Contains Important Information Pertaining to Your Aircraft Engine Compliance Will Enhance Safety

Similar documents
CRITICAL SERVICE BULLETIN Compliance Necessary to Maintain Safety

WARNING OPERATION OF AN ENGINE WITH A RESTRICTED OIL PASSAGE CAN CAUSE LOSS OF LUBRICATION AND SUBSEQUENT ENGINE FAILURE.

SERVICE BULLETIN American Legend Aircraft Company considers compliance mandatory

CSB 665A TECHNICAL PORTIONS FAA APPROVED

SID SERVICE INFORMATION DIRECTIVE Compliance Will Enhance Safety, Maintenance or Economy of Operation TELEDYNE CONTINENTAL AIRCRAFT ENGINE

COMPLIANCE: As required by Kelly Aerospace Service Bulletin 033 (Attached)

SUBJECT: Kelly Aerospace Energy Systems Service Bulletin 038 A ES TCM P/N Inspection of Slip Ring End Housings for Cracks

TELEDYNE CONTINENTAL AIRCRAFT ENGINE MANDATORY service bulletin

MANDATORY SERVICE BULLETIN The Subject Matter of this Service Bulletin is Incorporated In Whole or in Part in an FAA Airworthiness Directive

MANDATORY SERVICE BULLETIN

MSB00-6C Technical Portions FAA Approved Supersedes MSB00-6, 6A, 6B

Table 1: Alternator Models ES (CMI ), ALX-9524 (CMI ), ALX-9524R, & ALV-9610 Affected Serial Numbers

CONTINENTAL AIRCRAFT ENGINE service bulletin

The Subject Matter Of This Service Bulletin Is Incorporated In Whole Or In Part In An FAA Issued Airworthiness Directive

SERVICE BULLETIN HC-SB Propeller - Counterweight Clamp Inspection

201F Fuel Pump Shaft Seal Leak

ISSUE DATE REVISION DATE PAGE NO REVISION

MANDATORY SERVICE BULLETIN The Subject Matter Of This Service Bulletin Is Incorporated In Whole Or In Part In An FAA Issued Airworthiness Directive

201F Fuel Pump Valve Assembly Leakage

Alert Service Bulletin

SERVICE BULLETIN CATEGORY 3 SB00-2B CONTINENTAL MOTORS AIRCRAFT ENGINE. IO-346 Replacement Cylinder Assembly Kit

1154B. Piper Aircraft, Inc Piper Drive Vero Beach, Florida, U.S.A Date: March 28, 2007 (S)

To announce the issuance of Piper Service Bulletin 1157A

FJ44 SERVICE BULLETIN

SERVICE BULLETIN REVISION TRANSMITTAL

P.O. Box 3149 Albany, GA Phone (229) Fax (229) March 7, 2006 FLAP CONTROL TORQUE SHAFT REPLACEMENT

SERVICE BULLETIN. EFFECTIVITY SERIAL NUMBERS 680 (Citation Sovereign) thru (Citation Sovereign+) thru -0549

ENGINE, COMBUSTION ASSEMBLY - INSPECTION OF OUTER COMBUSTION CASE P/N M

SERVICE BULLETIN. Citation CIB TITLE FUEL - FIREWALL SHUTOFF VALVE GROUND IMPROVEMENT

HARTZELL PROPELLER INC. SERVICE BULLETIN TRANSMITTAL SHEET SERVICE BULLETIN HC-SB Propeller - Propeller Installation.

STARTER ADAPTER SHAFTGEAR AND CRANKSHAFT GEAR INSPECTION

SERVICE LETTER. Multi-engine TITLE NACELLES/PYLONS - NACELLE FITTING INSPECTION EFFECTIVITY

Instructions for Continued Airworthiness

PURPOSE: Notification and support of the Mandatory Inspections Called for in SB3-08A

Service Bulletin. SB-GA Issue 1. Subject: Horizontal Stabiliser Attachment Area Inspection and Reinforcement. Applicability: Amendments:

HARTZELL PROPELLER INC. SERVICE BULLETIN TRANSMITTAL SHEET HC-SB Propeller - Blade, Blade Retention Bearing, and Hub Inspection.

REASON FOR REVISION: To clarify effectivity by including RAM P/N cross reference. INTRODUCTION:

SERVICE BULLETIN. To prevent the wing fuel boost pump wiring from chafing on the wing structure and/or fuel tube assemblies.

1139A. The New Piper Aircraft, Inc Piper Drive Vero Beach, Florida, U.S.A Date: April 9, 2004 (S)(M)

SUBJECT: Volare Carburetors, LLC SB4 Service Bulletin, Carburetor Bowl to Float Clearance

MODIFICATION KIT. Serial Numbers 300 (LC40-550FG) thru (LC42-550FG) thru (LC41-550FG) thru

MANDATORY SERVICE BULLETIN NO. MSB40-046/3 NO. MSBD4-046/3

SERVICE LETTER REVISION TRANSMITTAL

SERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN

SUBJECT: Volare Carburetors, LLC SB2 Service Bulletin, Required Replacement of Foam and Hollow Floats

BULLETIN. Piper Aircraft, Inc Piper Drive Vero Beach, FL, U.S.A Date: October 29, 2015 (S) (M)

SERVICE BULLETIN No.: S , Rev. 0 Date: January 3, 2008

aileron rib inspection

TIME OF COMPLIANCE: At owner s discretion or when part replacement is necessary.

SERVICE BULLETIN. The equivalent of this service bulletin has been incorporated on production airplanes and On.

SERVICE BULLETIN. COMPLIANCE MANDATORY. This service bulletin must be accomplished at the next 100-hour or 12-month (annual-type) inspection.

OPTIONAL SERVICE BULLETIN OSB

SERVICE LETTER. SERIAL NUMBERS 210 & T thru P thru P

R1 Raytheon Aircraft Company: Amendment ; Docket No. FAA ; Directorate Identifier 2006-CE-33-AD.

SERVICE BULLETIN REVISION TRANSMITTAL

Superior Air Parts, Inc. Engines: Vantage Engine O-360-A XP360 Engine (Experimental) O-360-A, B IO-360-A,B

MANDATORY SERVICE BULLETIN

SERVICE BULLETIN. This service bulletin provides parts and instructions to install fuel caps that have a locking feature.

Service Information Letter

RECOMMENDED SERVICE BULLETIN NO. RSB /2

IOF-240-B4B ENGINE CONVERSION. All IOF-240-B4B Engines

SERVICE BULLETIN MANDATORY. SB , Rev Planning Information

SERVICE BULLETIN REVISION

SERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN

Service Bulletin No.: DAC Rev 0 Date Issued: 27 July 2018 Title: Installation of Diamond Flap Module and Microswitch Tray

Service Information Letter

Service Bulletin. Service Bulletin No. 064 Alternator Model ALV-9610 Series Through Bolt Inspection for Proper Torque

201F Fuel Pump Valve Housing Cap Screw Replacement

Airworthiness Directive Schedule

Airworthiness Directive Schedule

SERVICE BULLETIN. No. SB-AG-49 August 1, 2008 SEAT SUPPORT BRACKET INSPECTION AND REPAIR

The parts that follow are available from Cessna Parts Distribution through an appropriate Cessna Service Station.

ISSUE DATE REVISION DATE PAGE NO REVISION

SNS SUBJECT: NOSE GEAR - Nose Landing Gear Assembly Inspection and Reinforcement

AVIAT AIRCRAFT INC. P.O. Box South Washington Afton, WY USA Fax:

ATTACHMENT. Orders for the required parts listed below must be placed by using this form only. Service Station/Company Code: Company Name:

MANDATORY SERVICE BULLETIN NO. MSB

This Service Bulletin is applicable only to airplanes equipped with placards that are written in English.

Printed from Summit Aviation's Computerized Aviation Reference Library, 4/26/2000 Page 1

SERVICE LETTER TITLE EXHAUST - TRANSMITTAL OF LYCOMING SERVICE BULLETIN NO 627C, EXHAUST SYSTEM INSPECTION SERIAL NUMBERS

SERVICE LETTER REVISION TRANSMITTAL

PA Archer 28-E13; thru PA Archer II thru ; ; ; thru

SERVICE BULLETIN REVISION

SERVICE BULLETIN. To prevent the wing fuel boost pump wiring from chafing on the wing structure and/or fuel tube assemblies.

SUBJECT: Single Engine Service Bulletin SB Revision 1: Cosmetic Window Repair

Ayres service bulletin Corporation

ULTRALIGHT AIRCRAFT AIRWORTHINESS NOTICE

SERVICE BULLETIN FUEL - MODIFICATION OF THE ENGINE DRIVEN FUEL PUMP SYSTEM

SERVICE LETTER. COMPLIANCE DISCRETIONARY. This service letter should be accomplished at a scheduled Check 1, Check 2, or HSI. LABOR HOURS KEY WORD

SERVICE BULLETIN CERTIFICATION REQUIREMENTS - FOREIGN CERTIFICATION PLACARD INSTALLATION

SERVICE INSTRUCTION OIL LEAKAGES IN THE AREA OF THE CYLINDER BARREL FOR ROTAX. SI-912 i-006 R1 SI R3 SI R3

SERVICE INSTRUCTION. ISSUED REVISED PAGE NO. REVISION MO DAY YEAR MO DAY YEAR 1 of 8 BB

SERVICE BULLETIN. No. SB-AG-54 Revision IR; 6/6/2011 S2R-T660 ELEVATOR PUSH-PULL TUBE END FITTING INSPECTION

HARTZELL PROPELLER INC.

MANDATORY SERVICE BULLETIN

SERVICE BULLETIN MANDATORY

SERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN

SB663A Technical Portions FAA Approved

Revision Transmittal Sheet

READ THIS BEFORE INSTALLING AIR/OIL SEPARATOR DATA PERTINENT TO ALL INSTALLATIONS

Transcription:

CONTINENTAL MOTORS AIRCRAFT ENGINE SERVICE ULLETIN Contains Important Information Pertaining to Your Aircraft Engine Compliance Will Enhance Safety Category 3 S09-4 Supersedes S09-4A TECHNICAL PORTIONS FAA APPROVED SUJECT: Crankcase inspection for Permold engines equipped with Air Conditioner systems installed from 1998 to present. PURPOSE: To issue instructions for a required crankcase inspection at the forward Air Conditioner bracket attachment boss. To require replacement of the Air Conditioner bracket on all affected models listed below COMPLIANCE: At next maintenance event, no later than the next 100-hour or Annual inspection MODELS AFFECTED: IO520-A, IO550-, G, P, R TSIO520-E, L, L, U, W TSIO550-A,, C, E, G ACKGROUND All affected engines equipped with Continental Motors (CM) upper rear mounted, factory air conditioning bracket and Thinner Rib crankcase (see page 5) Continental Motors (CM) has confirmed reports of cracks in a rib of some Permold crankcases that are equipped with CM supplied air conditioning compressor brackets. The rib extends from the 11:00 o clock position of the number 1 cylinder to the forward air conditioner compressor bracket attachment boss. (See Figures 5 and 6) There are two crankcase rib configurations, a thinner rib and a thicker rib. These two rib configurations are shown in Figures 5 and 6. The cracks occur in the thinner rib crankcases near the forward air conditioner compressor bracket attach bolt point. Figure 3 exhibits a crack indication in a thinner rib crankcase. This service bulletin requires inspection of the thinner rib configuration for cracks and replacement of the air conditioning compressor bracket on all thinner rib crankcases. The CM supplied brackets are part of an EQ (equipment) kit that includes all parts to enable installation of an air conditioning compressor system by aircraft OEMs and other installers. See Figure 1 for a typical installation on an IO550 model engine. The cracks in the thinner rib are in the Non-critical area of the crankcase as identified in Figure 4 of this bulletin and prior in the latest revision of M-0, Standard Practice Maintenance Manual. Figure 4 shows an illustration of the areas designated as critical and non-critical. MO DAY YEAR MO DAY YEAR 1 of 7 P.O. ox 90 Mobile Alabama 36601 251-436-8299 S09-4 2016 Continental Motors, Inc.

FIGURE 1 Compressor Installation Right Magneto Right Magneto Forward FIGURE 2 FIGURE 3 General Area Compressor bracket attachment bolt boss crack indication MO DAY YEAR MO DAY YEAR 2 of 8 P.O. ox 90 Mobile Alabama 36601 251-436-8299 S09-4

FIGURE 4 Crankcase 1-3-5 half Critical area depicted in white. Non-critical area depicted in shaded area. Forward A/C bracket attach point FIGURE 5 FIGURE 6 Thinner Rib Thicker Rib (Approximate thickness 3/8 ) (Approximate thickness 3/4 ) CRANKCASE INSPECTION Thicker rib crankcases as pictured in Figure 6 require NO INSPECTION. No inspection is required on the thicker rib crankcases. Make a log book entry that this Service ulletin is Not Applicable by crankcase rib thickness. No further action is required on these thicker rib crankcase engines. All thinner rib crankcases, as pictured in Figure 5 MUST E INSPECTED. Recurring inspection is required each 50-hours of operation until the air conditioner bracket is replaced with the superseding bracket as listed on Page 6. Replacement with the superseding air conditioner bracket will remove the inspection requirements of this Service ulletin. MO DAY YEAR MO DAY YEAR 3 of 8 P.O. ox 90 Mobile Alabama 36601 251-436-8299 S09-4

Visual Inspection Criteria Inspection may normally be completed without removal of the air conditioning bracket or right magneto. Clean the pictured area (Figure 5) to remove any debris utilizing Stoddard solvent or mineral spirits. Utilizing an adequate light source and 10X magnification device, visually inspect the outside of the forward A/C bracket attach point boss as shown in Figure 5. Inspect the rib at the front air conditioner bracket attach point of bracket up to the Right Magneto flange attachment opening and magneto lower attachment clamp (See Figures 2 & 3). If any crack indication is found or if question of crack exists, proceed to the following Dye-penetrant inspection to assist in measurement of crack. If no crack is found, make a log book entry to include the inspection date, engine total time, results of inspection and the next 50-hour recurring inspection time. When the air conditioner bracket is replaced by the superseding bracket, make a logbook entry to include the replacement date, engine total time, results of inspection and compliance with Service ulletin S09-4. 2. Dye-penetrant inspection NOTE: Dye-penetrant inspection must be performed by a properly qualified mechanic in accordance with the dye-penetrant manufacturer s instructions. Use Magnaflux Portable Spotcheck Kit or equivalent. These kits can be purchased through many aviation industry distributors. Inspection may normally be completed without removal of air conditioner bracket or right magneto as shown in Figure 7. Using Dye-penetrant Cleaner/Remover, thoroughly clean the area between the A/C bracket base and Magneto as shown in Figure 5. Spray the Penetrant/Dye onto the clean/dry area as illustrated in Figure 7. Allow the Penetrant/Dye enough time to set in accordance with the manufacturer s instructions. Remove the excess Penetrant Dye and clean the area where the Penetrant/Dye was applied in accordance with the manufacturer s instructions. Spray the Developer onto the clean/dry area as illustrated in Figure 7. Allow the Developer enough time to dwell for the determination of the existence of a crack, in accordance with the manufacturer s instructions. If a crack is present, its appearance and location will be similar to that shown in Figure 3 and Figure 7. See following criteria for cracks to determine what specific further action is required Report any crack located to CM Customer support (see page 6) MO DAY YEAR MO DAY YEAR 4 of 8 P.O. ox 90 Mobile Alabama 36601 251-436-8299 S09-4

Crack inspection criteria Critical (white) and Non-critical (shaded) areas are illustrated in Figure 4. If a crack is observed in the non-critical (shaded) areas less than two (2) inches in length, it should be re-inspected for crack progression and signs of oil leakage at the next 50-hours of operation. If no crack progression is observed and no additional cracks are evident, continue to re-inspect at regular intervals not to exceed 100-hours duration or at Annual inspection. If a crack is observed in any of the non-critical (shaded) areas more than two (2) inches in length or if a previously observed crack has progressed to two (2) or more inches in length, remove the engine and repair or replace the crankcase or prior to further flight. If any crack is observed in a critical (white) area, remove the engine and repair or replace the crankcase or prior to further flight. SUMMARY - Reasons for Crankcase Repair or Replacement A. Any crack in the critical (White) area.. Any crack two (2) inches or more in length in the non-critical (shaded) area. C. Any size crack that is leaking oil (not seeping). Make an appropriate log book entry indicating compliance with this bulletin. Include engine total time in service, method of compliance (visual, dye-penetrant, other) appearance of crack, time for recurring inspection and date completed. FIGURE 7 Example of Dye-penetrant inspection area MO DAY YEAR MO DAY YEAR 5 of 8 P.O. ox 90 Mobile Alabama 36601 251-436-8299 S09-4

Air Conditioner racket Replacement CM has superseded the Air Conditioner bracket for all affected engine models. All brackets installed on Thinner Rib crankcases must be replaced with the superseding number. The superseding bracket, required hardware and installation instructions are included in a new EQ installation kit for ease of procurement The new air conditioning bracket replacement kit is Part Number *EQ7530 and includes the following material: 1 ea 657627 racket, Freon Compressor 1 ea 657629 Spacer, 1.00 O.D.X.375 Long 2 ea MS90728-65 Screw-Hex.38 X 1.75 Long 2 ea 24239 Washer-.375 Plain 5 ea 643956-20 Shim Idler Sheave to Spacer (rear) 5 ea 646064-20 Shim Driver Sheave to Spacer 1 ea 657653 Instruction Drawing- Freon Comp racket WARRANTY *EQ7530 kits may be ordered through any CM distributor All engines that are within published Teledyne Continental Motors Warranty coverage by type of engine, should contact CM Customer Support at 1-888-826-5465 for any questions or concerns on this issue. Warranty coverage examples: HC three years or 1000 operating hours from date of initial delivery; CM Factory New one year parts and labor warranty, two additional years, parts only or 1000 operating hours; CM Factory Rebuilt, one year parts and labor or 500 operating hours; Platinum Engines two years parts and labor warranty, three additional years parts only to published TO. The following labor will be allowed for all engines within warranty coverage, as above; Inspection of crankcase: 1.0 hour Additional time allowed if magneto must be removed to confirm crankcase condition: 1.5 hours Replacement of Air Conditioner racket: 4.0 hours Warranty coverage for compliance with this bulletin will be accepted only through June 1, 2010 for all claims filed in accordance with the warranty criteria above. No claims of warranty compensation for work accomplished on engines beyond the coverage criteria outlined above will be considered. MO DAY YEAR MO DAY YEAR 6 of 8 P.O. ox 90 Mobile Alabama 36601 251-436-8299 S09-4

Contact Continental Motors Technical Services at one of the numbers listed below if you have any questions concerning the technical content of this Service Document. 1.888.826.5465 toll free in United States +1.251.436.8299 international callers +1.305.964.0872 en Español CM Customer Support may be reached via email at www.continentalmotors.aero. Please have engine serial number, date of installation or date placed in service, aircraft serial and registration number ready at the time of call to customer service. MO DAY YEAR MO DAY YEAR 7 of 8 P.O. ox 90 Mobile Alabama 36601 251-436-8299 S09-4

Intentionally Left lank MO DAY YEAR MO DAY YEAR 8 of 8 P.O. ox 90 Mobile Alabama 36601 251-436-8299 S09-4