Maxem 550 SOM Amd 05

MAXEM AVIATION PTY LTD

CESSNA 550

SYSTEM OF MAINTENANCE

MASTER COPY

Revision: Initial

Date: 20/09/10

Maxem Aviation Pty Ltd System of Maintenance

Volume 1

Introduction

Page 1

Introduction

TABLE OF CONTENTS Page No.

Table of Contents ..................................................................................................................... 1 Record of Amendment .............................................................................................................. 2

List of Effective Pages .............................................................................................................. 3 Definitions ................................................................................................................................ 4

Manual Holders ........................................................................................................................ 5

VOLUME 1 System of Maintenance

Section No.

Introduction ............................................................................................................................... 0

General Information .................................................................................................................... 1

Document Control....................................................................................................................... 2

Inspection Schedule ................................................................................................................... 3

Overhaul, Replacement & Special Inspection Schedule .............................................................. 4

Additional Inspections ................................................................................................................. 5

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Introduction

RECORD OF AMENDMENT

Amendment Number

Amendment Date

Incorporated By

Incorporation Date

Initial 20/09/10 P Carey 25/09/10 01 23/05/11 P Carey 30/05/11 02 12/07/11 P Carey 15/07/11 03 07/09/11 P Carey 07/09/11 04 17/10/11 M Carey 24/10/11 05 12/10/11

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Introduction

Page 3

Introduction

LIST OF EFFECTIVE PAGES

VOLUME 1 System of Maintenance

SECTION PAGES REVISION DATE 0 Introduction

1 2 3 4 5

Initial Initial 05 Initial 05

20/09/2010 20/09/2010 16/01/2012 20/09/2010 16/01/2012

1 General Information

1 2

Initial 05

20/09/2010 16/01/2012

2 Document Control

1 2

Initial 05

20/09/2010 07/09/2011

3 Inspection Schedule

1 2 3 4 5 6

Initial Initial Initial Initial 05 05

20/09/2010 20/09/2010 20/09/2010 20/09/2010 16/01/2012 16/01/2012

4 Overhaul, Replacement & Special Inspection Schedule

1 2 3 4

Initial Initial Initial 03

20/09/2010 20/09/2010 20/09/2010 07/09/2011

5 Additional Inspections

1 2 3 4 5 6 7 8

Initial Initial Initial Initial Initial Initial Initial Initial

20/09/2010 20/09/2010 20/09/2010 20/09/2010 20/09/2010 20/09/2010 20/09/2010 20/09/2010

System of Maintenance Issue No Maxem Aviation Pty Ltd at Rev 05 Dated 17 / 10/ 2012 for Aircraft Type / Model Cessna 550 Has been approved IAW / CAR 1988 42M The list of effective Pages with this stamp attached details page applicability and issue date

Signed Inst / No 1-RHEN Issue 07 Date 17 / 10 / 2012. (Original approval in red)

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Date: 20/09/10


Volume 1

Introduction

Page 5

Introduction

Definitions

AD Airworthiness Directive AME Aircraft Maintenance Engineer AOC Air Operators Certificate CAME Corporate Aircraft Maintenance & Engineering CAAP Civil Aviation Advisory Publication CAO Civil Aviation Orders CAR Civil Aviation Regulations CASA Civil Aviation Safety Authority CD Compact Disc Check Perform an inspection detailed in the Cessna 550 Service Manual, or in the

part/component Manufacturers Maintenance, Repair and Overhaul Manual, observing the specific tension, rigging, travel limits, torque value and/or wear limits.

C of R Certificate of Registration CSN Cycles Since New CSO Cycles Since Overhaul EO Engineering Order HAMC Head of Aircraft Airworthiness and Maintenance Control IAW In Accordance With Inspect Perform a specific inspection. IPC Illustrated Parts Catalogue LAME Licenced Aircraft Maintenance Engineer LEP List of Effective Pages MA Maintenance Authority Maintenance Control The management responsibilities of the Maintenance Controller, as per Section 3

Volume 1 with regard to regulatory compliance and management of aircraft maintenance.

Maintenance Scheduling The co-ordination of aircraft flying, to ensure scheduled maintenance is performed as determined by maintenance control. Performed by the HAMC.

Maintenance Planning The co-ordination of maintenance sub-contractors to perform scheduled and unscheduled maintenance on aircraft at times determined by maintenance control. Performed by the HAMC.

MC Maintenance Controller MCM Maintenance Control Manual MR Maintenance Release N/A Not Applicable OMEL Operator's Minimum Equipment List Overhaul The part/component must be overhauled in accordance with either the Cessna

550 overhaul instructions, or the part or component Manufacturers overhaul instructions.

POH Pilot Operating Handbook PUS Permissible Unserviceability Replace Retire from service. SB Service Bulletin Service Perform a maintenance action IAW the Cessna 550 Service Manual, or the part or

component Manufacturers maintenance instructions. SI Service Instruction S/N Serial Number SOM System of Maintenance TBO Time Between Overhaul Test Perform a test detailed in the Cessna 550 Service Manual, or in the

part/component Manufacturers Maintenance, Repair and Overhaul Manual. TSN Time Since New TTIS Aircraft Total Time in Service in hours. TCIS Aircraft Total Cycles in Service in cycles. # Number

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Introduction

MANUAL DISTRIBUTION LIST

Holders of controlled copies of this manual.

Copy No Type Manual Holder

1 Hard Copy Maxem Aviation Pty Ltd Managing Director, HAMC, Chief Pilot

2 Hard Copy Maxem Aviation Pty Ltd Maintenance Controller

3 CD-ROM CASA Local Area Office

4 CD-ROM Hawker Pacific Pty Ltd

5 CD-ROM PremiAir Aircraft Maintenance Pty Ltd

6 CD-ROM Airflite ty Ltd

7 CD-ROM Aeromil Pty Ltd

1-RHEN Issue 07

VOLUME 1

1-RHEN Issue 05

Revision: Initial

Date: 20/09/10


Volume 1

Section 1

Page 1

Section 1

GENERAL INFORMATION

TABLE OF CONTENTS

Page No.

Table of Contents ...................................................................................................................... 1

Aircraft........................................................................................................................................ 2

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Section 1

GENERAL INFORMATION

1.1 Introduction This manual has been raised by Maxem Aviation Pty Ltd and constitutes the System of Maintenance for Cessna 550 identified in Para 1.2. The Registered Operator has the responsibility to ensure the system of maintenance is satisfactory and all amendments found necessary are advised to Maxem Aviation Pty Ltd for inclusion in the manual.

1.2 Aircraft

The following aircraft are maintained under this System of Maintenance:

AIRCRAFT REG S/N REGISTRATION HOLDER REGISTERED OPERATOR CLASS

Cessna 550 EJY 0141 Executive Jet Charter Pty Ltd Maxem Aviation Pty Ltd A

Cessna 550 JMK 0289 JM Kelly (Project Builders) Pty Ltd Maxem Aviation Pty Ltd A

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Section 2

DOCUMENT CONTROL

TABLE OF CONTENTS

Page No.


System of Certification ................................................................................................................ 2

Maintenance Release ................................................................................................................. 2

Log Books .................................................................................................................................. 2

Maintenance Control................................................................................................................... 2

System of Maintenance Continued Assessment .......................................................................... 2

Reference Manuals .................................................................................................................... 2

Servicing Procedures.................................................................................................................. 2

Specifications and Grades of Fluids ............................................................................................ 2

Maintenance Practices and Procedures ...................................................................................... 2

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Section 2

DOCUMENT CONTROL

2.1 System of Certification Certification of all aircraft covered by this System of Maintenance shall be IAW Schedule 6 and 42ZE of the CARs.

2.2 Maintenance Release The Maxem Aviation Pty Ltd Maintenance Release shall be CASA Form 918 and certified IAW CARs listed in Division 9 of the CARs.

The Maintenance Release shall be issued for a period of 160 flight hours or six months, whichever comes first.

2.3 Log Books Log Book records shall comply with CAR 1988, 50A.

2.4 Maintenance Control Maintenance Control shall be carried out by: Paul Carey Aero Group Pty Ltd P.O.Box 119, Maylands WA 6931

2.5 System of Maintenance Continued Assessment This System of Maintenance shall be continually assessed by the Maintenance Controller to ensure the continued airworthiness of aircraft nominated in this manual. New or revised CASA and manufacturer requirements shall be incorporated as an amendment and submitted to the local field office of the CASA for approval under CAR 42P. This System of Maintenance shall be continually monitored for deficiencies against existing, new and revised published maintenance data.

2.6 Reference Manuals Unless otherwise mentioned in this System of Maintenance, the following reference manuals are to be complied with for lubrication and maintenance.

(1) Cessna 550 Maintenance Manual (2) Cessna 500 Structural Repair Manual (3) Pratt & Whitney JD15D-4 Maintenance Manual (4) New Flight Corporation Maintenance Manual Supplement P/N MMS-921

2.7 Servicing Procedures Carry out in accordance with the Cessna 550 Maintenance Manual.

2.8 Specifications and Grades of Fluids Listed in the Cessna 550 Maintenance Manual.

2.9 Maintenance Practices and Procedures Carry out in accordance with the Cessna 550 Maintenance Manual.

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Section 3

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Section 3

INSPECTION SCHEDULE

TABLE OF CONTENTS

Page No.


Introduction ................................................................................................................................ 2

Daily Inspection .......................................................................................................................... 2

Continuous Airworthiness Inspection Program ............................................................................ 2

Special Inspections ..................................................................................................................... 5

Maintenance Release Inspection ................................................................................................ 5

Airworthiness Directives.............................................................................................................. 5

Time Lifed Components .............................................................................................................. 5

Radio Inspection ......................................................................................................................... 5

Service Bulletins & Instructions ................................................................................................... 5

Pilot Maintenance ....................................................................................................................... 5

Unscheduled Inspections ............................................................................................................ 6

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Section 3

INSPECTION SCHEDULE

3.1 Introduction Applicable aircraft are to be maintained in accordance with the following schedules contained within this manual.

3.2 Daily Inspection Daily inspection to be carried out prior to the first flight of the day in accordance with the Cessna 550 Flight Manual P/N 55FM-41.

3.3 Continuous Airworthiness Inspection Program The Cessna Continuous Airworthiness Inspection Program is nominated as the Inspection schedule.

Construction

A. Following is the recommended continuous inspection and maintenance schedule for Model 550 airplanes.

B. The program is divided into five primary phases (Phases 1 through 5), which are the main repetitive phases that make up the basic requirements of the inspection program. The remaining phases include all of the remaining inspection items. The phases and inspection interval of each are listed below.

C. The inspection program is divided into phases to better enable the continuous type inspection to be accomplished. Recommended continuous type inspection may be accomplished by one of three methods.

D. The remaining sections in the 5-12-XX series contain signoff sheets, which are listings of inspection items in inspection item code order. The last two digits (XX) of the chapter/section/subject correspond to the inspection phase.

E. For a complete inspection program when the continuous inspection program is selected, additional inspections shall be complied with as follows:

(1) Continuous - Phases 1 and on shall be performed.

(2) Component Time Limits - 5-11-00, components that require maintenance at a specified time (does not include on condition items).

(3) Unscheduled Maintenance Refer to 3.11

Continuous Inspection Program Procedure

A. The five primary phases (Phase 1 through 5) constitute the core of the continuous inspection program. The remaining phases, which consist of the higher time inspection requirements, are not included in Phase 1 through 5 continuous inspection cycle. There are four plans (Plans A, B, C and D), which combine the various methods of accomplishing Phases 1 through 5 into a continuous inspection program. Each plan offers different inspection intervals to meet the varying needs of the individual operators. Refer to step G for the continuous inspection program chart that defines which phases are due at a specific hourly interval for each plan.

This System of Maintenance nominates Plan C.

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Continuous Inspection Program Procedure (cont)

B. The five primary phases (Phase 1 through 5) constitute the core of the continuous inspection program.

(1) Phases 1 through 4, which each have an interval of 300 hours, are designed to be accomplished in a continuous, repetitive 300-hour cycle by three different optional methods as provided in Item G.

(2) Phase 5, which has an interval of 1200 hours, is designed to be accomplished in a continuous, repetitive 1200-hour cycle by four different optional methods as provided in Item H.

C. The remaining phases are to be accomplished when due or at any time earlier to coincide with a convenient inspection or maintenance down time.

D. The calendar time limits (such as 36 months in Phase 5) must be taken into consideration for airplanes accumulating less than the specified hours in the calendar period.

E. Component Time Limits (5-11-00) lists all components, which are to be replaced or overhauled on a scheduled basis. Replacement or overhaul of items listed is required to be accomplished when due or earlier to coincide with a convenient inspection or maintenance down time.

F. An operator may elect to perform the recommended inspections on a schedule other than that specified. Any inspection schedule requiring the various inspection items detailed in this chapter to be performed at a frequency equal to that specified herein or more frequently is acceptable. Any inspection item performed at a time period in excess of that specified herein must be approved by the appropriate regulating agency.

G. Three optional methods of accomplishing Phases 1 through 4 are provided, and this System of Maintenance nominates Method 2:

NOTE: Operators changing from one method to another of performing Phases 1 thru 4, must ensure that time from the previous inspection to the next inspection of an item does not exceed intervals indicated in this manual.

METHOD 2: Phase 1 and Phase 2 are combined and accomplished at alternate 150 hour intervals, with Phase 3 and Phase 4 being performed at the next 150-hour interval. Applicable additional phases are integrated at their due times with the first four phases. At the completion of Phase 3 and Phase 4, Phase 1 and Phase 2 will become due 150 hours later and the cycle is to be repeated.

PHASE 75 HOUR 150 HOUR 225 HOUR 300 HOUR PHASE 1 X PHASE 2 X PHASE 3 X PHASE 4 X

.

H. Four optional plans of accomplishing Phase 5 are provided, and this System of Maintenance nominates Plan A:

PLAN A: Phase 5 can be accomplished all at once, each 1200 hours concurrently with accomplishment at the end of the third cycle of Phases 1 through 4.

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Continuous Inspection Program Procedure (cont)

I. Hour Interval Items.

(1) Upon completion of Phase 1 through Phase 4, a continued program will repeat the cycle. When reaching the 1200-hour interval, Phase 5 will be performed in conjunction with a phase corresponding to the 1200-hour interval.

(2) Special inspections having hour interval will be performed with a phase corresponding to that particular hour interval.

J. Time Limit Items.

(1) Components and/or systems having time limits of 12 months, 24 months, 36 months, 48 months, 60 months, etc., may be performed at the specific time limit or with a phase inspection corresponding to interval. NOTE: A calendar month starts on the first day of the month. All inspections for that interval become due by the last day of that month.

K. STC Installations

When an STC installation is incorporated on the airplane, those portions of the airplane affected by the installation must also be inspected in accordance with the inspection program published by the owner of the STC. Requirements for STC installations not owned by Cessna are not included in this manual.

L. Inspection Time Limitations

NOTE: Any inspection time limit found in Section 4 of this SOM shall not be extended.

A. Phases 1, 2, 3, 4 and 5 due points can be extended for maintenance scheduling purposes only as provided below:

(1) Phases 1, 2, 3 and 4 can be extended up to a maximum of 30 flight hours or two calendar months from the due point.

(2) Phase 5 and 49 can be extended up to a maximum of 100 flight hours or two calendar months from the due point.

(3) Inspection Documents MA thru ME are Chapter 4 requirements and shall not be extended.

B. All remaining phase due points can be extended for maintenance scheduling purposes only up to a maximum of 10 flight hours from the due point for hourly driven inspections and 1 calendar month for calendar driven inspections.

C. Any portion of the allowable extension used need not be deducted from the subsequent due point.

D. Any inspection program based on the intervals of the items in this chapter, or more frequent intervals, is acceptable.

M. Program Startup

NOTE: This procedure for program startup applies only to airplanes that have been previously using an inspection program other than Cessna's recommended Continuous Inspection Program.

To start this continuous inspection program, the following steps must be accomplished for airplanes other than those newly manufactured.

(1) Conduct a Log Book Audit. (2) Conduct a complete airplane inspection by performing Phases 1 through 5. (3) Start the program at Phase number 1. (Refer to Continuous Inspection Program Procedure) (4) Continue performing inspections in the normal manner.

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3.4 Special Inspections To be carried out at the periods specified (at the completion of the interval occurring first) in Section 4 of this System of Maintenance.

3.5 Maintenance Release Inspection A Maintenance Release shall be issued at the Maintenance Release Inspection referred to in Section 5, for a period of 160 hours or 6 months.

3.6 Airworthiness Directives ADs called up in CASR 1998 Parts 39-105, 106, 107 and 108 must be complied with at all times.

3.7 Time Lifed Components To be carried out at the periods specified (at the completion of the interval occurring first) in Section 4 of this System of Maintenance.

3.8 Radio Inspection To be carried out at not more than 300 hours and at least each 12 months (or less) in accordance with Section 5 of this System of Maintenance.

3.9 Service Bulletins & Instructions Manufacturers special instructions in the form of Service Bulletins or Letters which call up additional instructions for the continued airworthiness of the aircraft on how maintenance should be carried out on the aircraft or any component fitted to the aircraft, shall be assessed for applicability to the type of maintenance being undertaken and actioned accordingly.

Manufacturers special instructions in the form of Service Bulletins or Letters which detail modifications to the aircraft, aircraft components or systems, or changes in component part numbers shall be assessed and actioned as necessary taking into account the manufacturer recommendations and operational experience.

The assessment of any Service Bulletin or Instruction and decision to comply or not comply shall be undertaken by the Maintenance Controller.

3.10 Pilot Maintenance

Maintenance by pilots shall only be carried out on authorisation of the Maxem Aviation Pty Ltd Maintenance Controller

Approved Maintenance Tasks: No Task 1 Carry out a daily/pre-flight inspection to ascertain the serviceability of the aircraft for an

intended flight. 2 Checking and replenishment of all aircraft fluids not under pressure. 3 Removal or re-configuration of aircraft cabin seating in accordance with the Pilot Operating

Handbook. 4 Checking and inflating of tyres. 5 Remove and fit cargo restraint devices not requiring the use of tools. 6 MEL Compliance Procedures as prefixed by the "(0)" symbol (Crew Operating procedure).

Defined the MEL Requirements. 7 Replace an updated GPS data card when required.

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3.11 Unscheduled Inspections

Lightning Strike Inspection: Inspect in accordance with Aircraft Maintenance Manual Chapter 5-50-00 and PW JT 15 Maintenance Manual Chapter 72-00-50 Table 603

Hard or Overweight Landing Inspection: Inspect in accordance with Aircraft Maintenance Manual Chapter 5-50-00

Inspection After Overspeed - Flaps, Landing Gear, or Airplane: Inspect in accordance with Aircraft Maintenance Manual Chapter 5-50-00

Inspection After Sever Air Turbulence or Maneuvers: Inspect in accordance with Aircraft Maintenance Manual Chapter 5-50-00

Inspection After Foreign Object Damage: Inspect in accordance with Aircraft Maintenance Manual Chapter 5-50-00 and PW JT 15 Maintenance Manual Chapter 72-00-50 Table 603

Inspection After Soft Object Damage: Inspect in accordance with PW JT 15 Maintenance Manual Chapter 72-00-50 Table 603

Inspection After Improper Towing or Ground Damage: Inspect in accordance with Aircraft Maintenance Manual Chapter 5-50-00

Inspection After Engine Loss of Oil: Inspect in accordance with PW JT 15 Maintenance Manual Chapter 72-00-50 Table 603

Inspection After Engine Windmilling In Flight: Inspect in accordance with PW JT 15 Maintenance Manual Chapter 72-00-50 Table 603

Inspection After Engine Over Speed Or Over temperature: Inspect in accordance with PW JT 15 Maintenance Manual Chapter 71-00-50 Figures 505 or 506 and

503 or 504 as applicable

Inspection After Aircraft Or Engine Bird strike: Inspect in accordance with Aircraft Maintenance Manual Chapter 5-50-00 and PW JT 15 Maintenance

Manual Chapter 72-00-50 Table 603

Inspection After Rejected Takeoff, or Brake Overheating: Inspect in accordance with Parker Aerospace CMM P/N CM030-18902

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Volume 1

Section 4

Page 1

Section 4

OVERHAUL, REPLACEMENT & SPECIAL INSPECTION SCHEDULE

TABLE OF CONTENTS

Page No.


Overhaul and Replacement Schedule ......................................................................................... 2

Special Inspection Schedule ....................................................................................................... 3

Special Inspection Schedule ....................................................................................................... 4

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Section 4

OVERHAUL and REPLACEMENT SCHEDULE

The following tables have been prepared by reference to manuals listed in Section 2 - 2.6. All life component times listed in the tables are subject to compliance with lifed component times in manuals listed in 2.6. The Maintenance Controller must ensure that the tables are maintained to the latest version of the manuals listed in 2.6, and shall audit the lifed component times in manuals listed in 2.6, and the tables below at the time any new aircraft entry onto this system, and shall ensure the tables reflect each aircraft configuration correctly.

A. Airframe Requirement Period 1 Fire Bottle Cartridge P/N 13083-5 Replace 6 Years 2 Flap Gearbox P/N 5565175-31 Overhaul 3,000 Hours 3 NLG Actuator P/N 9912063-13 * Replace 15,100 Ldgs 4 NLG Assembly P/N 5542000-9 * Replace 15,100 Ldgs 5 NLG Fork P/N 5542300-1* Replace 8,800 Ldgs 6 NLG Trunnion P/N 5542301-5 * Replace 15,100 Ldgs 7 NLG Piston Weld P/N 5542105-2 * Replace 8,800 Ldgs 8 MLG Assembly P/N 6541000-3/4 * Replace 18,800 Ldgs 9 MLG Torque Link Assembly Lower P/N 5541304-6 * Replace 26,800 Ldgs

10 MLG Outer Cylinder P/N 5541109-1 * Replace 10,900 Ldgs 11 MLG Actuator P/N 9912053-17, -18 * Replace 18,800 Ldgs 12 NLG Actuator Fittings P/N 5511169-1 * Replace 9,700 Ldgs 13 MLG Forward Trunnion Assembly P/N 5522700-5, -6 * Replace 17,000 Ldgs 14 MLG Aft Trunnion Fitting Assembly P/N 5522710-7, -8 * Replace 12,300 Ldgs 15 MLG Side Brace Support Fitting P/N 5522720-1, -2 * Replace 19,700 Ldgs 16 Pneumatic Blowdown/Emergency Brake Bottle P/N 9912103-2 Replace 20 Years 17 Oxygen Cylinder (lightweight) with DOT Rating of DOT3HT1850 Replace 24 Years 18 Cleveland Brake Assembly P/N 030-18902 IAW Parker Aerospace

CM030-18902 CMM (If Brake Lining Wear Check indicates worn condition)

Overhaul On Condition

19 Cleveland Main Wheel Assembly P/N 040-23901 IAW Parker Aerospace CM040-23901 CMM

Overhaul 500 Ldgs

20 Nose Wheel Assembly P/N 9544207 IAW Parker Aerospace CMM Overhaul 500 Ldgs * IAW New Flight Corporation Maintenance Manual Supplement MMS-921 latest revision.

B. Engine Requirement Period 1 P&WC JD15D-4 Engines Overhaul As per P&WC

SB 7003 latest amendment

2 P&WC JD15D-4 Engine Components Overhaul As per P&WC SB 7003 latest amendment

3 P&WC JD15D-4 Engine Rotor Components IAW AD/ENG/7 latest amendment.

Replace As per P&WC SB 7002 latest amendment

4 Engine Mounts Overhaul At engine overhaul.

5 Starter Generator Overhaul 1,000 Hours 6 Motive Flow Valve Overhaul At engine

overhaul.

C. Electrical Requirement Period 1 Defog Fan P/N 5703-3 Overhaul 3,500 Hours 2 Overhead Cabin Fan P/N 9912323-2 Overhaul 1,200 Hours 3 Environmental Control Unit (Hamilton Standard) Overhaul 5,000 Hours

D. Instrument Requirement Period 1 Oxygen Masks, Scott Eros Overhaul 6 Years

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OVERHAUL and REPLACEMENT SCHEDULE (cont)

E. Radio Requirement Period 1 ELT Battery Replace 5 Years 2 Underwater Locator Beacon Battery P/N DK120 Replace 6 Years 3 EPIRB Battery Replace 5 Years

Continuous Airworthiness Inspection Program Phase Period Applicability Phase 6 Every 14 days if operated in a corrosive environment As required Phase 7 Every 90 days if Drag Chute is not deployed. As required Phase 8 Not used N/A Phase 10 Every 100 Hours Yes Phase 11 N/A SB 550-22-06 incorporated. N/A Phase 12 N/A No ACM, SB 57-03 incorporated. N/A Phase 13 Every 3 months, or 100 Hours Yes Phase 14 First 10,000 Hours and every 3,000 Hours thereafter Yes Phase 15 First 10,000 Hours, at 15,000 Hours and every 1,000 Hours thereafter. Yes Phase 16 First 10,000 Hours, at 15,000 Hours and every 3,000 Hours thereafter. Yes Phase 17 10,000 Hours Yes Phase 18 Every one year Yes Phase 19 First 10,000 Hours and every 2,500 Hours thereafter Yes Phase 20 Every 24 Months and covered by AD/INST/9 Yes Phase 21 Every 24 Months and covered by AD/REC/1, AD/RAD/43 and AD/RAD/47 Yes Phase 22 Every 36 months Yes Phase 23 Every 60 months Yes Phase 25 Not used N/A Phase 34 Every 6 months but for Halon Fire Ext covered by AD/FPE/7 Yes Phase 35 Every 3 to 6 Months Yes Phase 37 Every 5,000 Hours Yes Phase 39 Role Equipment not fitted N/A Phase 40 First 10,000 Hours and every 5,000 Hours thereafter Yes Phase 41 N/A by Serial Number N/A Phase 42 Not used N/A Phase 43 Not used N/A Phase 45 Not used N/A Phase 46 Not used N/A Phase 47 Every 12 Years Yes Phase 48 Every 6 Years Yes Phase 49 First 6 Years or 2,400 Hours *, then every 1,200 Hours or 36 Months * Yes Phase 50 First 15 Years or 10,000 Hours *, then every 1,200 Hours or 36 Months * Yes Phase 53 N/A by Serial Number N/A Phase 54 Not used N/A Phase 55 Every 12 months Yes Phase 56 N/A by serial number N/A Phase 57 150 Hours after the copilots side window is replaced Yes Phase MA By 224 ldgs and every 200 ldgs until replacement life is reached (749 ldgs) Yes Phase MB At 425 ldgs and replace at replacement life (749 ldgs) Yes Phase MC N/A by serial number N/A Phase MD At 5,000 Landings and every 1,000 Landings thereafter Yes Phase ME N/A by serial number N/A

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SPECIAL INSPECTION SCHEDULE

A. Airframe Requirement Period 1 Reweigh Reweigh 3 Years 2 De-ice Boots apply Age-Master protective coating. P/N 74-451-127 Apply 6 Months 3 Hand Held Fire Extinguishers Section 5 Inspection Sheet Inspect 6 Months 4 Cleveland Brake Lining Wear Check Inspect IAW Parker

Aerospace CM030-18902 CMM Inspect 150 Hours

5 Cleveland Main Wheel Assembly P/N 040-23901 IAW Parker Aerospace CM040-23901 CMM

Inspect Tyre Change

6 Nose Wheel Assembly P/N 9544207 IAW Parker Aerospace CMM Inspect Tyre Change

B. Engine Requirement Period 1 Minor Inspection IAW the P&WC MM Table 601 Inspect 300 Hours or

24 Months* 2 Oil Filter Element - IAW the P&WC MM Inspect/clean

or replace 200 Hours

3 Engine Hot Section Inspection - as per P&WC SB 7003 latest amendment

Inspect As per doc

C. Electrical Requirement Period 1 Defog Fan P/N 5703-3 carry out brush check Inspect 1,200 Hours

D. Instrument Requirement Period 1 Flight Data Recorder P/N 980-4100-FWUS as per Sundstrand

Table Inspect 5,000 Hours

2 Flight Data Recorder Accelerometer P/N 981-3088-010 Calibrate 2,000 Hours 3 Barometric Altimeters (FAR Part 43 requirements) (AD/INST/9 latest

amendment) Calibrate 2 Years

4 Pitot/Static system test. (AD/INST/9 latest amendment) Test 2 Years 5 Direct Reading, and Remote Indicating Compass calibration IAW

CAO 108.6 Calibrate 3 Years, and at

each engine change.

E. Radio Requirement Period 1 Racked Avionics - inspect for security of racked Inspect avionics, and

wiring for condition and security. May be certified by an Airframe licensed AME IAW CAO 100.90 2.5 (a) (ii), or by an Engine licensed AME IAW CAO 100.90 3.6 (a) (ii)

Inspect 150 Hours +/- 15 hours.

2 ATC Transponder Systems with Active Mode C - calibration and test IAW AD/RAD/43 latest amendment.

Calibration and Test

2 Years

3 ATC Transponder System test IAW AD/RAD/47 latest amendment. Test 2 Years 4 Cockpit Voice Recorder (CVR) check and functional test as per

AD/REC/1 latest amendment. Test 12 months or

2,000 Hours* 5 Underwater Locator Beacon Clean battery contacts Service 3 months 6 Underwater Locator Beacon Functional Test as per AD/REC/1 latest

amendment. Test 1 Years

Whichever is the sooner.

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ADDITIONAL INSPECTIONS

TABLE OF CONTENTS

Page No.


Maintenance Release Inspection ............................................................................................... 2

Engine Operational Check ......................................................................................................... 3

Radio Periodic Inspection ........................................................................................................... 5

Hand Held Fire Extinguisher Inspection ..................................................................................... 8

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Section 5

MAINTENANCE RELEASE INSPECTION

Item #

CATEGORY AIRFRAME ACTION

AME LAME Sig & Lic.

#

Date

1 Daily Inspection perform IAW Cessna 550 Flight Manual P/N 55FM-41

2 Expired Maintenance Release ensure OPEN Part 1 Maintenance Required items are listed in the Maintenance Controller supplied Form 090. Endorse as transferred to new M/R If not contact the Maintenance Controller immediately

3 Perform Engine Operational Check. 4 Expired Maintenance Release ensure OPEN defects are

transferred through to Work and Survey Sheets for rectification, unless under cover of an MEL or PUS. Endorse as transferred to worksheets Transfer deferred items under cover of an MEL or PUS to the new M/R Part 3.

5 New Maintenance Release transfer Maintenance Due items from Form 090 to Part 1.

6 New Maintenance Release issue and place in the document file in the aircraft.

The Maintenance Release Inspection must be performed by an appropriately licensed Airframe and Engine AME. Any defect or discrepancy found during carrying out this inspection is to be entered onto Work & Survey Sheet, rectification actions recorded and certified on that document.

Coordination Certification: I hereby certify for the completion and coordination of the above inspection:

LAME: Licence #: .. Date: ..

Maintenance Release No: .. Issued: ..

This signature constitutes a certification pursuant to CAR42ZE.

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Revision: Initial

Date: 20/09/10


Volume 1

Section 5

Page 3

Section 5

ENGINE OPERATIONAL CHECK

Job No: ________________ TTIS:__________ Hours: ___________ Landings: ____________

Sheet 1 of 2

Item Requirement L/H

R/H Notes

1 Check the following during start procedure for correct operation: a) Starter button illuminates b) Fuel boost light on c) Fuel pressure low light out d) Throttle-move to idle at 8-10 % turbine RPM e) Ignition light on f) Fuel flow increasing g) ITT- check for increase. Record max start ITT.......L/H............

R/H............

Note: Abort start if there is no ITT indication within 10 seconds or if ITT exceeds 500 C

h) Oil pressure low light out Note - indicated oil pressure above 35 PSI

I) Start button, ignition & fuel boost lights OUT between 30 - 42 % turbine RPM j) Generator off light OUT above 40 % turbine RPM Note - Ammeter load indication k) Start second engine. Repeat steps a through j. CAUTION: for generator assisted starts of second engine limit turbine RPM of operating engine to 50 % for protection of the Starter/Gen drive.

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2 Inverters on. Check all gyro instruments for noisy or erratic operation.

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3 Pneumatic pressure system: Check for correct limits, 2 - 3 PSI. Check R/H horizon Gyro for noisy or erratic operation.

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4 Check fuel crossfeed system for correct operation. ......... .........

5 With engines operating at above 60% turbine RPM, check the following: a) Engine Anti-Ice system 1) L/H & R/H engine ice fail light ON (Will be on for

varying periods depending on OAT due to the sensors in the wing leading edge heaters)

2) Check for even ITT increase L/H & R/H. 3) Check for ignition operation and light illumination. 4) Check generator load even. 5) Turn system off and check for even ITT decrease.

b) Surface De-Ice system 1) Check for boot inflation. 2) Check for correct light operation. Light should illuminate

twice each cycle.

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1-RHEN Issue 05

Revision: Initial

Date: 20/09/10


Volume 1

Section 5

Page 4

ENGINE OPERATIONAL CHECK Sheet 2 of 2

Item Requirement L/H

R/H Notes

6 Generator Control Unit Voltage Check. (If Required.) Run engines at 60% turbine RPM. Check Generator voltage using an accurate voltmeter. Check voltage at test jacks on control units. Adjust generators as required to achieve the following settings: 19 cell battery 28.5 +/- 0.8 VDC 20 cell battery 29.5 +/- 0.8 VDC

After generator adjustment check generator balance. Establish electrical load of 150-300 amps, both generators on. Allowable difference between L/H & R/H generators is 40 amps.

7 Check windscreen bleed air anti-ice system for correct operation and indication. Run engine at 60% turbine RPM for this check.

8 Check operation of engine synchroniser in turbine and fan positions. Run engine above 70% for this check and synchroniser should operate within a 1.5% split in either turbine or fan positions.

9 Check operation of all engine indicators. 10 Check air conditioning in ground mode for correct operation. 11 Check idle RPM.

49 +/- 1% Record L/H...............

R/H...............

12 Check for clean shutdown on completion of engine run. 13 Inspect both engines for leaks following ground run.

Any defect or discrepancy found during carrying out this inspection is to be entered onto Work & Survey Sheet, rectification actions recorded and certified on that document.

Coordination Certification: I hereby certify for the completion and coordination of the above category:

LAME: Licence #: .. Date: .. This signature constitutes a certification pursuant to CAR42ZE.

1-RHEN Issue 05

Revision: Initial

Date: 20/09/10


Volume 1

Section 5

Page 5

Section 5

RADIO PERIODIC INSPECTION

Job No: ________________ TTIS:__________ Hours: ___________ Landings: ____________

Sheet 1 of 3 PERIODIC RADIO CATEGORY INSPECTION SCHEDULE

Item No Requirement -Radio

AME

LAME Licence No Date

1 Check maintenance release and rectify any reported defects

2 Check all antenna external fittings and supports for security and freedom from damage

3 Check that all units are securely mounted in their cases and that shock mounts and cases are securely attached to the airframe.

4 Check all switches, knobs, lamps bezels, circuit breakers, circuit breaker panels and microphone jacks for condition and security.

5 Check all visible bonding straps for condition and security

6 Check all visible cables and looms for condition and security.

7 Check all visible plugs and connectors for condition and security.

8 Check all safety wiring of units that require to be lockwired. 9 Clean all dust and foreign material from equipment cases

and components.

10 Check frequency charts, dials, placards and decals for legibility and security

11 Check speakers and muting system for correct operation

12 Check headphones for condition, security and operation

13 Check microphones for condition, security and operation.

14 Check VHF and HF communication systems with a suitable ground station and ensure that units operate correctly on the normally used channels. Check that meter readings, where provided, indicate satisfactory performance.

15 Check marker system for satisfactory performance in all modes of operation using an approved simulator, ensure correct visual and aural output.

16 Inspect ELT, wiring and antenna for security and condition. Inspect battery pack and surrounding area for corrosion. Record battery expiry date ....../...../..... Check ELT operation.

17 Check 1000MHz D.M.E. system for correct operation in accordance with procedures and that station identification coding is readable.

18 Check operation of both audio systems for correct function of switches, mic selector and that radio output is available in emergency mode to headphones. Ensure all audio switches are correctly identified.

1-RHEN Issue 05

Revision: Initial

Date: 20/09/10


Volume 1

Section 5

Page 6 Sheet 2 of 3

PERIODIC RADIO CATEGORY INSPECTION SCHEDULE


AME


19 Check operation or VOR and ILS systems using an approved simulator and ensuring that system accuracy is within limits as specified under: VOR Instrument Maximum Reading Course Width Error

CI/OBS + 3o 10o + 2 Either side of RMI + 4o selected radial OBI + 4o

ILS Localizer

Standard Centreing Standard Deviation

+ 10% of centre to full scale 40% to 80% of centre to (FSD) deflection (FSD) (2 to 4 dots on standard 5 dot-0-5 dot presentation).

NOTE FSD is defined as Course Bar Deflection to the outermost calibration mark on the instrument.

20 Check both Glidescope systems for correct operation using an approved simulator. Ensure that system accuracy is within limits as specified here under. Glidescope

Standard Centreing Standard Deviation

+ 10% of centre to full scale deflection 30% to 70% of centre to full scale deflection (FSD) (FSD) 1.5 to 3.5 dots on standard 5 dot-0-5 dot presentation.

NOTE: FSD is defined as course bar deflection to the outermost calibration mark on the instrument.

21 Check weather radar for correct performance by observation of meter readings and operation in all modes using the self test selection on the indicator.

NOTE: Before operating radar, position nose of aircraft clear of all buildings, obstructions and other aircraft. Ensure all precautions as per CAO 20-9 are observed

22 Transponder - Check transponder systems for correct function and condition on both positions 1 and 2 by using the self test selection.] TEST - Select code 2100. Turn function switch to stand-by position and allow to warm up. Select "test" function, reply lamp should light while in test position. Select normal "on" functions. Activate "Ident". Reply lamp should light for approximately 20 seconds then automatically extinguish. Switch Off.

1-RHEN Issue 05

Revision: Initial

Date: 20/09/10


Volume 1

Section 5

Page 7 Sheet 3 of 3

PERIODIC RADIO CATEGORY INSPECTION SCHEDULE


AME


23 Check Radio Altimeter for correct function and condition by using the self test selection

24 Check Flight Director NAV coupling systems in conjunction with Instrument L.A.M.E. for correct operation in all navigational modes

25 Cockpit Voice Recorder: Check security of installation, evidence of damage and general condition. Carry out functional test by using test switch facility.

26 GPS (if fitted) - Check for security, general cleanliness, and correct operation in accordance with the GPS Maintenance Manual.

27 Check and ensure all tools and maintenance equipment have been removed from the aircraft and that all access doors and inspection panels have been correctly secured.

Any defect or discrepancy found during carrying out this inspection is to be entered onto Work & Survey Sheet, rectification actions recorded and certified on that document.

Coordination Certification: I hereby certify for the completion and coordination of the above category:

LAME: Licence #: .. Date: .. This signature constitutes a certification pursuant to CAR42ZE.

1-RHEN Issue 05

Revision: Initial

Date: 20/09/10


Volume 1

Section 5

Page 8

Hand Held Fire Extinguisher Inspection

VH- J/N: Extinguisher Position: Type: P/N: S/N:

Table 3.1 Maintenance Schedule. Level 1, 2 and 3 Inspections for Vapourising Liquid (Halon) Extinguishers

No Action Required. AME SIG LAME SIG 1 Check that the extinguisher is conspicuous, readily accessible, and in

its assigned location, and the location sign is visible and correct.

2 Check that the anti-tamper device, where fitted, is intact.

3 Check that an appropriate support bracket is securely in place.

4 Check that the extinguisher is clean, that the instructions for operation are clearly legible, and that the maintenance record tag (where applicable) is attached.

5 Check that the extinguisher, including attachments, is not damaged.

6 Check that the exterior of the extinguisher is not pitted from corrosion.

7 Check that the discharge nozzle is the correct type.

8 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.

9 Check that the extinguisher is fully charged eg by overall mass. Record weight to two decimal places.

10 Check that the pressure indicator mechanism, where fitted, is registering within the operational range, and appears to be free and operating correctly.

11 Where possible, without discharging any contents, check that the actuating device is undamaged, free from corrosion, and moves freely.

12 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 its cradle):

No Action Required. AME SIG LAME SIG 1 Check the type of extinguisher is clearly marked; (write Halon in a

permanent marker, or affix a permanent tag)

2 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.

3 Check the charged weight, or empty weight and weight charge is clearly marked on the extinguisher, or tag.

4 Check the operating instructions and any special precautions for use are clearly marked.

Notes:

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1-RHEN Issue 05

Maxem 550 SOM Amd 05

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