N60781 Logbook Entries
6/15/04 5042.86 Tach 5061.77 TTAF
• Engine O-200-A S/N 66043-7-A removed for overhaul
• Wings and tail components removed for total aircraft refurbishment
8/4/15 5044.30 Tach 5063.21 TTAF
• Left entry door minor repair in area of upper hinge
• Installed new FAA-PMA front windshield P/N LP-303 CL see 8130-3 dated 6/21/04
• Installed new FAA-PMA rear windshield P/N LP-360 CL see 8130-3 dated 7/13/04
• Installed new left and right FAA-PMA windows P/N LP-365 CL see 8130-3s dated 6/16/04
• Airframe parts stripped, acid etched, alodined, primed and painted with white DuPont Imron
555, white PPG Delfleet 922515, light blue Dupont Imron 7165X, dark blue Dupont Imron
63203X and chestnut Dupont Centari B81351D
• All electrical wiring in engine compartment repaired and properly labeled with Cessna Service
Manual schematic reference numbers using Mil Spec MIL-C-27500 and MIL-W-22759 wiring
• Installed new battery-to-ground jumper cable P/N 0412007-9. See 8130-3 dated 5/2/07
• Installed new diode P/N 0770728-1 on battery contactor. See 8130-3 dated 7/2/12
• Installed all new silicone nipples on all appropriate electrical terminals
• Installed new Concord RG-25 battery
• Interior of airframe and interior parts primed and painted with DuPont Color Vinyl Oxford White
4163 C8432J
• All interior plastic panels replaced with new FAA-PMA panels from Vantage Plane Plastics.
All parts painted with DuPont Color Vinyl Oxford White 4163 C8432J
• Both control wheel shafts nylon grommets replaced with four new grommets P/N 0513056-4
• Clock replaced with new Davtron M800 weight and balance change negligible
• Hobbs meter replaced with new meter weight and balance change negligible
• New FAA-PMA instrument panel covers from Vantage Plane Plastics installed. All covers
painted with black DuPont Color Vinyl D8302JV A14149
• Installed new FAA-PMA Ultra Visor sun visor. See PMA approval dated 12/19/07
• Installed new left and right FAA-PMA steering rod boots P/N MC0413304-3 per Installation
Instructions Rev. A dated 5/12/99
• Replaced right steering rod end P/N S1823-3
• Replaced O Rings in left and right brake master cylinders
• Replaced O Rings in left and right brake calipers
• Replaced left and right brake lines
• Serviced brake system with MIL-H-5606 hydraulic fluid
• Repaired and adjusted parking brake system
• Installed new nose strut seal kit SK172-1F. See 8130-3 dated 8/5/04
• Replaced cowl mounts with new Lord mounts P/N LD J7444-14
• Installed new stainless steel Southco cowl fasteners
• Replaced left, right and nose wheel bearings with new bearings and races
• Installed new left and right window latches and strikes-see release dated 10-30-2006 and 928-2006
• Installed new FAA-PMA door and window seals P/N 500-600 from Aircraft Door Seals per
Installation Instructions 601A
• Installed new Pinchwelt window trim P/N P860029. See 8130-3 dated 3/24/08
• Disassembled left and right seats for refurbishment. Seat frames painted with DuPont Color
Vinyl and clear DuPont Imron
• Installed new FAA-PMA Airtex seat upholstery #44036 Type A Base: DT-77 Barley and Trim:
DT-83 Tan
• Reassembled seats
• Installed re-webbed seat belts. see Aero Fabricators MX release form dated 4-9-15
• Installed new Blue Sky door stops P/N 05-04563
• Installed new vacuum system filter D9-14-5
• Installed new vacuum regulator garter filter ARB3-5-1
• Installed new static system sump P/N S1258-1. See 8130-3 dated 7/19/04
• Installed fuel selector valve kit FS-KT-1. See 8130-3 dated 3/21/08
• Installed new fuel cap gaskets left and right P/N B100142-1
• Installed new fuel tank sump quick-drains
• Installed horizontal stabilizer with new hardware
• Installed vertical stabilizer with new dorsal fin-to-stabilizer seal P/N S1611-1 and new
hardware
• Installed new Comant VOR/LOC/GS antenna per Installation Instructions, Comant Industries,
Inc. Rev. C dated 12/3/08
• Installed new VOR/LOC/GS antenna cable in vertical fin.
• All flight control and trim cables, fittings and pulleys inspected over entire length
• Installed three new elevator bearings. See 8130-3s dated 12/19/2014
• Installed new rudder bushing at cable ends NAS74A3-004P
• Installed left and right wings
• Replaced right flap upper and lower skins. See 8130-3s dated 3/1/2007 and 3/2/2007
• New nylon flap wear buttons installed P/N S1093-1
• Re-installed flaps with new McFarlane flap roller kit FLP-KT-1. See 8130-3s dated 7/24/07,
12/7/07 and 1/8/08
• New left and right FAA-PMA horizontal stab tips installed
• New FAA-PMA vertical stabilizer cap installed
• New FAA-PMA left and right wing tips installed
• New left and right FAA-PMA elevator tips installed
• New FAA-PMA rudder cap installed
• New FAA-PMA rudder butt installed
• New FAA-PMA wing strut fairings installed
• Ailerons, elevators and rudder balanced and re-installed
• New FAA-PMA landing light lens P/N LP-373 CL installed. See 8130-3 dated 11/14/14
• Replaced left nav light bulb
• Removed red flashing beacon and flasher unit. Replaced with Whelen TSO LED flashing
beacon I/A/W Installation Guide Model 71055 series form No. 14036C dated 2006, aircraft
weighed and C.G. calculated
• Fabricated ELT mounting platform from .032” 2024T# aluminum. Platform mounted to lower
right stringers at station 101”. See 337 dated 8/4/15.
• Removed inoperative ELT, installed new Ameri-King AK-450 ELT, S/N 472621, remote, cable
and antenna. See 337 dated 8/4/15. Aircraft weighed and C.G. calculated
• Installed new FAA-PMA Airtex carpet #44036 113
• Installed four new seat stops P/N H916003
• Stripped, inspected, primed and painted engine mount with DuPont Imron. Reinstalled mount
using new hardware
• Installed Overhauled O-200-A Engine S/N 66043-7-A using new hardware and new lord
mounts P/N LD J3608-1
• Repaired and painted engine baffle assembly
• Replaced engine baffle seal material
• Installed all new scat hoses
• Installed new Stainless Steel fuel strainer standpipe. See 8130-3 dated 12/5/07
• Installed new fuel strainer Plunger P/N 0756010-11. See 8130-3 dated 3/14/07
• Installed new FAA-PMA fuel strainer drain kit
• Installed new fuel strainer cable P/N S1517-7. See 8130-3 dated 10/1/07
• Installed new Aero Fabricators left muffler P/N E477001 I/A/W Aero Fabricators Installation
Instructions Number E-477-001 and E-477-002 dated 4/7/08 and STC SA1143SW dated
9/13/12 . See 337 dated 8/4/15. No weight and balance change.
• Installed new left exhaust shroud modified with 3” fitting by Aero Fabricators see MX release
dated 10-13-15
• Installed new FAA-PMA left Aero Fabricators tailpipe P/N E47703
• Installed new FAA-PMA right Aero Fabricators tailpipe P/N E477009
• Installed new Stratoflex oil pressure hose
• Installed new Aeroquip fuel hose from fuel sump to carb
• Installed overhauled FAA-PMA Rapco-211CC vacuum pump S/N 157274 with new Rapco
fittings. See 8130-3 dated 11/19/13
• Installed new Stratoflex vacuum hose
• Painted propeller
• Installed new FAA-PMA spinner bulkhead P/N U0450040-1
• Installed new FAA-PMA spinner bulkhead P/N 0450039-1-791
• Installed propeller with new bolts
• Performed conformity inspection for previously installed Brackett Aero Filters, Inc. BA-4106
rev. D engine air filter assembly. Found filter assembly installed I/A/W instruction sheet Part.
No. 4105 dated 3/10/04 and STC SA71GL dated 6/20/2000. See 337 dated 8/4/15. Aircraft
weighed and C.G. calculated.
• Installed new Bracket air filter element BA-4108.
• AD 72-03-03 R3 Wing flap actuator jackscrew C/W Per SE70-16, Due again next annual or
8/2016,
• AD 79-08-03 cigar lighter wiring modification P/C/W by installation of inline fuse
• AD 80-11-04 vertical fin aft bracket nutplates C/W by inspection, due again 5144.30 tach
• AD 93-24-15 instrument panel light dimming rheostat P/C/W by installing rheostat P/N
0015H1600 per SEB93-33
• AD 00-06-01 fuel strainer assembly standpipe P/C/W by inspection,
• AD 09-10-09R2 AFM, placard, rudder travel stops P/C/W by installing rudder stop modification
Kit SK152-24B
• AD 11-10-09 seat track wear and seat pin engagement C/W by inspection, due again 5144.30
tach or 8/2016
• AD 76-07-12 Bendix switches C/W by inspection, due again 5143.40 tach
• ADs checked thru 2015-15. See AD listing in Aircraft Maintenance Records, Airworthiness
Directives section.
• Aircraft weighed and C.G. calculated; Nose-252lbs@ -10.5625”, Right Main-412lbs@ 48.250”,
Left Main-411lbs@ 48.25”, New empty weight 1075lbs. New Empty weight C.G. 34.46”. New
empty weight moment 37048. New useful load 525 lbs.
All work performed I/A/W Cessna 100 Series Maintenance Manual and AC43.13-1B
N60781 Engine Logbook
8/4/15 5044.30 Tach “0” SMOH
 Performed Engine Major Overhaul I/A/W O-200 Aircraft Engine Overhaul Manual form
number X30010
 Crankshaft S/N S170957-1 magnafluxed, journals ground M.010, re-nitride, cadmium plated,
baked flange and repaired oil seal as necessary by Aircraft Specialties Services, Inc. see
8130-3 dated 1/7/09
 Camshaft reconditioned by Aircraft Specialties Services, Inc. See 8130-3 dated 1/6/09
 All four rods magnafluxed, rebushed and inspected by Aircraft Specialties Services, Inc. See
8130-3 dated 1/6/09
 All eight rocker arms magnafluxed and rebushed by Aircraft Specialties Services, Inc. See
8130-3 dated 2/26/13
 All eight lifter bodies magnafluxed, and reground by Aircraft Specialties Services, Inc. See
8130-3 dated 1/6/9
 Crankcase repaired by Divco, Inc. See 8130-3 dated 3/18/13
 Engine assembled using new bearings and seals
 One new hydraulic unit P/N SA646846 installed
 Installed four new Millennium Cylinder kits P/N SA10200-A20P.
 Overhauled carburetor MA-3SPA P/N 10-4894-1 S/N MS863602 installed, see 8130-3 dated
12/11/13
 New Slick Magnetos M/N 4301 S/N left 13111257 and right 13111256 installed
 New Slick magneto harness installed
 Advanced magneto timing from 24 degrees B.T.C. to 28 degrees B.T.C. in accordance with
Superior Air Parts, Inc. Service Letter 93-04A dated 7/13/04 and STC SE8675SW dated
8/24/93. See 337 dated 8/4/15.
 New REM 40E spark plugs installed
 New FAA/PMA Sky-Tec starter M/N C12ST2 S/N 2CC-441333 installed per Installation
Instructions dated 05/08/00 . See Form CC1108-1 dated 11/6/13, aircraft weighed and C.G.
calculated
 Installed F. & M. Enterprises Inc. spin on oil filter adapter per Model T.A.F.-L Installation
Instructions dated 9/5/07 and STC SE7559SW dated 3/1/99, Rev. 5. See 337 dated 8/4/15.
Aircraft weighed and C.G. calculated.
 Installed new AA-48108 oil filter

Engine installed on N60781 S/N 15070574