24
This cruise altitude will yield a range of 875 miles
Following the same sequence for a flight at 8,000 feet with 140
gallons of fuel, a groundspeed of 165 and fuel burn of 27 gallons per
hour, a specific range of 855.6 is calculated. An additional 20 miles of
range is available at 12,000 feet.
APPENDIX A
SAMPLE PROBLEMS
TIME
4:45:00 + 2:15:30 = 07:00:30
6.7 - 5:20:00 = 01:22:00
CONVERSIONS
25 pounds to kilograms
11.3398
12 kilograms to pounds
26.4554
30 feet to meters
9.144
100 meters to feet
328.083
32° Fahrenheit to Celsius
0°
100° Celsius to Fahrenheit
212°
100 nautical miles to kilometers
185.2
50 kilometers to nautical miles
26.9978
9.5125 decimal hrs to hms
9:30:45
12:30:30 hms to decimal hrs
12.5083
87 nautical miles to statute miles
100.117
115 statute miles to nautical miles
99.9324
1 U.S. gallon to liters
3.78541
10 liters to U.S. gallons
2.64172
WT/ARM
WT
ARM
MOM
GW
Empty
2467 76.7
189218
2467
RF 1
Fuel
444
75.0
222518
2911
Front seat
340
75.0
248018
3251
2nd row
0
115
3rd row
0
148
Baggage 100 164
264418
3351
CG = 78.91
APPENDIX A (cont.)
SAMPLE PROBLEMS
WT/MOM
Payload computations
ITEM WEIGHT
MOMENT
(pounds)
/1000
Basic operating weight
8916
2809.0
Cabin
140.
150.
24.
875.
FPH
(FLASHING) SPCRNG
GS
FUEL