance	normal	Computations	14		action	yes	no	0	Density Altitude — Departure	2324.9999999999977		
	performance	normal	Computations	15		action	yes	no	0	Density Altitude — Arrival	3633.7999999999993		
	performance	normal	Computations	16		subtitle	no	no	0	WEIGHT-ADJUSTED V-SPEEDS (KIAS)			
	performance	normal	Computations	17		action	yes	no	0	Vso — MGW	60		
	performance	normal	Computations	18		action	yes	no	0	Vso — Your weight	52.6705309218182		
	performance	normal	Computations	19		action	yes	no	0	1.2 x Vso — MGW	72		
	performance	normal	Computations	20		action	yes	no	0	1.2 x Vso — Your weight	63.204637106181835		
	performance	normal	Computations	21		action	yes	no	0	1.3 x Vso — MGW	78		
	performance	normal	Computations	22		action	yes	no	0	1.3 x Vso — Your weight	68.47169019836366		
	performance	normal	Computations	23		action	yes	no	0	Vx — MGW	90		
	performance	normal	Computations	24		action	yes	no	0	Vx — Your weight	79.0057963827273		
	performance	normal	Computations	25		action	yes	no	0	Best glide — MGW	80		
	performance	normal	Computations	26		action	yes	no	0	Best glide — Your weight	70.22737456242426		
	performance	normal	Computations	27		action	yes	no	0	Vy — MGW	100		
	performance	normal	Computations	28		action	yes	no	0	Vy — Your weight	87.78421820303033		
	performance	normal	Computations	29		action	yes	no	0	Vfe — MGW	115		
	performance	normal	Computations	30		action	yes	no	0	Vfe — Your weight	100.95185093348488		
	performance	normal	Computations	31		action	yes	no	0	Va — MGW	111		
	performance	normal	Computations	32		action	yes	no	0	Va — Your weight	97.44048220536367		
	performance	normal	Computations	33		action	yes	no	0	Vno — MGW	126		
	performance	normal	Computations	34		action	yes	no	0	Vno — Your weight	110.60811493581821		
	performance	normal	Computations	35		action	yes	no	0	Vne — MGW	166		
	performance	normal	Computations	36		action	yes	no	0	Vne — Your weight	145.72180221703036		
	reference	normal	Old W&B	0		action	yes	no	0	Basic Empty Weight	Weight 1530.76, Arm 83.11, Moment 127221.4636		
	reference	normal	Old W&B	1		action	yes	no	0	Pilot	0		
	reference	normal	Old W&B	2		action	yes	no	0	Front Seat Passenger	0		
	reference	normal	Old W&B	3		action	yes	no	0	Rear Seat Passenger(s)	0		
	reference	normal	Old W&B	4		action	yes	no	0	Baggage (200lb Max)	0		
	reference	normal	Old W&B	5		action	yes	no	0	Fuel (gals x 6lbs.)	84		
	reference	normal	Old W&B	6		action	yes	no	0	Total	1614.76		
	reference	normal	Old W&B	7		challenge	yes	no	0	Total Moment / Total Weight = Center of Gravity in Inches			
	reference	normal	Old W&B	8		action	yes	no	0	Result	135350.1436 / 1614.76 = 83.82059476330849 (83-93)