| right-click on any row for available actions | Showing documents 361-370 from a total of 498 | Show documents per page | Show only documents in status: |
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Affected rules & codes
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RMT.0119 (27&29.003) | Yawing Conditions (Rotorcraft) | NPA 2013-21 | CS-27 CS-29 CS-VLR | |||||||||||||||||||||||||||||||||||||||||||||||||
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RMT.0069 (26.002) | Seat crashworthiness improvement on large aeroplanes — Dynamic testing 16g | NPA 2013-20 | CS-26 Part-26 | |||||||||||||||||||||||||||||||||||||||||||||||||
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RMT.0108 (21.039(g)) | CSs and GM for the development of the definition of scope of the aircraft validation source data to support the objective qualification of simulator(s) associated to the pilot type rating training (simulator data) — CS-SIMD | NPA 2013-17 | CS-FSTD(A) CS-FSTD(H) Part-21 | |||||||||||||||||||||||||||||||||||||||||||||||||
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RMT.0583 (MDM.003C) | Lead Flight Test Engineer Licence | A-NPA 2013-16 | Basic regulation | |||||||||||||||||||||||||||||||||||||||||||||||||
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RMT.0287 (MED.001 (a)) RMT.0288 (MED.001 (b)) | Update of Part-MED (Annex IV to Commission Regulation (EU) No 1178/2011) and Update of Acceptable Means of Compliance and Guidance Material to Part-MED (ED Decision 2011/015/R) | NPA 2013-15 | Part-MED Part-MED AMC/GM | |||||||||||||||||||||||||||||||||||||||||||||||||
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RMT.0518 | Safety Key Performance Indicators (SKPIs) (ATM performance IR) | NPA 2013-14 | SES | |||||||||||||||||||||||||||||||||||||||||||||||||
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RMT.0435 (OPS.087 (b)) RMT.0441 (OPS.089 (c)) | SACA & SAFA | NPA 2013-13 | Part-ARO AMC/GM | |||||||||||||||||||||||||||||||||||||||||||||||||
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RMT.0500 | Regular update of CS-25 | NPA 2013-11 | CS-25 | |||||||||||||||||||||||||||||||||||||||||||||||||
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RMT.0409 (OPS.093(a)) RMT.0410 (OPS.093(b)) | Helicopter offshore operations | NPA 2013-10 | Part-ARO Part-ARO AMC/GM Part-CAT Part-CAT AMC/GM Part-SPA Part-SPA AMC/GM | |||||||||||||||||||||||||||||||||||||||||||||||||
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RMT.0225 (MDM.028(a)) | Ageing aircraft structures | NPA 2013-07 | AMC 20-20 CS-25 CS-26 Part-21 Part-26 Part-M AMC/GM | |||||||||||||||||||||||||||||||||||||||||||||||||
