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 205/205A1 Information Letters

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View/DownloadIL_205-21-44.pdf04-Feb-21TAIL ROTOR BLADES 212-010-750-ALL LEAK CHECK.
View/DownloadIL_205-20-43.pdf20-Aug-20MAIN TRANSMISSION SUPPORT CASE MOUNTS, NEW INSPECTION REQUIREMENTS
View/DownloadIL_205-20-42.pdf16-Jul-20GLOBAL ALTERNATE METHOD OF COMPLIANCE (AMOC) FOR AIRWORTHINESS DIRECTIVE (AD) 2020-12-10.
View/DownloadIL_205-20-41.pdf13-Jul-20INSTALLATION OF ALPINE AEROTECH LP (AAL) CREW BARRIER KIT
View/DownloadIL_205-13-40.pdf07-Jan-13REMOVAL OF ZINC CHROMATE PRIMER STRIPES AS AN OVERHEAT CONDITION INDICATION.
View/DownloadIL_205-11-INDEX.pdf01-Mar-12INFORMATION LETTER INDEX
View/DownloadIL_205-04-35_Rev_B.pdf14-Sep-10BLR FastFin and STRAKE INSTALLATION ON ALL BELL 204,205, 205B, AND 212 MODEL HELICOPTERS.
View/DownloadIL205-10-39_Rev_A.pdf09-Apr-10DERIVED EMPTY WEIGHT CLARIFICATIONS.
View/DownloadIL_205-10-39.pdf19-Mar-10DERIVED EMPTY WEIGHT CLARIFICATIONS
View/DownloadIL_205-08-38_Rev_A.pdf23-Jul-08Grip Assembly P/N 204-011-121-125, Introduction Of
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