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CESSNA T-210 · Service Bulletins

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Type: Service Bulletins
Pages: 14
File size: 377 KB
Publisher: www.cessnaflyer.org

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Single Engine Service Bulletin April 29, 1988 Cessna SEB88-3 TITLE HORIZONTAL STABILIZER ATTACHMENT REINFORCEMENT EFFECTIVITY Model P206, U206, 207, 210 and P210 Series Airplanes normally aspirated and Turbocharger models. Serial numbers . . P206-0420 thru P20600647 U206-0915 thru U20607020 20700001 thru 20700788 21058819 thru 21064897 T210-0198 thru T210-0454 P21000001 thru P21000834 PURPOSE To provide a modification that incorporates additional structural members on the horizontal stabilizer attach bulkhead and new stabilizer attach fittings for improved stabilizer attachment service life. COMPLIANCE Recommended, should be accomplished whenever loose rivets or cracks in the stabilizer attach bulkhead, doublers or fittings are discovered during routine 100 hour or annual inspections, or during equivalent inspections for airplanes utilizing the Cessna Progressive Care Inspection Program. APPROVAL FAA approval has been obtained on technical data in this publication that affects airplane type design. Page 1 of 3 To obtain satisfactory results, procedures specified in this publication must be accomplished in accordance with accepted methods and prevailing government regulations. The Cessna Aircraft Company cannot be responsible for the quality of work performed in accomplishing the requirements of this publication. The Cessna Aircraft Company, Customer Services, P.O. Box 7704, Wichita, Kansas 67277 U.S.A. (316) 946-7550, Telex: 4319022, Facsimile (316) 942-9006 COPYRIGHT © 1988 MAN-HOURS For SK207-8 For both SK210-125 & -126 . • • For SK210-125 or SK210-126 • estimated 25.0 man-hours per airplane. estimated 32.0 man-hours per airplane. estimated 25.0 man-hours per airplane. MATERIAL Modification parts are available from the Cessna Supply Division thru an appropriate Cessna Dealer or Authorized Service Facility for the suggested list prices shown. Part Number Description Qty./Airplane Price *SK207-8 Stabilizer Attach 1 ea. $ 608.00 (D) ea. Fitting Replacement Kit - 207 *SK210-125 Stabilizer Attach 1 ea. $ 198.00 (S) ea. Bulkhead Mod. Kit - U206, 207, 210, P210 *SK210-126 Stabilizer Attach 1 ea. $ 606.00 (D) ea. Fitting Replacement Kit - P206, U206, 210, T210, P210 * Before ordering refer to attached copy of Service Kits for applicable airplane serial numbers. ALL PRICES SUBJECT TO CHANGE WITHOUT NOTICE ) ACCOMPLISHMENT INSTRUCTIONS Service Kits SK207-8, SK210-125 and SK210-126 modification instructions are attached. Horizontal stabilizer attachment parts that are found to be cracked or damaged must be replaced prior to accomplishing the modification. CREDIT Not applicable. Page 2 SEB88-3 April 29, 1988 OWNER NOTIFICATION On May 13, 1988 the following Owner Advisory message will be sent to applicable owners of record in SEB88-3A. Dear Cessna Owner, A modification which provides new horizontal stabilizer attach fittings and additional structural members on the horizontal stabilizer attach bulkhead has been developed to provide improved stabilizer attachment service life. Compliance is recommended and should be accomplished whenever loose rivets or cracks in the stabilizer attach bulkhead, doublers or fittings are discovered during routine inspections. Please contact your Cessna Single Engine Dealer and arrange to have the modification accomplished. SEB88-3 April 29, 1988 * * * Page 3 Service Kit APRIL 29, 1988 Cessna SK207-8 TITLE: STABILIZER ATTACH FITTING REPLACEMENT The following procedures provide instructions to install improved stabilizer attach fittings on the stabilizer front spar. EFFECTIVITY: MODELS AFFECTED 207 & T207 SERIALS AFFECTED 20700001 Thru 20700788 PARTS LIST: QUANTITY PART NUMBER NOMENCLATURE 222442442222121 AN315-4R AN4-13A Nut Bolt MS20470AD5-10 Rivet MS20470AD5-12 Rivet MS20470AD5-9 Rivet MS20470AD6-10 Rivet MS20470AD6-12 Rivet MS20470AD6-9 Rivet S1450-4A12-016 Washer S1450-4A12-020 Washer S1450-4A12-025 Washer S1450-4A12-032 Washer 1209084-1 Locator Bar 1232041-1 Fitting Instructions CHANGE IN WEIGHT AND BALANCE: WEIGHT INCREASE Negligible REF SEB88-3 1 of 4 FAA APPROVAL HAS BEEN OBTAINED ON TECHNICAL DATA IN THIS PUBLICATION THAT AFFECTS AIRPLANE TYPE DESIGN. . 1. A. SK207-8 MODIFICATION INSTRUCTIONS: B. Remove stinger, elevator, stabilizer and vertical fin per 207 Service Manual. NOTE Discard existing AN4 bolts that attach stabilizer to bulkhead. New bolts are provided in this Service Kit for reinstallation of this stabilizer. Remove existing stabilizer attach fittings and install new attach fittings. (Refer to Figure 1.) 1. 2. 3. 4. Remove fitting Carefully drill out rivets from one existing fitting at locations (5, 6 & 8) using 0.161 drill bit. from spar assembly (7). Deburr holes. CAUTION DO NOT DAMAGE OR ENLARGE EXISTING RIVET HOLES IN STABILIZER SPAR ASSY. Attach one end of locator bar (4) to remaining exisiting fitting and the other end to the new fitting (3), using bolts and nuts (9). Align holes in spar with holes in new fitting and cleco in place. Secure new fitting (3) with rivets (5, 6 & 9). NOTE Any oversized or damaged holes may be re-drilled with 0.193 bit for oversized rivets (MS20470AD6-12, MS20470AD6-10 or MS20470AD6-9 as required). Repeat Steps 1 thru 3 for other side of spar to replace existing fitting with new one. Use locator bar (4) to maintain proper spacing between fittings. 5. Discard locator bar (4) and nuts (9). 2 ( SK207-8 C. Reinstall stabilizer, vertical fin, elevator and stinger. 1. 2. 3. 4. Reinstall stabilizer per 207 Service Manual. If gap exists between stabilizer attach bulkhead (1) and fittings (3), install washers (2) as required to shim the gap. NOTE Do not use bolt tension to draw bulkhead and fittings together. Reinstall remaining control surfaces and rig per applicable Service Manual. Inspect all hardware, fasteners and structure for damage or corrosion and correct as necessary. Reinstall stinger and fairings per applicable Service Manual. Make an entry in the Airplane Logbook stating this Service Kit has been installed. )

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3 0 SK207-8 ⑪ STABILIZER ATTACH BULKHEAD (REF) 0°50' (2 S1450-4A12-016 WASHER S1450-4A12-020 WASHER S1450-4A12-025 WASHER S1450-4A12-032 WASHER AS REQD 31232041-1 FITTING (REF) (REF) 3.300 (REF) ⑦1232622 FWD STABILIZER SPAR (REF) VIEW B-B ⑦ FWD SPAR (REF) (9 AN4-13A BOLT AN315-4R NUT 2 EA REQD 4.45 4 1209084-1 LOCATOR BAR I REQD 8 0.161 HOLE MS20470AD5-12 RIVET 4 EA REQD B + + ++ + B 6 0.161 HOLE MS20470AD5-10 RIVET 2 EA REQD 3 1232041-1 FITTING 2 EA REQD (5) 0.161 HOLE MS20470AD5-9 RIVET VIEW A-A 4 EA REQD (VIEW LOOKING AFT AT FWD STABILIZER SPAR) Figure 1. Stabilizer Attach Fitting Modification ) ) Service Kit ☑ Cessna APRIL 29, 1988 TITLE: STABILIZER ATTACH BULKHEAD MODIFICATION SK210-125 The following procedures provide instructions to add reinforcement doublers to stabilizer attach fittings. MODELS AFFECTED U206, TU206 207, T207 210, T210 P210 MATERIAL REQUIRED SERIALS AFFECTED U20601875 thru U20607020 20700215 thru 20700788 21059720 thru 21064897 P21000001 thru P21000834 QUANTITY PART NUMBER NOMENCLATURE 62421121 MS20426AD5-8 Rivet MS20470AD4-4 Rivet MS20470AD4-8 Rivet MS20470AD5-8 Rivet 1212159-1 Doubler Assy -Fwd LH 1212159-2 Doubler Assy Fwd RH - 1212159-3 Doubler - Aft Instructions CHANGE IN WEIGHT AND BALANCE: WEIGHT INCREASE Negligible ARM RESULTANT MOMENT INDEX REF SEB88-3 Page 1 of 3 FAA APPROVAL HAS BEEN OBTAINED ON TECHNICAL DATA IN THIS PUBLICATION THAT AFFECTS AIRPLANE TYPE DESIGN. SK210-125 1. MODIFICATION OF STABILIZER ATTACH BULKHEAD A. Remove stinger, stabilizer fairings, vertical fin and horizontal stabilizer per appropriate Service Manual. Retain all components and hardware. Remove control surfaces, if required. B. Remove existing stabilizer attach fittings and install new attach fittings. C. D. 1. 2. 3. 4. 5. Carefully drill out existing rivets and remove and discard doublers (1) from fwd. and aft faces of bulkhead (5). Carefully inspect bulkhead (5) for cracks or damage. If repair- able cracks or damage is found, repair in accordance with Cessna Service Manual and F.A.R. PART 43. If patch is necessary, in- stall on fwd. face of bulkhead (5), allowing for installation of new doublers (9). Using an AN4 bolt for alignment, locate doublers (9) fore and aft on each side of bulkhead (5). Doublers will pick up five (5) existing holes that were used to attach removed doublers. Cleco the new doublers (9) in place at the end locations for rivets (6 & 8). Drill the remaining holds to 0.161 diameter for installation of 5/32 rivets and countersink holes (3) on the aft doubler. Install doublers (9) with rivets (3, 6, 7 & 8). Install rivets (4) on each side of plug hole left when removing doublers (1). 6. Inspect all fasteners and hardware and replace as necessary. Inspect fin and stabilizer attachments for corrosion and damage, and repair as required. Install horizontal stabilizer, vertical fin and any control surfaces removed. Refer to the appropriate Service Manual for installation of all components and rigging procedures. Make an entry in the airplane logbook stating this Service Kit has been installed. 2 ( A SK210-125 E ①1212127 DOUBLER ACFT ⑤12231 OR 1212136 (REF) BULKHEAD (REF) + 17115 #1171 VIEW A-A (BEFORE MODIFICATION) ⑨ 2259-3 DOUBLER AFT 1212159-1 DOUBLER FWD LH IEA REQD. - - E ACFT 8 0.128 HOLE MS20470AD4-8 RIVET 2 EA REQD. ⑦0.161 HOLE MS20470AD5-8 RIVET 2 EA REQD. ) ++ ② 2259-3 DOUBLER - AFT 1212159-2 DOUBLER - FWD RH | EA REQD. 0.161 HOLE -100° CSK MS20426AD5-8 RIVET 6 EA REQD. (6 0.128 HOLE MS20470AD4-8 RIVET 2 EA REQD. 1212131 OR 1212136 BULKHEAD (REF) VIEW A-A (4) 0.128 HOLE MS20470AD4-4 RIVET 2 EA REQD. (PLUG HOLE) VIEW LOOKING FWD AT STABILIZER ATTACH BULKHEAD (AFTER MODIFICATION) Figure 1. Stabilizer Attach Bulkhead Reinforcement. 3 Service Kit Cessna APRIL 29, 1988 TITLE: STABILIZER ATTACH FITTING REPLACEMENT SK210-126 The following procedures provide instructions to install improved stabilizer attach fittings on the stabilizer front spar. EFFECTIVITY: PARTS LIST: MODELS AFFECTED P206 U206 T210 210 210 & T210 P210 SERIALS AFFECTED P206-0420 thru P20600647 U206-0915 thru U20607020 T210-0198 thru T210-0454 21058819 thru 21059199 21059200 thru 21064897 P21000001 thru P21000834 QUANTITY PART NUMBER NOMENCLATURE 2 2 2 222442442222222 AN315-4R Nut AN4-12A Bolt MS20470AD5-10 Rivet 4 MS20470AD5-12 Rivet 4 MS20470AD5-9 Rivet MS20470AD6-10 Rivet MS20470AD6-12 Rivet 4 MS20470AD6-9 Rivet 2 S1450-4A12-016 Washer 2 S1450-4A12-020 Washer 2 S1450-4A12-025 Washer 2 S1450-4A12-032 Washer 1 1209084-1 Locator Bar 2 1232041-2 1 Fitting Instructions REF SEB88-3 1 of 4 FAA APPROVAL HAS BEEN OBTAINED ON TECHNICAL DATA IN THIS PUBLICATION THAT AFFECTS AIRPLANE TYPE DESIGN. CHANGE IN WEIGHT AND BALANCE: WEIGHT INCREASE SK210-126 Negligible 1) MODIFICATION INSTRUCTIONS. 1. A. Remove stinger, elevator, stabilizer and vertical fin per appropriate Service Manual. B. NOTE Discard exsiting AN4 bolts that attach stabilizer to bulkhead. New bolts are provided in this Service Kit for reinstallation of the stabilizer. Remove existing stabilizer attach fittings and install new attach fittings. (Refer to Figure 1.) 1. 2. 3. Carefully drill out rivets from one existing fitting at locations (5, 6 & 8) using 0.161 drill bit. Remove fitting from the stabilizer spar assembly (7). Deburr holes. CAUTION DO NOT DAMAGE OR ENLARGE EXISTING RIVET HOLES IN STABILIZER SPAR ASSEMBLY. Attach one end of locator bar (4) to remaining existing fitting and the other end to the new fitting(3), using bolts and nuts (9). Align holes in spar with holes in new fitting and cleco in place. Secure new fitting (3) to forward spar (7) with rivets (5, 6 & 8). NOTE Any oversized or damaged holes may be re-drilled with 0.193 drill bit for over- sized rivets (MS20470AD6-12, MS20470AD6-10 or MS20470AD6-9 as required). 2 SK210-126 C. 4. Repeat Steps 1 thru 3 for other side of spar to replace existing fitting with new one. Use the locator bar (4) to maintain proper spacing between fittings. 5. Discard locator bar (4) and nuts (9). Reinstall stabilizer, vertical fin, elevator and tailcone stinger. If gap 1. نه 3. 4. Reinstall stabilizer per appropriate Service Manual. existis between stabilizer attach bulkhead (1) and fittings (3), install washers (2) as required to shim the gap. NOTE Do not use bolt tension to draw bulkhead (1) and fittings (3) together. Reinstall remaining control surfaces and rig per appropriate Service Manual. Inspect all hardware, fasteners and structure for damage or corrosion and correct as necessary. Reinstall tailcone stinger and fairings. Make an entry in the airplane logbook stating this Service Kit has been installed. 3 ⑦FWD SPAR (REF) SK210-126 S1450-4A12-016 WASHER ⑪ STABILIZER ATTACH BULKHEAD (REF) 3°0' (REF) S1450-4A12-020 WASHER S1450-4A12-025 WASHER S1450-4A12-032 WASHER AS REQD 31232041-2 FITTING (REF) 3.300 (REF) 1232622 FWD STABILIZER SPAR (REF) VIEW B-B ⑨ AN4-12A BOLT AN315-4R NUT 2 EA REQD 4.45 1209084-1 LOCATOR BAR 1 REQD (8 0.161 HOLE MS20470AD5-12 RIVET 4 EA REQD ++ + ++ + + + (3)1232041-2 FITTING 6 0.161 HOLE MS20470AD5-10 RIVET 2 EA REQD MS20470AD5-9 RIVET 2 EA REQD 5 0.161 HOLE VIEW A-A 4 EA REQD (VIEW LOOKING AFT AT FWD STABILIZER SPAR) Figure 1. Stabilizer Attach Fitting Replacement 4

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