Airworthiness directives › 2018-19-02
AD 2018-19-02 Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A. (CASA)) Airplanes
Models named: C-212-CB, C-212-CC, C-212-CD, C-212-CE, C-212-DF. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to Airbus Defense and Space S.A. Model C-212-CB, C-212-CC, C-212-CD, C-212-CE, and C-212-DF airplanes; manufacturer serial numbers 009, 034, 039, 089, 092, 119, 125, 133, 138, 149, 150, 154, 159, 161, 162, 164, 165, 167 through 169 inclusive, 171, 172, 174, 175, 178, 180, 181, 190, 192, 193, 195, 209 through 212 inclusive, 214 through 216 inclusive, 219 through 222 inclusive, 224 through 227 inclusive, 229, 235, 236, 238, 240, 242, 247 through 257 inclusive, 261 through 263 inclusive, 265, 272 through 282 inclusive, 286, 287, 289 through 292 inclusive, 294, 308, 311, 320, 322 through 324 inclusive, 328, 332, 336, 343, 347 through 349 inclusive, 356, 359, 363, 371, 379, 393, 397, 398, 405, 410, 411, 413, 465, 470, 472, 474, 475, 478, and 480 through 482 inclusive; certificated in any category; except airplanes modified in accordance with the Accomplishment Instructions of EADS-CASA Service Bulletin SB-212-27-0057, dated May 21, 2014.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
(1) For the purposes of this AD, an affected part is defined as a rudder pedal support box having Part Number (P/N) 212-46195.1 and shaft P/N 212-46120-20. (2) For the purposes of this AD, a discrepancy or defect of the rudder pedal support box P/N 212-46195.1 is defined as any crack or deformation on any welded area. (3) For the purposes of this AD, a discrepancy or defect of the shaft P/N 212-46120-20 is defined as any crack or deformation.
Unsafe condition
This AD was prompted by reports of failures of the rudder pedal control system support. We are issuing this AD to address failure of the rudder pedal control system, which could result in reduced controllability of the airplane.
Affected ADs
This AD affects AD 2017-19-08, Amendment 39-19038 (82 FR 43835, September 20 2017) (“AD 2017-19-08”).
Read the original on the Federal Register →
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1