AIRFRAME LOGS - Steel Aviationinventory.steelaviation.com/aircraft/logbooks/miscLogbook-671.pdf ·...

AIRFRAME LOGS

Date: 1/19/2012; Aircraft: 598CD; Type: SR 22; S/N: 1653; Hobbs: 1406.20;Total Time: 1406.20; Engine - Type: TCM IO-550-N27, S/N: 917895, Time:1406.20; Prop - Type: Hartzell PHC-J3YF-1RF, S/N: FP4119B, Time:1406.20

**AIRFRAME**

-Complied with Savvy Prebuy Inspection Phase 1 & 2 .-Complied with the Annual Inspection in accordance with Dominion AviationServices FORM 0100 which meets the requirements of FAR 43 appendix Dand with reference to Cirrus SR22 maintenance manual chapter 05-20.-Serviced the brake reservoir as required with MIL-H-5606 hydraulic fluid.Ref. Cirrus SR-22 MM Chapter 12.-Serviced the tires as required.Nose to 40 psi with shop air.Mains to 62 psi with shop air.Reference POH-Removed failed battery (p/n RG24-15M s/n 40266306) and Installed newbattery (p/n RG24-15M s/n 40450002). All procedures done in reference toConcorde Maintenance Manual for RG Series Main Aircraft Battery (CMM24-30-71) and Cirrus Airplane Maintenance Manual Model SR22 Chapter 24.-Lubricated the aircraft in 100, 200, 300, 500 and 5yr intervals as required inaccordance with the Cirrus airplane maintenance manual model SR22Chapter 12-20-Installed new #3 Engine Exhaust header tube (p/n 15069-001) with newgaskets (p/n 652458) and lock nuts (p/n MS20500-428) in reference toCirrus Airplane Maintenance Manual Model SR22 Chapter 78-10 & TCMIO-550 Permold Series Engine Maintenance and Overhaul Manual AppendixB-10-R-eplaced Left red navigation light & Left white position light in reference toCirrus Illustrated Parts Catalog Model SR22 Chapter 33-40.-Replaced brake caliper O-rings (p/n MS28775-222) in reference toCleveland Wheels & Brakes Product Catalog.Complied with Cirrus SR2X Service Bulletin SB 2X-05-01 (SNS SUBJECT:05-10 Overhaul And Replacement Schedule - Brake Assembly O-RingReplacement Interval) by installing the yellow Temp Stickers (p/n 5698-003)and updating the POH in reference to Cirrus SR2X Service Bulletin SB 2X-05-01.-Replaced Right Main Landing Gear brake disc (p/n 164-01501) in referenceto Cleveland Wheels & Brakes Product Catalog & Maintenance Manual.-Removed / replaced (8) Duracell ELT batteries with new batteries size DDuracell MN1300. Batteries expire Mar 2018.Inspected the ELT as per FAR 91.207(d).MAKE :ACKMODEL :E-01SERIAL :054053THE BATTERY EXPIRES :March 2018-Removed line cutters for replacement and found : Model C1-8 and lot #1RRL0111, manufacture date of 01/2011and s/n's 804 and 821.Original line cutters expire 1/2017.Reinstalled original line cutters with new cord and new machine thread.Reference cirrus SR22 Caps Component Manual chapter 95-01.Up dated Maintenance Warning Report and life limited section of #1 airframelog book.-Removed corrosion from the right most inboard flap brackett and cleanedwith Alumiprep 33. Treated the area with Alodine 1201 and painted withCirrus Base White (PPG Concept DCC 92813).-Removed A/C compressor and found the drive assembly side of the mountto be worn. Installed .0020" thick washer between the aft compressormounting surface and the aft compressor drive mounting surface. Securedwith a new bolt (p/n AN5-37A), original flat washers, a new lock washer (p/nMS35338-45) and the original nut. Referenced Keith Products Inc.Maintenance Manual Air-conditioning System for Cirrus Design SR-22Document No. CR-220-10 STC No. SA10195SC.-Removed old double sided tape from left lower wing/fuselage fairing andreplaced with two feet of new double sided tape 1/2" X.045 (p/n 50640-0450)in reference to Cirrus Maintenance Manual Chapter 53-50-Accomplished the removal of the corroded screws. Removal required theextraction of one tuck screw on the left lower wing tip attach point.-Installed new Telex Microphone (p/n 62800-001) into the aircraft asrequested by owner.-Removed and replaced the air induction filter in reference to CirrusIllustrated Parts Catalog Chapter 71-60.

-Installed new ELT Remote Control Panel Indicator Battery in reference toCirrus Airplane Maintenance Manual Model SR22 Chapter 25-60.-Inspected fire extinguisher model RT-A400 s/n V-176548 per labelinstructions. Weight is 505 grams. Found acceptable for continued service.-Removed the fuel strainer. Cleaned and inspected as required. No defectsnoted. Reinstalled the fuel strainer with new o-rings (p/n NAS1523-8B & p/nMS29513-137) and secured in reference to Cirrus Aircraft MaintenanceManual Model SR 22 Chapter 28-20 & Cirrus IPC Model SR22 Chapter 28-20.-Removed the left engine baffle from engine. The cracked baffle had thecracks stop drilled and a doubler fabricated to repair the areas that wereaffected. Original type baffle skin metal was used to fabricate the repairdoubler. Solid aluminum rivets were used to install the doubler where theywere able to be used. The repaired baffle was reinstalled on the left side ofthe engine. Repair accomplished in accordance with AC43.13-1B.-Serviced the control quadrant with AeroShell 22 in reference to CirrusAirplane Maintenance Manual Model SR22 Chapter 76-10.-Performed Functional Check of the Redundant Circuit Breakers in referenceto Cirrus Airplane Maintenance Manual Model SR22 Chapter 24-50.-Performed Inspection/Check of theTransient Voltage Suppressor inreference to Cirrus Airplane Maintenance Manual Model SR22 Chapter 24-50-Checked aileron, rudder and elevator cable tensions and flight controltravels in reference with Cirrus SR22 maintenance manual chapter 27 andType Certificate.-Constructed profile of this aircraft into ATP navigator and verifiedcompliance of all ADs.-Adjusted elevator cable tension in reference to Cirrus Airplane MaintenanceManual Model SR22 Chapter 6 Figure 06-001.-Installed new left outboard aft tail pipe support bracket (p/n 20155-010) inreference to Cirrus Airplane Maintenance Manual Model SR22 Chapter 78.-Installed Reiff Preheat Systems Turbo System TL6 (approved forContinental 550) in reference to Reiff Preheat Systems' Hotband CylinderHeating System and HotStrip Oil Sump Heater installation & operatinginstructions.-Updated the POH in reference to Cirrus Service Publication Index For SR22Serial Number 1653 by adding SR22 POH Revision 7(p/n 13772-001RA7),Revision 8 (p/n 13772-001RA8), Revision 9 (p/n 13772-001RA9), & Revision10 (p/n 13772-001RA10).-Updated the Weight and Balance with the addition of the Reilff EngineHeater System.

I certify that this ____________________has been inspected in accordancewith a/an _____________________Inspection and was determined to be inairworthy condition. Details on file at this facility.

Signature___________________________.

Work Order #________________________.

Dominion Aviation CRS #ODAR018H7511 Airfield DriveRichmond, Virginia 23237(804) 271-7793

Fl!GHTLEVEL

Airframe Lo book Entr Name: Becker Thorsten Tail# N598CD Hobbs: 1457.5 W.O.: 8559 Serial#: 1653 Date: 2/18/2014 Model SR22 Completed annual inspection this date using a checklist conforming to FAR part 43 Appendix D and using

SR22 checklist as a guide. Replaced battery number 2 with 2 each P/N 50979-00 I batteries. Adjusted elevator and elevator pitch trim servo bridle cable tension. Replaced 0-rings 2 each PIN M83461/l-222 and temp. decal PIN 51698-003 on RH brake caliper and bleed brakes. Installed new well nuts 4 each PIN 50763-002 in baggage door kick plate. Removed Amsafe electronic control module PIN 508358-421 SIN RA05FEB 14-161 and sent to Amsafe for rebuild under WO# 74237-1dated2/5/2014. After rebuild installed same and tested, passed test. Next replacement date 02/2021. Replaced several well nuts 2 each P/N 5802-00 I and 4 each PIN QI 032 for LH and RH gear strut upper fairing. Replaced Cyl.#4 EGT probe PIN 16579-002. C/W FAR 91.207 (cl) battery next due 3/2018. I certify that this aircraft has been inspected IA W an annual inspection and is airworthy at this time and is approved ' ., re urn tsl~er':-ice.

Signature: ~ ,' ven Wolff A&P IA 16629146 fllightlevel Norwt ircraft Maintenance

209 Access Road, Norwood MA 02062 781-769-8686

FUGHTLEVEL

book Entr Name: Becker Thorsten Hobbs: 1457.5 W.O.: 8559 T.T 1457.5 Date: 2118/2014 Model # 10-550N27 Completed annual inspection this date using a checklist conforming to FAR part 43 Appendix D and using

SR22 checklist as a guide. Engine compressions Cyl.# I 62/80, Cyl.#2 62/80, Cyl.#3 64/80, Cyl.#4 72/80, Cyl.#5 70/80, Cyl.#6 62/80. 45 psi, master orifice reading. Borescopc cylinders. Took oil sample. Replaced oil filter with PIN CH48108 and serviced engine with 8 qts. 20W50 X/C oil. Replaced air filter PIN BA24. Replaced fuel drain seals on Cyl. 's 2,4 & 6 with 3 each PIN 633958-2. Replaced exhaust gaskets 3 each PIN 652458 on Cyl's 1,3 & 5. Replaced all spark plugs with 12 each P/N URHB32E. Adjusted air conditioning belt and safetied. Checked fuel pressures IA W Continental Motors SID 97-3F, all pressures within limits. At1er inspection ran up engine, no leaks noted, operational check good. I certity that this engine has been inspected IA Wan annual inspection and is airw. hy at this time and i approved for return to service.

Signature: -"'"-"'-u-------f-c,L/'"""'-cn-- Steven Wolff A&P IA 16629146 o '.t\.ircraft Maintenance w od MA 02062 781-769-8686

FUGHTLEVEL

P II L E t rope er o~ n ry Name: Becker Thorsten Tail# N598CD Hobbs: 1457.5

W.O.: 8559 Model PHC-JJYF- T.T. 1457.5 IRFIF7693DFB

Date: 2118/2014 SIN FP4119B Completed annual mspectwn this date using a checklist conforming to FAR part 43

Appendix D and using SR22 checklist as a guide. I certify that this propeller.has been ins ected l W an annual inspection and is

airworthy at this time and a proved

Flightleve o d Aircratl Maintenance 209 Access Roa , No wood MA 02062 781-769-8686

ENGINE

LOGS


**ENGINE***

Complied with Savvy Prebuy Inspection Phase 1 & 2 and found the following 1) Complied with a compression check on all engine cylinders. Thereadings were as follows: #1 - 60/80, #2 - 63/80, #3 - 70/80, #4 - 76/80, #5- 76/80, #6 - 66/80. Minimum orifice reading was 46/80. Cylinders #2 & #6had leakage by exhaust valve and rings, #1 cylinder by rings and #3 cylinderby exhaust valve. Boroscope inspection showed cylinders #'s 1, 2, 4 and 6have corrosion on walls. Exhaust valves appeared OK.2) TCM AD 2011-25-51 (12/28/11) Starter ADapter gear due.Researced andcomplied with AD 2011-25-51 and determined action was not reqiredbecause the effectivty requirements did not match this Aircraft.-Removed, inspected, and photographed all engine hydraulic lifters andcamshaft lobes. Detected signs of spalling on cylinder # 2 exhaust, cylinder#3 exhaust, cylinder #6 exhaust, and cylinder # 6 intake hydraulic lifters.Replaced exhaust hydraulic lifters (p/n 653877) with new supersededhydraulic lifters (p/n 658077) in cylinders #2, #3, & #6. Replaced intakehydraulic lifter (p/n 653888) with new superseded hydraulic lifter (p/n658088) on cylinder #6. Replaced Hydraulic lifters in reference to TeledyneContinental Aircraft Engine Service Information Directive SID 05-1. Installedpush rod tubes with new o-ring seals (p/n 630286) and push rod housingpackings (p/n 534610). Installed push rods and rocker arms. Replacedworn thrust washers (p/n 653788) on #4 exhaust rocker arm to gain correcttolerances. Replaced all washer lock tabs (p/n 501868) on rocker arms.Torqued rocker arm bolts to 17.5 ft lbs. and bent over tabs. Installed newrocker cover gaskets (p/n 665705) Torqued cover screws to 65 in lbs. Allprocedures done in reference to TCM IO-550 Permold Series EngineMaintenance and Overhaul Manual Chapter 10-8 & TCM IO550N CylinderAssembly parts listing Figure List 25_18.-Complied with the Annual Inspection in accordance with Dominion AviationServices FORM 0100 which meets the requirements of FAR 43 appendix Dand with reference to Cirrus SR22 maintenance manual chapter 05-20.-Removed the spark plugs.Inspected, cleaned, gapped and rotated the spark plugs.Re-installed the spark plugs with new gaskets, pn# M674.Reference : Champion aviation service manual AV6-R.-Complied with the oil and filter change. Serviced with 8 quarts of Phillips20w 50. Installed new oil filter p/n CH48108-1. Cut open the old filter andfound no defects. Removed, inspected, cleaned and reinstalled the sumpscreen with a new gasket. Ran the engine and no leaks detected.


Signature___________________________.

Work Order #________________________.


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PROP

LOGS


**PROPELLER*

-Complied with the Annual Inspection in accordance with Dominion AviationServices FORM 0100 which meets the requirements of FAR 43 appendix Dand with reference to Cirrus SR22 maintenance manual chapter 05-20.-Lubricated the propeller hub for the 100hr interval as required in accordancewith the Cirrus airplane maintenance manual model SR22 Chapter 12-20


Signature___________________________.

Work Order #________________________.


Fl!GHTLEVEL





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AIRFRAME LOGS - Steel Aviationinventory.steelaviation.com/aircraft/logbooks/miscLogbook-671.pdf ·...

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