CAP Aircraft Inspection Checklist
Wing
Tail#
Make
Cur Tach Time
Inspection Date
Inspector CAP ID
Model
Cur Hobbs Time
1. Aircraft Log Books / Records, POH, AIF
Y/N/NA
Notes
A. Mid Cycle/100-Hour/Annual) limits complied with (Ref: CFR 91.417, CAPR 66-1)
Date Cur
Tach Time
AD Comp
Date Prev
Tach Time
AD Comp
Date Prev
Tach Time
AD Comp
B. ELT Battery Checks Current
(12 Mo. Ref: CFR 91-207)
Date Cur
Date Prev
C. Corrosion Control – Entry in Log Book (biennial or annual in FL/HI/P-Rico - CAPR 66-1)
Date Cur
Date Prev
D. Altimeter/Pitot-Static/Transponder Systems Current – (24 Mo. Ref: CFR 91.411 & 413)
Date Cur
Date Prev
E. WMIRS open discrepancies accurately reflect current status of the aircraft
F. WMIRS snapshot page agrees with maintenance module status
G. FAA Fm 337 and STCs on file (180 hp engine, mods) checklist speeds match STC
1) CURRENT VERSION OF CONTENTS Ref (CAPR 60-1, 2-4e) on
H. AIF
2) All of the sections of the AIF are current IAW #1
- Current version
3) "Red Aircraft Grounded Placard" is in the AIF CAPR 60-1 2-4f
- Correct
4) VOR & Fire Extinguisher forms (CAPR 66-1)
- Accurate
6) CAP AIF cover sheet matches most current inspection data
I. Weight and Balance - Current factory or shop basic empty weight data (Tab 5 of AIF)
2. Aircraft Interior
Y/N/NA
1) Airworthiness Certificate
(Ref: CFR 91.203)
2) Registration
(Ref: CFR 91.203)
A. Required
3) Operating Handbook (Airplane Flight Manual / POH) (Ref: CFR 91.9)
Documents in Aircraft
4) Current Weight & Balance Data
(Ref: Acft Flight Manual / POH)
5) (G-1000 only) Garmin Avionics (Ref: Cockpit Reference Guide))
B. CAP-approved checklist date
Revision #
C. POH current revision
Revision #
D. No Obvious Defects, Leaks, Corrosion, Cleanliness, and Condition of Interior
E. “Not for Hire” Placard Displayed
(Ref: CAPR 66-1)
F. “Max Crosswind” Placard Displayed (Ref: CAPR 66-1)
G. “Cessna Seat Slippage Warning” Placard Displayed (CAPR 66-1)
H: "Remove Towbar Before Engine Start"
(CAPR 66-1)
I. Operating Limits / Placards (Ref: CFR 91.9)
J. Avionics or Control Lock Installed
(Ref: CAPR 66-1)
K. Serviceable Fire Extinguisher / with gauge Installed (Ref: CAPR 66-1)
L. Carbon Monoxide Detector – Serviceability, Expiration Date
(CAPR 66-1)
M. Cessna Seat Rails for Obvious Cracks and Wear
(Ref: AD 2011-10-09)
N. Cessna Secondary Seat Stop Installed
(All Models Prior to 1997)
O. Cargo Tie-Down or Net Installed
(Ref: CFR 91.525)
P. Survival Kit. (Ref: CAPR 66-1)
3. Aircraft Exterior
Y/N/NA
A. Acft Properly Chocked, Tied Down, and Condition of Tie downs (CAPR 66-1)
B. Obvious Defects, Leaks, Corrosion, Cleanliness
C. Condition of Prop – Nicks, Dents, Leaks, Corrosion, Evidence of Prop Strike
D. Appropriate CAP decals on wings, doors and vertical stabilizer. (Ref: CAPR 66-1 & CAP Policy)
E. Brakes for Leaks, Wear, Cracked Pads and Obvious Defects (Ref: Acft Service Manual)
F. Tires for Proper Air Pressure and Serviceability (Ref: Acft Service Manual/STC)
H. Engine Cowling for Proper Fit / Fasteners Serviceable and Secure
I. Cessna Factory Door Hinge Pins Installed (CAP-LGM guidance)
4. Exterior And Interior Lighting For Proper Operation (Ref: CFR 91.209)
Y/N/NA
A. Landing / Taxi / Pulse lite
B. Anti-Collision Strobe
C. Navigation / Position
D. Flashing Beacon
E. Cabin / Panel
F. Instruments
CAPF 71, SEPTEMBER 15
Previous Edition Will Not Be Used
OPR/ROUTING: LGM