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PERTH MAINTENANCE CONTROL OFFICE WORK PACKAGE INSTRUCTIONS AIRCRAFT TYPE: CESSNA 441 VH LWY DATE: 16-Sep-13... INSPECTION: Phases & D + MR MC NUMBER: 013-1430. ORGANISATION: Avwest.. No 1 Instruction Transfer any open endorsements from current Maintenance Release to Worksheets. Complete the OSIP events listed in Work Package certify. 3 Issue new Maintenance Release for 1 months and 110 hours. Attach Form 090 # 013-1430 to Part 1 of the new MR. 4 Complete Loose Logbook entries as required. Post immediately to: 5 Mail ONLY: Avtrac Pty Ltd P.O.Box 568, Belmont WA 6984 Consigned Freight ONLY (No mail): Avtrac Pty Ltd Unit, 61 Belmont Ave, Belmont WA 6104 Paul Carey Mobile: 0418 959 89 Corsaire Pty Ltd Phone: (08) 9477 505 Perth Maintenance Control Office Fax: (08) 9477 1170 P.O.Box 568, Belmont WA 6984 Mobile: 0418 959 89

EXPIRED MAINTENANCE RELEASE ASSESSMENT PROCEDURE VH- Job No: M/R No: MRO: M/R Part 1: Check issue details are correct in top section. NO Notify issuing MRO and Operator s Chief Pilot of the deficiency. YES M/R Part 1: Check Maintenance Required section for any OPEN items. YES Check Part for any clearing action. NO Notify issuing MRO and Operator s Chief Pilot of the deficiency. NO M/R Part : Check for any OPEN items. YES Check Work Package to determine of OPEN items have been transferred through. NO Check current M/R and determine if OPEN items were transferred. NO Notify issuing MRO and Operator s Chief Pilot of the deficiency. NO M/R Part : Check all cleared endorsements for correct certification. NO Check aircraft Log Books for a certification for the maintenance performed. NO Notify the MRO or LAME of the deficiency. YES M/R Part 3: Check all progressive totals are correct additions. NO Notify issuing MRO and Operator s Chief Pilot of the deficiency. Ensure current M/R totals (if affected) are adjusted for the correct totals. Ensure Work Package TTIS and Log Book entries are adjusted for the correct totals. Assessed by: Date: Sig: AVTRAC Maintenance Tracking Form 038 Initial Issue: 6 th Aug 011

WORK PACKAGE ITEMS: WORK REQUIRED TO BE PERFORMED. FORM 085 AIRCRAFT TYPE: INSPECTION: 441 VH - LWY SERIAL No: 441 MC No: MC013-1430 TRANSFER THE ITEMS BELOW IN TO THE APPROPRIATE WORKSHEETS AND INITIAL ADMIN BOX 1. (ADMIN BOX - MAINTENANCE CONTROLLER USE) ITEM WORK REQUIRED / DEFECT OSIP DETAILS ADMIN 8 Airframe Daily Inspection C441 Flight Manual 100.00 1 Mths 1 7,748.00 /03/013 7,848.00 1/03/014 9 ine Pre-flight Inspection Garrett TPE331-10N MM 100.00 1 Mths 7,748.00 /03/013 7,848.00 1/03/014 10 ine 100 Hour Inspection Garrett TPE331-10N MM Table 601 and Honeywell SB TPE331-7-0180 100.00 Mths 7,748.00 LH 7,848.00 11 ine 150 Hour Inspection Garrett TPE331-10N MM Table 601 and Honeywell SB TPE331-7-0180 150.00 Mths 7,748.00 RH 7,898.00 1 ine 300 Hour Inspection Garrett TPE331-10N MM Table 601 and Honeywell SB TPE331-7-0180 300.00 Mths 7,636.00 LH 7,936.00 13 Fwd Cabin Fire Extinguisher Avtrac Form 010 S/N X-837100 Amerex Model C35 Halon unit. 6 Mths /03/013 1/09/013 14 Transponders AD/RAD/47 amd Action: Test 4 Mths 9/1/01 8/01/014

WORK PACKAGE ITEMS: WORK REQUIRED TO BE PERFORMED. FORM 085 AIRCRAFT TYPE: INSPECTION: 441 VH - LWY SERIAL No: 441 MC No: MC013-1430 TRANSFER THE ITEMS BELOW IN TO THE APPROPRIATE WORKSHEETS AND INITIAL ADMIN BOX 1. (ADMIN BOX - MAINTENANCE CONTROLLER USE) ITEM WORK REQUIRED / DEFECT OSIP DETAILS ADMIN 15 LH Altimeter CAO 100.5 (4.4) Appendix A Clause of Attachment 1 P/N 43300-68 S/N 735 Action: Test 4 Mths 9/1/01 8/01/014 1 16 RH ine and Oil Filter SOAP Analysis 100.00 Mths 7,748.00 RH 7,848.00 17 Elevator Forward Spar AD/C400/10 amd 4 SB CQB 93-01 Para 1 Requirements 1 and 110.00 Mths 7,748.00 7,858.00 18 Racked Avionics Inspection Operator Supplemental Inspection Log Book Statement 110.00 Mths 7,748.00 7,858.00 19 Rosen Sunvisors Periodic Inspection R1180000-006 ICA Clean and adjust per ICA 100.00 Mths 7,748.00 7,848.00 0 Seat Belt and Shoulder Harness Periodic Inspection MSB CQB96-1 100.00 Mths 7,748.00 7,848.00 1 Aft Cabin Fire Extinguisher Avtrac Form 010 S/N Y-94073 Amerex Model C35TS Halon unit 6 Mths /03/013 1/09/013 3

WORK PACKAGE ITEMS: WORK REQUIRED TO BE PERFORMED. FORM 085 AIRCRAFT TYPE: INSPECTION: 441 VH - LWY SERIAL No: 441 MC No: MC013-1430 TRANSFER THE ITEMS BELOW IN TO THE APPROPRIATE WORKSHEETS AND INITIAL ADMIN BOX 1. (ADMIN BOX - MAINTENANCE CONTROLLER USE) ITEM WORK REQUIRED / DEFECT OSIP DETAILS ADMIN Emergency Exit AD/Gen/37 amd 9 6 Mths 1 /03/013 1/09/013 3 RH Altimeter CAO 100.5 (4.4) Appendix A Clause of Attachment 1 P/N 5934PAM-3 S/N 494637 Action: Test 4 Mths 9/1/01 8/01/014 4 RH ine 100 Hour Inspection Garrett TPE331-10N MM Table 601 and Honeywell SB TPE331-7-0180 100.00 Mths 7,748.00 RH 7,848.00 5 ine 300 Hour Inspection Garrett TPE331-10N MM Table 601 and Honeywell SB TPE331-7-0180 300.00 Mths 7,636.00 RH 7,936.00 6 ine 150 Hour Inspection Garrett TPE331-10N MM Table 601 and Honeywell SB TPE331-7-0180 150.00 Mths 7,748.00 LH 7,898.00 7 Compensating Resistor Garrett TPE331-10MMN Honeywell SB TPE331-7-0180 Test temperature compensating value 150.00 Mths 7,748.00 LH 7,898.00 8 LH Torque Limiter Bypass Valve Filter Honeywell SB TPE331-7-0180 Rev 34 34 Table 8 Pg 3 Remove and clean 400.00 Mths 7,379.40 7,779.40 4

WORK PACKAGE ITEMS: WORK REQUIRED TO BE PERFORMED. FORM 085 AIRCRAFT TYPE: INSPECTION: 441 VH - LWY SERIAL No: 441 MC No: MC013-1430 TRANSFER THE ITEMS BELOW IN TO THE APPROPRIATE WORKSHEETS AND INITIAL ADMIN BOX 1. (ADMIN BOX - MAINTENANCE CONTROLLER USE) ITEM WORK REQUIRED / DEFECT OSIP DETAILS ADMIN 9 Plenum Drain Valves 800 hr Inspection Honeywell SB TPE331-7-0180 Remove and Test for opening and closing 800.00 Mths 7,077.00 1 LH 7,877.00 30 Compensating Resistor Garrett TPE331-10N MM Honeywell SB TPE331-7-0180 Test temperature compensating value 150.00 Mths 7,748.00 RH 7,898.00 31 RH Torque Limiter Bypass Valve Filter Honeywell SB TPE331-7-0180 Rev 34 34 Table 8 Pg 3 Remove and clean 400.00 Mths 7,379.40 7,779.40 3 Plenum Drain Valves 800 hr Inspection Honeywell SB TPE331-7-0180 Remove and Test for opening and closing Action: Check 800.00 Mths 7,077.00 RH 7,877.00 33 LH ine and Oil Filter SOAP Analysis 100.00 Mths 7,748.00 LH 7,848.00 34 AIr Speed Indicator CAO 100.5 (5.4) Appendix A (5.3) P/N 43300-68 S/N 735 Action: Test 4 Mths 9/1/01 8/01/014 35 Pitot Static Test CAO 100.5 (3.4) Appendix A Clause 1 of Attachment 1 Action: Test 4 Mths 9/1/01 8/01/014 5

AIRCRAFT: VH - LWY TYPE: 441 MC No: MC013-1430 MR No:... FORM 090 COMPONENTS, SPECIAL INSPECTIONS, AD s AND SCHEDULED INSPECTIONS: Action Name AD/Reference Pos Tolerance Due Hours Due Date Due Cycles Due Inspect Daily Inspection 441 AFM Daily Replace Fire Extinguisher Cartridge 3090383 LH 0 mths 16 Feb 014 Inspect Phase 13 Oxygen Cylinder 176000-115 10 Mar 014 Test Oxygen Cylinder AD/GAS/1 amd 9 0 mths 10 Mar 014 Inspect Inspect Inspect Inspect Magnesium Housing Inspection Garrett TPE331-10N MM LH +/- 10 hrs 1 Mar 014 Magnesium Housing Inspection Garrett TPE331-10N MM RH +/- 10 hrs 1 Mar 014 ELT Yearly Test 1 Mar 014 Garmin GNS530WT Yearly Periodic Inspection 1 Mar 014 Inspect Wing Spars Delamination and AD/C400/103 amd 3 0 hrs 1 Mar 014 Replace Davcon Clock Battery 4 mth replacement 0 mths 19 May 014 Inspect Inspect LH ine 00 Hour Inspection Garrett TPE331-10N MM LH +/- 10 hrs 7,948.00 RH ine 00 Hour Garrett TPE331-10N MM RH +/- 10 hrs 7,948.00 Inspect Phase 3 C441 MM +/- 10 hrs 7,974.50 06 Jun 014 Inspect Radio Periodic Inspection CASA Schedule 5 0 hrs 7,984.50 06 Jun 014 INSTRUCTIONS FOR EACH NEW UPDATED FORM 090: Endorse Form 090 MC00X-XXX attached on current Maintenance Release Part 1, and attach this form. On completion of any items on the list above, complete Final Certification on Maintenance Release Part or complete Log Book entry, and Strike Through the entry and initial. Form revision status:

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL INSPECTION PHASE Date: Registration Number: Serial Number: Total Time: 1. Description A. Phase consists of 100-hour or 1 calendar months, whichever occurs first, interval inspection items. B. Inspection items are listed in order of the zone in which the inspection is to be performed. A descriptive statement of the inspection requirement and the Item Code Number for cross reference to section 5-10-01 is provided. In many instances, tasks define more specifically the scope and extent of each required inspection. These tasks are printed in the individual chapters of this manual. C. The right portion of each page provides room for the mechanic s and inspector s initials and remarks. These pages may be reproduced as a checklist for use when performing this inspection phase.. General Inspection Criteria A. During accomplishment of each of the specific inspection tasks within this phase, additional general inspections of the surrounding areas should be performed while access is available. These general inspections are intended to detect obvious conditions which may warrant further action. B. If a component or system is disturbed (due to maintenance being performed) after completion of an initially required task, then that specific task must be re-confirmed after completion of any maintenance before returning the system or component to service. C. Conduct a preflight inspection upon completion of this inspection phase to ensure all required items are properly serviced. Refer to the Approved Airplane Flight Manual. ITEM CODE NUMBER A43003 TASK ZONE MECH INSP REMARKS Batteries - Inspect overboard vents and vent lines for damage and obstructions. 131 A4500 Emergency Bus Fuses - Check Condition. 131 D43001 Battery - Recondition. 131 A1500 Air Cycle Machine Oil Level- Inspect oil level. 13 A306001 Propeller Deice Slip Rings, Brushes and Boots - Check for condition and security of attachment. A70000 ine - (refer to Garrett ine Maintenance Manual for Periodic Inspection Requirements and Checks. A731001 Fuel Lines - Inspect fuel supply lines for deterioration, chafing, fuel leaks and security of installation. A761001 ine Controls - Check travel and security of installation, routing and evidence of damage (engine compartment). 410, 40 410, 40 410, 40 410, 40 5-1-0 Page 1 Jul 1/00

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL ITEM CODE NUMBER TASK ZONE MECH INSP REMARKS A781001 ine Exhaust System - Inspect for cracks, distortion, security of installation and evidence of damage. A801001 Starter-Generator Brush Holders - Inspect for cracks, wear, cleanliness; brush springs for proper tension and looseness. A80100 Starter-Generator Brushes - Inspect for cracks, wear and cleanliness. A801004 Starter-Generators - Inspect for security of installation, terminal block and electrical connections for cleanliness, evidence of heat or electrical arcing and evidence of damage. 410, 40 410, 40 410, 40 410, 40 C611001 Propeller Blade Clamps - Lubricate (Hartzell only). 410, 40 A3400 Tires - Inspect for pressure, wear and cuts. 710, 70, 730 *** End of Phase Inspection Items *** 5-1-0 Page Jul 1/00

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL INSPECTION PHASE 1 Date: Registration Number: Serial Number: Total Time: 1. Description A. Phase 1 consists of items to be inspected every two years. B. Inspection items are listed in order of the zone in which the inspection is to be performed. A descriptive statement of the inspection requirement and the Item Code Number for cross reference to section 5-10-01 is provided. In many instances, tasks define more specifically the scope and extent of each required inspection. These tasks are printed in the individual chapters of this manual. C. The right portion of each page provides room for the mechanic s and inspector s initials and remarks. These pages may be reproduced as a checklist for use when performing this inspection phase.. General Inspection Criteria A. During accomplishment of each of the specific inspection tasks within this phase, additional general inspections of the surrounding areas should be performed while access is available. These general inspections are intended to detect obvious conditions which may warrant further action. B. If a component or system is disturbed (due to maintenance being performed) after completion of an initially required task, then that specific task must be re-confirmed after completion of any maintenance before returning the system or component to service. C. Conduct a preflight inspection upon completion of this inspection phase to ensure all required items are properly serviced. Refer to the Approved Airplane Flight Manual. ITEM CODE NUMBER A34100 B345003 TASK ZONE MECH INSP REMARKS Altimeter System and Altitude Reporting Equipment - Inspect as required by FAR Part 91, Paragraph 91.411 in accordance with FAR, Part 43, Appendix E, by authorized repair station. Transponder Control - Operate Individual Control and Operational Test Transponder System to comply with FAR 91.413. *** End of Phase 1 Inspection Items *** 31, 3 31, 48 5-1-1 Page 1 Jul 1/00

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL INSPECTION PHASE D Date: Registration Number: Serial Number: Total Time: 1. Description A. Phase D consists of items to be inspected at 600 hours or 4 calendar months, whichever occurs first. This special phase is a combination of Phases 4, 5 and 6 provided for the convenience of those operators performing the three phases at the same time. B. Inspection items are given in the order of the zone in which the inspection is to be completed. A general description of the inspection required and the Item Code Number for cross-reference to section 5-10-01 are shown. Frequently, tasks give more information about each required inspection. These tasks are printed 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. A copy of these pages can be used as a checklist when these inspections are completed.. General Inspection Criteria A. Whileeachofthespecified inspection tasks in this section is done, more general inspections of the adjacent areas must be done while access is available. These general inspections are used to find apparent conditions which may need more maintenance. B. If a component or system is changed after a required task has been completed, then that specified task must be done again to make sure it is correct before the system or component is returned to service. C. Do a preflight inspection after these inspections are completed to make sure all the required items are correctly serviced. Refer to the Pilot's Operating Handbook. ITEM CODE NUMBER TASK ZONE MECH INSP REMARKS A340001 General Nose Compartment Inspection - All components for security of installation and evidence of damage. A1003 Nose Ram Air Valve - Check for security and proper operation. 110, 11, 1, 131, 13, 11, 1, 1A 13 D1500 Air Cycle Machine Oil - Change. 13 A15003 A15004 ACM Bypass Valve and Actuator - Inspect for security of installation and evidence of electrical component damage. Air Cycle Machine - Inspect for security of installation and evidence of damage. Inspect line from aspirator to water separator for damage. Inspect all plumbing in and out of air cycle machine for security. A17001 Water Separator - Inspect water separator for security of installation. Inspect water separator coalescer bag, clean bag or replace damaged bag. 13 13 13 5-1-0D Page 1 Cessna Aircraft Company Jun 1/007

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL ITEM CODE NUMBER A304007 A304010 A361001 TASK ZONE MECH INSP REMARKS Windshield Bleed Air Solenoid Valve (Airplanes -004 and On) - Inspect for security of installation. Windshield Bleed Air Heat Exchangers - Inspect for security and condition. Instrument Air Water Separator - Inspect for security of installation and evidence of damage. 13 13 13 D361001 Instrument Air Water Separator - Replace filter. 13 A361004 Air Pressure Lines - Inspect for security of installation, corrosion and evidence of damage. A31001 A43006 A304009 A301004 A7005 A76100 Antenna (COM 1) - Inspect for security of installation and evidence of damage. Generator Control Units - Inspect for security of installation and evidence of damage. Windshield Bleed Air Temperature Control Unit - Inspect for Security and evidence of damaged electrical components. Surface Deice System - Check lines for condition and clamps for security. Rudder Cables - Inspect cables for broken wires. Inspect cable fittings for cable slippage, cracks and distortion. Inspect rudder fuselage cable pulleys for freedom of rotation. Inspect interconnect spring and guide tube for security of installation. ine Controls - Check travel and security of installation, routing and evidence of damage (cabin area). A34004 Brake System Plumbing (Fuselage and Wing) - Inspect for leaks, condition and security of installation; check for proper routing and support. A7103 A100 C71008 C71108 Rudder Trim Tab Cables - Inspect cables for broken wires. Inspect cable fittings for cable slippage, cracks and distortion. Inspect cable pulleys for freedom of rotation. Inspect travel stop blocks for security. Inspect cable tension and turnbuckle for proper safetying. Inspect chain for condition and proper alignment on sprocket. Cabin Ventilation Fan - Inspect fan assembly for security of installation, evidence of damage, air leaks at air duct connections. Aileron Wing Cable Seals - Inspect cable seals for deterioration and lubrication. Aileron Trim Cable Seals - Check cable seals for deterioration and lubrication. 13, 141, 14, 151, 15, 141 141 141 141, 14 151, 15, 16, 17 141, 14, 151, 15, 161, 16, 171, 17, 311, 31, 31, 3 141, 14, 151, 15, 43 141, 151, 15 141, 151, 161, 171, 43, 311, 31, 350 151 151, 15 151, 15 5-1-0D Page Cessna Aircraft Company Jun 1/007

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL ITEM CODE NUMBER A15105 A45004 A73108 A1001 A71005 A75005 A75006 TASK ZONE MECH INSP REMARKS Air Conditioning Lines (Freon System) - Inspect for evidence of chafing and damage. Inspect for security of installation. Starter Relay Box - Inspect all internal components for security of installation and damaged electrical components. Elevator Trim Tab Cables - Inspect cable tension and turnbuckle safetying. Aileron Servo Actuator - Inspect for security of installation, evidence of damage and evidence of overheating. Inspect electrical components for damage. Aileron Bell Crank - Visually inspect bell crank for security of installation, cleanliness, corrosion, evidence of damage to cable attach points. Flap Actuator - Check for security of installation and for indication of hydraulic fluid leaks. Center Flap Bell Crank - Inspect bell crank and pushrods for evidence of damage and security of installation. Check pushrod boots for evidence of deterioration and security of installation. Inspect electrical components for evidence of damage and security of installation. A13010 Vacuum Regulator - Inspect for security of installation and evidence of damage. A13011 A16001 Pressurization Solenoid Valves - Inspect for security of installation and evidence of damage. Cabin Temperature Sensor and Blower - Inspect for cleanliness. A3001 Flitefone Antenna - Inspect for security of installation, evidence of damage and corrosion. A44001 C73103 A13003 A13004 A351004 External Power Receptacle - Inspect for security of installation and damage. Elevator Trim Tab Cable Seals - Check cable seals for deterioration and lubrication. Outflow Valve and Safety Valve - Inspect for security of installation; check line assemblies for proper installation on fittings; check for broken diaphragm retention ring and evidence of damage. Outflow Valve and Safety Valve - Clean units and filters. Refer to Chapter 1, Pressurization Control System - Maintenance Practices, Cleaning/Painting. Oxygen Altitude Compensating Regulator - Inspect for security of installation and evidence of damage. 15, 16, 17, 311, 31 161 161 161, 16 161, 16 161, 16 161, 16 16 16, 17 171 171 171 171, 17 17 17 17 5-1-0D Page 3 Cessna Aircraft Company Jun 1/007

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL ITEM CODE NUMBER A341001 TASK ZONE MECH INSP REMARKS Static Sumps - Inspect sumps for cracks, leaks and presence of water; drain sumps. Inspect static system plumbing (in the tailcone) for security of installation and evidence of damage. Airplanes with air data computer in tailcone, inspect plumbing for adequate clearance with air data computer. A5300 Avionics and Nose Baggage Doors - Check condition, security of installation and operation. Inspect door latches for proper adjustment. Inspect latch handle for binding and chafing in latch housing. Inspect key lock for proper operation. A30400 Windshield Overheat Switch and Temperature Sensors - Inspect for security of installation and evidence of electrical damage. A33006 Emergency Blowdown Bottle - Check bottle and cable for security of installation. A304004 Windshield Anti-Ice System (Alcohol) - Inspect reservoir, pump and plumbing for condition and security of installation. A304006 A361003 A8003 A73007 A1001 A7001 Windshield Bleed Air Solenoid Valve (Airplanes -0001 thru -003) - Inspect for security of installation. Instrument Air Pressure Regulator - Inspect for security of installation. Cross feed Selector Switch - Inspect for security of installation and evidence of damaged electrical components. Elevator Cables - Inspect cables for broken wires. Inspect cable fittings for cable slippage, cracks and distortion. Inspect elevator fuselage cable pulleys for freedom of rotation. Windshield Defog Blowers - Check for security of installation. Rudder Pedals - Check rudder pedals, brake pedal return springs and rudder for freedom of movement. 17, 311, 31 11A, 1A, 1B 1 1 31 31, 141, 14, 151, 15, 161, 16, 171, 31, 3 31, 3 C700 Rudder Pedal Linkage - Service. 31, 3 C7003 Rudder Pedal Bearing Halves and Cockpit Rudder Gust Lock - Service. A36100 Air Pressure Hoses - Inspect for hardness, deterioration, looseness and bulging. A71007 Aileron Fuselage Cables - Inspect cables for broken wires. Inspect cable fittings for cable slippage, cracks and distortion. Inspect control wheel chains for condition and proper alignment on the sprockets. Inspect fuselage cable pulleys for freedom of rotation. Check cable tension. Inspect cable turnbuckle safetying. 31, 3 31, 3 31, 3, 141, 14, 151, 15, 161, 16 5-1-0D Page 4 Cessna Aircraft Company Jun 1/007

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL ITEM CODE NUMBER TASK ZONE MECH INSP REMARKS A73001 Control Column - Inspect bob weights, control column for evidence of damage, failed fasteners and security of installation. A34000 A13008 Cockpit Instrument Panels - Inspect instrument panels and area forward to pressure bulkhead. Inspect all components and related structures for security of installation, cracks, corrosion and damaged electrical components. Pressurization Air Controller - Inspect controller for security and evidence of damage. Clean filter. 31, 3, 46, 47 31, 3, 48 43 C53001 Control Pedestal Bearings - Service. 43 A71107 A73110 A45005 A45003 A6100 A13009 A75001 Aileron Trim Fuselage Cables - Inspect cables for broken wires. Inspect cable fittings for cable slippage, cracks and distortion. Inspect aileron trim fuselage cable pulleys for freedom of rotation. Inspect cable tension and turnbuckle safetying. Elevator Trim Tab Cables - Inspect cables for broken wires. Inspect cable fittings for cable slippage, cracks and distortion. Inspect cable pulleys for freedom of rotation. Inspect travel stop blocks for security of installation. Inspect cable tension and turnbuckle safetying. Side Console (Right) - Inspect circuit breaker panel for security of installation and damaged electrical components. Side Console (Left) - Inspect all internal components for security of installation and damaged electrical components. Fire Detection Control Units - Inspect for security of installation and evidence of damage. Pressurization Volume Tank - Inspect for security of installation and evidence of damage. Flap Preselect System - Inspect control and indicator for security of installation and evidence of damage. Check cable for deterioration and security of installation. A3500 Passenger Mask and Stowage Compartments - Inspect mask and hoses for deterioration, cleanliness and proper stowage. Inspect pintle pin, lanyard cord and stowage compartment for cleanliness, evidence of damage, deterioration. A3100 A15101 Antenna (COM ) - Inspect for security of installation and evidence of damage. Evaporator Assembly (Freon System) - Check for cleanliness and security. 43, 141, 151, 161 43, 141, 151, 161, 171, 311, 31, 31 44 45 45 48 48, 43, 141, 151, 161 51, 5, 61, 6 5 or 350 5, 6 5-1-0D Page 5 Cessna Aircraft Company Jun 1/007

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL ITEM CODE NUMBER A383001 TASK ZONE MECH INSP REMARKS Flush Toilet - Inspect seat assembly for corrosion, security of installation, evidence of damage, damaged electrical components, and proper service. 6 A38300 Non-flush Toilet - Inspect for security of installation. 6 A383003 Relief Tube - Inspect for security of installation, deterioration and evidence of damage. A1510 Air Conditioner Compressor Belt (Freon System) - Inspect for wear and tension. A15103 A15104 A001 A7301 A15107 A3001 C7007 C7104 C73008 Condenser Fan Blade (Freon System) - Check blades for nicks and security of installation. Air Conditioner Condenser (Freon System) - Check coils for debris or damage. Rudder/Yaw Damper Actuator - Inspect actuator for security of installation, mount for cracks and structure for evidence of damage. Electric Elevator Trim Actuator - Inspect actuator for evidence of damage, damaged electrical components and security of installation. Inspect mount structure for cracks. Dorsal Fin Air Inlet Water Drain (Freon System) - Inspect drain hose for deterioration, chafing and security of installation. Inspect drain hole for obstruction. Elevator Servo Actuator - Inspect for security of installation, evidence of damage and overheating. Inspect electrical components for damage. Rudder Cable Seals - Inspect cable seals for deterioration and lubrication. Rudder Trim Tab Cable Seals - Check cable seals for deterioration and lubrication. Elevator Cable Seals - Check cable seals for deterioration and lubrication. A73009 Elevator Cables - Inspect cable tension and turnbuckle safetying. A340003 A533001 Tailcone Electronic and Avionics Equipment Wire Bundles - Check for drip loop to keep moisture from entering connectors. Tailcone Drain Tubes - Inspect for any blockage and remove any trash in tailcone area which might cause blockage. Refer to Service Bulletin CQB88-4. A7006 Rudder Cables - Inspect cable tension and turnbuckle safetying. D13005 Outflow and Safety Valve Static Ports - Inspect pressurization static ports for obstruction and evidence of damage. 6 311 311 311 311 311 311, 31 311, 31 311, 31 311, 31 311, 31 311, 31 311, 31 311, 31 311, 31, 31, 3 31 5-1-0D Page 6 Cessna Aircraft Company Jun 1/007

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL ITEM CODE NUMBER A31003 A351003 TASK ZONE MECH INSP REMARKS Antenna (High Frequency) - Inspect for security of installation, corrosion and electrical bond. Oxygen Cylinder, Pressure Regulator and Shutoff Valve - Inspect for security of installation, corrosion, cleanliness and evidence of damage. A351005 Oxygen Filler Valve - Inspect for security of installation, corrosion, cleanliness and evidence of damage. A301001 A1100 A7009 Surface Deice System - Check lines for condition and clamps for security. Airplane ID Plate - Inspect for security of installation and legibility. Rudder Gust Lock (Tailcone) - Inspect for security of installation. B7010 Rudder Gust Lock (Tailcone) - Perform side load check and check for smooth operation and disengagement at correct elevator travel. Check that locking pin is completely retracted when it is in the UNLOCKED position. B73005 Elevator Horn Bearing Side Play - Inspect elevator horn bearing side play. Refer to Elevator - Maintenance Practices, Check Elevator Horn BearingSidePlay. A531001 Horizontal and Vertical Stabilizer Attach Bulkheads - Check for cracks, loose or failed fasteners and evidence of structural damage. (Removal of stabilizer not required). A73006 Elevators - Check elevator balance weights for looseness. 31 31 31 31, 331, 33, 350 31 31, 3 31, 3 31, 3 31, 3 331, 33 B73010 Elevator - Check elevator travel. 331, 33 C73104 Elevator Trim Tab Actuators - Service (disassembly required). 331, 33 B73106 Elevator Trim Tabs - Check elevator trim tab travels. 331, 33 A551001 A36001 A3600 Horizontal Stabilizer - Inspect for cracks, loose or failed fasteners and evidence of structural damage. Inspect hinge bracketry for cracks and loose and/or working fasteners; inspect hinge bearings for looseness. Control Surface Bond Jumpers - Verify integrity of bond connection. Static Wicks - Inspect for security of installation, corrosion and erosion of the tip. 331, 33 331, 33, 350, 54, 550, 64, 650 331, 33, 350, 54, 550, 64, 650 5-1-0D Page 7 Cessna Aircraft Company Jun 1/007

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL ITEM CODE NUMBER A15106 TASK ZONE MECH INSP REMARKS Air Conditioner (Freon System) - Inspect dorsal air inlet for obstructions. A7011 Rudder - Check rudder balance weight for looseness. 350 350 B701 Rudder - Check rudder travel. 350 C7101 Rudder Trim Tab Actuator - Lubricate Actuator Screws. 350 B7107 Rudder Trim Tab - Check rudder trim tab travel. 350 A553001 Vertical Stabilizer - Inspect for cracks, loose or failed fasteners and evidence of structural damage. D91005 Hydraulic Filter Elements - Replace. 410, 40 A54100 A71700 Nacelle Firewall Structure - Inspect for condition and proper sealing. ine Compartment Hoses - Inspect for condition; inspect fuel (inspect fuel lines under pressure), oil vacuum and hydraulic hoses for leaks, chafing, deterioration discoloration, bleaching. Inspect rubber hoses for stiffness. 350 410, 40 410, 40 D7300 ine EPA System Filter - Clean. 410, 40 A78100 A800 A761003 A301005 A75007 A9100 Exhaust Pipe Swirl Vanes - Inspect for security and evidence of damage. Fuel Cross feed Valves - Inspect for leaks, security of installation and damaged electrical components. Inspect cross feed plumbing for condition, security and leaks. ine Controls - Check travel and security of installation, routing and evidence of damage (wing area). Surface Deice System - Check lines for condition and clamps for security. Flap Control Valve and Plumbing - Inspect control valve for security of installation and for hydraulic fluid leakage. Check plumbing for security of installation, chafing, routing and for leakage. Hydraulic Reservoir - Inspect for leaks, security of installation and cleanliness. A91003 Hydraulic Components - Inspect plumbing and component mounting for condition, security and system for leaks. 410, 40 511, 611 511, 611 511, 611, 51, 61 51 51 51 5-1-0D Page 8 Cessna Aircraft Company Jun 1/007

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL ITEM CODE NUMBER A71106 TASK ZONE MECH INSP REMARKS Aileron Trim Wing Cables - Inspect cables for broken wires. Inspect cable fittings for cable slippage, cracks and distortion. Inspect aileron trim wing cable pulleys for freedom of rotation. Inspect tab stop blocks for security of installation. Inspect chain for condition and proper alignment on actuator sprocket. A8400 Signal Conditioners - Inspect for security of installation and evidence of damage to electrical components. A34005 Brake System Plumbing (Fuselage and Wing) - Inspect for leaks, condition and security of installation; check for proper routing and support. A71006 Aileron Wing Cables - Inspect cables for broken wires. Inspect cable fittings for cable slippage, cracks and distortion. Inspect aileron wing cable pulleys for freedom of rotation. A75003 Inboard and Outboard Flap Bell Cranks and Pushrods - Inspect bell cranks and pushrods for evidence of damage and security of installation. A75008 Flaps - Inspect flap track rollers, pushrods and fittings for evidence of damage or wear and security of installation. 51, 51, 53, 54 51, 61 51, 61 51, 61, 51, 61, 53, 63, 54, 64 513, 53, 613, 63 513, 53, 613, 63 B75009 Flaps - Check flap travel. 513, 53, 613, 63 A75004 A8004 A541001 B7110 C71103 Flap Idler Bell Crank - Inspect bell crank arm for looseness. Fuel Firewall Shutoff Valves - Inspect for leaks and security of installation and damaged electrical components. Nacelle Structure - Visually inspect for cracks, dents and other damage. Aileron Trim Tab Travel - Check aileron trim tab travel. Aileron Trim Tab Actuator - Lubricate actuator screws. 513, 613 51, 61 51, 61 A71009 Aileron - Check aileron travel. 54, 64 A7330 Stall Warning Transmitter - Inspect for security of installation, cleanliness, vane operates freely and evidence of damage. C33400 Landing Light Exposed Sector Gear - Lubricate. 550, 650 C334003 Landing Light Hinge Point - Lubricate. 550, 650 54 54 550 5-1-0D Page 9 Cessna Aircraft Company Jun 1/007

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL ITEM CODE NUMBER A13006 A13007 A304008 TASK ZONE MECH INSP REMARKS Emergency Pressurization Valve - Inspect valve for security of installation and evidence of damage. Inspect electrical wires at valve for evidence of damage. Ejector Pump - Inspect for security of installation, evidence of damage and plugged vent line. Windshield Bleed Air Regulating Valve - Inspect for security of installation. 61 61 61 A35003 Nose Wheel Steering Cables - Check cable tension. 710 A531003 A35004 Nose Wheelwell Structure - Check for security and cracks. Nose Wheel Steering Cables - Inspect cables for broken wires. Inspect cable fittings for cable slippage, cracks and distortion. Inspect cable pulleys for freedom of rotation and the presence of cable guard pins. B33008 Landing Gear Actuators and Control/Indicating Systems Functional Test - Perform test as scheduled or any time the landing gear emergency blow down bottle has been discharged or a landing gear actuator is replaced. A33009 A33001 A5001 C51005 A11001 A113001 A45001 A530001 Perform Landing Gear Rigging Inspection - (Refer to Expanded Inspection and Maintenance Checks). Main Landing Gear Uplock Hook Support Bracket - Inspect for cracks. Airplanes -0001 thru -005 except airplanes incorporating Service Bulletin CQB87-4. Emergency Exit Door - Check for condition, security of installation and operation. Cabin Door Hinges, Latch Pins, Step Hinges and Stop Assembly - Lubricate. Exterior Placards, Decals, and Markings - Inspect for security of installation and legibility. Interior Placards and Decals - Inspect for security of installation and legibility. All Wire Bundle/Electrical Components - Visually inspect electrical components for damage. Visually inspect wiring for damage such as chafing, cuts and cracked insulation. Pay particular attention to the fuel tank boost pump wiring. Fuselage Exterior Surfaces - Inspect for cracks, loose or failed fasteners and evidence of structural damage. B35001 Passenger Mask and Stowage Compartments - Operational test to verify oxygen mask drop. 710 710, 131, 13, 141, 14 710, 70, 730 710, 70, 730 70, 730 80 830 All Zones All Zones All Zones All Zones AUX 5-1-0D Page 10 Cessna Aircraft Company Jun 1/007

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL ITEM CODE NUMBER B730 TASK ZONE MECH INSP REMARKS Electric Elevator Trim - Operate electric trim; check trim travel time. Refer to Chapter 7, Elevator Electric Trim Actuator - Maintenance Practices. B1300 Cabin Pressurization System - Perform an operational test. Refer to Chapter 1, Pressurization Control System - Adjustment/Test, Pressurization System Operational Test. B15001 Environmental System - Perform an operational test of the air cycle machine. Refer to Chapter 1, Cooling System - Maintenance Practices, Air Conditioning System Operational Test. *** End of Phase D Inspection Items *** BAT ENG ENG 5-1-0D Page 11 Cessna Aircraft Company Jun 1/007

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL INSPECTION PHASE 55 Date: Registration Number: Serial Number: Total Time: 1. Description A. Phase 55 gives the Corrosion Prevention and Control Program Inspections (Baseline Program) items that are to be examined every 60 months. Refer to Section 5-30-00, Corrosion Prevention and Control Program for additional information concerning repeat Corrosion Program Inspection intervals. B. Inspection items are given in the order of the zone in which the inspection is to be completed. A general description of the inspection required and the Item Code Number for cross-reference to section 5-10-01 are shown. Frequently, tasks give more information about each required inspection. These tasks are printed 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. A copy of these pages can be used as a checklist when these inspections are completed.. General Inspection Criteria A. Whileeachofthespecified inspection tasks in this section is done, more general inspections of the adjacent areas must be done while access is available. These general inspections are used to find apparent conditions which may need more maintenance. B. If a component or system is changed after a required task has been completed, then that specified task must be done again to make sure it is correct before the system or component is returned to service. C. Do a preflight inspection after these inspections are completed to make sure all the required items are correctly serviced. Refer to the Pilot's Operating Handbook. ITEM CODE NUMBER TASK ZONE MECH INSP REMARKS A53105 Fuselage external skin. Make sure you examine these areas: (A.) Fuselage skin underneath antenna installations. NOTE: Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Section 5-30-00 for additional inspection information and illustrations). A55101 Antenna installation. Make sure you examine this area: (A.) Skin under any existing antenna installations. NOTE: Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Chapter 5, Section 5-30-00 for additional inspection information). 11, 1, 131, 13, 141, 14, 151, 15, 161, 16, 171, 17, 41, 4, 51, 61, 6, 311, 31 350 5-1-55 Page 1 Cessna Aircraft Company Jun 1/007

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL ITEM CODE NUMBER A611001 A571009 TASK ZONE MECH INSP REMARKS Propeller assembly. Make sure you examine these areas: (A.) Propeller blade and attachment. (B.) Propeller hub. (C.) Propeller assembly bearings and pins. NOTE: Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Chapter 5, Section 5-30-00 for additional inspection information). Wing skin external. Make sure you examine these areas: (A.) Bonded wing skin. (B.) Leading edge skin under de-ice boot. NOTE: Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Chapter 5, Section 5-30-00 for additional inspection information). A571010 Wing structure internal. Make sure you examine these areas: (A.) Front spar lower cap from BL 3.00 to CWS 30.00. (B.) Bonded wing skin. NOTE 1: Make sure you examine the bonded waffle doublers for corrosion. NOTE : Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Chapter 5, Section 5-30-00 for additional inspection information). A571011 Wing skin external. Make sure you examine this area: (A.) Bonded wing skin. NOTE: Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Chapter 5, Section 5-30-00 for additional inspection information). A57101 Wing structure internal. Make sure you examine these areas: (A.) Front spar upper and lower caps. (B.) Main spar upper and lower caps in gear well. (C.) Rear spar upper and lower caps in gear well. (D.) Wing rear spar web. (E.) Main spar center wing attach fittings at CWS 111.00. (F.) Rear spar center wing attach fittings at CWS 11.10. (G.) Bonded wing skin. NOTE 1: Make sure you examine the bonded waffle doublers for corrosion. NOTE : Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Section 5-30-00 for additional inspection information). A571013 Wing structure external. Make sure you examine these areas: (A.) Rear spar upper cap. (B.) Rear spar lower cap. (C.) Rear spar web. (D.) Bonded wing skin. NOTE: Make sure you examine the bonded waffle doublers for corrosion. NOTE: Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Chapter 5, Section 5-30-00 for additional inspection information). 410, 40 511, 611 511, 611 511, 611 51, 61 513, 613 5-1-55 Page Cessna Aircraft Company Jun 1/007

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL ITEM CODE NUMBER A571014 TASK ZONE MECH INSP REMARKS Wing skin external. Make sure you examine these areas: (A.) Bonded wing skin. (B.) Leading edge skin under de-ice boot. NOTE 1: Make sure you examine the bonded waffle doublers for corrosion. NOTE : Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Chapter 5, Section 5-30-00 for additional inspection information). A571015 Wing structure internal. Make sure you examine these areas: (A.) Main spar cap and outer wing attach fittings. (B.) Bonded wing skin. NOTE: Make sure you examine the bonded waffle doublers for corrosion. NOTE: Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Chapter 5, Section 5-30-00 for additional inspection information). A571016 Wing structure external. Make sure you examine these areas: (A.) Bonded wing skin. (B.) Rear spar upper cap. (C.) Rear spar lower cap. (D.) Rear spar web. NOTE: Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Chapter 5, Section 5-30-00 for additional inspection information). A571017 Wing structure internal. Make sure you examine these areas: (A.) Main spar upper and lower caps and outer wing attach fittings. (B.) Rear spar upper and lower caps and outer wing attach fittings. NOTE: Make sure you examine the bonded waffle doublers for corrosion. NOTE: Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Section 5-30-00 for additional inspection information). A571018 Wing skin external. Make sure you examine these areas: (A.) Bonded wing skin. (B.) Leading edge skin under de-ice boot. NOTE: Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Chapter 5, Section 5-30-00 for additional inspection information). A571019 Wing structure internal. Make sure you examine these areas: (A.) Bonded wing skin. (B.) Main spar upper and lower caps. NOTE: Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Chapter 5, Section 5-30-00 for additional inspection information). 531, 631 531, 631 53, 63 53, 63 541, 641 541, 641 5-1-55 Page 3 Cessna Aircraft Company Jun 1/007

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL ITEM CODE NUMBER TASK ZONE MECH INSP REMARKS A57100 Wing structure external. Make sure you examine these areas: (A.) Bonded wing skin. (B.) Rear spar upper cap. (C.) Rear spar lower cap. (D.) Rear spar web. NOTE 1: Make sure you examine the bonded waffle doublers for corrosion. NOTE : Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Chapter 5, Section 5-30-00 for additional inspection information). A57101 Wing structure internal. Make sure you examine these areas: (A.) Main spar upper and lower caps. (B.) Rear spar upper and lower caps. (C.) Wing rear spar webs. (D.) Bonded wing skin. NOTE 1: Make sure you examine the bonded waffle doublers for corrosion. NOTE : Corrosion Prevention and Control Program Inspection item (baseline interval, refer to Section 5-30-00 for additional inspection information). *** End of Phase 55 Inspection Items *** 54, 64 54, 64 5-1-55 Page 4 Cessna Aircraft Company Jun 1/007

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL INSPECTION PHASE 56 Date: Registration Number: Serial Number: Total Time: 1. Description A. Phase 56 consists of items to be inspected every 0 years (mild environment) or 10 years (moderate/ severe environment) and every 5 years (mild environment) or 3 Years (moderate/severe environment) thereafter. Refer to 51-1-00, Corrosion Severity Maps - Description and Operation for additional information concerning corrosion environments. 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 Phase.. General Inspection Criteria A. As you complete each of the inspection tasks in this Inspection Phase, 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. When these inspections are completed, do a preflight inspection to make sure that all necessary items are serviced correctly. Refer to the Approved Airplane Flight Manual. D. Phase Kits are available for some Phase Documents. They supply consumable materials used to complete the inspection item(s) given for the interval. Refer to the Model 441 Illustrated Parts Catalog, Introduction, Phase Inspection Kit List to find applicable part numbers. ITEM CODE NUMBER TASK ZONE MECH INSP REMARKS A551014 Horizontal Stabilizer Skin-to-Honeycomb Bond - Inspect. Refer to Chapter 5, Section 5-14-51, Supplemental Inspection Document Number 55-10-11. *** End of Inspection Phase 56 Inspection Items *** 331, 33 D518-16-13 Temporary Revision Number 5-4 - Jun /008 5-1-56 Page 1 Cessna Aircraft Company Jun 1/007

Garrett TPE331-8/-10N Combined Periodic Inspection Honeywell SB TPE331-7-0180 R34 01 Mar 013 and Garrett TPE331-8/-10N MM Table 601 Garrett TPE331-8/-10N Combined Periodic Inspection Schedule VH-. Serial Number. Date Job Number.. Job Co-ordinator. TTIS.. Landings ine.. LH RH 100 Hour Inspection 1 AIR INLET AME SIG LAME SIG A AIR INLET Check for obstruction and evidence of foreign object damage (FOD), and for oil leakage from the compressor air/oil seal. 7-00-00 (Refer to TROUBLE SHOOTING Section or FAULT ISOLATION Section, as applicable) FIRST STAGE COMPRESSOR IMPELLOR AME SIG LAME SIG A Check for evidence of foreign object damage (FOD) 7-30-01 3 OIL LEVELS AME SIG LAME SIG A Must be above ADD mark. If not acceptable, refer to Servicing. 7-00-00 (Refer to SERVICING Section) 4 EXHAUST PIPE AME SIG LAME SIG A Check for oil leakage from turbine air-oil seals. 7-00-00 (Refer to TROUBLE SHOOTING Section or FAULT ISOLATION Section, as applicable) 5 FUEL CONTROL MANUAL SHUTOFF LEVER AME SIG LAME SIG A Cycle shutoff lever and associated linkage to ensure sufficient freedom of operation. Refer to 73-1-05, Maintenance Practices. 6 ANTI-ICE AIR FILTER AME SIG LAME SIG A Remove and clean. Refer to 75-10-01, Maintenance Practices. 7 OIL FILTER AME SIG LAME SIG A Remove and inspect. Replace filter element. 8 FEATHER VALVE AME SIG LAME SIG A Manual test 7-00-00 (Refer to ADJUSTMENT/TEST Section or TESTING Section, as applicable.) 9 NTS SYSTEM AME SIG LAME SIG A Check operation of NTS System. 7-00-00 (Refer to ADJUSTMENT/TEST Section or TESTING Section, as applicable.) Page 1 of 5

Garrett TPE331-8/-10N Combined Periodic Inspection Honeywell SB TPE331-7-0180 R34 01 Mar 013 and Garrett TPE331-8/-10N MM Table 601 150 Hour Inspection 1 FUEL FILTER AME SIG LAME SIG A (Pre SE 73-0110) Remove, clean, and inspect for damaged or separated screen. (Post SE 73-0110) Remove and replace with new filter element. (Refer to 73-1-03, Maintenance Practices.) INPUT GEARBOX DRAIN AME SIG LAME SIG A (Check to ensure drain is open) Use air to check drain port passage as damage to crossover duct could result from the used of hard articles to check passages. 7-00-05 3 COMPENSATION RESISTOR AME SIG LAME SIG A Test temperature compensation value. 7-00-00 (Refer to applicable INSPECTION/CHECK Section) 4 SPECTOGRAPHIC OIL ANALYSIS PROGRAM (SOAP) AME SIG LAME SIG A Remove and replace filter element. 79-0-0 00 Hour Inspection 1 (PRE SE 7-0416) STARTER-GENERATOR DRIVE SPLINES AME SIG LAME SIG A Inspect and lubricate. 7-10-13 FIRST STAGE COMPRESSOR IMPELLER AME SIG LAME SIG A Inspect for foreign object damage. 7-30-01 3 P3 AIR FILTER AME SIG LAME SIG A Remove and clean. 4 EMERGENCY SHUTDOWN SYSTEMS AME SIG LAME SIG A Operate airframe emergency feather/fuel shutoff systems to determine if engine feathering valve and fuel shutoff valve have actuated. 7-00-00 (Refer to applicable INSPECTION/CHECK Section) 5 FUEL CONTROL/FUEL PUMP INTEGRITY INSPECTION AME SIG LAME SIG A (Pre SE 73-017) Perform Fuel Control/Fuel Pump Integrity inspection. 7-00-00 (Refer to applicable INSPECTION/CHECK Section) 300 Hour Inspection 1 OVERSPEED GOVERNOR AME SIG LAME SIG A Operational check. (Refer to Adjustment/Test.) PLENUM DRAIN VALVES AME SIG LAME SIG A Check operation of plenum drain valves without removing from engine as follows. With engine not operating plenum drain valves should be open. Open position may be assured if air passes freely through valve when slight air pressure is applied at the attached drain tubes. 3 FUEL MANIFOLD PURGE SYSTEM 10 MICRON FILTER AME SIG LAME SIG A Remove and clean filter element. 73-10-13 Page of 5