# AAI Alert Service Bulletin AA-08055: Revision B - Rights: © AAI. Filed by the FAA in regulations.gov docket FAA-2012-0502, the docket of AD 2012-22-06. Not covered by OpenAirDocs’ CC0 dedication. - Document: [AAI Alert Service Bulletin AA-08055](https://openairdocs.org/service-documents/aai/aa08055.md) - Title as filed: Aeronautical Accessories, Inc. - Alert Service Bulletin - Pages: 16 - PDF: https://openairdocs.org/files/sha256/12/f0/12f09bf5cb5bbd3c5109fb6584acff19c1156690b7f035677beb3255c8cf436c - Page: https://openairdocs.org/service-documents/aai/aa08055/file/12f09bf5cb5b ## Text This text is OCR from a scan. OCR can misread letters and numbers. Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 (OCR) AERONAUTICAL ACCESSORIES, INC. P.O. BOX 3689 BRISTOL, TENNESSEE 37625-3689 USA TELEPHONE: 423-538-5151 TOLL FREE: 800-251-7094 TELEFAX: 423-538-8469 E-MAIL: sales@aero-access.com techsupport@aero-access.com ALERT SERVICE BULLETIN ASB No. AA-08055 Revision B August 12, 2009 SUBJECT: High Landing Gear Forward Crosstubes P/N 212-321-103 MODELS AFFECTED: Bell Helicopter Textron model 205A, 205A-1, 205B, 212, 412, 412EP and 412CF and Agusta S.p.A. model AB412, AB412EP helicopters with Aeronautical Accessories, Inc. P/N 212-321-103 High Forward Crosstubes installed in accordance with STC SR01052AT. Garlick Helicopters, US Helicopters, Inc., Western International Aviation, Inc., Southwest Florida Aviation model UH-1B, UH-1H, SW204, SW205 helicopters with Aeronautical Accessories, Inc. P/N 212-321-103 High Forward Crosstubes installed in accordance with STC SR01924AT. IF OWNERSHIP OF AIRCRAFT HAS CHANGED, PLEASE FORWARD THIS BULLETIN TO NEW OWNER ### Page 2 (OCR) 205A, 205A-1, 205B, 212 ALERT SERVICE BULLETIN ASB No. AA-08055 412, 412EP, 412CF HIGH FORWARD CROSSTUBE Revision B AB412, AB412EP UH-1B, UH-1H, SW204, SW205 COMPLIANCE: Part A: Within the next 50 flight hours, but not later than September 1, 2009, create an Historical Record to determine/track P/N 212-321-103 high forward crosstube takeoff/landing events. Part B: 7500 or greater takeoff/landings. High forward crosstubes with historical information establishing a number of takeoff/landings greater than 7500 must accomplish Part B within 25 flight hours or 200 takeoff/landings, whichever comes first, of the receipt of this bulletin. Part C: Within 200 takeoff/landings after accomplishment of Part B, and every 200 takeoff/landings thereafter. Part D: Prior to 10,000 takeoff/landings and every 12 months or 2500 takeoff/landings, whichever comes first, thereafter. High forward crosstubes with historical information establishing a number of takeoff/landings greater than 10,000 must accomplish Part D within 1 month of the receipt of this bulletin. Part E: Prior to 12,500 takeoff/landings and every 5000 takeoff/landings thereafter. High forward crosstubes with historical information establishing a number of takeoff/landings greater than 12,500 must accomplish Part E within 3 months of the receipt of this bulletin. ### Page 3 (OCR) 205A, 205A-1, 205B, 212 ALERT SERVICE BULLETIN ASB No. AA-08055 412, 412EP, 412CF HIGH FORWARD CROSSTUBE Revision B AB412, AB412EP UH-1B, UH-1H, SW204, SW205 DESCRIPTION: Aeronautical Accessories, Inc. has conducted a review of the high forward crosstube in response to two reported field failures. Our analysis indicates additional scheduled inspections must be conducted on P/N 212-321-103 high forward crosstubes. Part A of this bulletin establishes a takeoff/landing history for P/N 212-321-103 high forward crosstubes. This bulletin provides the information necessary to calculate the number of takeoff/landings. Part B of this bulletin provides instructions to clean and inspect two areas on the bottom of the high forward crosstube. Means to protect this area with primer and a clear coat are also included. P/N 212-321-103, serial number AA-1250 and subsequent, crosstubes are manufactured with the two inspection areas primed and clear-coated. Part C of this bulletin provides instructions to conduct a recurring visual inspection of the two primed and clear coated areas of the high forward crosstube after the accomplishment of Part B. Part D of this bulletin provides instructions to conduct a recurring dimensional inspection of the skid gear to identify permanent deformation of the crosstube. Part E of this bulletin provides instructions to conduct a recurring fluorescent penetrant inspection of the high forward crosstube. APPROVAL: The engineering aspects of this bulletin are FAA/DER approved. MANPOWER: PART A: Approximately 0.5 hours. PART B: Approximately 3.0 hours. PART C: Approximately 0.5 hours PART D: Approximately 1.0 hours. PART E: Approximately 24.0 hours. Manhours are based on hands-on time and may vary with personnel or facilities available. ### Page 4 (OCR) 205A, 205A-1, 205B, 212 ALERT SERVICE BULLETIN ASB No. AA-08055 412, 412EP, 412CF HIGH FORWARD CROSSTUBE Revision B AB412, AB412EP UH-1B, UH-1H, SW204, SW205 LOG OF REVISIONS Date Revision Description Affected Pages 03/20/09 NR Original Release All 07/28/09 Reformatted Title Page; added Log of Revisions; corrected All document formatting errors; revised Figure 1 08/12/09 Revised BL 50 to BL 40 in Part B step 2 7 Revised dimensioning in View D - D, Figure 1 14 Reviewed: B/12/09 Engineering Date Put Lamast 8-12-09 Airworthiness Date AERONAUTICAL ACCESSORIES, INC. August 12, 2009 Page 4 of 16 ### Page 5 (OCR) 205A, 205A-1, 205B, 212 ALERT SERVICE BULLETIN ASB No. AA-08055 412, 412EP, 412CF HIGH FORWARD CROSSTUBE Revision B AB412, AB412EP UH-1B, UH-1H, SW204, SW205 MATERIAL: The following Customer supplied materials are required to comply with this bulletin: TABLE 1 - PARTS LIST CUSTOMER SUPPLIED CONSUMABLE MATERIALS Qty Description AR MIL-R-81294, Type I or II Chemical Paint Remover AR MIL-PRF-85582 Primer (PRC-DeSoto EWDE 072A/B) AR MIL-PRF-85285, Type I Gloss Clear Coat Paint (Deft 03X085) AR MIL-PRF-87937 Cleaning Compound, Aerospace Equipment NOTE The MIL-PRF-85582 primer (PRC-DeSoto EWDE 072A/B) [packaged as a 1-gallon, 1-qt (Parts A&B) kit (P/N EWDE072)] and the MIL-PRF-85285, Type I clear coat paint (Deft 03X085) [packaged as a 3-qt kit (P/N MIL-PRF-85285)] may be procured from a Bell Helicopter Supply Center. The primer and paint may also be procured [packaged in 1-qt, primer and paint, kits (P/N 1272K)] from Aerospace Products, Inc., 6413 Midway Road, Halton City, TX 76117 (817-332-1669). SPECIAL TOOLS REQUIRED: 10X magnifying glass WEIGHT AND BALANCE: Not affected PUBLICATIONS AFFECTED: Installation Instructions, report number AA-95005 Instructions for Continued Airworthiness, report number AA-01136 ADDITIONAL INFORMATION: Any questions regarding this bulletin should be addressed to: AERONAUTICAL ACCESSORIES, INC. P.O. Box 3689 Bristol, 37625-3689 TN PRODUCT SUPPORT 1-800-251-7094 techsupport@aero-access.com AERONAUTICAL ACCESSORIES, INC. August 12, 2009 Page 5 of 16 ### Page 6 (OCR) 205A, 205A-1, 205B, 212 ALERT SERVICE BULLETIN ASB No. AA-08055 412, 412EP, 412CF HIGH FORWARD CROSSTUBE Revision B AB412, AB412EP UH-1B, UH-1H, SW204, SW205 ACCOMPLISHMENT INSTRUCTIONS Upon receipt of this bulletin, determine by part number if affected high forward crosstube is installed. If affected crosstube is installed, perform the actions contained in this bulletin. Verify all high forward crosstubes, P/N 212-321-103, comply with the inspection criteria of Instructions for Continued Airworthiness report number AA-01136 and the applicable model Bell Helicopter Maintenance Manual. Any crosstube failing inspection shall be removed from service and replaced with an airworthy crosstube. PART A HISTORICAL RECORDS 1. An Historical Record Form is provided (Figure 4) for recording of takeoff/landing operations for high forward crosstubes, P/N 212-321-103, per the compliance section of this bulletin. NOTE Helicopters with takeoff/landings that are higher than the average of 10 per hour must substitute the higher value in all estimated calculations. 2. If the actual takeoff/landing information is not available it is permissible to estimate the number. To determine the number of takeoff/landings on the crosstube, multiply the airframe hours by a factor of ten. 3. Place the calculated takeoff/landing information on the Historical Record form and track the applicable takeoff/landing events as per the compliance section of the bulletin. AERONAUTICAL ACCESSORIES, INC. August 12, 2009 Page 6 of 16 ### Page 7 (OCR) 205A, 205A-1, 205B, 212 ALERT SERVICE BULLETIN ASB No. AA-08055 412, 412EP, 412CF HIGH FORWARD CROSSTUBE Revision B AB412, AB412EP UH-1B, UH-1H, SW204, SW205 PART B INITIAL INSPECTION REQUIREMENT FOR P/N 212-321-103 CROSSTUBES NOTE Crosstube visual inspection is conducted with aircraft at rest on skid landing gear; minimum gross weight at inspection is 9,000 pounds. CAUTION Chemical removers shall be used only in areas of adequate ventilation. Suitable goggles or face masks, chemical resistant gloves, boots and clothing shall be worn to avoid contact of chemical removers with eyes, skin and clothing. Chemical removers shall further be handled in accordance with applicable OSHA regulations, state and local safety codes, and company established safety standards and policies. 1. Use MIL-PRF-87937 cleaning compound prepared in accordance with the manufacturer's recommendations to clean all residue and dirt from the cross tube surfaces (left side and right side) shown in Figure 1. NOTE P/N 212-321-103 Crosstubes with serial number AA-1250 and subsequent are manufactured with the two inspection areas primed and clear-coated. Steps 2 thru 5, 7 and 8 of Part B may be skipped unless opaque paint has been applied to inspection area described below and in Figure 1. 2. Prepare crosstube inspection areas by chemically removing crosstube paint and primer from an area 2.0 10.25 inches wide extending from BL 40 to BL 2.5 at the center-bottom surtace of the crosstube on both the left and the right sides of the crosstube (see Figure 1). 3. Apply MIL-R-81294, Type I or II chemical paint remover with a brush and allow it to set from 15 to 45 minutes to soften paint. 4. Using a stiff fiber brush and clean water, rinse paint from crosstube. If required, use abrasive pad (Scotch-Brite, Type A) and MIL-R-81294, Type I or II chemical paint remover to aid in lifting paint. Brush crosstube with abrasive pad in the longitudinal direction, using care so as not to abrade crosstube metal surface. WARNING DO NOT SAND CROSSTUBE IN A CIRCUMFERENTIAL DIRECTION. 5. Rinse part clean with clean water and dry thoroughly. AERONAUTICAL ACCESSORIES, INC. August 12, 2009 Page 7 of 16 ### Page 8 (OCR) 205A, 205A-1, 205B, 212 ALERT SERVICE BULLETIN ASB No. AA-08055 412, 412EP, 412CF HIGH FORWARD CROSSTUBE Revision B AB412, AB412EP UH-1B, UH-1H, SW204, SW205 NOTE Reapplication of chemical paint remover may be required to ensure that paint and primer is completely removed so that the metal surface of the cross tube is clearly visible. If required, repeat steps 2 thru 5. 6. Using at least 10X magnification and a strong light source, visually inspect the stripped, or clear coated, areas for indications of cracking. If cracking is suspected, fluorescent penetrant inspect crosstube per ASTM E1417, Type I, Method B, C, or D, Level 2 in accordance with Bell Helicopter Standard Practices Manual (BHT-ALL-SPM). WARNING IF CRACKING IS DISCOVERED, THE CROSSTUBE IS NO LONGER AIRWORTHY AND MUST BE IMMEDIATELY REPLACED. REPLACE CROSSTUBE PER APPLICABLE INSTRUCTIONS IN INSTRUCTIONS FOR CONTINUED AIRWORTHINESS, REPORT NUMBER AA-01136. 7. Following crosstube inspection, coat the stripped crosstube area with MIL-PRF-85582 primer (.0006 - .0009 thick) by spraying in accordance with manufacturer's instructions. Allow primer to cure per manufacturer instructions. NOTE The MIL-PRF-85582 primer (PRC-DeSoto EWDE 072A/B) [packaged as a 1-gallon, 1-qt (Parts A&B) kit (P/N EWDE072)] and the MIL-PRF-85285, Type | clear coat paint (Deft 03X085) [packaged as a 3-qt kit (P/N MIL-PRF-85285)] may be procured from a Bell Helicopter Supply Center. The primer and paint may also be procured [packaged in 1-qt, primer and paint, kits (P/N 1272K)] from Aerospace Products, Inc., 6413 Midway Road, Halton City, TX 76117 (817-332-1669). 8. Following primer cure, paint the area with MIL-PRF-85285 polyurethane clear coat paint by spraying in accordance with manufacturer's instructions. Allow paint to cure per manufacturer instructions. 9. Annotate aircraft records that Part B of this bulletin has been accomplished. 10. Return aircraft to service. AERONAUTICAL ACCESSORIES, INC. August 12, 2009 Page 8 of 16 ### Page 9 (OCR) 205A, 205A-1, 205B, 212 ALERT SERVICE BULLETIN ASB No. AA-08055 412, 412EP, 412CF HIGH FORWARD CROSSTUBE Revision B AB412, AB412EP UH-1B, UH-1H, SW204, SW205 PART C SCHEDULED VISUAL INSPECTION REQUIREMENTS FOR P/N 212-321-103 NOTE The following crosstube inspection is to be incorporated into the inspection intervals/methods identified in Instructions for Continued Airworthiness, report number AA-01136. NOTE Crosstube visual inspection is conducted with aircraft at rest on skid landing gear; minimum gross weight at inspection is 9,000 pounds. 1. Use MIL-PRF-87937 cleaning compound prepared in accordance with the manufacturer's recommendations to clean all residue and dirt from the cross tube surfaces shown in Figure 1. 2. Using at least 10X magnification and a strong light source, visually inspect the clear coated areas for indications of cracking. 3. If cracking is suspected, remove clear coat and primer per steps 2 thru 5 of Part B, and fluorescent penetrant inspect crosstube per ASTM E1417, Type I, Method B, C, or D, Level 2, in accordance with Bell Helicopter Standard Practices Manual (BHT-ALL-SPM). If cracking is not confirmed, reapply clear coat and primer per steps 7 and 8 of Part B. If cracking is confirmed, remove crosstube from service. WARNING IF CRACKING IS DISCOVERED, THE CROSSTUBE IS NO LONGER AIRWORTHY AND MUST BE IMMEDIATELY REPLACED. REPLACE CROSSTUBE PER APPLICABLE INSTRUCTIONS IN INSTRUCTIONS FOR CONTINUED AIRWORTHINESS, REPORT NUMBER AA-01136. 4. Annotate aircraft records to indicate that Part C of this bulletin has been accomplished; and return aircraft to service. AERONAUTICAL ACCESSORIES, INC. August 12, 2009 Page 9 of 16 ### Page 10 (OCR) 205A, 205A-1, 205B, 212 ALERT SERVICE BULLETIN ASB No. AA-08055 412, 412EP, 412CF HIGH FORWARD CROSSTUBE Revision B AB412, AB412EP UH-1B, UH-1H, SW204, SW205 PART D SCHEDULED LANDING GEAR DEFLECTION INSPECTION REQUIREMENTS FOR P/N 212-321-103 The following crosstube inspection is to be incorporated into the inspection intervals/methods identified in Instructions for Continued Airworthiness, report number AA-01136. 1. Hoist or jack the helicopter until no weight is on the skid gear. 2. Measure the Crosstube horizontal deflection from the centerline of the helicopter, BL 0.00, to the outside of the skid tubes, as shown in Figure 2. 3. The Crosstube horizontal deflection as measured in step 2 must be within the limits as shown in Figure 2. Crosstubes that measure outside of the limits must be replaced. 4. Inspect landing gear assembly in accordance with Instructions for Continued Airworthiness report number AA-01136 and applicable model BHT maintenance manual damage limits. 5. Repair or replace components that are damaged in excess of repairable limits. 6. Annotate aircraft records to indicate that Part D of this bulletin has been accomplished; and return aircraft to service. AERONAUTICAL ACCESSORIES, INC. August 12, 2009 Page 10 of 16 ### Page 11 (OCR) 205A, 205A-1, 205B, 212 ALERT SERVICE BULLETIN ASB No. AA-08055 412, 412EP, 412CF HIGH FORWARD CROSSTUBE Revision B AB412, AB412EP UH-1B, UH-1H, SW204, SW205 PART E COMPONENT OVERHAUL REQUIREMENTS FOR P/N 212-321-103 The Component Overhaul Schedule, Table 2, summarizes the overhaul interval for high forward crosstube components. NOTE Neither the assignment of a time period overhaul of a component nor failure to assign a time period for overhaul of a component constitutes a warranty of any kind. The only warranty applicable to the component is that warranty included in the Purchase Agreement for the component. Time between overhauls and inspection periods is based upon experience, testing, and engineering judgment and is subject to change at the sole discretion of Aeronautical Accessories Inc. or an appropriate government agency. WARNING ALL PARTS REMOVED DUE TO REACHING THEIR LIMITS OR AS A RESULT OF AN ACCIDENT/INCIDENT DEEMED UNAIRWORTHY, SHALL PERMANENTLY MARKED AS SCRAP OR PHYSICALLY DESTROYED TO THE EXTENT THAT THERE IS NO CHANCE OF REPAIR OR INSTALLATION ON ANY HELICOPTER OR COMPONENT. TABLE 2 - COMPONENT OVERHAUL SCHEDULE PART NUMBER NOMENCLATURE OVERHAUL INTERVAL 212-321-103 Forward Crosstube, Prior to 12,500 Takeoff/Landings and High Skid Gear every 5000 Takeoff/Landings thereafter E.1 Disassembly Instructions 1. Remove fairings from Forward Crosstube Assembly, if installed. 2. Hoist or jack the helicopter until no weight is on the skid tubes. 3. Remove forward straps and associated hardware from forward fuselage fittings. 4. Remove aft straps and associated hardware from aft fuselage fittings. 5. Raise helicopter until it is clear of skid landing gear, and remove landing gear. 6. Remove crosstube supports from Forward Crosstube Assembly: a. Remove support U-bolts securing each crosstube support to Forward Crosstube Assembly. AERONAUTICAL ACCESSORIES, INC. August 12, 2009 Page 11 of 16 ### Page 12 (OCR) 205A, 205A-1, 205B, 212 ALERT SERVICE BULLETIN ASB No. AA-08055 412, 412EP, 412CF HIGH FORWARD CROSSTUBE Revision B AB412, AB412EP UH-1B, UH-1H, SW204, SW205 b. Remove the Supports from the Crosstube Assembly. Use of a heat gun to soften the sealant may facilitate removal. NOTE Inspect the inner surface coating material for deterioration in accordance with Instructions for Continued Airworthiness AA-01136. Replace Supports if required. E.2 Cleaning and Preparation 1. Remove aged sealant by scraping with a sharp piece of plastic. Finish by lightly sanding with 400 grit abrasive cloth or paper in the longitudinal direction of the crosstube. WARNING DO NOT SAND CROSSTUBE IN A CIRCUMFERENTIAL DIRECTION. 2. Prepare crosstube by chemically removing crosstube paint and primer to top of saddles. See Figure 3. a. Apply MIL-R-81294, Type I or II chemical paint remover with a brush and allow it to set from 15 to 45 minutes to soften paint. b. Using a stiff fiber brush and clean water, rinse paint from crosstube. If required, use abrasive pad (Scotch-Brite, Type A) and MIL-R-81294, Type I or Il chemical paint remover to aid in lifting paint. Brush crosstube with abrasive pad in the longitudinal direction, using care so as not to abrade crosstube metal surface. WARNING DO NOT SAND CROSSTUBE IN A CIRCUMFERENTIAL DIRECTION. c. Rinse part clean with clean water and dry thoroughly. Reapplication of chemical paint remover may be required to ensure that paint and primer is completely removed so that the (bare) metal surface of the cross tube is clearly visible. 3. When parts are not to be processed immediately after cleaning, apply corrosion preventive oil, to all parts to protect against corrosion. Wrap parts in barrier material and secure with tape. AERONAUTICAL ACCESSORIES, INC. August 12, 2009 Page 12 of 16 ### Page 13 (OCR) 205A, 205A-1, 205B, 212 ALERT SERVICE BULLETIN ASB No. AA-08055 412, 412EP, 412CF HIGH FORWARD CROSSTUBE Revision B AB412, AB412EP UH-1B, UH-1H, SW204, SW205 E.3 Inspection 1. Inspect crosstube using fluorescent penetrant method per ASTM E1417, Type I, Method B, C, or D, Level 2, in accordance with Bell Helicopter Standard Practices Manual (BHT-ALL-SPM). Refer to BHT-ALL-SPM for fluorescent penetrant inspection procedures. 2. Damage limits are specified in Instructions for Continued Airworthiness, report number AA-01136 and the applicable model Bell Helicopter Maintenance Manual. E.4 Repair 1. Repair damage within repairable limits in accordance with Instructions for Continued Airworthiness report number AA-01136. 2. Refinish crosstube by applying MIL-PRF-85582 primer and MIL-PRF-85285 paint (or equivalent) per manufacturer instructions to the stripped areas. The areas to be inspected per Part B should be masked to omit MIL-PRF-85285 paint as shown in Figure 1. Paint inspection areas with MIL-PRF-85285 Type I Gloss Clear coat as described in Part B of this bulletin. E.S Assembly Instructions 1. Assemble both Crosstube Clamp Assemblies in accordance with Instructions for Continued Airworthiness report number AA-01136. 2. Install Crosstube Assembly to aircraft in accordance with Instructions for Continued Airworthiness report number AA-01136. 3. Annotate aircraft records to indicate that Part E of this bulletin has been accomplished; and return aircraft to service. PART F TOWING AIRCRAFT Helicopter towing operations must be conducted in accordance with applicable model Bell Helicopter Maintenance Manual. Manufacturer towing requirements are applicable to any aircraft being towed with weight on gear. This includes towing aircraft with ground handling wheels installed and aircraft resting on moveable platforms. CAUTION Failure to follow manufacturer towing instructions may result in crosstube damage and/or failure. AERONAUTICAL ACCESSORIES, INC. August 12, 2009 Page 13 of 16 ### Page 14 (OCR) 205A, 205A-1, 205B, 212 ALERT SERVICE BULLETIN ASB No. AA-08055 412, 412EP, 412CF HIGH FORWARD CROSSTUBE Revision B AB412, AB412EP UH-1B, UH-1H, SW204, SW205 40 - 2.5} 13.970 13.940 212-321-103 FORWARD CROSSTUBE ASSEMBLY SYMMETRY ARC LENGTH CLEARCOAT / INSPECTION AREA 2.00 LEFT SIDE AND RIGHT SIDE OF TUBE 605-005-121 DECAL 45° 40 VIEW D-D VIEW E-E FIGURE 1 - CLEAR COAT AND INSPECTION AREA (NOT TO SCALE) AERONAUTICAL ACCESSORIES, INC. August 12, 2009 Page 14 of 16 ### Page 15 (OCR) 205A, 205A-1, 205B, 212 ALERT SERVICE BULLETIN ASB No. AA-08055 412, 412EP, 412CF HIGH FORWARD CROSSTUBE Revision B AB412, AB412EP UH-1B, UH-1H, SW204, SW205 WEIGHT REMOVED • PLUMBLINE 57.0 TO 59.0 IN (1447.8 TO 1498.6 mm) 57.0 TO 59.0 IN (1447.8 TO 1488.6 mm) - 118.0 INCHES MAX. (2997.2 mm) Checking landing gear crosstube deflection Forward Crosstube (High) MIN MAX Part Number Model Effectivity in. mm in. mm 212-321-103 205A, 205A-1, 205B, 212, 412, 57.00 1448 59.00 1499 412EP, 412CF, AB412, AB412EP, UH-1B, UH-1H, SW204, SW205 FIGURE 2 - HIGH LANDING GEAR DEFLECTION LIMITS REMOVE PAINT/PRIMER FROM CROSSTUBE, BOTH SIDES - HIGH FWD CROSSTUBE B.L. 0.0 FIGURE 3 - PAINT REMOVAL AREA AERONAUTICAL ACCESSORIES, INC. August 12, 2009 Page 15 of 16 ### Page 16 (OCR) 205A, 205A-1, 205B, 212 ALERT SERVICE BULLETIN ASB No. AA-08055 412, 412EP, 412CF HIGH FORWARD CROSSTUBE Revision B AB412, AB412EP UH-1B, UH-1H, SW204, SW205 REASON FOR REMOVAL REMOVAL DATA COMPONENT CYCLES SINCE REMAINING TO RETIREMENT REMOVED AT A/C HOURS ACCUMULATED TAKE-OFF / LANDINGS HISTORICAL SERVICE RECORD FWD CROSSTUBE ASSEMBLY SERVICE LIFE (TAKE-OFF/LANDINGS) COMPONENT CYCLES SINCE DATE NEW TIME/DATE INSTALLATION DATA INSTALLED ON BY (ACTIVITY) INSTALLED AT A/C HOURS REMAINING TO ACCUMULATED TAKE-OFF / LANDINGS RETIREMENT Component Name: Part Number: Serial Number: A/C NUMBER TIME/DATE FIGURE 4 - HISTORICAL SERVICE RECORD AERONAUTICAL ACCESSORIES, INC. August 12, 2009 Page 16 of 16 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. 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