AIRWORTHINESS

CHECKLIST
Completed By:____________________________ Date:_________________ N-Number:_________________
Documents Out Hobbs:______________________ In Hobbs:________________________
Airworthiness Certificate (91.203(a)(1)) Off Hobbs:______________________ On Hobbs:_______________________
Registration Certificate (91.203(a)(2)) Expiration Date: _____________ “Airworthy” means an aircraft and component parts meet its type design (or properly altered configuration)
Radio Station License (47 CFR 87.18) - if flying outside US and is in a condition for safe operation. (Ref: FAR 21.31, FAR 21.41, FAR 21.183)
Operating Handbook (91.9(b)) Airworthiness Directives (Part 39)
Weight & Balance (23.2620) (official - in POH/AFM)
List available at
External Data Plate (45.11) https://www.faa.gov/regulations_policies/airworthiness_directives/
Compass Deviation Card (not required in G1000 Archer w/ Aspen EBD) Applicable ADs and compliance listed in MX Summary sheet and FAA
Offset Airworthiness Directives Compliance Record sheets
Recent compliance actions in maintenance logs
Total AC Time at most recent 100-hr: _____________ To verify recurring AD currency (if required):
(-) Off/On Hobbs at most recent 100-hr: _____________ Total AC Time at next due (from MX summary): _____________
(=) Offset: _____________ (-) Offset: _____________
Inspections (=) Off/On Hobbs at next due: _____________

Annual (91.409(a)) - 12 calendar months Form 337s (Part 43 Appendix B)

Most recent: _____________ Next due: _____________ Required for major repairs and alterations (in Appendix A)
VOR equipment check (91.171) - 30 days (if using VOR for IFR flight) Review MX Blue Book for any 337s present
Most recent: _____________ Next due: _____________
Inoperative Equipment (91.213(d))
100-hour (91.409(b)) - 100 flight hours less previous overflight
Total AC Time at next due (from MX summary): _____________ List inoperative equipment: _______________________________________________
(-) Offset (taken from above section): _____________ ________________________________________________________________________
(=) Off/On Hobbs: _____________ ________________________________________________________________________
(-) Current Off/On Hobbs: _____________ ________________________________________________________________________
(=) Hours left to 100-hour: _____________ If any inop equipment present, verify:
Altimeter / Static / Encoder (91.411) - 24 calendar months (for IFR flight) Not required by
Most Recent: _____________ Next due: _____________ 91.205(b) (day VFR), (c) (night VFR) and/or (d) (IFR)
Transponder (91.413) - 24 calendar months (if using transponder) Equipment list in POH/AFM
Most Recent: _____________ Next due: _____________ Airworthiness directive
ELT (91.207) Deactivated and placarded “Inoperative”, OR…
Battery replacement - 1 hr use or 50% life Removed, control placarded, and maintenance recorded
Next due: _____________ PIC determines that inop equipment is not a hazard to the aircraft
Inspection - 12 calendar months
Most Recent: _____________ Next due: _____________

Revised 2019-06-21
 CESSNA 172 PIPER ARCHER
Weight & Balance Weight & Balance

Weight × Arm = Moment Specific ATP Aircraft Weight × Arm = Moment

Basic Empty Weight >>> Weight & Balance Info <<< Basic Empty Weight
Front Pilots + + Front Pilots + 80.50 +
Important information specific to
Rear Passengers + + your N-Number, including Basic Rear Passengers + 118.10 +
Empty Weight and Moment, is
Baggage 120lbs. max + + Baggage 200lbs. max + 142.80 +
available on the ATP Student
Extranet and in the ATP Documents
Zero Fuel Weight = CG = folder in ForeFlight. Zero Fuel Weight = CG =
Usable Fuel + + Usable Fuel + 95.00 +

Ramp Weight = = Ramp Weight = =

Taxi Fuel – – Taxi Fuel – 8 95.00 – 760

Takeoff Weight = CG = Takeoff Weight = CG =

Fuel Burn – – Fuel Burn – –

Landing Weight = CG = Landing Weight = CG =

Sign in to your Student Extranet

Performance 2600
account. Go to Library > Archer Performance
Short Field
2500 Aircraft Information Manuals 88
89 90 91 92 93
Takeoff
Takeoff Distance 2400
> Aircraft Quick Reference, 2500
87 Performance
Ground Roll 50ft Obst. and enter the N-Number of the 2400 86 Flaps Up Flaps 25°
2300 aircraft you are flying.
Normal 2300 85
2200
Category 84
2200
2100 83
Short Field 2100 UTILITY CATEGORY
Landing Distance 2000 82
Engine Performance:
Formulas 2000
Ground Roll 50ft Obst. 1900
Utility
• Weight x Arm = Moment

Aircraft Weight -Lbs.

1900
1800 Category
• Total Moment ÷ Total Weight 1800
1700 Glide Range:
= Center of Gravity (CG) 1700
1600
• Max Ramp Weight – Zero Fuel 1600

172R 1500 Weight

1500
34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 = Usable Fuel Weight
Landing
172S CG Location • Fuel Weight ÷ 6 = Fuel Gallons
1400 Performance
1300 Dep. APT Dest. APT
• 100 LL (Blue) Fuel Weighs 6 lbs./gal.
1200 82 83 84 85 86 87 88 89 90 91 92 93
• Oil Weighs 7.5 lbs./gal.
CG Envelopes depicted for 172R and S-Models are for training purposes only. Other fleet models are not depicted. Always use the
approved Operators Manual or POH/AFM specific to the airplane you are flying. These examples are to be used as a reference only.
ATP assumes no responsibility or liability for any errors or inaccuracies that may appear on this guide and it is not intended to
replace the approved POH/AFM or FAA approved publications and procedures.

Revised 2019-06-21
 PIPER SEMINOLE
Weight & Balance

Weight × Arm = Moment Specific ATP Aircraft

Basic Empty Weight >> Weight & Balance Info
Front Pilots + 80.50 + Important information specific to your
N-Number, including Basic Empty
Rear Passengers + 118.10 + Weight and Moment, is available on
the ATP Student Extranet and in the
Baggage 200lbs. max + 142.80 + ATP Documents folder in ForeFlight.

Zero Fuel Weight = CG =

Usable Fuel + 95.00 +

Ramp Weight = =
Taxi Fuel – 95.00 –
Sign in to your Student
Extranet account. Go
Takeoff Weight = CG = to Library > Aircraft
Information Manuals >
Fuel Burn – – Aircraft Quick Reference,
and enter the N-Number of
the aircraft you are flying.
Landing Weight = CG =

Revised 2019-06-21