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WORK PACKAGE INSTRUCTIONS

1. 211 212 217 218 233 234 203 254 251 252 503 525 603 625 Aileron Trim Tab Actuator 2660044 1 Lubrication Task 551 571 27 10 02 641 651 671 Elevator Trim Tab Actuator 2660017 1 Lubrication 371 372 Task 27 30 02 640 375 376 Fuel Quantity and Low Fuel Warning Systems Functional AUX Check Task 28 41 00 720 Flight Data Recorder Underwater Locator Beacon Func 312 tional Check Task 31 31 00 721 Brakes Operational Check Task 32 40 00 710 mo ff fo Passenger Cargo Compartment Lighting Operational AUX Check Task 33 20 00 710 Crew Doors Detailed Inspection Task 52 00 00 220 801 802 ef fp Passenger Cargo Doors and Door Frames Detailed In 255 256 spection Task 52 00 00 221 257 Primary and Secondary Exhaust Duct General Visual In 130 spection Task 78 10 00 21 1 TASK ZONE MECH REMARKS Spoiler System Functional Check Task 27 10 00 720 KKK End of Inspection Document 10 Inspection Items 2013 Cessna Aircraft Company Retain printed data for historical reference only For future maintenance use only current data Page 2 Print Date Wed Oct 23 13 12 56 WST 2013 MODEL 208 MAINTENANCE MANUAL Rev 26 5 15 11 Rev 24 INSPECTION DOCUMENT 11 Date Registration Number Serial Number Total Time 1 Description A Inspection Document 11 gives a list of item s which are completed at every 1600 Hours or 24 calendar months whichever occurs first B Inspection items are given
2. 00 224 Magnetic Compass Functional Check Task 34 21 00 ee Pf fp 720 Oxygen System Operational Check Task 35 01 00 710 231 232 251 252 255 256 311 312 801 802 Engine Wash Ring Air Plenum and Thermocouple T1 130 Detailed Inspection Task 71 41 00 220 TASK ZONE MECH REMARKS KkKk End of Inspection Document 01 Inspection Items 2013 Cessna Aircraft Company Retain printed data for historical reference only For future maintenance use only current data Page 2 Print Date Wed Oct 23 13 08 20 WST 2013 MODEL 208 MAINTENANCE MANUAL Rev 26 5 15 02 Rev 24 INSPECTION DOCUMENT 02 Date Registration Number Serial Number Total Time 1 Description A Inspection Document 02 gives a list of item s which are completed at every 24 calendar months B Inspection items are given in the sequence of the zone in which the inspection is completed A description of the inspection as well as the Item Code Number are supplied for cross reference to section 5 10 01 Frequently tasks give more information about each inspection These tasks are found in the individual chapters of this manual C The right portion of each page gives space for the mechanic s and inspector s initials and remarks You can use copies of these pages as a checklist while you complete the tasks in this Inspection Document 2 General Inspection Criteria A As you complete each of the inspection tasks in this Inspection
3. 1 2 S No ON RN No AME 4 Fuel Pump Vickers PART No OFF _ I 8X FF 3034792 acta S No ON RN No AME HEREBY CERTIFY THAT ALL WORK DETAILED HAS BEEN COMPLETED AND CERTIFIED FOR IN ACCORDANCE WITH THE REQUIREMENTS OF APPLICABLE MANUALS AND SCHEDULES THIS SIGNATURE CONSTITUTES A CERTIFICATION PURSUANT TO CAR 422ZE HEATER APU AIR CYCLE MACHINE VDO HOURS JOB CO ORDINATOR LAME SIGNATURE LIC No Date 2 AVTRAC Goes es AIRCRAFT TYPE 208 REGISTRATION VH OPH Aero Jacks Pty Lid INSPECTION M R Inspections MC No MC2013 1599 SERIAL No 0157 JOB No VDO LDGS TTIS FORM 100 WORKSHEET JOB CO ORDINATOR Lic No DATE ITEM WORK REQUIRED DEFECT COMPLIANCE RECTIFICATION COMPONENT CHANGES LAME Sig Lic 5 Fuel Control Unit PART No OFF Sine OFF 3244897 4 sac Eng S No ON 6 Oil to Fuel Heater PART No OFF E i R SiN OFF 3032710 ee Eng S No ON 7 ignition Regulator PART No OFF SiN OFF 3035889 eens S No ON RN No me 8 Comp Bleed Valve PART No OFF SOA SiN OFF 3049038 02 ee S No ON RN No me HEREBY CERTIFY THAT ALL WORK DETAILED HAS BEEN COMPLETED AND CERTIFIED FOR IN ACCORDANCE WITH THE REQUIREMENTS OF APPLICABLE MANUALS AND SCHEDULES THIS SIGNATURE CONSTITUTES A CERTIFICATION PURSUANT TO CAR 42ZE HEATER APU AIR CYCLE MACHINE VDO HOURS JOB CO ORDINATOR LAME SIGNATURE LIC No Date 2 AVTRAC yp MAINTENANCE TRACKI
4. Check Task 5 20 01 280 M A110001 Interior and Exterior Placard and Decal Detailed Inspec a a a tion Task 11 00 00 220 a on nonenennane a A E A mai pas i Oe OD iil iaciacineneanoncncl G H H A TASK ZONE MECH REMARKS 2013 Cessna Aircraft Company Retain printed data for historical reference only For future maintenance use only current data Page 1 Print Date Mon Nov 04 09 15 34 WST 2013 ITEM CODE NUMBER B212401 B221203 B255201 C270001 B273101 C275001 A281001 B284101 B313101 B322001 A353001 B761003 MODEL 208 MAINTENANCE MANUAL Rev 26 5 15 0A Rev 26 IN TASK SP ZONE MECH REMARKS Avionics Cooling Fan Operational Check Task 21 24 00 710 211212 Garmin Autopilot GFC 700 Slip Clutch Override Oper ational Check Task 22 12 00 710 226 232 Cargo Pod Drains Operational Check Task 25 52 00 710 901 902 903 904 905 906 Flight Controls Lubrication Task 27 00 00 640 Stall Warning System Operational Check Task 27 31 00 211 212 710 503 Flap Tracks and Rollers Lubrication Task 27 50 00 640 525 527 625 627 Fuel Filler Assembly Detailed Inspection Task 28 10 01 521 621 220 Fuel Reservoir Warning System Operational Check Task 28 41 00 710 i JHN Shimmy Damper Functional Check Task 32 20 02 720 w ff fo Emergency Power Lever Annunciator Light EPL Oper AUX ational Check Task 76 10 01 710 Flight Data Recorder System Functional Check Task
5. N2 FUEL FLOW WF FUEL FLOW WF GAS GEN NG N1 OIL PRESSURE GAS GEN NG N1 OIL PRESSURE Table 5 e a ee AVTRAC Maintenance Tracking Form 009 Initial Issue 25 May 2010
6. should be identified before further inspection operation Ref 79 20 02 Inspection Check A Oil System 1 Check oil level Ref SERVICING Bf 2 Check condition and locking of oil filler cap Ref 72 60 00 3 Oil Filter Elements Elements must be inspected and cleaned Ref 79 20 02 Light traces of sediment only may be removed from the main filter screen All other contamination requires replacement of filter element Any foreign material found in main oil filter or on chip detector should be identified before further inspection operation Ref 79 20 02 MAINTENANCE PRACTICES NOTE 2 If carbon like deposits are found drain accessory gearbox oil into a clean container and examine debris Varnish flakes are non metallic and are usually dark on one side and shiny similar to bronze on the other side They are hard and will not form into paste when rubbed between fingers Ref step 7 Page 2 PT6A 114A Maintenance Manual P N3043512 Chapter 72 00 00 R29 Mar 08 2013 Table 601 3 SYSTEMS CONT AMESIG LAMESIG A Oil System cont 5 Bridge chip detector s magnetic pins with suitable jumper and using a suitable ohmmeter check continuity between connector pins If NOT APPLICABLE OSIP continuity does not exist replace chip detector CARDS RAISED IN CONTROL Any foreign material found on chip detector or in SYSTEM main oil filter should be identified before further inspection operation Ref 79 20 04 MAI
7. the airplane is exposed to salt or X and inspect surfaces hardware and strut polluted water the chances for or connections for corrosion corrosion increase dramatically mor X Daily basic cleaning is essential eoft en Check installed placards against the AFM or POH and installation drawings X X Hulls amp Float Installation Float exterior inspect for damage Struts wrinkled metal corrosion paint X X loss etc Boarding steps disassemble as needed If the floats are installed remove and grease the step slide tubes the center section fairings for access Struts and attach fittings X X clean upper attach fittings and dog bone saddle area If off aircraft re grease bolts and return Spreader Bars inspect for loose screws and cracks amp seal between fairing and side skin Insp fairings X for cracking and loose screws On the aircraft and floats re coat exposed hardware with suitable X X coating for corrosion protection Closely inspect for wrinkled metal amp cracked flanges watch closely bulk X X heads 9 21 After hardware inspection coat with anti corrosion grease to X X protect Disassemble and grease the flying wire clevis bolts pins Float structure interior pull up baggage floors and inspect bulkheads Baggage compartment covers and seals inspect for condition security operation excessive wear and corrosion under nutplates Pumper Tube Installation inspect for condition securi
8. 31 31 00 720 Portable Oxygen Mask Detailed Inspection Task 35 30 00 220 kkk End of Inspection Document OA Inspection Items 2013 Cessna Aircraft Company Retain printed data for historical reference only For future maintenance use only current data Page 2 Print Date Mon Nov 04 09 16 43 WST 2013 MODEL 208 MAINTENANCE MANUAL Rev 26 5 15 01 Rev 25 INSPECTION DOCUMENT 01 Date Registration Number Serial Number Total Time 1 Description A Inspection Document 01 gives a list of item s which are completed at every 12 calendar months B Inspection items are given in the sequence of the zone in which the inspection is completed A description of the inspection as well as the Item Code Number are supplied for cross reference to section 5 10 01 Frequently tasks give more information about each inspection These tasks are found in the individual chapters of this manual C The right portion of each page gives space for the mechanic s and inspector s initials and remarks You can use copies of these pages as a checklist while you complete the tasks in this Inspection Document 2 General Inspection Criteria A As you complete each of the inspection tasks in this Inspection Document examine the adjacent area while access Is available to find conditions that need more maintenance B If it is necessary to replace a component or to make a change to a system while you complete a task do the task again b
9. 4 217 218 233 234 293 254 25 7 258 311 312 320 341 2013 Cessna Aircraft Company Retain printed data for historical reference only For future maintenance use only current data Page 1 Print Date Wed Oct 23 13 12 56 WST 2013 MODEL 208 MAINTENANCE MANUAL Rev 26 5 15 11 Rev 24 ITEM CODE IN NUMBER TASK ZONE MECH Sp REMARKS C272001 Rudder Bar Bearings and Rudder Pedals Lubrication 211 212 Task 27 20 00 640 213 214 B273001 Elevator System Functional Check Task 27 30 00 720 B275001 Flap System Functional Check Task 27 50 00 720 251 252 511 611 525 625 End of Inspection Document 11 Inspection Items 2013 Cessna Aircraft Company Retain printed data for historical reference only For future maintenance use only current data Page 2 PT6A 114A Maintenance Manual P N3043512 Chapter 72 00 00 R29 Mar 08 2013 Table 601 PT6A 114A Table 601 Periodic Inspection Schedule VH aaan Serial Number Bee Ce eee eee JOD NUMDET cocir eescnneetantexcaecs Job Co ordinator ccc ccc cceccecceeccuccuuces FEO asec weet WANING Sisters ceeneetcewcgse2 1 ENGINE EXTERNALS AME SIG LAME SIG 1 All accessible connections clamps and brackets for attachment NOTE Inspect accessible lockwire and safety A Tubing Wiring Control Linkages Hose Assemblies cable for security and installation 2 Wear chafing cracks and corrosion NOTE Visually inspect insulated air tubes f
10. Document examine the adjacent area while access is available to find conditions that need more maintenance B If it is necessary to replace a component or to make a change to a system while you complete a task do the task again before the system or component is returned to service C Inspection Kits are available for some Inspection Documents They supply consumable materials used to complete the inspection item s given for the interval Refer to the Model 208 Illustrated Parts Catalog Introduction Service Kit List to find applicable part numbers ITEM CODE NUMBER B560001 Functional Check of the Windshield Task 56 00 01 720 po ff fo A710001 Engine Compartment Zonal Inspection Task 71 00 01 f fp 210 End of Inspection Document 02 Inspection Items re TASK ZONE MECH REMARKS 2013 Cessna Aircraft Company Retain printed data for historical reference only For future maintenance use only current data Page 1 Print Date Thu May 16 17 28 00 WST 2013 MODEL 208 MAINTENANCE MANUAL Rev 26 5 15 06 Rev 26 INSPECTION DOCUMENT 06 Date Registration Number Serial Number Total Time 1 Description A Inspection Document 06 gives a list of item s which are completed at every 200 Hours or 12 calendar months whichever occurs first B Inspection items are given in the sequence of the zone in which the inspection is completed A description of the inspection as well as the Item Code Number are supplied fo
11. EN items have determine if OPEN items been transferred through were transferred Notify issuing MRO and Operator s Chief Pilot of the deficiency M R Part 2 Check aircraft Log Books for a Notify the MRO or LAME Check all cleared certification for the of the deficiency endorsements for correct maintenance performed certification Ensure current M R totals if affected are adjusted for the correct totals M R Part 3 Notify issuing MRO and Check all progressive totals Operator s Chief Pilot of the are correct additions deficiency Ensure Work Package TTIS and Log Book entries are adjusted for the correct totals AVTRAC Maintenance Tracking Form 038 Initial Issue 26 Aug 2011 2 AVTRAC Goes es AIRCRAFT TYPE 208 REGISTRATION VH OPH Aero Jacks Pty Lid INSPECTION M R Inspections MC No MC2013 1599 SERIAL No 0157 JOB No VDO LDGS TTIS FORM 100 WORKSHEET JOB CO ORDINATOR Lic No DATE ITEM WORK REQUIRED DEFECT COMPLIANCE RECTIFICATION COMPONENT CHANGES LAME Sig Lic q4 Maintenance Release PART No OFF Action Replace CASA I SNe FF e Ba Sir Release and S No ON l ge 2 ELT Functional Test PART No OFF I 8X FF P N 453 6603 eile Can be performed and certified by an Airframe Eng Category licence S No ON RIN No AME 3 Propeller Governor PART No OFF _ I SNe FF 3035926 TER Cessna 208 Component Time Limits 2
12. ENT 0A Date Registration Number Serial Number Total Time 1 Description A Inspection Document OA gives a list of item s which are completed during the Annual inspection interval B Inspection items are given in the sequence of the zone in which the inspection is completed A description of the inspection as well as the Item Code Number are supplied for cross reference to section 5 10 01 Frequently tasks give more information about each inspection These tasks are found in the individual chapters of this manual C The right portion of each page gives space for the mechanic s and inspector s initials and remarks You can use copies of these pages as a checklist while you complete the tasks in this Inspection Document 2 General Inspection Criteria A As you complete each of the inspection tasks in this Inspection Document examine the adjacent area while access is available to find conditions that need more maintenance B If it is necessary to replace a component or to make a change to a system while you complete a task do the task again before the system or component is returned to service C Inspection Kits are available for some Inspection Documents They supply consumable materials used to complete the inspection item s given for the interval Refer to the Model 208 Illustrated Parts Catalog Introduction Service Kit List to find applicable part numbers ITEM CODE NUMBER IN SP 1052001 Aircraft Records
13. Eng Eng1 14 VFR IFR Radio Periodic Inspection Action Inspect Chapter 4 Catalina Airlines Pty Ltd SOM Eng 45 1st Stage Compressor IRN B 10 Action Inspect AD Eng 5 amd 8 Appendix A 8 16 Engine Oil Filter IRN B 12 Action Service AD Eng 5 amd 8 Appendix A 5 AIRCRAFT TYPE 208 REGISTRATION VH OPH INSPECTION M R Inspections MC No MC2013 1599 0157 JOB No VDO LDGS JOB CO ORDINATOR Lic No COMPLIANCE RECTIFICATION PART No OFF S No OFF PART No ON S No ON COMPONENT CHANGES LAME Sig Lic R N No PART No OFF S No OFF PART No ON S No ON R N No S No OFF PART No ON S No ON PART No OFF R N No S No OFF PART No ON S No ON PART No OFF R N No HEREBY CERTIFY THAT ALL WORK DETAILED HAS BEEN COMPLETED AND CERTIFIED FOR IN ACCORDANCE WITH THE REQUIREMENTS OF APPLICABLE MANUALS AND SCHEDULES THIS SIGNATURE CONSTITUTES A CERTIFICATION PURSUANT TO CAR 422ZE HEATER APU AIR CYCLE MACHINE VDO HOURS JOB CO ORDINATOR LAME SIGNATURE Date 2 AVTRAC Goes es AIRCRAFT TYPE 208 REGISTRATION VH OPH Aero Jacks Pty Lid INSPECTION M R Inspections MC No MC2013 1599 SERIAL No 0157 JOB No VDO LDGS TTIS FORM 100 WORKSHEET JOB CO ORDINATOR Lic No DATE ITEM WORK REQUIRED DEFECT COMPLIANCE RECTIFICATION COMPONE
14. NG Aero Jacks Pty Ltd FORM 100 WORKSHEET ITEM WORK REQUIRED DEFECT 9 Flow Divider IRN Action Overhaul 3019906 20027 Eng Eng1 10 Engine Insp IRN B 3 Action Carry Out PT6 Health Check Run P amp W MM Use Form 009 Eng Eng1 41 Engine Oil IRN B 1 Action Replace AD Eng 5 amd 8 Appendix A 7 42 Power Recovery Wash IRN B 4 Action Carry Out Catalina Airlines Pty Ltd C208 SOM AIRCRAFT TYPE 208 REGISTRATION VH OPH INSPECTION M R Inspections MC No MC2013 1599 0157 JOB No VDO LDGS JOB CO ORDINATOR Lic No COMPLIANCE RECTIFICATION PART No OFF S No OFF PART No ON S No ON COMPONENT CHANGES LAME Sig Lic R N No PART No OFF S No OFF PART No ON S No ON R N No S No OFF PART No ON S No ON PART No OFF R N No S No OFF PART No ON S No ON PART No OFF R N No HEREBY CERTIFY THAT ALL WORK DETAILED HAS BEEN COMPLETED AND CERTIFIED FOR IN ACCORDANCE WITH THE REQUIREMENTS OF APPLICABLE MANUALS AND SCHEDULES THIS SIGNATURE CONSTITUTES A CERTIFICATION PURSUANT TO CAR 422ZE HEATER APU AIR CYCLE MACHINE VDO HOURS JOB CO ORDINATOR LAME SIGNATURE Date 2 AVTRAC yp MAINTENANCE TRACKING Aero Jacks Pty Ltd FORM 100 WORKSHEET ITEM WORK REQUIRED DEFECT 43 Engine Chip Detector IRN B 11 Action Carry Out AD ENG 5 amd 8 Appendix A 6
15. NT CHANGES LAME Sig Lic 7 Fuel Pump Outlet PART No OFF senso SNe OFF Filter P N 3033355 saad Eng S No ON 48 Hand Held Cockpit Fwd PART No OFF eons SiN OFF Avtrac Form 010 2 i pI PART No ON Eng Use Form 010 SON RIN No AME 19 Life Jackets PART No OFF Action Inspect none SiN OFF Date inspection Check for expire date on each jacket packet is S No ON sealed 20 Daily Inspection PART No OFF an R SiN OFF Pilots Operating Handbook S No ON RN No Co HEREBY CERTIFY THAT ALL WORK DETAILED HAS BEEN COMPLETED AND CERTIFIED FOR IN ACCORDANCE WITH THE REQUIREMENTS OF APPLICABLE MANUALS AND SCHEDULES THIS SIGNATURE CONSTITUTES A CERTIFICATION PURSUANT TO CAR 422ZE HEATER APU AIR CYCLE MACHINE VDO HOURS JOB CO ORDINATOR LAME SIGNATURE LIC No Date s AVTRAC Spon acer AIRCRAFT TYPE 208 REGISTRATION VH OPH Aero Jacks Pty Lid INSPECTION M R Inspections MC No MC2013 1599 SERIAL No 0157 JOB No VDO LDGS TTIS FORM 100 WORKSHEET JOB CO ORDINATOR Lic No DATE ITEM WORK REQUIRED DEFECT COMPLIANCE RECTIFICATION COMPONENT CHANGES LAME Sig Lic 21 Engine PART No OFF IRN B 2 Action Inspect S No OFF Vibration Isolator Mounts PART No ON Inspect for general condition deterioation and S No ON Eng Sagging Eng1 R N No 22 Aileron Trim PART No OFF Action Service SINo OFF Actuator 2 P N 2661615 1 PART No ON En
16. NTENANCE PRACTICES 6 Check scavenge oil pump housing for leaks S 7 Check the AGB internal scavenge oil pump inlet screen Ref Chapter 72 60 00 CLEANING INSPECTION Collect drained oil Using a hp Eei aia EAE mirror and a flashlight inspect the scavenge oil RELATIVE pump inlet screen Any foreign material found HUMIDITY TROPICAL blocking the screen or contained in the oil ENVIRONMENT should be identified before further operation Ref Unscheduled Inspection 2 Check fuel pump for installation and leaks Ref 73 10 02 NOTE If airframe fuel boost pump fails or is inadvertently left off for an accumulative time in excess of 10 hours the engine driven fuel pump must be removed and replaced The removed pump should be sent to an approved overhaul facility 3 Check inlet screen for foreign matter or distortion clean and reinstall or install new screen Ref 73 10 02 4 Check outlet filter for foreign matter or distortion Ref 73 10 02 Install new filter as service conditions dictate not to exceed 600 hours and when fuel system contamination is suspected 5 If Sundstrand fuel pump installed a Check fuel pump coupling in situ for fretting and corrosion Ref 73 10 02 b Remove fuel pump and inspect the drive coupling and cover accessory gearbox side for signs of reddish brown iron oxide stains If NOT APPLICABLE OSIP stains are observed return the fuel pump to an CARDS RAISED IN CONTROL appro
17. PERTH MAINTENANCE CONTROL OFFICE Avtrac Gold Portal AIRCRAFT TYPE CESSNA 208 VH OPH DATE 5 Nov 13 INSPECTION Interval Inspections MC NUMBER MC2013 1599 ORGANISATION Aero Jacks Pty Ltd Instruction No 1 Transfer any open endorsements from current Maintenance Release to Worksheets Complete the Inspections and events listed in Work Package certify Complete the OSIP Inspections and events listed in Work Package Strike through items on Form 090 attached to Maintenance Release Belmont WA 6984 Belmont WA 6104 Post immediately to NOTE CHANGE OF ADDRESS 4 Mail ONLY Consigned Freight ONLY No mail Avtrac WA Pty Ltd Avtrac WA Pty Ltd P O Box 568 Unit 2 61 Belmont Avenue Paul Carey Mobile 0418 959 892 Avtrac WA Pty Ltd Phone 08 9477 5205 Perth Maintenance Control Office Fax 08 9477 1170 P O Box 568 Belmont WA 6984 Mobile 0418 959 892 2 AVTRAC apres TRACKING EXPIRED MAINTENANCE RELEASE ASSESSMENT PROCEDURE M R Part 1 Notify issuing MRO and Check issue details are correct in Operator s Chief Pilot of the top section deficiency YES Notify issuing MRO and M R Part 1 Check Part 2 for any R Check Maintenance Required YES clearing action Operator s Chief Pilot of the deficiency section for any OPEN items M R Part 2 Check Work Package to Check current M R and Check for any OPEN items YES determine of OP
18. T No ON S No ON R N No HEREBY CERTIFY THAT ALL WORK DETAILED HAS BEEN COMPLETED AND CERTIFIED FOR IN ACCORDANCE WITH THE REQUIREMENTS OF APPLICABLE MANUALS AND SCHEDULES THIS SIGNATURE CONSTITUTES A CERTIFICATION PURSUANT TO CAR 422ZE HEATER APU AIR CYCLE MACHINE VDO HOURS JOB CO ORDINATOR LAME SIGNATURE Date 2 AVTRAC acca AIRCRAFT TYPE 208 REGISTRATION VH OPH Aero Jacks Pty Lid INSPECTION M R Inspections MC No MC2013 1599 SERIAL No 0157 JOB No VDO LDGS TTIS FORM 100 WORKSHEET JOB CO ORDINATOR Lic No DATE ITEM WORK REQUIRED DEFECT COMPLIANCE RECTIFICATION COMPONENT CHANGES LAME Sig Lic 33 Main Battery PART No OFF Electrolyte Check 2 Eng S No ON 34 Relief Valve Air Filter PART No OFF Action Replace I SiN FF Vacuum System Eng S No ON m RIN No AME 35 Hand Held Cabin Fwd PART No OFF Avtrac Form 010 2 S No ON RN No me 36 Jan PART No OFF 5 15 20 Action Inspect Functional Check S No ON RN No me HEREBY CERTIFY THAT ALL WORK DETAILED HAS BEEN COMPLETED AND CERTIFIED FOR IN ACCORDANCE WITH THE REQUIREMENTS OF APPLICABLE MANUALS AND SCHEDULES THIS SIGNATURE CONSTITUTES A CERTIFICATION PURSUANT TO CAR 42ZE HEATER APU AIR CYCLE MACHINE VDO HOURS JOB CO ORDINATOR LAME SIGNATURE LIC No Date Print Date Mon Nov 04 09 15 34 WST 2013 MODEL 208 MAINTENANCE MANUAL Rev 26 5 15 0A Rev 26 INSPECTION DOCUM
19. cklist while you complete the tasks in this Inspection Document 2 General Inspection Criteria A As you complete each of the inspection tasks in this Inspection Document examine the adjacent area while access is available to find conditions that need more maintenance B If it is necessary to replace a component or to make a change to a system while you complete a task do the task again before the system or component is returned to service C Inspection Kits are available for some Inspection Documents They supply consumable materials used to complete the inspection item s given for the interval Refer to the Model 208 Illustrated Parts Catalog Introduction Service Kit List to find applicable part numbers ITEM CODE NUMBER C221201 Autopilot Servos Lubrication Task 22 12 00 640 226 232 ef fp A245001 Power Distribution Boxes Detailed Inspection Task 24 121 122 50 00 220 A251001 Crew Seats Detailed Inspection Task 25 10 00 220 231 232 ef pf A251003 Passenger Seats Detailed Inspection Task 25 21 00 220 231 232 ef fp a TASK ZONE MECH REMARKS 2013 Cessna Aircraft Company Retain printed data for historical reference only For future maintenance use only current data Page 1 Print Date Fri May 17 09 09 00 WST 2013 ITEM CODE NUMBER B271001 C271003 C273001 B284103 B313103 B324001 B332001 A520001 A520003 A781001 MODEL 208 MAINTENANCE MANUAL Rev 26 5 15 10 Rev 26 IN SP
20. eal Ref 72 10 00 Page 1 PT6A 114A Maintenance Manual P N3043512 Chapter 72 00 00 R29 Mar 08 2013 Table 601 1 ENGINE EXTERNALS AMESIG LAME SIG G Accessories 1 Attachment and linkages air oil and fuel lines Ref 73 10 07 08 NOTE Visually inspect insulated air tubes for signs of swelling cracking bulging of rubber sheath material Refer to repair section and SB1687 Replace as necessary a a 3 Starter Generator Gearshaft Splines for wear NOT APPLICABLE OSIP CARDS RAISED IN CONTROL SYSTEM Ea ENGINE INTERNALS AMESIG LAMESIG Compressor The CT disk and blade set must be sent for an Turbine CT Disk inspection per the overhaul manual instructions NOT APPLICABLE OSIP Assembly at the intervals that follow CARDS RAISED IN CONTROL NOTE 1 PT6A 114 114A refer to SB1703 SYSTEM B Hot Section 1 Examine with borescope Ref Para 9 3 SYSTEMS s S lt 273 3 H AMESIG LAMESIG Replace disposable filter elements Post SB1282 Examine and clean permanentPre SB1 282 filter ap parle a E elements at an overhaul facility The filter may be utilized for further 1500 hour periods Sal maintaining the same inspection cleaning schedule 4 Check magnetic chip detector s for continuity open circuit must exist indicating no contamination at pole tips If continuity exists remove and inspect for contamination Any foreign material found on the chip detector or in the main oil filter
21. ed so as to ensure that the system or component remains serviceable for the period between inspections subject to normal operation inservice maintenance and reporting When carrying out an inspection the Manufacturers Maintenance Manual amp Bulletins should be referred to for the complete inspection and test procedures EEE E EE we ce eee AME LAME 1 Accessible interwiring for security damage and deterioration microphones headset cords for damage and deterioration accessible plugs and sockets for damage and security 2 Fuses for adequacy of spares Check all active fuses for correct type and rating 3 Wire aerials for fraying and deterioration fixed antennae for damage and security associated fittings and supports for security deterioration and damage aerial insulators for freedom from accumulated dirt and or grease 4 Removable units for security in racks isolators mounting racks and accessible bonding straps for damage deterioration and security 5 Switches and controls for correct mechanical operation radio panel lamps for serviceability frequency charts decals and controls for legibility 6 Communication systems for correct performance 7 ADF system for accuracy and correct performance in all modes of operation 8 VOR and ILS systems for correct operation using an approved simulator Test VOR on 0 90 180 270 and one other widely separated radial for system accuracy within the following limi
22. efore the system or component is returned to service C Inspection Kits are available for some Inspection Documents They supply consumable materials used to complete the inspection item s given for the interval Refer to the Model 208 Illustrated Parts Catalog Introduction Service Kit List to find applicable part numbers ITEM CODE NUMBER IN SP A251000 Smoke Goggle General Visual Inspection Task 25 10 801 802 00 210 B262001 Portable Fire Extinguisher Functional Check Weight 215 216 Check Task 26 20 00 720 251 252 B272003 Rudder System Functional Check Float Kit Installation Task 27 20 00 721 TASK ZONE MECH REMARKS 211 212 213 214 21 218 233 234 203 254 25 258 311 312 320 341 B301102 Inboard TKS Wing Panel Pressurization Functional 501 601 Check Task 30 11 00 721 AUX 2013 Cessna Aircraft Company Retain printed data for historical reference only For future maintenance use only current data Page 1 Print Date Mon Nov 04 09 16 43 WST 2013 ITEM CODE NUMBER A321001 A324001 A324005 A324009 B342101 B350101 A714101 MODEL 208 MAINTENANCE MANUAL Rev 26 5 15 01 Rev 25 IN SP Main Landing Gear Detailed Inspection Task 32 10 00 721 722 220 Brakes Detailed Inspection Task 32 40 00 220 721 722 ef fp Main Landing Gear Wheels and Tires Detailed Inspec 721 722 tion Task 32 40 00 222 Nose Landing Gear Wheel and Tire Detailed Inspection 710 Task 32 40
23. elease and S No ON include in Work Package 28 12 Month Inspection PART No OFF 5 15 01 Action Inspect Interval 1C Inspection S No ON RIN No AME HEREBY CERTIFY THAT ALL WORK DETAILED HAS BEEN COMPLETED AND CERTIFIED FOR IN ACCORDANCE WITH THE REQUIREMENTS OF APPLICABLE MANUALS AND SCHEDULES THIS SIGNATURE CONSTITUTES A CERTIFICATION PURSUANT TO CAR 422ZE HEATER APU AIR CYCLE MACHINE VDO HOURS JOB CO ORDINATOR LAME SIGNATURE LIC No Date 2 AVTRAC yp MAINTENANCE TRACKING Aero Jacks Pty Ltd FORM 100 WORKSHEET ITEM WORK REQUIRED DEFECT 29 24 Month Inspection 5 15 02 Action Inspect Interval 2C Inspection Cessna CIP Eng 30 200hr 12 month Inspection 5 15 06 Action Inspect Interval 200hrs 1C Inspection Cessna CIP Eng 34 800hr 24 month Inspection 5 15 10 Action Inspect Interval 2A 2C Inspection Cessna CIP 32 1 600hr 24 month Inspection 5 15 11 Action Inspect Interval 4A 2C Inspection Cessna CIP AIRCRAFT TYPE 208 REGISTRATION INSPECTION M R Inspections MC No MC2013 1599 VH OPH JOB No VDO LDGS JOB CO ORDINATOR Lic No COMPLIANCE RECTIFICATION PART No OFF S No OFF PART No ON S No ON 0157 COMPONENT CHANGES LAME Sig Lic R N No PART No OFF S No OFF PART No ON S No ON R N No PART No OFF S No OFF PART No ON S No ON R N No PART No OFF S No OFF PAR
24. g Disassemble inspect and lubricate S No ON ees RIN No 23 100 Hour Inspection A6 Action Inspect Float Inspection Wipline 8000 SM Wipline Model 8000 Service Manual Inspection and Time Limits PART No OFF S No OFF PART No ON S No ON R N No PART No OFF S No OFF PART No ON S No ON R N No 24 200 Hour Inspection A7 Action Inspect Float Inspection Wipline 8000 SM Wipline Model 8000 Service Manual Inspection and Time Limits HEREBY CERTIFY THAT ALL WORK DETAILED HAS BEEN COMPLETED AND CERTIFIED FOR IN ACCORDANCE WITH THE REQUIREMENTS OF APPLICABLE MANUALS AND SCHEDULES THIS SIGNATURE CONSTITUTES A CERTIFICATION PURSUANT TO CAR 422ZE HEATER APU AIR CYCLE MACHINE VDO HOURS JOB CO ORDINATOR LAME SIGNATURE LIC No Date 2 AVTRAC ii AIRCRAFT TYPE 208 REGISTRATION VH OPH Aero Jacks Pty Ltd INSPECTION M R Inspections MC No MC2013 1599 SERIAL No 0157 JOB No VDO LDGS TTIS FORM 100 WORKSHEET JOB CO ORDINATOR Lic No DATE ITEM WORK REQUIRED DEFECT COMPLIANCE RECTIFICATION COMPONENT CHANGES LAME Sig Lic 25 25 Hour Inspection PART No OFF A5 Action Inspect Float Inspection Eng an ene Service Manual Inspection S No ON 26 Annual Inspection PART No OFF a Site FF Intervs OA 2 Eng S No ON _ RIN No AME 27 Table 601 PART No OFF Action Inspect Photocopy issued Maintenance R
25. ht to two decimal places Check that the pressure indicator mechanism where fitted is registering within the operational range and appears to be free and operating correctly Where possible without discharging any contents check that the actuating device is undamaged free from corrosion and moves freely Replace the extinguisher in the assigned location and record maintenance on maintenance tag where applicable CASA CAO 103 Section 103 16 Issue 2 requirements The following information at least shall be clearly marked on each extinguisher and able to be clearly read by the pilot without removing the unit from it s cradle No Action Required CT AME SIG LAMESIG Check the type of extinguisher is clearly marked write Halon ina permanent marker or affix a permanent tag Check that the termination date of current service life both the next 6 month inspection and the 12 year inspection due dates available online are clearly marked on the extinguisher or tag ae ea e CT clearly marked on the extinguisher or tag Ke S are clearly marked Notes AVTRAC Maintenance Tracking Form 010 Initial Issue 25 May 2010 2 AVTRAC APTE Anc TRACKING PT6 ENGINE GROUND RUN RECORD SHEET Aircraft Type Type of check And Model Table 1 r o e Table 2 Current Aircraft Status TTIS Cyc Table 3 ameron e J onesna START ITT MAX LIMIT a START MAX ITT rr an an an PROP RPM NP
26. in the sequence of the zone in which the inspection is completed A description of the inspection as well as the Item Code Number are supplied for cross reference to section 5 10 01 Frequently tasks give more information about each inspection These tasks are found in the individual chapters of this manual C The right portion of each page gives space for the mechanic s and inspector s initials and remarks You can use copies of these pages as a checklist while you complete the tasks in this Inspection Document 2 General Inspection Criteria A As you complete each of the inspection tasks in this Inspection Document examine the adjacent area while access is available to find conditions that need more maintenance B If it is necessary to replace a component or to make a change to a system while you complete a task do the task again before the system or component is returned to service C Inspection Kits are available for some Inspection Documents They supply consumable materials used to complete the inspection item s given for the interval Refer to the Model 208 Illustrated Parts Catalog Introduction Service Kit List to find applicable part numbers ITEM CODE IN NUMBER TASK ZONE MECH SP REMARKS B271003 Aileron System Functional Check Task 27 10 00 721 211 212 217 218 233 234 253 254 251 252 503 525 603 625 B272001 Rudder System Functional Check Standard Rudder In stallation Task 27 20 00 720 211 212 213 21
27. llation Ref 73 10 01 MAINTENANCE PRACTICES C Ignition System 1 Check ignition exciter current regulator for installation and condition Ref 74 10 00 2 Check ignition cables for chafing wear and installation Ref 74 20 00 3 Check spark igniter glow plugs for cleanliness and erosion Check function Ref 74 20 00 Pneumatic System 1 Check P3 filter for installation Ref 73 10 07 2 Inspect pneumatic tubes and lines for cracks and damages especially at the end fittings and joints 3 Clean or replace filter dependent on condition service experience or environment Ref 73 10 07 NOTE Visually inspect the P3 filter for corrosion If the filter shows presence of corrosion discard the filter and replace with a new filter 4 Clean and inspect Post SB1495 P3 filter drain valve housing assembly Ref 73 10 07 5 Replace disposable filter based on condition service experience or environment 6 Clean or replace permanent filter based on NOT APPLICABLE OSIP condition service experience or environment CARDS RAISED IN CONTROL Ship to an approved overhaul facility for SYSTEM ultrasonic cleaning 7 Check the bleed valve Ref 75 30 00 Inspection Check END Page 4 WIPLINE MODEL 8000 SERVICE MANUAL 5 6 INSPECTION TIME LIMITS AND CHECKLIST INSTRUCTIONS PROCEEDURES er ae ee eee ae General Wash aircraft and floats with fresh water If
28. nel lamps for serviceability frequency charts decals and controls for legibility 6 Communication audio systems for correct performance 7 Inspect the Emergency Locator Transmitter Batteries for electrolyte leakage and battery life Refer Continued Airworthiness Requirements for all avionic equipment POST INSPECTION CHECK On completion of the inspection check that no tooling maintenance equipment or rags have been left in the aircraft and all panels access doors detachable fairings and fillets have been correctly secured Radio inspection completed for VFR Operations 1 CACC E LAME No Date Note Correct performance or operation means meeting the system manufacturers in service test specifications and tolerances in all functions A signature on this Document constitutes a certification pursuant to CAR 42ZE Issue Date 05 2013 CA C208 CIP 013 1 RHEN Issue 07 Section 5 Page 1 of 1 CATALINA AIRLINES PTY LTD CESSNA 208 Aircraft MAINTENANCE SYSTEM ADDITIONAL INSPECTION VH Date l The inspections detailed in this schedule shall be inspected or tested so as to ensure that the system or component remains serviceable for the period between inspections subject to normal operation inservice maintenance and reporting When carrying out an inspection the Manufacturers Maintenance Manual amp Bulletins or releavant EO s should be referred to for the complete inspection and test procedu
29. or signs of swelling cracking bulging of rubber sheath material Refer to repair section and SB1687 Replace as necessary 3 Fuel and oil lines for leaks 4 Depending on operating conditions and environment examine linkages at regular intervals Pay particular attention to rear linkage cam box fuel control unit arm telescopic rod and rod end fittings Disconnect rod ends and clean using solvent PWC11 027 or PWC11 031 Lubricate with light grease PWC04 001 after engine external wash Examine rod end for corrosion roughness in rotation side play and radial play After lubrication reinstall rod ends and torque to specified value Ref 76 10 00 Check free movement of linkage NOTE With the exception of rod end fittings linkages generally will operate satisfactorily without lubrication While lubrication will be effective in some instances it must be realized that grease and oil attracts dirt and foreign matter Depending on local conditions operators should take these facts into consideration before deciding to lubricate components Air Inlet Screen Cleanliness Ref 72 20 00 C Gas Generator External surfaces and fireseal mount ring Case brackets for cracks distortion and corrosion Ref 72 30 04 Fireseal Mount Cracks and attachment of brackets and seals Rings Ref 72 30 01 02 E Exhaust Duct 1 Cracks and distortion Ref 72 50 05 MAINTENANCE PRACTICES F Propeller Shaft Check for oil leaks S
30. pecifications and tolerances in all functions A signature on this Document constitutes a certification pursuant to CAR 42ZE Issue Date 05 2013 CA C208 CIP 013 1 RHEN Issue 07 Section 4 Page 2 of 2 CATALINA AIRLINES PTY LTD CESSNA 208 Aircraft MAINTENANCE SYSTEM VFR RADIO INSPECTION VH Date _ lI The radio systems amp components detailed in this schedule shall be inspected or tested so as to ensure that the system or component remains serviceable for the period between inspections subject to normal operation inservice maintenance and reporting When carrying out an inspection the Manufacturers Maintenance Manual amp Bulletins should be referred to for the complete inspection and test procedures PE A E A E EN AE AME LAME 1 Accessible interwiring for security damage and deterioration microphones headset cords for damage and deterioration accessible plugs and sockets for damage and security 2 Fuses for adequacy of spares Check all active fuses for correct type and rating 3 Wire aerials for fraying and deterioration fixed antennae for damage and security associated fittings and supports for security deterioration and damage aerial insulators for freedom from accumulated dirt and or grease 4 Removable units for security in racks isolators mounting racks and accessible bonding straps for damage deterioration and security 5 Switches and controls for correct mechanical operation radio pa
31. pray Check side play 3 32 to 1 16 inches max tolerance 1002554 Rev H Page 35 of 63 WIPLINE MODEL 8000 SERVICE MANUAL INSTRUCTIONS PROCEEDURES HOURLY LIMITS MECHANIC General Petals PE FO 100 200 Aone Right Lett N ivot blocks and forks i t or sonaton tuoeaten corossat TXT FL nee ed a a S a E a Insp Main gear slide tube ram and locking Grease with HCF p n 605 hooks for lubrication Lube carriage zerk Spray locking hooks form the X liberally top with LPS 2 to penetrate x Wheels and tire inspect for wear pressure condition 45lbs _ 5lbs X X Brake assemblies inspect for wear X X corrosion leakage Hydraulic fluid screen clean and inspect NOTE If floats sit for extended periods of time l e If removed during winter months screen should be cleaned before putting X X floats back into service Hydraulic fluid in reservoir should be checked for moisture or other contaminates and changed if necessary Insp FWD slide tube mounting bolt for corrosion and wear when the gear are out X Clean and lube the slide tube before returning Main and Nose gear actuator assemblies inspect for condition lubrication leakage corrosion and cleanliness X X With gear out Inspect FWD slide tube mounting bolt for corrosion and wear Clean amp grease FWD slide tube a inspect for cracks delamination and paint Main gear drag link garlock bushings inspect for condition lubrication and X co
32. r cross reference to section 5 10 01 Frequently tasks give more information about each inspection These tasks are found in the individual chapters of this manual C The right portion of each page gives space for the mechanic s and inspector s initials and remarks You can use copies of these pages as a checklist while you complete the tasks in this Inspection Document 2 General Inspection Criteria A As you complete each of the inspection tasks in this Inspection Document examine the adjacent area while access is available to find conditions that need more maintenance B If it is necessary to replace a component or to make a change to a system while you complete a task do the task again before the system or component is returned to service C Inspection Kits are available for some Inspection Documents They supply consumable materials used to complete the inspection item s given for the interval Refer to the Model 208 Illustrated Parts Catalog Introduction Service Kit List to find applicable part numbers ITEM CODE NUMBER IN SP B236001 Static Discharge System Functional Check Task 23 60 00 720 B243401 Marathon Ni Cad Battery Functional Check Capacity Check Task 24 34 00 720 A255101 Cargo Nets Detailed Inspection Task 25 51 00 220 251 252 255 256 25 258 B281001 Fuel Vent Line Float Valve Operational Check Task 28 575 675 ff 10 03 710 TASK ZONE MECH REMARKS 2013 Cessna Aircraft Company Retain p
33. racket is securely in place i a Check that the extinguisher is clean that the instructions for operation are Clearly legible and that the maintenance record tag where applicable is attached Check that the extinguisher including attachments is not damaged a ae Check that the exterior of the extinguisher is not pitted from corrosion i a Check that the discharge nozzle is the correct type a Check that the discharge nozzle is not blocked or damaged and the hose is free from obstructions or cracking or other signs of damage or deterioration and is securely fitted Check that the extinguisher is fully charged eg by overall mass Record weight to two decimal places Check that the pressure indicator mechanism where fitted is registering within the operational range and appears to be free and operating correctly Where possible without discharging any contents check that the actuating device is undamaged free from corrosion and moves freely Replace the extinguisher in the assigned location and record maintenance on maintenance tag where applicable CASA CAO 103 Section 103 16 Issue 2 requirements The following information at least shall be clearly marked on each extinguisher and able to be clearly read by the pilot without removing the unit from it s cradle No Action Required CT AME SIG LAMESIG Check the type of extinguisher is clearly marked write Halon ina permanent marker or affix a permanen
34. res PEENE NOES EEEE E E E ET E E ETEEN AME LAME Airframe Repairs 1 Lower Fuselage Bulkhead Flange EO 400 684 Inspect repaired area for security amp corrosion 2 Beam Truss repair EO 400 447 Inspect repaired area for security amp corrosion 3 Vertical Fin Repair EO 400 634 Inspect repaired area for security amp corrosion 4 Fuselage Bulkhead Repair EO 400 662 Inspect repaired area for security amp corrosion 5 Beam Axle Repair EO 400 620 Inspect repaired area for security amp corrosion POST INSPECTION CHECK On completion of the inspection check that no tooling maintenance equipment or rags have been left in the aircraft and all panels access doors Notes Indicate results of inspection amp any rectification necessary to maintain satisfactory condition LAME Signature 0ccecceeeeseeeeees Dale weaves essen A signature on this document constitutes a certification pursuant to CAR 42ZE Issue Date 05 2013 CA C208 CIP 013 1 RHEN Issue 07 Section 6 Page 1 of 1 MA VTRAC aprons TRACKING S N Table 3 1 Maintenance Schedule Level 1 2 and 3 Inspections for Vapourizing Liquid Halon Extinguishers No Action Required AME SIG LAME SIG Check that the extinguisher is conspicuous readily accessible and in its assigned location and the location sign Is visible and correct Check that the anti tamper device where fitted is intact a ee Check that an appropriate support b
35. rinted data for historical reference only For future maintenance use only current data Page 1 Print Date Thu May 16 17 28 00 WST 2013 MODEL 208 MAINTENANCE MANUAL Rev 26 5 15 06 Rev 26 ITEM CODE IN NUMBER TASK ZONE MECH Sp REMARKS B301003 Bleed Air Pressure Regulator Functional Check without 122 AUX TKS and not incorporating CAB93 2 Task 30 10 00 720 B341101 Pitot Tube Heaters Operational Check Task 34 11 00 710 End of Inspection Document 06 Inspection Items 2013 Cessna Aircraft Company Retain printed data for historical reference only For future maintenance use only current data Page 2 Print Date Fri May 17 09 09 00 WST 2013 MODEL 208 MAINTENANCE MANUAL Rev 26 5 15 10 Rev 26 INSPECTION DOCUMENT 10 Date Registration Number Serial Number Total Time 1 Description A Inspection Document 10 gives a list of item s which are completed at every 800 Hours or 24 calendar months whichever occurs first B Inspection items are given in the sequence of the zone in which the inspection is completed A description of the inspection as well as the Item Code Number are supplied for cross reference to section 5 10 01 Frequently tasks give more information about each inspection These tasks are found in the individual chapters of this manual C The right portion of each page gives space for the mechanic s and inspector s initials and remarks You can use copies of these pages as a che
36. rrosion Page 36 of 63 1002554 Rev H WIPLINE MODEL 8000 SERVICE MANUAL INSTRUCTIONS PROCEEDURES HOURLY LIMITS MECHANIC ee I ic ii iad id cei bs Clean the wheel wells to facilitate general X X condition inspection Main gear oleos inspect for evidence of leakage proper extension check cylinder for X X corrosion pitting cleanliness and security Hydraulic lines and fittings inspect for leaks Perr wocedons 2 X X condition and security Hydraulic Manifolds if equipped inspect for X X condition security and leaks Brake system plumbing inspect for leaks X X condition and security AN ea EOR ee ote ale If full servicing is required use 5606 hydraulic fluid amp Nitrogen X X Refer to section 5 2 compression leaks and proper pressure The oleo should be fully serviced or replaced with overhauled as required Perform retraction test Inspect main gear up and down lock hooks for proper engagement Inspect nose gear trolley for proper travel Inspect nose gear for excessive play in the down position Perform emergency gear extension amp retraction Nose and main wheel bearings disassemble pe eae ei WIIN g recommended water resistant X X and inspect grease 1002554 Rev H Page 37 of 63 CATALINA AIRLINES PTY LTD CESSNA 208 Aircraft MAINTENANCE SYSTEM IFR RADIO INSPECTION VH Date _ The radio systems amp components detailed in this schedule shall be inspected or test
37. t tag Check that the termination date of current service life both the next 6 month inspection and the 12 year inspection due dates available online are clearly marked on the extinguisher or tag ae ea e CT clearly marked on the extinguisher or tag Ke S are clearly marked Notes AVTRAC Maintenance Tracking Form 010 Initial Issue 25 May 2010 MA VTRAC aprons TRACKING S N Table 3 1 Maintenance Schedule Level 1 2 and 3 Inspections for Vapourizing Liquid Halon Extinguishers No Action Required AME SIG LAME SIG Check that the extinguisher is conspicuous readily accessible and in its assigned location and the location sign Is visible and correct Check that the anti tamper device where fitted is intact a ee Check that an appropriate support bracket is securely in place i a Check that the extinguisher is clean that the instructions for operation are Clearly legible and that the maintenance record tag where applicable is attached Check that the extinguisher including attachments is not damaged a ae Check that the exterior of the extinguisher is not pitted from corrosion i a Check that the discharge nozzle is the correct type a Check that the discharge nozzle is not blocked or damaged and the hose is free from obstructions or cracking or other signs of damage or deterioration and is securely fitted Check that the extinguisher is fully charged eg by overall mass Record weig
38. tations Course Bar Nav Indicator tolerance 3 degrees RMD s tolerance 4 degrees Course width tolerance 8 to 12 degrees Test LOC GS function On course tolerance 0 5 dot Up left tolerance 1 dot Down right tolerance 1 dots A signature on this Document constitutes a certification pursuant to CAR 42ZE Issue Date 05 2013 CA C208 CIP 013 1 RHEN Issue 07 Section 4 Page 1of2 CATALINA AIRLINES PTY LTD CESSNA 208 Aircraft MAINTENANCE SYSTEM IFR RADIO INSPECTION VH Date _ AME LAME 9 Marker system for correct performance 10 DME system for correct performance 11 Weather radar system for correct performance 12 Audio systems for correct operation 13 ATC transponder for correct performance 14 GPS system for correct operation 15 T CAS for correct operation 16 Radio altimeter system for correct operation 17 Inspect the Emergency Locator Transmitter Batteries for electrolyte leakage and battery life POST INSPECTION CHECK On completion of the inspection check that no tooling maintenance equipment or rags have been left in the aircraft and all panels access doors detachable fairings and fillets have been correctly secured Equipment not fitted should be shown as N Fin LAME column Refer Continued Airworthiness Requirements for all avionic equipment Note Correct performance or operation means meeting the system manufacturers in service test s
39. ty routing of hoses X X Page 34 of 63 1002554 Rev H INSTRUCTIONS PROCEEDURES Water rudder boots inspect for cuts tears and condition Water rudder steering and retract systems inspect the following cables for broken wire fittings for cable slippage cracks and distortion cable pulleys for freedom of rotation and cable guard pins for presence rigging On the aircraft remove clean inspect and grease the aux finlets on the horizontal stabilizer Electrical Pump and indicator light wiring inspect System for chafing broken or loose terminals and general condition Solenoids inspect wiring mounting and general condition Landing Gear Systems Pressure Switches inspect wiring mounting and general condition Pump Motors inspect wiring mounting and general condition Inspection and servicing nose gear tracks Nose gear box block tracks measured at slide route for wear 050 inches or less wear tolerance WIPLINE MODEL 8000 SERVICE MANUAL HOURLY LIMITS MECHANIC a a T Water rudder blades and posts inspect for damage security of attachment corrosion paint rigging Check post bolts and bushings and lube with LPS 2 Check top and bottom rollers for rotation and lube with LPS 2 or similar product Tension cables to 30 Ibs 5 Gold and white track and block clean and use grease Black track and block clean and dry or clean and wipe with silicone s
40. ved overhaul facility Ref 73 10 02 SYSTEM c Remove fuel pump and inspect the drive coupling and cover accessory gearbox side for signs of reddish brown iron oxide stains If stains are observed return the fuel pump to an approved overhaul facility Ref 73 10 02 6 Check drain valve for installation and leaks Ref 73 10 06 7 Check FCU for installation linkages and pneumatic tubes Ref 73 20 00 Page 3 PT6A 114A Maintenance Manual P N3043512 Chapter 72 00 00 R29 Mar 08 2013 Table 601 SYSTEMS CONT AMESIG LAMESIG Fuel System cont 9 Check FCU for bearing wash out indicated by blue dye grease and fuel mixed at FCU vent 8 For engines fitted with a manual override on the fuel control check FCU Manual Override System for static operation Ref 71 00 00 ADJUSTMENT TEST Ref Fault Isolation Operating Problems 10 a Remove FCU Ref 73 20 00 for drive body inspection driveshaft bearing replacement in accordance with the component maintenance NOT APPLICABLE OSIP manual Ref IPC P N 3043514 CARDS RAISED IN CONTROL 10 b Remove FCU and send for overhaul SASS 11 Check starting flow control flow divider for installation and leaks Ref 73 10 04 12 Leak test and function test fuel manifold NOT APPLICABLE OSIP adapter and nozzle assemblies Ref 73 10 05 CARDS RAISED IN CONTROL SYSTEM 13 Check oil to fuel heater insta

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