SERVICE LETTER REVISION

Transcription

1 Citation Revision 2 SERVICE LETTER REVISION SL TRANSMITTAL SHEET This sheet transmits Revision 2 to SL , which: A. Made minor editorial changes throughout the Service Letter and 650 Conversion Matrix. B. Changed the flight hour/time frequency on the 650 Conversion Matrix 0512MI Phase inspection from every 2000 hours and 4 years to every 2400 hours and six years. NOTE: This revision replaces the original issue of SL in its entirety. NOTE: Change bars and pointing hands are not used in this publication to denote revised material. This transmittal sheet provides a complete description of the changes made by this revision, except for editorial changes. REVISION COMPLIANCE NO EFFECT. Airplanes previously modified by this service letter are not affected by this revision. SUMMARY OF REVISIONS Original Issue Feb 26/2008 Revision 1 Mar 13/2008 Revision 2 Dec 15/2008

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3 Citation Revision 1 SERVICE LETTER REVISION SL TRANSMITTAL SHEET This sheet transmits Revision 1 to SL , which: A. Made minor editorial changes throughout the Service Letter and 650 Conversion Matrix. B. Attached all of Chapter 5-12, Revision 29 from the Model 650 Maintenance Manual. NOTE: This revision replaces the original issue of SL in its entirety. NOTE: Change bars and pointing hands are not used in this publication to denote revised material. This transmittal sheet provides a complete description of the changes made by this revision, except for editorial changes. REVISION COMPLIANCE NO EFFECT. Airplanes previously modified by this service letter are not affected by this revision. SUMMARY OF REVISIONS Original Issue Feb 26/2008 Revision 1 Mar 13/2008

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5 Citation TITLE SERVICE LETTER SL TIME LIMITS/MAINTENANCE CHECKS - NEW 650 TASK BASED INSPECTION PROGRAM EFFECTIVITY MODEL SERIAL S 650 (Citation III) thru -0199, thru (Citation VI) thru -0202, thru (Citation VII) thru REASON Citation Maintenance Engineering has incorporated a new task-based inspection program in the Model 650 Maintenance Manual, Revision 30. DESCRIPTION This service letter provides the instructions necessary to incorporate the new task-based inspection program on the Model 650. Many item codes were incorporated into one task. Item codes that were found to be not applicable or not effective were eliminated. Many item code intervals were extended within the new tasks. The scheduled maintenance checks in Chapter were removed from the Maintenance Manual. Chapter 5-12 has incorporated inspection documents to replace the inspection phases. Inspection time limits in Chapter have tasks incorporated. S will be eliminated March 31, A conversion matrix is provided that allows translating the previous inspection plan into the new task based plan. COMPLIANCE MANDATORY. This service letter must be accomplished no later than March 31, MANPOWER WORK PHASE MAN-HOURS Modification * REFERENCES Cessna Model 650 Citation Maintenance Manual, Revision 30 Cessna Model 650 Citation Maintenance Manual, Revision 29, Chapters 5-12 and (attached) Conversion Matrix (attached) Feb 26/ Revision 2 - Dec 15/2008 Page1of2 Cessna Aircraft Company, Citation Marketing Division, P.O. Box 7706, Wichita, KS 67277, U.S.A , Fax COPYRIGHT 2008

6 Citation PUBLICATIONS AFFECTED None SERVICE LETTER SL ACCOMPLISHMENT INSTRUCTIONS 1. Attached are the necessary documents from Revision 29, (Chapter 5-12 Continuous Inspection and Chapter Expanded Inspections) which are valid until you change to the new task-based inspection program. A conversion matrix that will allow you to translate the previous inspection plan into the new task based plan is provided with this service letter. NOTE: Be sure to keep this service letter with the attached documents. 2. This service letter and Revision 11 of the 's are valid until March 31, At that time, the only Cessna scheduled maintenance plan will be Revision 30 or later to the maintenance manual. 3. Attached is a mandatory information form for you to complete and return as soon as possible. This will help us determine if you will require individual help with your transition to the new task-based program. 4. Any questions about the new inspection program can be directed to Ron Barber at , Don Detwiler at or Jerry Morris at Any questions regarding the CESCOM reports that show the new task-based inspection program can be directed to: Kim Purcell at , Kim Dumcum at or Julio Urbina at Record that this service letter has been completed. This will indicate the date of conversion. A. Complete a Maintenance Transaction Report. B. Put a copy of the completed Maintenance Transaction Report in the airplane logbook. C. Send a copy of the completed Maintenance Transaction Report to: CESCOM, P.O. Box 7706, Wichita, KS or Fax or form to cescom@cessna.textron.com. D. Ifyoudonotchangetothetask-basedinspectionprogramcompletetheformontheserviceletter attachment. (1) Send the completed form to: CESCOM, P.O. Box 7706, Wichita, KS or Fax or form to cescom@cessna.textron.com Feb 26/ Revision 2 - Dec 15/2008 Page 2

7 Citation ATTACHMENT SL FORM Serial Number Company Name Maintenance Manager Name/Contact Please give the reason if you cannot make the change to the task-based inspection program: Please fill out and send to: CESCOM, P.O. Box 7706, Wichita, KS or Fax or form to

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9 650 Conversion Matrix 650 CONVERSION MATRIX OWNER CONVERSION DATE UNIT ENGINE 2 ENGINE 1 AIRFRAME APU EXISTING CURRENT C/W TIME B PHASE B INSPECTION 150 HOURS OR 24 MONTHS DROP - NOT USED N/A NEW ITEM CODE NEW INTERVAL PHASE 3 INSPECTION 300 HOURS OR 24 MONTHS INSPECTION DOCUMENT 4 1A/2C PHASE 4 INSPECTION PHASE 5 INSPECTION 1200 HOURS OR 3 YEARS INSPECTION DOCUMENT 8 3A/3C PHASE 6 INSPECTION 100 HOURS INSPECTION DOCUMENT 20 EXT SERV TOILET INSP 200 HOURS B PHASE 6 INSPECTION L RECONDITION 150 HOURS INSPECTION DOCUMENT HOURS OR CUSTOMER CURRENT INTERVAL B PHASE 6 INSPECTION R RECONDITION 150 HOURS INSPECTION DOCUMENT HOURS OR CUSTOMER CURRENT INTERVAL PHASE 8 INSPECTION 600 HOURS INSPECTION DOCUMENT HOURS MONTHS/ CFR , , AND RVSM 24 MONTHS/ CFR , , AND RVSM L R L R 24 MONTHS/ CFR , , AND RVSM 24 MONTHS/ CFR , , AND RVSM 24 MONTHS/ CFR , , AND RVSM 24 MONTHS/ CFR , , AND RVSM 24 MONTHS/ CFR , , AND RVSM PHASE 9 INSPECTION RVSM SKIN WAVINESS 24 MONTHS/ CFR , , AND RVSM INSPECTION DOCUMENT 43 AL CAL.SYS CK INSPECTION DOCUMENT 43 AL CAL.SYS CK INSPECTION DOCUMENT 43 AL CAL.SYS CK INSPECTION DOCUMENT 43 AL CAL.SYS CK INSPECTION DOCUMENT 43 XPD CAL INSPECTION DOCUMENT 43 XPD CAL INSPECTION DOCUMENT 43 RVSM SKIN WAVINESS PHASE 10 INSPECTION YEARS INSPECTION DOCUMENT 34 OXYGEN BOTTLE L R PATS & EXISTING INSPECTION PHASE 1 INSPECTION PHASE 2 INSPECTION PHASE 9 INSPECTION ALT CAL/SYS CK PHASE 9 INSPECTION ALT CAL/SYS CK PHASE 9 INSPECTION ADC CAL/SYS CK PHASE 9 INSPECTION ADC CAL/SYS CK PHASE 9 INSPECTION XPD CAL PHASE 9 INSPECTION XPD CAL PHASE 10 INSPECTION ENG FIRE EXT LH PHASE 10 INSPECTION ENG FIRE EXT RH PHASE 10 INSPECTION APU FIRE EXT BOTTLE PHASE 10 & 11 INSPECTIONS GEAR AND BRAKE BOTTLE 24 MONTHS/ CFR , , AND RVSM 24 MONTHS/ CFR , , AND RVSM 24 MONTHS/ CFR , , AND RVSM 24 MONTHS/ CFR , , AND RVSM 24 MONTHS/ CFR , , AND RVSM 24 MONTHS/ CFR , , AND RVSM 3 YEARS FROM THE DATE OF MANUFACTURE STAMPED ON THE CYLINDER, THEN EVERY 3 YEARS THEREAFTER 5 YEARS INSPECTION DOCUMENT 10 5C 5 YEARS INSPECTION DOCUMENT 10 5C 5 YEARS INSPECTION DOCUMENT 10 5C 3 YEARS PHASE 10 INSPECTION YEARS GEAR BOTTLE NEW DOCUMENT INSPECTION DOCUMENT 36 BRAKE AND GEAR BOTTLE INSPECTION DOCUMENT 35 GEAR BOTTLE FIVE YEARS FROM THE DATE OF MANUFACTURE, THEN EVERY 5 YEARS THEREAFTER FIVE YEARS FROM THE DATE OF MANUFACTURE, THEN EVERY 3 YEARS THEREAFTER 1 NEW DUE

10 650 Conversion Matrix EXISTING EXISTING INSPECTION CURRENT C/W TIME NEW ITEM CODE NEW DOCUMENT PHASE 10 INSPECTION YEARS INSPECTION DOCUMENT 37 OXYGEN BOTTLE EI**L E2**R A PHASE 11 INSPECTION PHASE 11 INSPECTION PHASE 14 INSPECTION CONCURRENT WITH EACH MAJOR PERIODIC INSPECTION (MPI) CONCURRENT WITH EACH MAJOR PERIODIC INSPECTION (MPI) FIRST 6000 HOURS OR 10 YEARS, WHICHEVER OCCURS FIRST, AND EVERY 2400 HOURS OR 6 YEARS THERAFTER FIRST 6000 FLIGHTS AND EVERY 2000 FLIGHTS THEREAFTER INSPECTION DOCUMENT 41 INSPECTION DOCUMENT 41 INSPECTION DOCUMENT 19 NEW INTERVAL 10 YEARS FROM THE DATE OF MANUFACTURE STAMPED ON THE CYLINDER, THEN EVERY 5 YEARS THEREAFTER CONCURRENT WITH ENGINE MAJOR PERIODIC INSPECTION (MPI) CONCURRENT WITH ENGINE MAJOR PERIODIC INSPECTION (MPI) FIRST 6000 HOURS OR 10 YEARS, WHICHEVER OCCURS FIRST, AND EVERY 2400 HOURS OR 6 YEARS THERAFTER FIRST 6000 LANDINGS AND EVERY 2000 LANDINGS THEREAFTER PHASE 18 INSPECTION INSPECTION DOCUMENT PHASE 19 INSPECTION EVERY 4800 HOURS LIFE LIMITED ITEM, REFER TO SECTION 5-1 EVERY 4800 HOURS PHASE 21 INSPECTON AT 2000, 2750, 3500, 4250 AND 5000 LANDINGS INSPECTION DOCUMENT 44 FIRST 2000 LANDINGS, THEN EVERY 750 LANDINGS THEREAFTER UNTIL 5000 LANDINGS PHASE 25 INSPECTION EVERY 12 CALENDAR MONTHS INSPECTION DOCUMENT 3 EVERY 12 CALENDAR MONTHS PHASE 26 INSPECTION FIRST 12,000 AND 22,000 LANDINGS DROP - NOT USED N/A AT 3000 HOURS AT 3600 HOURS A F FIRST 4000 HOURS AND EVERY 2000 HRS THEREAFTER EVERY 12 YEARS INSPECTION DOCUMENT 25 CBN BOND ASSY WINDOW INSPECTION DOCUMENT 18 INSPECTION DOCUMENT 13 PORTABLE FIRE HYDRO INSPECTION DOCUMENT 13 PORTABLE FIRE HYDRO FIRST 4000 HOURS, THEN 2000 HOURS THEREAFTER EVERY 12 YEARS 12C EVERY 6 YEARS INSPECTION DOCUMENT 11 6C A EVERY 6 YEARS PHASE 39 INSPECTION EVERY 6 YEARS F PORTABLE FIRE BOTTLE INSP PHASE 41 INSPECTION EVERY 500 AUXILIARY POWER UNIT HOURS APU-500 HR INSP/BRUSH AT 6 YEARS OR 2400 HOURS, WHICHEVER OCCURS FIRST, AND EACH 1200 HOURS OR 3 YEARS THEREAFTER INSPECTION DOCUMENT 11 PORTABLE FIRE BOTTLE INSP INSPECTION DOCUMENT 11 PORTABLE FIRE BOTTLE INSP INSPECTION DOCUMENT 31 APU-500 HR INSP/BRUSH INSPECTION DOCUMENT 17 SKIN JOINT INSPECTION 12C 6C 6C EVERY 500 APU HOURS FIRST 2400 HOURS OR 72 MONTHS, THEN 1200 HOURS OR 36 MONTHS EVERY 3 MONTHS DROP - NOT USED N/A E1**L E2**R A EVERY 1400 HOURS EVERY 1400 HOURS EVERY 6 MONTHS INSPECTION DOCUMENT 41 AFT COWL INSP INSPECTION DOCUMENT 41 AFT COWL INSP INSPECTION DOCUMENT 3 HALON FIRE EXT-WT CK PHASE 45 INSPECTION INSPECTION DOCUMENT 3 EVERY 6 MONTHS F HALON FIRE EXT-WT CK HALON FIRE EXT-WT CK PHASE 46 INSPECTION EVERY 6300 HOURS INSPECTION DOCUMENT L R PHASE 27 INSPECTION CBN BOND ASSY WINDOW PHASE 31 INSPECTION PHASE 38 INSPECTION PORTABLE FIRE BOTTLE HYDRO PHASE 38 INSPECTION PORTABLE FIRE BOTTLE HYDRO PHASE 39 INSPECTION PHASE 39 INSPECTION PORTABLE FIRE BOTTLE INSP PHASE 42 INSPECTION SKIN JOINT INSPECTION PHASE 43 INSPECTION PHASE 44 INSPECTION COMPOSITE AFT COWL PHASE 44 INSPECTION COMPOSITE AFT COWL PHASE 45 INSPECTION HALON FIRE EXT-WT CK PHASE 47 INSPECTION LEAD ACID BATT INSPEC PHASE 47 INSPECTION LEAD ACID BATT INSPEC AT 600 HOURS OR 12 CALENDAR MONTHS, WHICHEVER COMES FIRST, WITH SUBSEQUENT INSPECTIONS AT 200 HOUR INTERVALS OR 3 CALENDAR MONTHS INSPECTION DOCUMENT 23 LEAD ACID BATT INSPEC INSPECTION DOCUMENT 23 LEAD ACID BATT INSPEC CONCURRENT WITH ENGINE MAJOR PERIODIC INSPECTION (MPI) CONCURRENT WITH ENGINE MAJOR PERIODIC INSPECTION (MPI) 1C 1C CONCURRENT WITH ENGINE MAJOR PERIODIC INSPECTION (MPI) AT 600 HOURS OR 12 CALENDAR MONTHS, WHICHEVER COMES FIRST, WITH SUBSEQUENT INSPECTIONS AT 200 HOUR INTERVALS OR 3 CALENDAR MONTHS WHICHEVER OCCURS 2 NEW DUE

11 650 Conversion Matrix EXISTING A E1**L EXISTING INSPECTION CURRENT C/W TIME NEW ITEM CODE NEW DOCUMENT NEW INTERVAL ENGINE INSPECTION ITEMS DROP - NOT USED N/A A PHASE 48 INSPECTION ENGINE INSPECTION ITEMS E2**R ENG OIL CHANGE PHASE 49 INSPECTION EVERY 24 CALENDAR MONTHS INSPECTION DOCUMENT 30 EVERY 24 CALENDAR MONTHS EVERY 24 CALENDAR MONTHS EVERY 24 CALENDAR MONTHS EVERY 12 CALENDAR MONTHS AS REQUIRED BY TITLE 14 OF THE CODE OF FEDERAL REGULATIONS INSPECTION DOCUMENT 30 CVR BEACON PINGER TEST INSPECTION DOCUMENT 42 ELT INSPECTION EVERY 12 CALENDAR MONTHS AS REQUIRED BY TITLE 14 OF THE CODE OF FEDERAL REGULATIONS PHASE 52 INSPECTION ITEMS TO BE INSPECTED ON THE VAPOR CYCLE COOLING SYSTEM DROP - NOT USED N/A PHASE 53 INSPECTION EVERY 36 CALENDAR MONTHS INSPECTION DOCUMENT 9 3C N/A N/A N/A New INSPECTION DOCUMENT 1 1A/1C N/A N/A N/A New INSPECTION DOCUMENT 2 1A N/A N/A N/A New INSPECTION DOCUMENT 5 2A/2C N/A N/A N/A New INSPECTION DOCUMENT 6 2A N/A N/A N/A New INSPECTION DOCUMENT 7 2C N/A N/A N/A New INSPECTION DOCUMENT HOURS N/A N/A N/A New INSPECTION DOCUMENT DAYS N/A N/A N/A New INSPECTION DOCUMENT 28 6 MONTHS N/A N/A N/A New INSPECTION DOCUMENT HOURS N/A N/A N/A New INSPECTION DOCUMENT 40 IN ACCORDANCE WITH (IAW) MANUFACTURERS REQUIREMENT 0512MA PHASE MA INSPECTION 100 HOURS INSPECTION DOCUMENT MA 100 HOURS 0512MC 150 HOURS DROP - NOT USED N/A 0512MD 600 HOURS INSPECTION DOCUMENT MD 600 HOURS 0512ME 900 HOURS INSPECTION DOCUMENT ME 900 HOURS 0512MF & 0512MG O512MH 0512MI 0512MJ 0512MK PHASE 48 INSPECTION ENG OIL CHANGE PHASE 49 INSPECTION CVR BEACON PINGER TEST PHASE 50 INSPECTION ELT INSPECTION PHASE MC INSPECTION PHASE MD INSPECTION PHASE ME INSPECTION PHASE MF & MG INSPECTIONS PHASE MH INSPECTION PHASE MI INSPECTION PHASE MJ INSPECTION PHASE MK INSPECTION 1200 HOURS INSPECTION DOCUMENT MG 1200 HOURS FIRST 6000 HOURS OR TEN YEARS, WHICHEVER OCCURS FIRST, AND EVERY 2000 HRS OR FOUR YEARS, WHICHEVER OCCURS FIRST THEREAFTER FIRST 6000 HOURS OR TEN YEARS, WHICHEVER OCCURS FIRST, AND EVERY 2400 HRS OR SIX YEARS, WHICHEVER OCCURS FIRST THEREAFTER FIRST HOURS AND EVERY 2500 HOURS THEREAFTER FIRST 4000 HRS OR HRS, THEN EVERY 3000 HOURS THEREAFTER INSPECTION DOCUMENT MH INSPECTION DOCUMENT MI INSPECTION DOCUMENT MJ INSPECTION DOCUMENT MK INSPECTION DOCUMENT ML FIRST 6000 HOURS OR TEN YEARS, WHICHEVER OCCURS FIRST, AND EVERY 2400 HRS OR FOUR YEARS, WHICHEVER OCCURS FIRST THEREAFTER FIRST 6000 HOURS OR TEN YEARS, WHICHEVER OCCURS FIRST, AND EVERY 2400 HRS OR SIX YEARS, WHICHEVER OCCURS FIRST THEREAFTER FIRST HOURS AND THEN EVERY 2500 HOURS THEREAFTER FIRST 4000 HOURS, THEN EVERY 3000 HOURS THEREAFTER FIRST 12,000 HRS, THEN EVERY 3000 HOURS THEREAFTER 3 NEW DUE

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13 CONTINUOUS INSPECTION 1. Continuous Airworthiness Inspection Program A. Purpose and Use. (1) As detailed in Part , paragraph (e), of the Federal Aviation Regulations, turbojet airplanes must be inspected in accordance with an authorized inspection schedule. This section presents the continuous inspection program for the Model 650, recommended by Cessna Aircraft Company. 2. Federal Aviation Regulations A. General Operating and Flight Rules, Part (1) No person may operate a large airplane, or a turbojet multi-engine airplane, or turbopropeller-powered multi-engine airplane, or turbine-powered rotorcraft unless the replacement times for life-limited parts specified in the aircraft specifications, type data sheets or other documents approved by the Administrator are complied with and the airplane, or turbine-powered rotorcraft including the airframe, engines, propellers, rotors, appliances, survival equipment and emergency equipment, is inspected in accordance with an inspection program selected under the provisions of paragraph (f) of this section, except that, the owner or operator of a turbine-powered rotorcraft may elect to use the provisions of paragraph (a), (b), (c) or (d) in lieu of an inspection option of paragraph (f). (2) The registered owner or operator of each airplane or turbine powered rotorcraft described in paragraph (e) of this section must select, identify in the aircraft maintenance records and use one of the following programs for the inspection of the aircraft: (a) A continuous airworthiness inspection program that is a part of a continuous airworthiness maintenance program currently in use by a person holding an air carrier operating certificate issued under Part 121 or 135 of this chapter and operating that make and model aircraft under Part 121 of this chapter and maintaining it under paragraph (a) (2) of this chapter. (b) An approved aircraft inspection program approved under paragraph of this chapter and currently in use by a person holding an operating certificate under Part 135 of this chapter. (c) A current inspection program recommended by the manufacturer. (d) Any other inspection program established by the registered owner or operator of that airplane or turbine-powered rotorcraft and approved by the Administrator under paragraph (g) of this section. However, the Administrator may require revision to this inspection program in accordance with the provisions of Part (3) Each operator shall include in the selected program the name and address of the person responsible for scheduling the inspections required by the program and make a copy of that program available to the person performing inspections on the aircraft and, upon request, to the Administrator. (4) Each operator of an airplane or turbine-powered rotorcraft desiring to establish or change an approved inspection program under paragraph (f) (4) of this section must submit the program for approval to the local FAA Flight Standards District Office having jurisdiction over the area in which the aircraft is based. The program must include the following information: (a) Instructions and procedures for the conduct of inspections for the particular make and model airplane, including necessary tests and checks. The instructions and procedures must set forth in detail the parts and areas of the airframe, engines, propellers, rotors and appliances, including emergency equipment required to be inspected. (b) A schedule for performing of the inspections that must be performed under the program expressed in terms of the time in service, calendar time, number of system operations, or any combination of these. (c) When an operator changes from one inspection program, under paragraph (f) of this section, to another, the time in service, calendar times, or cycles of operation accumulated under the previous program must be applied in determining inspection due times under the new program Page 1 Cessna Aircraft Company Jan 2/2006

14 3. Construction A. Following is the recommended continuous inspection and maintenance schedule for Model 650 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 (Phases 6 and on) include all of the remaining inspection items. NOTE: Phase B is also provided and is required to be accomplished at 150-hour intervals when Phases 1 thru 4 are combined at 300-hour intervals (Method 3 of accomplishing Phases 1 through 4). 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 zone order. The last two digits (XX) of the chapter/section/subject correspond to the inspection phase. The signoff sheets have a column which lists the corresponding to the inspection item. Operators using the system should use the number to reference the appropriate for inspection requirements and details of specific procedures. Operators not using the system must reference the item as described in section for an expanded description of inspection items. Operators not using the system must refer to the appropriate system chapter for details required for conducting operational and functional tests requiredininspectionitems. 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 through 45 shall be performed. Expanded information detailed in will describe inspection items in Since is in chapter order, select the inspection item's corresponding chapter. (2) Component Time Limits , components that require maintenance at a specified time (does not include on condition items). (3) Unscheduled Maintenance , this includes the following: (a) Hard overweight landings. (b) Overspeed-flaps, gear or airplane. (c) Severe air turbulence or maneuvers. (d) Lightning strikes. (e) Foreign object damage. (f) Improper towing or ground damage. 4. Continuous Inspection Program Procedure A. The five primary phases (Phases 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 Phases 1 through 5 continuous inspection cycle. There are four plans (Plan 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. B. The five primary phases (Phases 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 different optional methods as provided in Item H Page 2 Cessna Aircraft Company Jan 2/2006

15 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 ( ) lists all components which are to be replaced or overhauled on a scheduled basis. Those items which are underlined are also listed in Chapter 4, Airworthiness Limitations. 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 as follows: METHOD 1: Phase 1 through Phase 4 inspections are based on 300-hour cycles, with one of the phase inspections accomplished every 75 hours of airplane operation. Applicable additional phases are integrated at their due times with the first four phases. At the completion of Phase 4, Phase 1 will become due 75 hours later and the cycle is to be repeated. PHASE 1 PHASE 2 PHASE 3 PHASE 4 75-HOUR 150-HOUR 225-HOUR 300-HOUR X X X X 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 1 PHASE 2 PHASE 3 PHASE 4 75-HOUR 150-HOUR 225-HOUR 300-HOUR X X X X METHOD 3: Phase 1 through Phase 4 are all combined and accomplished at 300-hour intervals. Applicable additional phases are integrated at their due times with the first four phases. Those that cannot be so integrated, must be performed early or separately. PHASE B PHASE 1 75-HOUR 150-HOUR 225-HOUR 300-HOUR X X Page 3 Cessna Aircraft Company Jan 2/2006

16 PHASE 2 PHASE 3 PHASE 4 75-HOUR 150-HOUR 225-HOUR 300-HOUR X X X NOTE: With all of the phases combined into 300-hour intervals, an inspection is required to be accomplished on certain items every 150 hours. These inspections are listed in Phase B. The 150-hour inspections are listed in two of the phases. Duplicated items need only be accomplished one time when combining phases. H. Four optional plans of accomplishing Phase 5 are provided as follows: (1) PLAN A: Phase 5 can be accomplished all at once, each 1200 hours concurrently with accomplishment at the end of the fourth cycle of Phases 1 through 4. (2) PLAN B: Phase 5 can be accomplished partially (approximately 1/12th) with each accomplishment of Phases 1 through 4 when they are performed each 75 hours (Method 1 of Phases 1 through 4). (3) PLAN C: Phase 5 can be accomplished partially (approximately 1/8th) with each accomplishment of combined Phases 1 through 4 when they are performed each 150 hours (Method 2 of Phases 1 through 4). (4) PLAN D: Phase 5 can be accomplished partially (approximately 1/4th) with each accomplishment of combined Phases 1 through 4 when they are performed each 300 hours (Method 3 of Phases 1 through 4). (5) Plan A may be used for all airplanes regardless of hourly usage. (6) Plans B, C and D are only recommended for airplanes whose annual flight time exceeds 400 hours per year. CHECK NUM- BER HOUR INTER- VAL PLAN A METHOD 1 METHOD 2 METHOD 3 PHASE PLAN B PLAN C PLAN D ,2 B 2,5A 1,2,5A,5B B ,5B , ,5C 3,4,5C,5D 1,2,3,4,5A, 5B,5C,5D ,2 B 2,5D 1,2,5E,5F B ,5E , ,5F 3,4,5G,5H 1,2,3,4,5E, 5F,5G,5H ,2 B 2,5G 1,2,5I B ,5H , ,5I 3,4,5J 1,2,3,4,5I, 5J,5K Page 4 Cessna Aircraft Company Jan 2/2006

17 CHECK NUM- BER HOUR INTER- VAL PLAN A METHOD 1 METHOD 2 METHOD 3 PHASE PLAN B PLAN C PLAN D ,2 B 2,5J 1,2,5K B ,5K ,5 3,4, ,5L 3,4,5L 1,2,3,4,5L 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. (2) Special inspections (Phases 6 through 45) 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 tointerval. 5. STC Installations A. Inspection requirements for STC installations are not included in this manual. When an STC installation is incorporated on the airplane, those portions of the airplane affected by the installation must be inspected in accordance with the inspection program published by the owner of the STC. Since STC installations may change systems interface, operating characteristics and component loads or stresses on adjacent structures, Cessna provided inspection criteria may not be valid for airplanes with STC installations. 6. Inspection Time Limitations NOTE: Any inspection time limit found in Chapter 5 and also required in Chapter 4 must not be extended. Any inspection required by the Code of Federal Regulations (CFR) and Reduced Vertical Separation Minimums (RVSM) must 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) Phases 5 and 42 can be extended up to a maximum of 100 flight hours or two calendar months from the due point. (3) The Phase B, when used, can be extended up to a maximum of 30 flight hours or two calendar months from the due point. (4) Any portion of the permitted extension used need not be deducted from the subsequent due point. B. All remaining phase due points, except Chapter 4, Airworthiness Limitations beginning with M, 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 inspection program based on the intervals of the items in this chapter, or more frequent intervals, is permitted. 7. A. is an optional work card system available from Cessna Citation Customer Services developed to assist maintenance and inspection personnel to more efficiently perform the inspection procedures required in this chapter Page 5 Cessna Aircraft Company Jan 2/2006

18 B. The various procedures published on the S are excerpted from the maintenance manual, structural repair manual and other miscellaneous manuals. Having this excerpted information on a single group of cards greatly reduces the number of pages of reference information required by the personnel performing the inspections. Additionally, a listing of any parts, consumables or special tools and equipment required is provided. C. The phase inspection pages have a column which lists the number which contains instructions for the inspection task. D. Although highly recommended, the system is not essential to performing the various phase inspections. 8. 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. A. To start this continuous inspection program, the following steps must be accomplished for airplanes other than those newly manufactured. (1) Conduct a complete airplane inspection by performing Phases 1 through 5. (2) Start the program at check number 1. (Refer to Continuous Inspection Program Procedure) (3) Continue performing inspections in the normal manner. 9. Logbook Forms, Pilot Information A. Airplane Flight Log, Section 1. (1) Provides a convenient place to maintain individual and cumulative flight records, total hours on the airplane and each engine, total landings for the airplane and the cycles of each engine. (2) The original of the Flight Log form is placed in Section 1 of the FAA Approved Airplane Flight and Maintenance Log Book and kept as part of the permanent airplane log. B. Form Completion. (1) The basic information at the top of this form should be completed. Enter the number of the page as it sequentially falls in the logbook section beginning with 1. The line entitled "Accumulated Totals Brought Forward" is the cumulative recorded information which is being carried forward from the previous page. This is a journey log and one line represents one flight. Under the following columns should be recorded: 1. The date of each flight. 2a. City where flight originated. 2b. City of flight destination. 3. The number of persons aboard, including crew. 4. Distance of flight in nautical miles. 5. The flight duration in hours and tenths from flight hour meter. 6. Accumulated total airplane time in hours and tenths. 7. Accumulated total time for engine 1 in hours and tenths. 8. Accumulated total time for engine 2 in hours and tenths. 9. Number of landings this flight. 10. Accumulated total airplane landings. 11. Accumulatedengine1cycles. 12. Accumulatedengine2cycles Page 6 Cessna Aircraft Company Jan 2/2006

19 13. The discrepancy sheet number column provides a reference to the airplane discrepancy form which details the airplane discrepancies on particular flight. If there are no discrepancies, NONE should be entered in this column. This provides the pilot with a convenient method of determining whether previous airplane discrepancies have been corrected. 14. The last name of the pilot and copilot for each flight should be recorded in the last column. 15. Theline"AccumulatedTotals"shouldbefilled in: When the form is completely filled. At the end of the CESCOM reporting period. (a) When the form is completely filled. (b) At the end of the CESCOM reporting period. (2) The totals of these lines should be carried forward to the line entitled "Accumulated Totals Brought Forward" on the next airplane flight log form used. (3) The original (white sheet) should be placed in the Airplane Flight and Maintenance Logbook in Section 1. (4) The first copy (pink sheet) should be mailed to the address at the top of the form and is used by CESCOM to report airplane utilization. (5) The second copy (yellow sheet) provides an extra customer copy and should be filed at the airplane base. Table 1. Log Book includes airplane and engine logs in the following: SECTION 1 Flight Time Information SECTION 6 Left Engine Maintenance SECTION 2 Pilot Squawk on Last Flight SECTION 7 Left Engine Service Bulletin SECTION 3 General Airplane Maintenance SECTION 8 Right Engine Maintenance SECTION 4 Service Bulletin SECTION 9 Right Engine Service Bulletin SECTION 5 Engine Change SECTION 10 Service Condition Reports SECTION 11 Component Master Inventory Cross-Reference List Table 2. New pages for the airplane logbook are listed below: Airplane SECTION 1 Airplane Flight Log Airplane SECTION 2 Airplane Discrepancies Airplane SECTION 3 Maintenance Transaction Report Airplane SECTION 4 Maintenance Transaction Report Airplane SECTION 5 Engine Change Record Left Engine SECTION 6 Maintenance Transaction Report Left Engine SECTION 7 Maintenance Transaction Report Right Engine SECTION 8 Maintenance Transaction Report Right Engine SECTION 9 Maintenance Transaction Report Airplane SECTION 10 Service Condition Report SECTION 11 Component Master Inventory Cross Reference List C. Mechanic Information: (1) Mechanics will fill out the airplane and engine maintenance records and use "Maintenance Transaction Report" for additional pages in the airplane logbook in Sections 3, 4, 6, 7, 8 and Page 7 Cessna Aircraft Company Jan 2/2006

20 (2) Place copies of the inspection program selected (sample letter), inspection record of phase due and completed in the front of the airplane log, for pilot and mechanics; information on inspection coming due. 10. Maintenance Transaction Report A. Maintenance Log - Airplane or engine entry. B. Date - Put the month, day and year the maintenance is performed. C. Airplane Serial Number and Airplane Registration Number. D. Total Airplane Hours. E. Complete When Applicable. F. Write in the three-letter identifier for the city in which the maintenance transaction is performed. (1) ItemName-Thecomponent for which the transaction is being performed. (2) Position - Left or Right, Inboard or Outboard. (3) Part Number. (4) Serial Number of InstalledPart. (5) Removal Reason - Check the box which corresponds to the reason for the component removal. (6) Status of Installed Part - Check the status of the part installed. Page 3 (Yellow) to Airplane base files. (7) Time Between Overhaul (TBO) - Check one of the boxes under (check one); next, place the TBO change in the blank and check one of the TBO controls. If the (OK as is) box is checked, nothing else need be done in this box. (8) Time Since Overhaul (TSO) - If an overhaul component is being installed, place its present TSO in the block and check the type of control. (9) Section and Page Numbers. (10) Type of Maintenance. (11) For Information and Other Log Entries: (12) How to enter Pages in Logbook - Page 1 (White) in logbook, Page 2 (Pink) in CESCOM Page 8 Cessna Aircraft Company Jan 2/2006

21 INSPECTION PHASE 1 Date: Registration Number: Serial Number: Total Time: 1. Description A. Phase 1 consists of 150-hour and 300-hour or 24 calendar months, whichever occurs first, interval inspection items contained in the forward nose section, cockpit area, instrument panel, control pedestal and cabin area. Items from other areas are included to meet their required time interval. B. Inspection items are given in order of the zone in which the inspection is to be done. A descriptive statement of the inspection requirement and the Item Code Number for cross-reference to section are supplied. The applicable number is given for the convenience of operators that use the system. C. For items or components that require an applicable lubrication, refer to Chapter 12, Scheduled Servicing - Description and Operation, or to the appropriate for the correct lubricant, lubricating points and method. Refer to Chapter 6, Airplane Zoning - Description and Operation for airplane zone definition. D. Non users can refer to the Expanded Inspection section of this chapter for any detailed information about the inspections required in this phase, which are uniquely required by this chapter. E. The right portion of each page has room for the mechanic's and inspector's initials and remarks. These pages can be reproduced, and used as a checklist when this inspection phase is done. F. Inspection item(s) were removed from this Inspection Document. For more details refer to the Introduction, Inspection Program Summary. 2. General Inspection Criteria A. During accomplishment of each of the specific inspection tasks within this phase, additional general inspections of the adjacent areas are done, while access is available. These general inspections are to find obvious conditions that need further procedures. B. If a component or system is changed (because of completed maintenance procedures) after an initially required task is completed, then that specific task must be done again, before the system or component is returned to service. C. Complete a preflight inspection after this inspection phase is completed to make sure all the required items are correctly serviced. Refer to the Approved Airplane Flight Manual Page 1

22 49-01 A Auxiliary Power Unit (Cessna designed and installed Auxiliary Power Unit and STC SA289NE Auxiliary Power Unit) - Inspect (refer to Hamilton Sundstrand Service Bulletin SB-T-62T for inspection requirements). NOTE: The intent of this item code is to refer to the Service Bulletin SB-T-62T and logbooks to determine if auxiliary power unit maintenance is required. If there is, perform maintenance, if not, no further action is required A Auxiliary Power Unit (STC SA755NE Auxiliary Power Unit only) - Inspect. (Refer to Honeywell Maintenance Manual GTCP36-150(W) for inspection requirements). NOTE: The intent of this item code is to refer to the Honeywell Auxiliary Power Unit Maintenance Manual and logbooks to determine if auxiliary power unit maintenance is required. If there is, perform maintenance, if not, no further action is required A Engine - Inspection. (Refer to TFE731 Engine Light Maintenance Manual Chapter 72 for inspection requirements). Note: the intent of this item code is to refer to the TFE-731 Light Maintenance Manual and logbooks to determine if engine maintenance is required. If there is, perform the required maintenance. If not, no further action is required A Radome Surface Mounted Lightning Diverter Strips - Inspect for missing segments, corrosion, damage and electrical continuity to airplane structure C Cabin Door Hinges (Airplanes thru without Stainless Steel Hinge Bolts and Bushings) - Lubricate with grease C Cabin Door Hinges (Airplanes and On and Airplanes thru with Stainless Steel Hinge Bolts and Bushings) - Lubricate with oil C Door Locks - Lubricate lock tumblers 211, 212, 323, 331, Page 2

23 30-07 A Windshield Alcohol Reservoir - Inspect for security of installation, cleanliness, cracks, dents, corrosion or evidence of damage. Check vent line for obstruction or damage D Windshield Alcohol Pump Filter - Inspect and clean A Crew Seat Tracks/Seat Attachments - Inspect for damage to seat track holes, seat track cracks and worn seat attachment hardware. (Refer to Expanded Inspection in ) D Airplanes thru -7000, Side Window Desiccant Systems - Check desiccant for need of servicing. Refer to Chapter 12, Window Servicing A Airplanes thru -7000, Windshield - Inspect windshield and side windows for scratches, cracks, delamination, discoloration and deformities. Check windshield alcohol assembly for deformities, damage and clearance from windshield A Fuselage Interior Cabin Structure - Inspect for corrosion (Refer to expanded inspection in ) A Environmental Control Unit - Check the environmental control unit for oil leakage and proper oil level A Vapor Cycle Cooling System - Check and record the hours on the unit hour meter. Check the components time limits C Entrance Door Lubrication - Lubricate the following items: latch handle and linkage lock pins and sockets counter balance spring and shaft bushings pulley bearings (Airplanes thru not incorporating SB internal spring push rods and folding step pivot point bolts and screws) B Autopilot and Yaw Damper (Airplanes with SPZ-650 Only) - Perform self test and lockout check B Horizontal Stabilizer Primary Trim Actuator Motor Brake Torque Check - Perform torque check on motor brake , , , , 242, 251, 252, 261, 262, 271, , AUX AUX Page 3

24 30-07 B Windshield Alcohol Pump - Perform operational test B Ram Air Temperature Transmitter Anti- Ice - Perform an operational check of the RAT transmitter heater AUX AUX B No Takeoff System - Operational check AUX B Angle-of-Attack/Stall Warning System (Teledyne) - Perform a warning system test B Standby Gyro - Perform an operational test B Cabin Door Warning System - Operational check cabin door warning system by opening and verifying enunciator illumination. Verify that no individual switches failed and are closed B Battery Disconnect and Battery Disable Switches - Perform operational check B Emergency Lighting System - Perform operational test *** End of Phase 1 Inspection Items *** AUX AUX AUX BAT BAT Page 4

25 INSPECTION PHASE 2 Date: Registration Number: Serial Number: Total Time: 1. Description A. Phase 2 consists of 150-hour and 300-hour or 24 calendar months, whichever occurs first, interval inspection items contained in the wings, landing gear and tailcone. Items from other areas are included to meet their required time interval. B. Inspection items are given in order of the zone in which the inspection is to be done. A descriptive statement of the inspection requirement and the Item Code Number for cross-reference to section are supplied. The applicable number is given for the convenience of operators that use the system. C. For items or components that require an applicable lubrication, refer to Chapter 12, Scheduled Servicing - Description and Operation, or to the appropriate for the correct lubricant, lubricating points and method. Refer to Chapter 6, Airplane Zoning - Description and Operation for airplane zone definition. D. Non users can refer to the Expanded Inspection section of this chapter for any detailed information about the inspections required in this phase, which are uniquely required by this chapter. E. The right portion of each page has room for the mechanic's and inspector's initials and remarks. These pages can be reproduced, and used as a checklist when this inspection phase is done. 2. General Inspection Criteria A. During accomplishment of each of the specific inspection tasks within this phase, additional general inspections of the adjacent areas are done, while access is available. These general inspections are to find obvious conditions that need further procedures. B. If a component or system is changed (because of completed maintenance procedures) after an initially required task is completed, then that specific task must be done again, before the system or component is returned to service. C. Complete a preflight inspection after this inspection phase is completed to make sure all the required items are correctly serviced. Refer to the Approved Airplane Flight Manual Page 1

26 49-01 A Auxiliary Power Unit (Cessna designed and installed Auxiliary Power Unit and STC SA289NE Auxiliary Power Unit) - Inspect (refer to Hamilton Sundstrand Service Bulletin SB-T-62T for inspection requirements). NOTE: The intent of this item code is to refer to the Service Bulletin SB-T-62T and logbooks to determine if auxiliary power unit maintenance is required. If there is, perform maintenance, if not, no further action is required A Auxiliary Power Unit (STC SA755NE Auxiliary Power Unit only) - Inspect. (Refer to Honeywell Maintenance Manual GTCP36-150(W) for inspection requirements). NOTE: The intent of this item code is to refer to the Honeywell Auxiliary Power Unit Maintenance Manual and logbooks to determine if auxiliary power unit maintenance is required. If there is, perform maintenance, if not, no further action is required A Engine - Inspection. (Refer to TFE731 Engine Light Maintenance Manual Chapter 72 for inspection requirements). Note: the intent of this item code is to refer to the TFE-731 Light Maintenance Manual and logbooks to determine if engine maintenance is required. If there is, perform the required maintenance. If not, no further action is required A Center Wing Wet (Carry-Thru) Areas - Inspect center wing tank external area lower surface for damage, fuel leaks, seeps and fuel stain. Check boost pump installation for leakage and seeps. Check moisture drains for operation and obstruction C Main Gear Trunnion Pins - Lubricate with LPS D Environmental Control Unit - Clean or replace, as required, the two coalescer cloths in the environmental control unit water separators. Inspect the water separators for security and damage 171, , , Page 2

27 78-02 A Left and Right Thrust Reverser Deploy Limit and Stow Limit Switches - Inspect limit switch for security of installation, adjustment and security of electrical connections C Lubrication of the Thrust Reverser Pivot Points (WC-393 Non-Aerosol Spray Lubrication Method). Refer to Chapter 78, Thrust Reverser - Maintenance Practices C Lubrication of the Thrust Reverser Guide Rods (D-5100NS Aerosol Spray Lubrication Method). Refer to Chapter 78, Thrust Reverser - Maintenance Practices A Starter-Generator - Inspect for security of installation. Inspect terminal block and electrical connections for cleanliness, evidence of heat or arcing and evidence of damage C Lubricate Speed brake/spoiler Control Bellcranks located at number 1, 2, 3, 4, 5, 6, 7 and 8 speed brakes/spoilers A Fuel Caps - Inspect lock mechanism ando-ringforsecurityanddamage 410, , , , , 622, 532, , C Fuel Caps - Lubricate lock tumblers 541, C Nose Gear Torque Link - Lubricate A Nose Gear Friction Brake - Inspect friction brake for damage, adjustment and safetying of the adjustment nuts. Checktorqueonfrictionbrake C Nose Gear Friction Brake Shoe Wick - Lubricate A Nose Gear Centering System - Inspect nose gear centering ramp, link, bearing andswitch for security of installation and damage A Nose Gear Wheels - Inspect for nicks, abrasions, cracks, and corrosion. Research logbooks to determine when the last tire change occurred on the wheel assembly installed on the airplane. NOTE: If tire change is required, refer to the wheel assembly manufacturer's maintenance manual for inspection requirements Page 3

28 32-13 C Nose Gear Wheel Bearings - Inspect for corrosion and evidence of damage. Repack lubricant A Nose Wheel Extended Switch and Nose Wheel Off Center Switch - Inspect switches for security of installation, evidence of damage and security of electrical connections A Nose Gear Steering Hydraulic Power Unit Wire Bundle - Inspect for wear and damage A Tires - Inspect for wear, sidewall cracks, cuts, injuries and proper inflation. NOTE: If tire change is required, refer to the wheel assembly manufacturer's maintenance manual for inspection requirements C Main Landing Gear Up Lock Rollers (located inboard of gear trunnion) - Clean and lubricate. Mark current position of strike plate, disassemble roller assembly, clean and lubricate bolt with LPS-3 spray lubricant (MIL-C ). Position and reassemble roller assembly A Main Gear Up Lock Switch Wire Bundles - Check for proper security and positioning. Verify that bundle position or security does not introduce stress or strain on the wires exiting the switch A Main Gear Wheels - Inspect for nicks, abrasions, cracks, and corrosion. Research logbooks to determine when the last tire change occurred on the wheel assembly installed on the airplane. NOTE: If tire change is required, refer to the wheel assembly manufacturer's maintenance manual for inspection requirements C Main Gear Wheel Bearings - Inspect for corrosion and evidence of damage. Repack lubricant , 720, , , , , Page 4