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| View/Download | IL_205B-21-38.pdf | 04-Feb-21 | TAIL ROTOR BLADES 212-010-750-ALL LEAK CHECK. |
| View/Download | IL_205B-20-27.pdf | 20-Aug-20 | MAIN TRANSMISSION SUPPORT CASE MOUNTS, NEW INSPECTION REQUIREMENTS |
| View/Download | IL_205B-20-26.pdf | 16-Jul-20 | GLOBAL ALTERNATE METHOD OF COMPLIANCE (AMOC) FOR AIRWORTHINESS DIRECTIVE (AD) 2020-12-10. |
| View/Download | IL_205B-20-25.pdf | 13-Jul-20 | INSTALLATION OF ALPINE AEROTECH LP (AAL) CREW BARRIER KIT |
| View/Download | IL_205B-14-24.pdf | 25-Jul-14 | GLOBAL ALTERNATE METHOD OF COMPLIANCE (AMOC) FOR AIRWORTHINESS DIRECTIVE (AD) 2014-12-04. |
| View/Download | IL_205B-14-23.pdf | 10-Jul-14 | MAIN ROTOR GRIPS 204-011-121-009/-121 LIFE LIMITATION PER FAA AD 2014-12-04. |
| View/Download | IL_205B-13-22.pdf | 07-Jan-13 | REMOVAL OF ZINC CHROMATE PRIMER STRIPES AS AN OVERHEAT CONDITION INDICATION. |
| View/Download | IL_205B-11-INDEX.pdf | 01-Mar-12 | INFORMATION LETTER INDEX |
| View/Download | IL_205B-04-18_Rev_B.pdf | 14-Sep-10 | BLR FastFin and STRAKE INSTALLATION ON ALL BELL 204,205, 205B, AND 212 MODEL HELICOPTERS. |
| View/Download | IL_205B-08-21_Rev_A.pdf | 23-Jul-08 | Grip Assembly P/N 204-011-121-125, Introduction Of |
205B Information Letters