Widespread Fatigue Damage (WFD)

Considerations Related to FAA Supplemental Structural Inspection Programme (SSIP)

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Supplemental Structural Inspection Programme

November 03, 2023

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Sofema Aviation Services (SAS) www.sassofia.com considers the development of the Supplemental Structural Inspection SSI requirements Introduction On 14 May 1977, a Boeing 707 (Cargo Aircraft) operated by UK Operator Dan Air Services Ltd. crashed some 3 miles short of the runway at Lusaka International Airport. The Boeing 707 was certified failsafe, however, the Model 707-300 flown by Dan Air…

ICAO Structural Integrity Expectations I.A.W. ICAO Doc 9769 Airworthiness Manual

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Structural Integrity

February 21, 2023

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Steve Bentley FRAeS, CEO of Sofema Aviation Services (SAS) considers the obligation of the State & Operator to demonstrate compliance with Aircraft Structural Integrity Obligations. How to Check Operator Compliance with Aircraft Structural Obligations What is the difference between a Design Service Goal (DSG) & Limit of Validity (LOV) Introduction – Compliance with Structural Integrity…

Upscale your knowledge regarding FAA & EASA Corrosion Protection and Control Program with the new SAS training

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Polish your aviation knowledge with the new SAS trainig – FAA & EASA Corrosion Protection and Control Program

October 27, 2021

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Sofema Aviation Services (SAS) www.sassofia.com is delighted to share that a new course regarding FAA & EASA Corrosion Protection and Control Program is now a part of our training portfolio: FAA & EASA Corrosion Protection and Control Program – 2 Days Available as a Classroom or Webinar training – Register at team@sassofia.com What is the course about? The aim…

EASA Part 26 – CS 26 Definitions & Terms Used Ref – Regulation (EU) 2020/1159

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EASA Part 26 – CS 26 Definitions & Terms Used Ref – Regulation (EU) 2020/1159

October 05, 2021

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EASA Part 26 – CS 26 Definitions & Terms Used Ref – Regulation (EU) 2020/1159. Review by Sofema Aviation Services (SAS) www.sassofia.com Introduction Regulation (EU) nÂş 2015/640 establishes additional airworthiness specifications for operations and contains two annexes. Annex I (Part 26), Subpart A, is devoted to general provisions on the appropriate authority, temporarily inoperative equipment…