N9879Q
CESSNA 172M
Airworthiness Checklist
Completed by: __________________________________________________ Date: __/__/20__
Hobbs out: _________ Hobbs in: _________ Tach out: _________ Tach in: _________
Aircraft Documents
Last renewed: __/__/20__ Experies: __/__/20__
Last updated: __/__/20__
Aircraft Inspections
Last completed: __/__/20__ Experies: __/__/20__
Last completed: __/__/20__ Experies: __/__/20__
Tach time at last 100 hour: _______
Time remaining: _______
Last completed: __/__/20__ Experies: __/__/20__
Last completed: __/__/20__ Experies: __/__/20__
Battery replacement: 1 hour of cumulative use or 50% life
Expires: __/__/20__
Inspection: 12 calendar months
Last completed: __/__/20__ Experies: __/__/20__
Tach time at last 100 hour: _______
Time remaining: _______
Pilot Documents
Last renewed: __/__/20__ Experies: __/__/20__
Last renewed: __/__/20__ Experies: __/__/20__
Last renewed: __/__/20__ Experies: __/__/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
N9879Q
CESSNA 172M
Weight & Balance
Last Revised: 6/13/2024
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) |
Aircraft Empty Weight | 1443 | 39.2 | 56597.01 |
Oil (15lb max) | | -13.33333333 | |
Front Seat Occupants (34-46) | | 37 | |
Rear Seat Occupants | | 73 | |
Baggage (120lb max) | | 95 | |
Baggage area 2 (50lb max) | | 123 | |
Zero Fuel Weight and CG | | CG = | |
+ Usable Fuel (228lb max) | | 48 | |
Full Fuel Weight | | CG = | |
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
- Fuel Used | | 48 | |
Takeoff Weight | | CG = | |
- Fuel Used | | 48 | |
Landing Weight | | CG = | |