INSTALLATION MANUAL FOR NOSE WHEEL CONVERSION KIT 199-126 FOR BEECH MODELS 65, 90, 99, 100, 200, AND 300

22..22 After final certification, substitution of critical parts or changes of processes or materials are not permitted without requalification of the assemblies and resubmittal of the test data to the FAA for approval. 22..33 FAA regulations subject both Parker Hannifin, Aircraft Wheel and Brake Division and the user to constant surveillance to assure that uncompromising Quality Assurance material and processing controls are maintained in order to provide replacement parts that are the same as the parts originally certified in the assembly. 33.. A AP PP PLLIIC CA AB BIILLIITTY Y.. 33..11 "KIT 199-126": MAKE MODELS Beech 300, B300, B300C Beech 200, 200C, 200CT, 200T, B200 Beech B200C, B200CT, B200T, B200GT, B200CGT Beech 100, A100, B100 Beech 99, A99, A99A, B99, C99 Beech 65-90, 65-A90, B90, C90, C90A, C90GT, C90GTi, E90, F90, H90 Beech 70, 65, A65, 65-80, 65-A80 Beech 65-B80, 65-88 44.. O OR RD DE ER R IIN NFFO OR RM MA ATTIIO ON N.. 44..11 To order spare parts, contact the nearest Parker Hannifin, Aircraft Wheel & Brake distributor in your area. 55 D DE ES SC CR RIIP PTTIIO ON N.. 55..11 The wheel is forged aluminum and conforms to all Tire and Rim Association Standards for a 22 x 6.75- 10 and a 6.50-10 divided type wheel. The wheel is a tubeless/tube-type and incorporates an O-ring seal. Rubber lip seals on both wheel halves protect the bearings. It is composed of the following parts listed on page 9. INSTALLATION INSTRUCTIONS Cleveland Nose Wheel Assembly Conversion Kit 199-126 Page 2 Jan. 1984, Rev. A 4-30-84 Rev. G 01-21-10 66.. IIN NS STTA ALLLLA ATTIIO ON N.. 66..11 Jack aircraft in accordance with Beech Service Manual and remove the old wheel and retain the original axle nut, washer and spacer. 66..22 The wheel assembly Item #1 is shipped from the factory completely assembled. The bearings are packed with Mobil Aviation Grease SHC-100 and may be installed as received. -- N NO OTTE E -- EXTENDED STORAGE OF LUBRICATED BEARINGS MAY REQUIRE RELUBRICATION. 66..33 Remove snap rings Item #14, grease seals Item #5 and bearing cones Item #8 from the wheel assembly Item #1 and place on a clean surface to avoid contamination. 66..44 Remove nuts Item #12, washers Item #11, washers Item #10 and tie bolts Item #9 to separate wheel halves. 66..55 Position inner wheel half Item #3 on a flat surface with register side up. 66..66 Place O-ring Item #17 on register portion of wheel half. --C CA AU UTTIIO ON N-- SEAL SHOULD NOT BE TWISTED, BUT FULLY ALIGNED IN GROOVE. 66..77 Place serviceable tire over inner wheel half item #3 and then place outer wheel half Item #7 in tire, making sure to properly align inner and outer registers. Slide tie bolts Item #9 and washers Item #10 thru wheel assembly. --C CA AU UTTIIO ON N-- COUNTER-SUNK SIDE OF WASHER ITEM #10 SHOULD BE TOWARD THE BOLT HEAD. 66..88 Install washers Item #11, and nuts Item #12 on tie bolts Item #9 and torque to 300 in-lbs. When all nuts have been torqued, retorque a second time to make sure that the required value has been achieved. Sometimes O-Ring compression will give false initial readings. 66..99 Inflate tire to proper pressure in a safety cage. 66..1100 Reinstall bearing cone Item #8 into inner wheel half Item #3 and install inner grease seal Item #5 using a snap ring Item #14. 66..1111 Check for burrs or rough threads on axle nut. 66..1122 Mount wheel and tire assembly on axle. INSTALLATION INSTRUCTIONS Cleveland Nose Wheel Assembly Conversion Kit 199-126 Page 3 Jan. 1984, Rev. A 4-30-84 Rev. B 3-18-85 Rev. G 01-21-10 66..1133 Apply a thin coat of bearing grease Mobil Aviation Grease SHC-100 on axle nut threads. Install outer bearing cone Item #8 and grease seal Item #5 and snap ring Item #14, and apply a layer of bearing grease on threads of the axle. Install original spacer, washer and axle nut. 66..1144 Tighten axle nut to 150 to 200 in-lbs of torque while rotating the wheel. Back off the axle nut to zero torque then retorque to 40 in-lbs while rotating the tire. If holes do not align with axle nut, continue tightening to first locking hole and secure by prescribed methods. --N NO OTTE E-- AXLE NUT TORQUE TO BE 40 IN-LB MINIMUM OF TORQUE. 77.. W WE EIIG GH HTT A AN ND D B BA ALLA AN NC CE E C CO OM MP PU UTTA ATTIIO ON NS S: Weight: 11.2 lbs. Complete Form 337 and make appropriate log book entries. 88..00 FFLLIIG GH HTT M MA AN NU UA ALL IIN NS SE ER RTTS S: (located in front cover pocket) 88..11 Attach label "Item installed in airplane" in flight manual as close to the original item nose wheel assembly. Enter the correct arm and moment in block provided. Zero items out for the original nose wheel assembly which was removed. 99..00 W WA AR RR RA AN NTTY Y R RE EG GIIS STTR RA ATTIIO ON NS S. 99..11 Completely fill out enclosed warranty card and return promptly. Postage is prepaid. INSTALLATION INSTRUCTIONS Cleveland Nose Wheel Assembly Conversion Kit 199-126 Page 4 Jan. 1984, Rev. A 4-30-84 1100.. M MA AIIN NTTE EN NA AN NC CE E 1100..11 Inspect wheel half flanges for cracks and corrosion. 1100..22 Check for loose bolts and nuts and retighten or replace if necessary. --N NO OTTE E-- No repair or replacement is recommended while equipment is on aircraft. 1111.. O OV VE ER RH HA AU ULL 1111..11 D Diissm moouunnttiinngg 1111..11..11 Deflate tire. Remove valve stem to assure complete deflation. Remove axle nut, tang washer, spacer and bearing cone Item #8. Remove wheel and tire assembly from axle as a unit. Remove snap rings Item #14, grease seals Item #5 and bearing cones Item #8 from both wheel halves Item #3, and Item #7. 1111..11..22 Break tire beads away from wheel flange with a bead breaker or pneumatic tire dismounter. --C CA AU UTTIIO ON N-- DO NOT USE TIRE IRONS. THEY MAY DAMAGE THE WHEEL FLANGES OR TIRE BEADS AND PREVENT PROPER AIR RETENTION. --N NO OTTE E-- A soap solution around the bead seat will usually help in breaking the bead 1111..11..33 Remove eight (8) nuts Item #12, washers Item #11, washers Item #10, and bolts Item #9 from the wheel assembly. 1111..11..44 Separate the wheel halves and remove the tire --N NO OTTE E-- Bearing cups Item #4 are shrunk fit into the wheel halves and should not be removed unless replacement is necessary. If a bearing cup Item #4 is to be replaced, heat the wheel half to 149 degrees C (300 degrees F) maximum for 20 minutes before trying to remove the cup. Support the wheel hub while removing the bearing cup as shown in Figure #1. INSTALLATION INSTRUCTIONS Cleveland Nose Wheel Assembly Conversion Kit 199-126 Page 5 Jan. 1984, Figure 1 Supporting Wheel Hub 1111..22 C Clleeaanniinngg 1111..22..11 Clean all metal parts in a suitable solvent and dry with a lint free cloth. 1111..22..22 Wipe bearing grease seal clean with dry cloth. Do not use cleaning solvents on rubber components used in this wheel assembly. 1111..22..33 Wash bearing cones in uncontaminated cleaning solution, rotate the bearing cones by hand while submerged in the solution. Repack bearings with grease immediately after inspection to prevent corrosion and place in a clean, closed container. --C CA AU UTTIIO ON N-- DO NOT SPIN DRY BEARINGS OR HANDLE BEARINGS WITH BARE HANDS. 1111..22..44 Parts requiring fluorescent inspection are to be completely stripped using acetone or equivalent. Air dry parts after stripping is completed. INSTALLATION INSTRUCTIONS Cleveland Nose Wheel Assembly Conversion Kit 199-126 Page 6 Jan. 1984, Rev. C 6-17-94 1111..33 IInnssppeeccttiioonn --N NO OTTE E-- Inspect bolts Item #9 and wheel halves Item #3 and Item #7 after the fifth tire change, and then after the third subsequent tire change, for a total of twenty tire changes, and then at each and every tire change thereafter. 1111..33..11 Magnaflux bolts Item #9 for cracks and breaks. 1111..33..22 With dye penetrant inspect wheel halves Item #3 and Item #7 for cracks and breaks. Note in particular the bead seat, tubewell, and webbed junction areas. 1111..33..33 Visually inspect all metal parts for pitting, corrosion, cracks, breaks, uneven wear, and other surface defects. 1111..44 R Reeppaaiirr aanndd R Reeppllaacceem meenntt 1111..44..11 Repair scratches, nicks, corrosion, and other surface blemishes on wheel halves Item #3 and Item #7 by sanding with emery cloth, removing as little material as possible. Polish repaired surfaces with 400 grit emery cloth. Swab exposed aluminum areas with Iridite 14 or Alodine 1200 per MIL-C-5541. 1111..44..22 Paint repaired areas with one coat of Sherwin-Williams specification E61 G 510 primer followed by one coat of Sherwin-Williams specification F63 W 66, topcoat. (Contact Sherwin-Williams at (216) 271-6766 for detailed paint information). --C CA AU UTTIIO ON N-- NEVER PAINT WORKING SURFACES OF BEARING CUPS. --N NO OTTE E-- Use only one coat of primer and no finish coat on O-ring grooves and mating surfaces of wheel halves. 1111..44..33 Replace all parts worn or damaged beyond limits of repair. 1111..44..44 Replace O-rings Item #17 at each overhaul. 1111..44..55 Clean reworked areas with solvent and/or emery cloth. 1111..44..66 Surface treat bare aluminum with Alodine 1200 or Iridite 14. 1111..44..77 Paint reworked areas with a minimum of two coats of zinc-chromate primer (MIL-P-8585). 1111..44..88 To replace bearing cups, proceed as follows: 1111..44..88..11 Heat wheel halves to 149o C (300o F.) maximum and cool cups to -18o C. (0o F). INSTALLATION INSTRUCTIONS Cleveland Nose Wheel Assembly Conversion Kit 199-126 Page 7 Jan. 1984, Rev. A 4-30-84 Rev. G 01-21-10 1111..44..88..22 Support wheel hub and paint the ID of the hub with zinc chromate primer. Then press cup into wheel half as in Figure 2. Figure 2, Supporting Wheel Hub --N NO OTTE E-- The wet zinc chromate primer lubricates the parts to be pressed together and acts as protection against galvanic corrosion between the parts. 1111..55 LLuubbrriiccaattiioonn 1111..55..11 Pack Mobil Aviation Grease SHC-100 into bearing cones and smear grease on ends of rollers. Do not over lubricate. Spread a thin coat of grease on the surface of the bearing cups. 1111..55..22 Lubricate threads of bolts and nuts and face of washers with thread compound. 1111..55..33 Apply a thin layer of bearing grease to grease seal Item #5 before installing in wheel. INSTALLATION INSTRUCTIONS Cleveland Nose Wheel Assembly Conversion Kit 199-126 Page 8 Jan. 1984, Rev. A 4-30-84 1111..66 R Reeaasssseem mbbllyy 1111..66..11 Prior to wheel assembling, coat O-Ring Item #17 liberally with Dow Corning Molykote 55M, or equivalent. 1111..66..22 Position inner wheel half Item #3 on a flat surface with register side up. 1111..66..33 Place O-Ring Item #17 on register portion of inner wheel half. --C CA AU UTTIIO ON N-- Seal should not be twisted, but fully aligned in groove. 1111..66..44 Place a serviceable tire over inner wheel half Item #3 and then place outer wheel half Item #7 in tire, making sure to properly align inner and outer wheel registers. Slide tie bolts Item #9 and washers Item #10 through wheel assembly. --C CA AU UTTIIO ON N-- Counter-sunk side of washer Item #10 should be toward the bolt head. 1111..66..55 Install washers Item #11 and nuts Item #12 on tie bolts Item #9 and torque to 300 in-lbs. When all nuts have been torqued, retorque a second time to insure that the required value has been achieved. Sometimes O-Ring compression will give a false initial reading 1111..66..66 Inflate tire to proper pressure in a safety cage. 1111..66..77 Reinstall bearing cones Item #8 into cups Item #4 and install inner grease seals Item #5 using snap rings Item #14. 1122.. TTE ES STTIIN NG G 1122..11 W Whheeeell TTeessttiinngg 1122..11..11 The wheel shall be required to hold the normal inflation pressure for 24 hours, with not more than four percent loss in pressure after tire growth has stabilized. INSTALLATION INSTRUCTIONS Cleveland Nose Wheel Assembly Conversion Kit 199-126 Page 9 Jan. 1984, Rev. A 4-30-84 Rev. B 3-18-85 Rev. C 6-17-94 1133.. P PA AR RTTS S LLIIS STT 1133..11 W Whheeeell P Paarrttss LLiisstt PARKER HANNIFIN CORPORATION AIRCRAFT WHEEL AND BRAKE DIVISION AVON, OHIO PARTS LIST 40-204 WHEEL ASSEMBLY 6.50-10 TYPE III ITEM PART NO. DESCRIPTION QUANTITY 1 40-204 Wheel Assembly 1 2 161-12500 Inner Wheel Half Assembly 1 3 151-12000 Inner Wheel Half 1 4 214-00100 Cup - Bearing 1 5 154-03600 Grease Seal 2 A 6 162-11500 Outer Wheel Half Assembly 1 7 152-11900 Outer Wheel Half 1 4 214-00100 Cup - Bearing, 13836 1 8 214-00200 Cone - Bearing, 13889 2 9 103-31200 Bolt, MS21250H06034 8 10 095-03100 Washer, MS20002C6 8 11 095-10600 Washer, AN960-616 8 12 094-91500 Nut, AN365-624 8 14 155-00100 Snap Ring 2 15 166-09400 Nameplate 1 16 160-01200 Inflation Valve Assembly, TR716-03 1 17 101-25800 O-Ring (N304-75), MS28775-267 1 INSTALLATION INSTRUCTIONS Cleveland Nose Wheel Assembly Conversion Kit 199-126 Page 10 Jan. 1984, Rev. A 4-30-84 Rev. B 3-18-85 004400--2200440000 N Noossee W Whheeeell A Asssseem mbbllyy INSTALLATION INSTRUCTIONS Cleveland Nose Wheel Assembly Conversion Kit 199-126 Page 11 Jan. 1984, 1133..22 K Kiitt P Paarrttss LLiisstt PARKER HANNIFIN CORPORATION AIRCRAFT WHEEL & BRAKE DIVISION AVON, OHIO PARTS LIST 199-126 CONVERSION KIT BEECH SUPER KING AIR ITEM OLD P/N CODE NO. DESCRIPTION QUANTITY 1 40-204 040-20400 Nose Wheel Assembly* 1 -- Installation Booklet 1 50-91 Drawing 1 Warranty Registration Card 1 STC 1 This kit will convert one aircraft to Cleveland Nose Wheel * For Subassembly and Parts Identification: See 40-204 Parts List ClevelandWheels & Brakes Parker Hannifin Corporation Aircraft Wheel & Brake 1160 Center Road Avon, Ohio 44011 USA 1-800-BRAKING (272-5464) 216-937-1272 l FAX 216-937-5409 PRODUCT REFERENCE MEMO Initial Release February 01, 1997 PRM69 Page 1 of 1 AVAILABILITY OF GENERAL MAINTENANCE INFORMATION AND TORQUING PROCEDURES EFFECTIVITY: All Parker Hannifin (Cleveland Wheels & Brakes) External Disc Design wheel & brake assemblies. APPLICABILITY: Aircraft converted per STC approved kits to use Cleveland External Disc Design wheel & brake assemblies. REASON: This PRM is issued to inform Wheel & Brake Conversion Kit users and installers that information regarding general maintenance and proper bolt / nut torquing procedures is available. This information is contained in the Cleveland Wheels & Brakes Component Maintenance Manual (CMM) and in the Cleveland Technicians Service Guide, PRM64. Most Cleveland Conversion Kits were designed prior to creation of the CMM. Parker Hannifin is in process of upgrading kit paperwork to include a requirement to use the CMM and PRM64 as wheel & brake service information. This PRM serves the same purpose for kits whose paperwork has not yet been upgraded. DESCRIPTION: The Cleveland Wheels & Brakes Component Maintenance Manual and PRM64, Technician’s Service Guide shall be used as service information when performing general maintenance on Cleveland External Disc Design wheels & brakes. Particular attention should be paid to instructions regarding wheel bolt torquing procedures. NOTE: Refer to the CMM or PRM64 to determine the required torque procedure (Dry or Lubtork). While using the required torque procedure, observe the torque required to turn the nut (free running torque). This value must be added to the value stated on the casting or nameplate (or in the CMM or PRM64) to obtain a true torque value. Proper torque is imperative to prevent premature bolt or mating component failure. COMPLIANCE: Highly Recommended. APPROVAL: The engineering contents of this Product Reference Memo are FAA DER approved. WEIGHT & BALANCE: Not applicable. PUBLICATIONS: Cleveland Wheels & Brakes Component Maintenance Manual and PRM64 are available from: Customer Support Parker Hannifin Corporation Aircraft Wheel & Brake 1160 Center Road Phone: 1-800- BRAKING (272-5464) Avon, Ohio FAX: 216-937-5409 European Aviation Safety Agency SUPPLEMENTAL TYPE CERTIFICATE 10048423 This Supplemental Type Certificate is issued by EASA, acting in accordance with Regulation (EC) No. 216/2006 on behalf ofthe European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation and in accordance with Commission Regulation (EU) No. 748/2012 to PARKER HANNIFIN CORPORATION AIRCRAFT WHEEL & BRAKE DIVISION 1160 CENTER ROAD AVON OH 44011 USA and certifies that the change in the type design for the product listed below with the limitations and conditions specified meets the applicable Type Certification Basis and environmental protection requirements when operated within the conditions and limitations specified below: Original Original Type Certificate Number Type Certificate Number Type Certificate Holder Type Design - Model Type Design - Model Type Design - Model Original STC Number 1. FAA A24CE 2. EASAIM.A.277 BEECHCRAFT CORPORATION 1. 200, 20CC, 200CT, 200T 2. B200, B200C, B200CT, 2. B200T, B200GT, B200CGT. FAA SA75ZGL Description of Design Change: Replacement of Main Wheels & Brakes and/or Nose Wheel. EASA Certification Basis: The Certification Basis (CB) for the original product remains applicable to this certificate! approval. The requirements for environmental protection and the associated certified noise and! or emissions levels of the original product are unchanged and remain applicable to this certificate! approval. For the European Aviation Safety Agency, Date of issue: 10 March 2014 Note: The following numbers are listed on the certificate: EASA current Project Number: 0010027435-001 See Continuation Sheet(s) SUPPLEMENTAL TYPE CERTIFICATE - 10048423- PARKER HANNIFIN CORPORATION AIRCRAFT WHEEL & BRAKE DIVISION Aviation Michael Düslng Project Certification Manager TE.STC.00091-003 - Copyright European Aviation Safety Agency. All rights reserved. 1/2 European Aviation Safety Agency Associated Technical Documentation: nstallation of Main Wheel and Brakes in accordance with Parker Hannifin Conversion kit 199-125 Rev R, dated September 07, 2010, per Installation Manual, Rev L, dated January 21, 2010, and Installation Drawing 50-90, Rev K, dated January 21, 2010, and/or: Installation of Nose Wheel in accordance with Parker Hannifin Conversion kit 199-126 Rev L, dated September 07, 2010, per Installation Manual, Rev G, dated January 21, 2010, and Installation Drawing 50-91, Rev H, dated January 21, 2010. or later revisions of the above listed documents approved by EASA in accordance with EASA ED Decision 2004/04/CF (or subsequent revisions of this decision) and! or the Technical Implementation Procedures of EU! USA Bilateral Agreement. Lim itationslConditions: These modifications are approved for individual or joint installation on specified models that are equipped with landing gear that support 10 inch High Floatation equipment. Prior to installation of this design change it must be determined that the interrelationship between this design change and any other previously installed design change and/ or repair will introduce no adverse effect upon the airworthiness of the product. Note: The following numbers are listed on the certificate: EASA current Project Number: 0010027435-001 - end - SUPPLEMENTAL TYPE CERTIFICATE - 10048423- PARKER HANNIFIN CORPORATION AIRCRAFT WHEEL & BRAKE DIVISION TE.STC.00091-003 - Copyright European Aviation Safety Agency. All rights reserved. 2/2 1 Parker Hannifin Corporation Aerospace/Aircraft Wheel & Brake 1160 Center Road Avon, OH 44011 Date: _ _/_ _/20_ _ Subject: Letter of Authorization for Installation of STC’d Conversion Kits To whom it may concern: Parker Hannifin Corporation, Aircraft Wheel & Brake Division, hereby states that the following item(s): KIT NUMBER: 199-___________ FAA APPROVAL: 1) STC # ________________________ NO OTHER APPROVALS NECESSARY AUTHORIZATION TO INSTALL: With the sale of this STC KIT, OWNER of the Supplemental Type Certificate agrees to permit the buyer or buyer’s agent or agency to use the certificate to alter the product under the terms and conditions of this STC. A/C MAKE: ______________________ A/C MODEL______________________ TAIL # __________________________ Regards, Technical Support Team Technical Hotline (800) 272-5464 Clevelandwbhelp@parker.com Web-site: www.clevelandwheelandbrake.com Manufacturer of Cleveland Wheels & Brakes