Skip to main content

Service Bulletin - AeroForce

CESSNA TURBO 210L · Service Bulletins

Free account — keep the POHs & checklists you reference in one place.

Overview

This Service Bulletin (SB) 039 issued by Kelly Aerospace Energy Systems addresses a critical issue affecting certain rebuilt turbocharger models. It mandates the inspection and potential replacement of turbocharger T-wheel assemblies that may lead to engine oil loss and loss of engine power. The bulletin specifically targets turbochargers manufactured between January 2007 and June 2009. Compliance with this bulletin is mandatory and should be performed at the next scheduled inspection, not exceeding ten hours of flight time. The document provides detailed instructions for identifying affected turbochargers, the procedure for replacement, and the necessary steps for returning the turbocharger to service. It is essential for maintenance personnel to follow the guidelines to ensure safety and compliance with FAA regulations.

  • Turbocharger T-wheel assemblies from January 2007 to June 2009 may be affected.
  • Mandatory compliance at the next inspection, not exceeding 10 hours of flight time.
  • Affected turbochargers must be removed and evaluated by KAES.
  • Operational tests are required after turbocharger reinstallation.
  • No KAES parts are needed for compliance, but incidental parts may be required.

Document

Source

Originally published by aeroforce.aero. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

Report a problem or request removal

Document details

Type
Service Bulletins
Year
2010
Pages
9
File size
119 KB
Publisher
aeroforce.aero
How rare is it?
539CESSNA TURBO 210L registered worldwide · 483 active

Common. One of the most common aircraft types we track.

Documentation completeness
7/7

Full essential library on file for the CESSNA TURBO 210L.

More CESSNA TURBO 210Lmanuals & documents

See all 37
Similar aircraft

If you fly the CESSNA TURBO 210L, you may also be researching these.

In this document

Introduction

The introduction outlines the reason for the service bulletin, highlighting the risk of turbocharger failure due to a processing condition in certain turbine wheel assemblies. It emphasizes the importance of removing and replacing affected parts to prevent engine power loss.

Compliance

Compliance with the service bulletin is mandatory and should be performed at the next scheduled inspection, not exceeding ten hours of flight time. It is recommended to limit flights to delivering the aircraft to a service facility if an affected turbocharger is in use.

Procedure

The procedure section details the steps for identifying affected turbochargers, including checking part and serial numbers against provided tables. It specifies that T-wheel replacements must be performed at the KAES factory and outlines the return process for repaired turbochargers.

Return to Service

This section describes the steps to take once the turbocharger has been reinstalled, including operational tests and ensuring no leaks are present before returning the aircraft to service.

Parts Required

No KAES parts are required to comply with this service bulletin, but incidental parts may be necessary for turbocharger installation.

Contact Information

For questions regarding the service bulletin, contact Kelly Aerospace Energy Systems Technical Support at 888-461-6077. Written communications should be directed to their Montgomery, AL address.

Safety notes

  • Continued operation of a suspect turbocharger may lead to total engine power loss without warning.
  • Only qualified personnel should perform the procedures outlined in this bulletin.

Full document text

REASON FOR REVISION: Correct Table I chart by adding P/N 406610-9028, Ref. Table page 6 correct. T TU UR RB BIIN NE E W WH HE EE EL L R RE EP PL LA AC CE EM ME EN NT T INTRODUCTION: Kelly Aerospace Energy Systems, LLC (KAES) has become aware of an in-house processing condition affecting some turbine wheel assemblies reclaimed for a number of rebuilt turbocharger models. This condition may result in an inoperable turbocharger and partial or total loss of engine oil. On both the 400 series (Garrett type) and 600 series (Rajay type) turbochargers , field inspection of the T-wheel for a suspect condition is not feasible. Turbochargers must be removed and evaluated using specialized equipment not generally available in most repair centers. Any Service spare T-wheel supplied by KAES will not apply to this service bulletin as we sell only new assemblies. Continued operation of the turbocharger with a suspect T-wheel, may result in a complete loss of turbocharger function without warning causing a partial or total loss of engine power. This Service Bulletin is being issued to mandate the removal and replacement of suspect T-Wheel assemblies as installed by KAES between January 2007 and June 2009 and as listed in the effectivity Table I below. New T-wheel assemblies used in any application on any model are not affected. COMPLIANCE: At the next scheduled inspection event not to exceed ten (10) hours time in service. The possibility of turbocharger failure without warning with partial or total loss of engine power exists, it is recommended that flights be limited to delivering the aircraft to a service facility. EFFECTIVITY: Any aircraft or engine utilizing a rebuilt KAES turbocharger manufactured between January 2007 and June 2009 as per the part number effectivity Table I below. (For basic identification guidance, see reference Table IV page 6 and 7.) * Part Number may have a CF prefix. If you have any questions concerning the instructions in this service bulletin, please contact Kelly Aerospace Energy Systems Technical Support at 888-461-6077. Questions concerning aircraft service or operation must be forwarded to the applicable manufacturer of that product. Rev A Kelly Aerospace Energy Systems Service Bulletin 039 Page 1 of 7 Service Bulletin Compliance is Considered Mandatory The technical content of this bulletin is FAA Approved Bulletin No. 039 A Issue Date: Feb. 10, 2010 406610-9005 406610-9015 406610-9018 406610-9019 406610-9020 406610-9021 406610-9025 406610-9026 406610-9028 406610-9029 406610-9030 406610-9032 407810-9001 406990-9004 408610-9001 409170-9001 409680-9011 465680-9001 465680-9004 465680-9005 465930-9002 465930-9003 465292-9002 465292-9004 465398-9002 407540-9003 466881-9001 466642-9001 466642-9002 466642-9005 466304-9003 600572-9000* 600573-9000* 600574-9001* 600575-9001* 600575-9002* 600576-9000* 600700-9001* 600803-9001* 600803-9002* TABLE I - Rebuilt Turbocharger Part Numbers Page 2 of 7 Kelly Aerospace Energy Systems Service Bulletin 039 Rev. A PROCEDURE: IDENTIFICATION: CAUTION:: This procedure must be performed by competent and qualified personnel familiar with engine and airframe maintenance activities that are specific to turbocharged aircraft. CAUTION:: Do not depend on this Service Bulletin for gaining access to the aircraft or engine. This will require that you use the applicable manufacturers maintenance manuals or service instructions. In addition, any preflight or inflight operational checks require use of the appropriate AFM or POH. TABLE II - Rebuilt Turbocharger T-Wheel Part Numbers * Part Number may have a CF prefix. 1. Access the aircraft turbochargers in accordance with the instructions in the aircraft maintenance manual. (Do not rely on the aircraft or engine paperwork alone to identify your turbocharger serial number.) 2. Refer to Table I on page one and determine if the turbocharger being inspected is an affected part number. If you have an affected turbocharger by part number, refer to the serial numbers on Table III on page 4 to see if your turbocharger needs further inspection. The part number and serial number will be found on the data plate. If the serial number does not appear, go to step 5 below. If it does appear continue with step 3. TURBOCHARGER (T-WHEEL) REPLACEMENT 3. If it has been determined that the T-Wheel is affected per Table II, the affected turbocharger(s) must be removed and the T-wheel replaced. Some aircraft installations may have two turbochargers, be sure you check both. T-Wheel Replacement can only be done at the KAES factory. Special arrangement request may be made in writing for international customers. All turbochargers will be returned as a REPAIRED component. Removal must be in accordance with the applicable aircraft and/or engine manufacturers maintenance manuals or service instructions. Do not return turbo with fittings, oil reservoir, or other engine or airframe parts as they cannot be returned. 4. Upon return of the repaired turbocharger check that the unit is received in undamaged condition with proper paperwork. Verify the turbocharger has the correct part number and serial number. If not, do not install on your aircraft, contact KAES product support. 5. Utilizing the applicable aircraft and/or engine manufacturers maintenance manuals or service instructions, re-install the turbocharger assembly and proceed to “Return to Service” below. 406304-9008 406304-9009 406787-9009 406787-9010 407276-9019 407293-9003 408493-9017 410188-9025 410188-9028 600366-9000* 600563-9000* RETURN TO SERVICE: 1. When the turbocharger has been re-installed, the aircraft is now ready for return to service. 2. Refer to Kelly Aerospace Energy Systems Service Bulletin 23 and perform the recommended turbocharger operational tests. This consists of turbocharger pre-lubrication, ground running tests, and

Show full text

and operational flight test. Make sure no air, exhaust, or oil leaks are present. Service Bulletin may be viewed or downloaded online via www.kellyaerospace.com. 4. Utilizing the applicable aircraft and engine manufacturers maintenance manuals, install any portion of the aircraft removed to gain access. 5. Upon successful completion of this service bulletin per the applicable compliance time listed on page 1, make an appropriate log book entry. PARTS REQUIRED: No KAES parts are required to comply with this service bulletin. Incidental parts may be required for the turbocharger installation. These parts must be obtained from the applicable engine or airframe manufacturer. PARTS IN INVENTORY: Affected KAES turbochargers in unused inventory may be returned for credit only. Replenishment stock must be re-ordered. Affected unused stock in customers hands must be returned thru place of purchase. WARRANTY STATEMENT: The sole warranty remedy applicable to this service publication is related to the terms and conditions stated in the Kelly Aerospace Energy Systems, LLC Limited Warranty Policy delivered with each new or rebuilt component. Labor allowance under KAES Limited Warranty Policy does not apply, any labor allowance is done as a special consideration outside warranty. Only units currently within warranty shall be offered Option 1 or 2 as reimbursement. IDENTIFICATION: KAES does not provide any labor allowance for Identification of an affected turbocharger. REPLACEMENT T-WHEEL: KAES will repair any turbocharger affected by this service bulletin provided the unit is returned undamaged with the appropriate form included in the shipping container. Reimbursement for labor expended will be one of two options: (customer choice) OPTION 1: KAES will offer the recommended OE removal and installation labor allowance for an affected turbocharger, of up to four (4) man hours at 55 USD not to exceed a total of 220 USD. No other charges apply. OPTION 2: KAES will pay no labor expenditures but offer instead a renewed Limited Warranty policy for each affected turbocharger. The renewed warranty shall be for eighteen (18) months from the date the repaired turbocharger is returned (based on shipping date). This is not an 18 month addition to standard warranty. Option 1 or 2 must be selected on the Attachment A Form and signed for, or Option 2 shall be applied. This publication does not imply or state any responsibility for the workmanship of any person or entity performing work or maintenance on the turbocharger, engine, or aircraft. All claims for the warranty repair “special consideration” must be forwarded to KAES Warranty Dept. except as noted above. SHIPPING INFORMATION: Turbocharger must be securely packed and packaged so no oil will seep into the shipping container. The form is “Attachment A” at the end of this service bulletin must be included inside the shipping container. The turbocharger must be received assembled and undamaged to qualify for repair. Use only the address on the form for return and mark “WARRANTY DEPT” clearly on the outside of the shipping container. (The return form may also be obtained from the KAES website at www.kellyaerospace.com.) KAES will only pay for return shipping by the same method as received. (next day, ground, etc.) Rev. A Kelly Aerospace Energy Systems Service Bulletin 039 Page 3 of 7 TABLE III - List of Affected Rebuilt Turbocharger Serial Numbers TABLE III - Continued next page Page 4 of 7 Kelly Aerospace Energy Systems Service Bulletin 039 Rev. A KAR00003 KAR00251 KDR01054 KER00159 KER00160 KER00161 KER00162 KER00163 KER00164 KER00166 KER00167 KER00168 KER00169 KER00170 KER00171 KER00172 KER00173 KER00174 KER00175 KER00176 KER00177 KER00178 KER00179 KER00180 KFO00267 KFO00268 KFR00003 KFR00004 KFR00005 KFR00006 KFR00007 KFR00008 KFR00009 KFR00010 KFR00011 KFR00012 KFR00013 KFR00014 KFR00015 KFR00016 KFR00017 KFR00018 KFR00019 KFR00020 KFR00021 KFR00022 KFR00072 KFR00073 KFR00074 KFR00075 KFR00076 KFR00077 KFR00078 KFR00079 KFR00080 KFR00081 KFR00083 KFR00084 KFR00085 KFR00087 KFR00088 KFR00089 KFR00090 KFR00091 KFR00092 KFR00093 KFR00096 KFR00101 KFR00102 KFR00139 KFR00140 KFR00141 KFR00142 KFR00143 KFR00144 KFR00145 KFR00146 KFR00147 KFR00148 KFR00149 KFO00266 KFR00188 KFR00189 KGR00165 KGR00166 KGR00184 KGR00185 KGR00186 KGR00189 KGR00190 KGR00191 KGR00192 KGR00193 KGR00194 KGR00195 KGR00196 KGR00197 KGR00198 KGR00199 KGR00200 KGR00201 KGR00202 KGR00204 KGR00205 KGR00206 KIO01201 KIO01202 KIO01203 KIO01204 KIO01205 KIO01206 KIR00792 KIR00793 KIR00794 KIR00795 KIR00796 KIR00797 KIR00798 KIR00799 KIR00800 KIR00801 KIR00802 KIR00803 KIR00804 KIR00805 KIR00806 KIR00807 KIR00808 KIR00809 KIR00810 KIR00811 KIR00812 KIR00813 KIR00814 KIR00815 KIR00816 KIR01070 KIR01071 KIR01072 KIR01073 KIR01074 KIR01075 KIR01076 KIR01077 KIR00822 KJR00211 KJR00212 KJR00214 KJR00215 KJR00216 KJR00217 KJR00463 KJR00464 KJR00465 KKR00151 KKR00152 KKR00153 KKR00154 KKR00155 KKR00156 KKR00157 KKR00158 KKR00159 KKR00160 KKR00161 KKR00162 KKR00163 KKR00164 KKR00165 KKR00166 KKR00167 KKR01212 KKR01213 KKR01214 KKR01215 KKR01216 KKR01960 KKR01961 KKR01962 KKR01963 KKR01964 KKR01965 KKO00122 KLR00177 KLR00272 KLR00273 KLR00274 KLR00275 KLR01104 KLR01105 KLR01106 KLR01107 KLR01108 KLR01109 KLR01110 KLR01111 KLR01112 KLR01113 KLR01114 KLR01115 KLR01116 KLR01117 LAR00008 LAR00009 LAR00047 LAR00048 LCR00241 LDR00245 LDR00246 LDR00247 LDR00248 LDR00249 LDR00250 LDR00251 LDR00252 LDR00253 LDR00254 LDR00255 LDR00256 LDR00259 LDR00276 LDR00315 LDR00316 LDR00317 LDR00318 LDR00319 LDR00321 LDR00322 LDR00323 LDR00335 LDR00336 LER00059 LFR00195 LFR00196 LFR00197 LFR00198 LFR00199 LFR00200 LFR00201 LFR00202 LFR00203 LFR00204 LFR00205 LFR00264 LGR00179 LGR00180 LGR00181 LGR00182 LGR00183 LGR00184 LGR00185 LGR00186 LGR00187 LGR00188 LGR00189 LGR00191 LGR00192 LGR00193 LGR00325 LGR00326 LGR00327 LGR00328 LGR00329 LGR00330 LHR00025 LHR00026 LHR00027 LHR00028 LHR00029 LHR00030 LHR00031 LHR00032 LHR00033 LHR00044 LHR00045 LHR00100 LHR00101 LHR00102 LHR00103 LHR00104 LHR00105 LHR00106 LHR00107 LHR00108 LHR00109 LHR00110 LHR00112 LHR00113 LHR00115 LHR00116 LHR00117 LHR00118 LHR00119 LHR00120 LHR00121 LHR00122 LHR00123 LHR00124 LHR00125 LHR00126 LJR00017 LJR00109 LJR00110 LJR00183 LJR00184 LJR00185 LJR00186 LJR00187 LJR00188 LJR00189 LJR00190 LJR00192 LJR00193 LJR00194 LJR00195 LJR00196 LJR00197 LKR00001 LKR00002 LKR00003 LKR00004 LKR00005 LLR00254 LLR00255 LLR00256 LLR00257 LLR00258 LLR00259 LLR00260 LLR00261 LLR00262 LLR00263 LLR00268 LLR00300 LLR00301 LLR00302 LLR00303 LLR00304 LLR00330 MAR00044 MAR00045 MAR00046 MAR00047 MAR00048 MAR00049 MAR00130 MAR00131 MAR00132 MAR00133 MAR00134 MAR00207 MAR00208 MAR00209 MBR00003 MBR00026 MBR00053 MBR00054 MBR00055 MBR00056 MBR00057 MBR00058 MBR00059 MBR00185 MBR00186 MBR00187 MBR00189 MBR00190 MBR00191 MBR00192 TABLE III - List of Affected Rebuilt Turbocharger Serial Numbers (cont’d) CONTACT INFORMATION: All comunications regarding this service bulletin, must be placed either through Kelly Aerospace Energy Systems Technical Support at 888-461-6077 or via Fax 334-386-5450. Written comunications must be placed through Kelly Aerospace Energy Systems Technical Support, 2900 Selma Highway, Montgomery, AL 36108, USA. Rev. A Kelly Aerospace Energy Systems Service Bulletin 039 Page 5 of 7 MCR00001 MCR00002 MCR00057 MCR00058 MCR00059 MCR00060 MCR00061 MCR00062 MCR00063 MCR00064 MCR00076 MCR00077 MCR00078 MCR00079 MCR00080 MDR00003 MDR00004 MDR00050 MDR00051 MDR00052 MDR00053 MDR00054 MDR00081 MDR00082 MDR00083 MDR00084 MDR00085 MDR00104 MDR00105 MDR00106 MDR00107 MDR00108 MDR00173 MIR00026 MJR00080T R1007055 TR1007056 TR1007057 TR1007058 TR1007059 TR1007060 TR1007061 TR1007062 TR1007063 TR1007064 TR1007065 TR1007066 TR1007067 TR1007068 TR1107001 TR0309013 TR0309014 TR0308008 TR0308009 TR0607012 TR0607013 TR0607014 TR0108013 TR0108014 TR0108015 TR0108016 TR0108017 TR0108018 TR0108019 TR0108020 TR0108021 TR0108022 TR0108023 TR0108025 TR0108027 TR0108028 TR0108029 TR0108030 TR0108031 TR0108032 TR0108033 TR0108034 TR0108035 TR0108036 TR0108037 TR0108038 TR0108039 TR0108040 TR0109026 TR0109027 TR0109028 TR0109029 TR0109032 TR0109033 TR0109034 TR0109035 TR0109036 TR0109037 TR0109038 TR0109039 TR0109040 TR0109041 TR0109042 TR0109043 TR0109044 TR0109045 TR0109046 TR0109047 TR0109048 TR0109049 TR0109050 TR0109051 TR0109052 TR0109053 TR0109054 TR0208212 TR0208213 TR0208214 TR0208215 TR0208216 TR0208217 TR0208218 TR0208219 TR0208220 TR0208221 TR0209014 TR0209016 TR0209017 TR0209018 TR0209019 TR0209020 TR0209021 TR0209022 TR0309015 TR0508002 TR0508007 TR0508008 TR0508009 TR0508010 TR0508011 TR0508012 TR0508013 TR0508014 TR0508015 TR0508017 TR0508020 TR0508021 TR0508033 TR0508034 TR0508035 TR0508036 TR0508037 TR0508038 TR0508039 TR0508040 TR0508041 TR0508042 TR0508045 TR0508046 TR0508047 TR0508048 TR0508049 TR0508050 TR0508051 TR0508052 TR0508053 TR0508054 TR0508055 TR0508056 TR0508057 TR0509017 TR0509018 TR0509019 TR0509020 TR0509021 TR0509023 TR0509024 TR0509025 TR0509026 TR0607002 TR0607003 TR0607004 TR0607005 TR0607006 TR0607007 TR0607008 TR0607009 TR0607010 TR0607011 TR0607021 TR0607022 TR0607023 TR0607024 TR0607025 TR0607026 TR0607027 TR0607028 TR0607029 TR0707001 TR0707002 TR0707003 TR0707004 TR0707005 TR0707006 TR0707007 TR0707008 TR0707009 TR0907080 TR0907081 TR0907082 TR0907083 TR0907084 TR0907085 TR0907086 TR0907087 TR0907088 TR0907089 TR0907090 TR0907091 TR0907092 TR0907093 TR0907094 TR0907095 TR0907096 TR0907097 TR0907098 TR0907099 TR0907123 TR0907124 TR0907125 TR0907126 TR0907130 TR0907131 TR0907132 TR0907133 TR0907134 TR0907135 TR0908007 TR0908008 TR0908009 TR0908010 TR0908011 TR0908012 TR0908013 TR0908014 TR0908023 TR1007007 TR1007008 TR1007009 TR1007010 TR1007011 TR1007012 TR1008019 TR1008020 TR1008021 TR1008022 TR1008023 TR1008024 TR1008025 TR1008026 TR1008027 TR1008028 TR1008029 TR1008030 TR1008031 TR1008032 TR1008033 TR1008034 TR1008035 TR1008036 TR1008037 TR1008038 TR1008039 TR1008040 TR1008041 TR1008042 TR1108017 TR1108018 TR1108019 TR1108020 TR1108021 TR1108022 TR1108023 TR1108024 TR1108025 TR1108026 TS0907031 TS0907032 TS0907033 TR0909011 TR0109055 TR0109057 TR0109056 TR0109055 TR0109055 TR0109056 TR0109057 TR0708005 TR0708006 TR0708007 TR0708008 TR0708009 TR0708010 TR0708011 TR0808001 TR0808002 TR0808003 TR0808004 TR0808005 TR0808006 TR0808007 TR0808008 TR0808009 TR0808010 TR0907203 TR0907204 TR0907205 TR0907206 TR0907207 TR0907208 TR0907209 TR0907215 TR0909011 TR0909012 TR1007029 TR1007030 TR1007031 TR1007032 TR1007033 TR1007034 TR1007035 TR1007036 TR1007037 TR1007038 TR1007054 Page 6 of 7 Kelly Aerospace Energy Systems Service Bulletin 039 Rev. A T-Wheel Ass’y Turbocharger Ass’y Engine Ass’y Aircraft (not limited to) 406304-9008 406610-9004 TSI0-520-D 406304-9008 406610-9005 TSIO-520-C, H, R TSIO-520-C, M TSIO-520-G, M Cessna T210F thru N T(P,U)-206A-F, TU-206G T-207, T-207A 406304-9008 406610-9015 TVO-435-D1A, -D1B,- E1A, - G1A, -F1A 47G3B1 D & E Eng., 47G3B2, 47G3B2A 406304-9008 406610-9019 TSIO-520-B, E 406304-9008 406610-9020 TIO-540-A1A, A1B, A2A, A2B, A2C, L/TIO-540-F2BD Piper PA31-310, PA31-325 406304-9008 406610-9021 TIO-540-C1A, E1A, G1A, H1A Piper PA23-250 406304-9008 406610-9025 TSIO-520-B, D, -BB, E, -EB Beech V35-STC, Cessna T310 P thru R Cessna 320 D thru F, 335, 401/402, 401A/402A,401B/402B, 406304-9008 406610-9026 TIO-540-S1AD Piper PA32R-301T, PA32-301T, PA32R-301, PA32RT-301, PA32RT-300T 406304-9008 406610-9028 TSIO-520-VB Cessna 402C 406304-9008 406610-9029 TSIO-520-UB Beech A,B36TC 406304-9008 406610-9030 TSIO-520-AE Cessna T303 406304-9008 406610-9032 TIO-540-AA1AD Lake 250 Renegade 406304-9009 406970-9001 TSIO360A, B, D (frt) Cessna T337A thru F, T337RG 406304-9009 406610-9018 TSIO360C (Frt) Cessna T337G, P337 406787-6009 407810-9001 TSIO520K Cessna 340 406787-6010 406990-9004 GTSIO-520-D Cessna 421/421A 406787-6010 408610-9001 GTSIO520H Cessna 421B 406787-6010 409170-9001 L/TIO-540-J2BD, TIO-540-J2B, TIO-540-N2BD Piper PA31-350 406787-6010 409680-9011 TSIO-520-L; TSIO-520-WB Beech 58P/58TC 406787-9010 465680-9004 TSIO-520-P, -AF Cessna P210N 406787-6010 465680-9005, TIO-540-V2AD, TIO-540-W2A Piper PA31P-350 406787-6010 465930-9002 GTSIO-520-M Cessna 404 406787-6010 465930-9003 GTSIO520L/N Cessna 421C 407276-6019 465292-9002 0540L3C5D Cessna T182, TR182 407276-6019 465292-9004 TSIO-520-T Cessna T188C 407276-6019 465398-9002 TO-360-E1A6D, LTO-360-E1A6D Piper PA44-180T 407293-9003 407540-9003 TIO-541-E1C4, E1D4 Beech A56TC, A60 408493-9017 466881-9001 TIO-540-AJ1A Cessna T206H TABLE IV - Affected T-Wheel Reference Table (list for basic reference only) NOTE:: The reference Table IV on page 6 and 7 should be used as a guide only for turbocharged aircraft. Not every aircraft or engine combination is listed and not every STC or other field application is included. This list is provided to help identify which aircraft may be affected by this service bulletin. Rev. A Kelly Aerospace Energy Systems Service Bulletin 039 Page 7 of 7 T-Wheel Ass’y Turbocharger Ass’y Engine Ass’y Aircraft (not limited to) 410188-9025 466304-9003 TSIO-520-BE, TSIO-550-B, E Malibu Conversion, Lancair IV & IVP 410188-9028 466642-9005 TIO-540-AE2A Piper PA46-350P 600563-9000* 600572-9000* TSIO-520-D, O-470-G-C1, IO-470-C, IO-470-J, IO-470-K, IO-470-N, IO-470-M, IO-540- B1A5, -E1A5, E1B5, O-470-A, J, K, L, R , O-470-E, S, D, O-540-E4C5, IO-540-C4B5, - C4C5, O-540-E4B5, IO-540-K1G5D, IO-540-G1E5, IO-540-K1E5, Bonanza series 33, 35, Commander 500A, B, U, S, Cessna 180, 182, 210, 210 A thru C, 205, 310 C thru G, Islander BN-2, BN-2A, BN- 2A-6, BN-2A-8, BN-2A-9, Piper PA23, PA23- 235, PA23-250,PA-24-250, PA-32-260, PA- 32R-300, Viking & Super Viking, 17-31TC Turbo, 600366-9000* 600573-9000* IO-720, O-360-A1A, -A1D, IO-360-A1D6D, A3D6D, O-360-A1A or, O-360-A1D, IO-360-A1B, TSIO-360, L/IO-320-B1A & C1A, L/IO-360-C1E6, TSIO-360, Commander 680 FP, L, FLP, Mooney M20A thru M20D, M20G, E, F, M20J, K, Lake LA-4 & LA-4A, LA-4-200, Piper PA-30 & PA-39, Seneca I PA-34-200, Seneca II PA-34-200T, Seneca III PA-34-220T, PA-28-200, PA-28 RT201T, 600563-9000* 600574-9001* TIO-540-S1AD Aerostar 601P 600563-9000* 600575-9001* TIO-540-S1AD Aerostar 601P (Later S/N’s) 600563-9000* 600575-9002* TIO-540-S1AD Aerostar 601P (Later S/N’s) 600366-9000* 600576-9000* IO-720, IO-540-G1E5, IO-470-N O-360-A1A, IO-360-B1A, B1B Commander 680 FP, L, FLP, Bonanza N35, P35, Travel Air, Piper PA23 Apache, Seneca I PA-34-200 600366-9000* 600700-9000* HIO-360-E1A, HIO-360-E1BD, -F1AD Enstrom Helicopter, F28C, F28F 600366-9000* 600803-9001* TIO-540-U2A, LTIO-540-U2A Aerostar 700P 600366-9000* 600803-9002* TIO-540-U2A, LTIO-540-U2A Aerostar 700P * Part Number may have a CF prefix. TABLE IV - Affected T-Wheel Reference Table (cont’d) SB 039 A Turbocharger Return Form Customer Info. Customer Name: Company Name: Shipped by: Address: Tracking no. City: State: E-Mail: Tel. No: Fax No: Country: Aircraft Info: Make: Model: Year: Total Time: “N” number: Engine Model: Total Time on Engine: Unit Info: Name: TURBOCHARGER Part Number: Hours in Service: Date Installed: Serial No: Date Removed: Reason for Claim: RETURNED FOR SB 039 REV A. TURBOCHARGER REPAIR. INSTRUCTIONS Complete ALL information on the form and return with FORM IN THE SHIPPING CONTAINER with the turbocharger. Select option 1 or 2 below. Detach label below and send to the address given using the label if appropriate. If an unused inventory unit is in stock it must be returned to the a KAES distributor. The distributor must fill out a standard warranty claim form to apply for warranty credit. Option 1 or 2 not applicable. IF ALL INFORMATION IS NOT PROVIDED OR THE FORM IS NOT IN THE BOX, THE REPAIR WILL NOT BE PROCESSED AND THE UNIT MAY BE RETURNED AT CUSTOMERS EXPENSE. OPTION 1: (Labor reimbursement) r Customer must sign & date: OPTION 2: (Warranty extension) r Customer must sign & date: (Place check in desired option, if not selected, Option 2 shall apply. Customer or representative must sign and date.) Return to: Warranty Department KELLY AEROSPACE ENERGY SYSTEMS, LLC 2900 Selma Highway Montgomery, AL 36108, USA From: (Your address info. below, include contact name & tel. number.) ATTACHMENT A - SB 039 RETURN SHIPPING LABEL - DETACH HERE SB 039 A Turbocharger Return Form Customer Info. Customer Name: Company Name: Shipped by: Address: Tracking no. City: State: E-Mail: Tel. No: Fax No: Country: Aircraft Info: Make: Model: Year: Total Time: “N” number: Engine Model: Total Time on Engine: Unit Info: Name: TURBOCHARGER Part Number: Hours in Service: Date Installed: Serial No: Date Removed: Reason for Claim: RETURNED FOR SB 039 REV A. TURBOCHARGER REPAIR. INSTRUCTIONS Complete ALL information on the form and return with FORM IN THE SHIPPING CONTAINER with the turbocharger. Select option 1 or 2 below. Detach label below and send to the address given using the label if appropriate. If an unused inventory unit is in stock it must be returned to the a KAES distributor. The distributor must fill out a standard warranty claim form to apply for warranty credit. Option 1 or 2 not applicable. IF ALL INFORMATION IS NOT PROVIDED OR THE FORM IS NOT IN THE BOX, THE REPAIR WILL NOT BE PROCESSED AND THE UNIT MAY BE RETURNED AT CUSTOMERS EXPENSE. OPTION 1: (Labor reimbursement) r Customer must sign & date: OPTION 2: (Warranty extension) r Customer must sign & date: (Place check in desired option, if not selected, Option 2 shall apply. Customer or representative must sign and date.) Return to: Warranty Department KELLY AEROSPACE ENERGY SYSTEMS, LLC 2900 Selma Highway Montgomery, AL 36108, USA From: (Your address info. below, include contact name & tel. number.) ATTACHMENT A - SB 039 Rev. A RETURN SHIPPING LABEL - DETACH HERE

Type certificate, explained

What's in the CESSNA TURBO 210L TCDS

A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.

TCDS 3A21Rev 47· Issued 2009
Read the full TCDS

240 CESSNA TURBO 210L parts for sale

See all →

Parts listed for sale by vetted eBay sellers — confirmed on eBay at checkout.