Search report text, read a short matching passage, then open the source page.
Exact phrases match first; otherwise all words must occur close together. Six excerpts maximum. Text extraction cannot search image-only charts. Warsaw uses a report transcription with missing figures and appendices.
16 matching PDF pages. Showing 6 short source excerpts. Open the document for full context.
Printed page label not indexed. PDF page 26.
fatigue cracking." The SB program outlined "the minimum requirements for maintaining the structural integrity of the lap joints." Corrosion and fatigue inspection details and intervals and repair instructions were presented. Operator compliance was not made mandatory by theOpen official document at PDF page 26NTSB AAR-89/03: Aloha Airlines flight 243, N73711
Printed page label not indexed. PDF page 28.
Items (SSI) that have damage or fatigue characteristics that could affect the airplane's structural integrity. Should cracking occur, the examination of SSIs allows operators to detect fatigue damage before the airplane's residual strength falls below the regulatory fail-saOpen official document at PDF page 28NTSB AAR-89/03: Aloha Airlines flight 243, N73711
Printed page label not indexed. PDF page 40.
requirement was to allow for failure within two frame bays without compromising the structural integrity of the fuselage. Boeing demonstrated the ability of the fuselage to fail safely within two frame bays during certification of the airplane by "guillotine" testsOpen official document at PDF page 40NTSB AAR-89/03: Aloha Airlines flight 243, N73711
Printed page label not indexed. PDF page 42.
requirement for a structural reassessment or audit and the development of a continuing structural integrity program for older transport airplanes. The air transport airframe manufacturers developed the required programs, utilizing different concepts, to achieve continuedOpen official document at PDF page 42NTSB AAR-89/03: Aloha Airlines flight 243, N73711
Printed page label not indexed. PDF page 48.
engineering representatives and engineers from Boeing's Customer Support group to. assure structural integrity. In addition, Boeing has maintained an on-site customer support office manned by a Boeing customer service representative since 1969. Aloha has an effective programOpen official document at PDF page 48NTSB AAR-89/03: Aloha Airlines flight 243, N73711
Printed page label not indexed. PDF page 67.
knowledge, or the required programs to meet its responsibility to ensure the continued structural integrity of its airplanes. 2.5 FAA Responsibilities 2.5.1 Issuance and Clarity of Airworthiness Directives In-service fatigue cracking in a disbonded area of a B-737_ lap joOpen official document at PDF page 67NTSB AAR-89/03: Aloha Airlines flight 243, N73711