41![LESSONS LEARNED BY ONE AEROSPACE STRUCTURES ENGINEER IN A 40-YEAR CAREER by Dr. L. J. Hart-Smith LESSONS LEARNED BY ONE AEROSPACE STRUCTURES ENGINEER IN A 40-YEAR CAREER by Dr. L. J. Hart-Smith](https://www.pdfsearch.io/img/baac9b64e8e61f9aa0a56669f3d296a6.jpg) | Add to Reading ListSource URL: www.raes.org.auLanguage: English - Date: 2014-11-01 01:51:19
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42![Photographs of Damaged Fuselage Appendix 17 Photographs of Damaged Fuselage Appendix 17](https://www.pdfsearch.io/img/8d1a71512a015ce19d71fadf33ceb8b9.jpg) | Add to Reading ListSource URL: www.cad.gov.hk- Date: 2013-10-03 20:16:53
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43![Microsoft Word - Edge48manual Microsoft Word - Edge48manual](https://www.pdfsearch.io/img/7c4fabfc7bc0162715bc7b1104e7933d.jpg) | Add to Reading ListSource URL: www.3dhobbyshop.comLanguage: English - Date: 2014-12-18 16:01:12
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44![Background Information about the Dornier[removed]More than 1,500 examples of the Dornier 17 medium bomber were built. The twin engine, twin fin configuration together with the narrow fuselage and shouldermounted engines ga Background Information about the Dornier[removed]More than 1,500 examples of the Dornier 17 medium bomber were built. The twin engine, twin fin configuration together with the narrow fuselage and shouldermounted engines ga](https://www.pdfsearch.io/img/9dce0f8a7e42b6a1b8236b307f702567.jpg) | Add to Reading ListSource URL: www.rafmuseum.org.ukLanguage: English - Date: 2013-06-01 17:45:50
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45![VAN’S AIRCRAFT, INC[removed]NE Keil Road, Aurora, Oregon, USA[removed]PHONE[removed] • FAX[removed] • www.vansaircraft.com • [removed] Service Bulletin SB[removed] VAN’S AIRCRAFT, INC[removed]NE Keil Road, Aurora, Oregon, USA[removed]PHONE[removed] • FAX[removed] • www.vansaircraft.com • [removed] Service Bulletin SB[removed]](https://www.pdfsearch.io/img/2131d337d0b8d20aed767f0f2ae95ccf.jpg) | Add to Reading ListSource URL: www.vansaircraft.comLanguage: English - Date: 2009-01-28 14:13:21
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46![Step 1: Rivet nutplates to the F-1004B, F-1004D-L and - R Center Section Bulkheads as shown in Figure 2. LEAVE OPEN LEAVE OPEN Step 1: Rivet nutplates to the F-1004B, F-1004D-L and - R Center Section Bulkheads as shown in Figure 2. LEAVE OPEN LEAVE OPEN](https://www.pdfsearch.io/img/f64758e6024f2d88d7777ec81c491bd3.jpg) | Add to Reading ListSource URL: www.vansaircraft.comLanguage: English - Date: 2009-01-28 14:09:59
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47![cult and slow process on the fire ground to reposition the penetrator in the correct location. It is also necessary to keep the hardened tip sharpened for an easy purchase on the fuselage skin. When targeting the fuselag cult and slow process on the fire ground to reposition the penetrator in the correct location. It is also necessary to keep the hardened tip sharpened for an easy purchase on the fuselage skin. When targeting the fuselag](https://www.pdfsearch.io/img/50c20bc3593940d568eea229c25d4fdd.jpg) | Add to Reading ListSource URL: www.aviationfirejournal.comLanguage: English - Date: 2015-01-11 13:43:22
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48![though external fires are effectively extinguished, secondary fires within the aircraft fuselage are difficult to control with existing equipment and procedures. Upon arrival to any accident site in which a post crash fu though external fires are effectively extinguished, secondary fires within the aircraft fuselage are difficult to control with existing equipment and procedures. Upon arrival to any accident site in which a post crash fu](https://www.pdfsearch.io/img/09840d1cfba6f0b000398b4cda00d3e9.jpg) | Add to Reading ListSource URL: www.aviationfirejournal.comLanguage: English - Date: 2015-01-11 13:43:29
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49![SERVICE BULLETIN Date issued: [removed]Number: [removed]Subject: RV-4 Rear Sear Bulkhead Reinforcement Synopsis: The RV-4 rear seatback may, under adverse flight conditions, have enough load applied by the rear seat passeng SERVICE BULLETIN Date issued: [removed]Number: [removed]Subject: RV-4 Rear Sear Bulkhead Reinforcement Synopsis: The RV-4 rear seatback may, under adverse flight conditions, have enough load applied by the rear seat passeng](https://www.pdfsearch.io/img/9e7f2f14a62abd9371416eae7013fcad.jpg) | Add to Reading ListSource URL: www.vansaircraft.comLanguage: English - Date: 2009-01-28 14:13:42
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50![3/8 DIA. DRIFT PIN 2 PLACES Step 1: Slide the wing spar (left shown) into the fuselage and temporarily pin as shown in Figure 1. 3/8 DIA. DRIFT PIN 2 PLACES Step 1: Slide the wing spar (left shown) into the fuselage and temporarily pin as shown in Figure 1.](https://www.pdfsearch.io/img/e63c797d382b36e2af416174931f3b11.jpg) | Add to Reading ListSource URL: www.vansaircraft.comLanguage: English - Date: 2009-01-28 14:10:02
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