N6389R
PA-28-140
Airworthiness Checklist
Completed by: __________________________________________________ Date: __/__/20__
Hobbs out: _________ Hobbs in: _________ Tach out: _________ Tach in: _________
Aircraft Documents
Last renewed: __/__/20__ Expires: __/__/20__
Last updated: __/__/20__
Aircraft Inspections
Last completed: __/__/20__ Expires: __/__/20__
Last completed: __/__/20__ Expires: __/__/20__
Tach time at last 100 hour: _______
Time remaining: _______
Last completed: __/__/20__ Expires: __/__/20__
Last completed: __/__/20__ Expires: __/__/20__
Battery replacement: 1 hour of cumulative use or 50% life
Expires: __/__/20__
Inspection: 12 calendar months
Last completed: __/__/20__ Expires: __/__/20__
Tach time at last 100 hour: _______
Time remaining: _______
Pilot Documents
Last renewed: __/__/20__ Expires: __/__/20__
Last renewed: __/__/20__ Expires: __/__/20__
Last renewed: __/__/20__ Expires: __/__/20__
Pilot Self Assessment
Squawks and Inop Equipment
___________________________________________________________
___________________________________________________________
___________________________________________________________
___________________________________________________________
Inoperative equipment checklist
Instructions: This sheet is to be completed before every flight. Ensure each item is checked off if acceptable or crossed out if not required. Leave items unchecked if you are unsure and ask your instructor when they become available. Circle unsatisfactory items for review with your instructor. Refer to Flight Circle for current aircraft squawks and the maintenance records for maintenance information
N6389R
PA-28-140
Weight & Balance
Last Revised: 7/2/24
Normal Category
Utility Category
Conversions and Equations
Weight x Arm = Moment
Total Moment / Total Weight = CG
Cruise gal/hour x Fuel Remaining = Endurance
Fuel Weight = ~6 lbs/gal
Oil Weight = ~1.875 lbs/quart
| Weight (lbs) x | Arm (inches) = | Moment (in-lbs) |
Departure Takeoff Distance to Clear 50 ft Obstacle | |
Destination Takeoff Distance to Clear 50 ft Obstacle | |
Cruise % Horsepower | |
Cruise Gal/Hour | |
Endurance at Top of Climb (Hours) | |
Glide Range at Cruising Altitude of ft | |
Departure Landing Distance to Clear 50 ft Obstacle | |
Destination Landing Distance to Clear 50 ft Obstacle | |
Aircraft Performance
Aircraft Empty Weight | 1267.57 | 85.56312 | 108457.3 |
Oil (8qts max) | | 32.5 | |
Front Seat Occupants | | 85.5 | |
Rear Seat Occupants | | 117 | |
Baggage (200lb max) | | 117 | |
Zero Fuel Weight and CG | | CG= | |
+ Required Fuel (288lbmax) | | 95 | |
Ramp Weight | | CG= | |
- Taxi & Runup Fuel | | 95 | |
Takeoff Weight | | CG = | |
- Fuel Used | | 95 | |
Landing Weight | | CG= | |