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 212 Information Letters

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Date Posted 
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View/DownloadIL_212-20-71.pdf20-Aug-20MAIN TRANSMISSION SUPPORT CASE MOUNTS, NEW INSPECTION REQUIREMENTS
View/DownloadIL_212-20-70.pdf16-Jul-20GLOBAL ALTERNATE METHOD OF COMPLIANCE (AMOC) FOR AIRWORTHINESS DIRECTIVE (AD) 2020-12-10.
View/DownloadIL_212-20-69.pdf13-Jul-20INSTALLATION OF ALPINE AEROTECH LP (AAL) CREW BARRIER KIT
View/DownloadIL_212-14-68.pdf25-Jul-14GLOBAL ALTERNATE METHOD OF COMPLIANCE (AMOC) FOR AIRWORTHINESS DIRECTIVE (AD) 2014-12-04.
View/DownloadIL_212-14-67.pdf10-Jul-14MAIN ROTOR GRIPS 204-011-121-009/-121 LIFE LIMITATION PER FAA AD 2014-12-04.
View/DownloadIL_212-13-66.pdf07-Jan-13REMOVAL OF ZINC CHROMATE PRIMER STRIPES AS AN OVERHEAT CONDITION INDICATION.
View/DownloadIL_212-12-65.pdf10-Sep-12ENGINE NII (NF) GOVERNOR POSSIBLE ANOMALY
View/DownloadIL_212-11-INDEX.pdf01-Mar-12INFORMATION LETTER INDEX
View/DownloadIL_212-11-64.pdf26-Apr-11FUEL FILTER LIGHT FLICKERING
View/DownloadIL_212-04-55_Rev_B.pdf14-Sep-10BLR FastFin and STRAKE INSTALLATION ON ALL BELL 204,205, 205B, AND 212 MODEL HELICOPTERS.
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