Revision Transmittal Sheet
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1 ASB Dornier 328 Alert Service Bulletin Customer Support Global Support Centre P. O. Box 1252 Phone: D Wessling Telefax: Revision Transmittal Sheet This sheet transmits Revision 1 of Alert Service Bulletin ASB-328J titled: Flight Controls - Inspection of the Rudder Spring Tab Lever Assembly This is a complete revision. This has been reprinted in its entirety. All previous editions must be destroyed. Reason for Revision: Inspection setting and equipment altered: General: Page 2: Page 3/4: Page 9: Page 10: Layout adapted and adapted to Simplified Technical English where needed. Calibration standard SE.4.64 added to Special Tools Eddy current test frequency set to 3.1 khz (instead of 2.1 MHz). Calibration procedure revised. Fig. 3 added. NDT signal references and required NDT equipment settings are illustrated. Fig. 4 added showing calibration standard SE.4.64 NOTE: The changes are marked with revision bars at the outside margin. This Revision Transmittal Sheet is part of ASB-328J Revision 1. Model: Dornier No.: ASB-328J Date of Issue: Jan 02, 2018 Page 1 of 1
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4 Compliance Mandatory. This Alert Service Bulletin must be performed before the next 500FH or not later than three months from approval date of this ASB; then to be repeated every 5000 FH or 30 MTH, whichever comes first. Manpower Access: Inspection/Modification: Close-up: Functional checks: Total: 0.5 Mhrs. 0.5 Mhrs. 0.5 Mhrs. 1.0 Mhrs. 2.5 Mhrs. Material Refer to Material Parts List. Special Tools NDI Equipment Eddy current probe Calibration standard Set of Rigging Pins Dynamometer Approved eddy current test equipment. Rohmann PKA-27 H-1359 or equivalent SE.4.64 Calibration standard - gear lever spring tab GSE No (required for lever replacement only). GSE No. GM.4.07 (required for lever replacement only). Weight and Balance Not affected. Electrical Load Data Not affected. References Not affected. Other Publications Affected Maintenance Review Board Report Aircraft Maintenance Manual (MRB) (AMM) Reporting Compliance of this Service Bulletin must be reported to Customer Services Department using the Compliance Report for Configuration Control. Page 2 of 10 ASB-328J Rev. 1
5 ASB Dornier 328 Alert Service Bulletin Customer Support Global Support Centre P. O. Box 1252 Phone: D Wessling Telefax: ACCOMPLISHMENT INSTRUCTIONS CAUTION: OBEY THE SAFETY PRECAUTIONS AND THE GENERAL MAINTENANCE PRACTICES. REFER TO AMM JIC CHAPTER 00. CAUTION: OBEY THE APPLICABLE SAFETY PRECAUTIONS WHEN YOU WORK ON THE ADJUSTABLE PLATFORM. WARNING: PUT A WARNING NOTICE IN THE FLIGHT COMPARTMENT TO TELL PERSONS NOT TO OPERATE THE FLIGHT CONTROLS: A Preparation (1) Make the aircraft safe for maintenance. Refer to AMM JIC (2) Put a correct platform around the work area. (3) Remove the following access panels 324-HL and 324-CL. Refer to AMM JIC B Inspection (1) Do a detailed inspection of the rudder spring tab lever assembly P/N 001D272A (item 1) refer to detail B figure 2. Do an inspection for signs of cracks around the edges of the two lugs which retain the swaged bearings. (2) NDI Instrument Calibration. (a) Operate the test equipment as given in the manufacturer s instructions. (b) Set the necessary frequency to 3.1 khz. Refer to fig. 3. NOTE: Alternative instruments can have different settings. The frequency must stay the same but the other parameters must be adjusted in regard to the responses of the calibration standard. Model: Dornier Rev. No.: 1 No.: ASB-328J Rev. Date: Jan 02, 2018 Date of Issue: Feb 12, 2003 Page 3 of 10
6 NOTE: (c) Put the probe on the outside of calibration standard SE.4.64 in a slot-free area, refer to fig. 4. (d) Calibrate the instrument as given in the manufacturer s instructions for the lift-off at 270 on the display as shown in figure 3. (e) Put the probe on the outside of the calibration standard. Move the probe over the 1.0 and 1.7mm slots and adjust the sensitivity so, that the signal at the 1.7 mm slot is at 40 % of the full scale, refer to figure 3. (3) Do an Eddy current NDI on both bearing lug peripherals, refer to figure 2. (a) Put the probe on the compensation point near to the inspection area and set the lift-off as necessary, refer to figure 2 and 3. (b) Do the inspection as given in figure 2. Use the probe position and scan along path movements as illustrated, refer to detail C figure 2. If possible use a suitable tool to guide the probe centered around the lug. Make sure no crack indications are given as a result of positioning the probe too near to the edge of lug. NOTE: (c) Look at the display for signals that are different from those of the compensation point and the undamaged bearing lug area at Pos. 2, refer to fig. 2 & 3. For any signal that exceeds the dashed line (signal level of the compensation point, refer to fig. 3), it is necessary to remove the bearing and do a special detailed inspection (eddy current) of the bearing seat from inside. Refer to NTM In case of findings continue with paragraph C. CAUTION: NO CRACKS ARE PERMITTED. IF CRACKS ARE FOUND CONTACT 328 SUPPORT SERVICES GMBH. PLEASE SUPPLY IMPORTANT DETAILS AND PHOTOS ETC. INCLUDING NDI TEST EQUIPMENT USED AND ITS SETTINGS. (4) If a crack is found then a replacement lever assembly (item 1) must be installed, continue with paragraph C. If no crack is found continue with paragraph D. Page 4 of 10 ASB-328J Rev. 1
7 ASB Dornier 328 Alert Service Bulletin Customer Support Global Support Centre P. O. Box 1252 Phone: D Wessling Telefax: C Replacement (1) Remove the damaged rudder spring tab lever assembly (item 1). Refer to AMM JIC AA0. NOTE: Send the damaged Lever Assembly to the 328 Global Support Center: Oberpfaffenhofen Airport, Geb. 346 Süd Attn. Global Support Centre Wessling (1) Install the new rudder spring tab lever assembly (item 1). Refer to AMM JIC (2) Do a functional test of the rudder control system. Refer to AMM JIC D Close-up (1) Do a foreign object inspection of the complete modification area. (2) Install all opened panels. Refer to AMM JIC (3) Remove the platform from the work area. (4) Remove the warning notice from the flight compartment. (5) Return aircraft to a flyable status. Model: Dornier Rev. No.: 1 No.: ASB-328J Rev. Date: Jan 02, 2018 Date of Issue: Feb 12, 2003 Page 5 of 10
8 MATERIAL INFORMATION E Material Parts List Item Part Number Qty. Nomenclature Remarks D272A Spring Tab Lever Assy Replacement, if necessary after inspection. The following expendables have to be provided by the operator and/or ordered separately (not part of the kit) MS MS A/R Split Pin Necessary for replacement of lever. A/R Split Pin Necessary for replacement of lever. The following consumables have to be provided by the operator and/or ordered separately (not part of the kit) A/R Zinc-chromate Putty Necessary for replacement of lever. A/R Safety Wire Necessary for replacement of lever. Page 6 of 10 ASB-328J Rev. 1
9 ASB Dornier 328 Alert Service Bulletin Customer Support Global Support Centre P. O. Box 1252 Phone: D Wessling Telefax: Fig. 1: Location of Rudder Spring Tab Lever Assembly Model: Dornier Rev. No.: 1 No.: ASB-328J Rev. Date: Jan 02, 2018 Date of Issue: Feb 12, 2003 Page 7 of 10
10 Fig. 2: Definition of compensation point (Pos. 1) and detailed inspection area (Pos. 2). Page 8 of 10 ASB-328J Rev. 1
11 ASB Dornier 328 Alert Service Bulletin Customer Support Global Support Centre P. O. Box 1252 Phone: D Wessling Telefax: Fig. 3: NDT equipment settings in general and display readings for compensation point (Pos.1, refer to fig. 2), and damaged and undamaged bearing lug (Pos.2, refer to fig. 2). Model: Dornier Rev. No.: 1 No.: ASB-328J Rev. Date: Jan 02, 2018 Date of Issue: Feb 12, 2003 Page 9 of 10
12 Fig. 4a: Calibration standard SE The exploded view on the R/H side shows the artificial damages (slots) in the bearing seat of the aluminum ring representing the bearing lug of the spring tab lever. For details refer to fig. 4b. The calibration standard includes a ball bearing according to DON58-4 or -4P, since the bearing influences the response signal significantly. Fig. 4b: Details of calibration standard SE.4.64 shown without required bearing. Page 10 of 10 ASB-328J Rev. 1
13 CR Dornier 328 Compliance Report Customer Support Global Support Centre P. O. Box 1252 Phone: D Wessling Telefax: Please complete this compliance form for each aircraft only when it is applicable, and mail, , or fax to: Global Support Centre P. O. Box 1252 D Wessling Telefax: From Company: Doc. No. Rev. Title ASB-328J Flight Controls - Inspection of the Rudder Spring Tab Lever Assembly Aircraft Serial Number: Operator: Total Flight Hours: Total Landings: Date of Compliance: Comments: Date Authorized Signature
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