| Clear Filter | | | |
| View/Download | IL_212-24-75.pdf | 29-Jan-24 | TRANSITION TO KAMATICS KAFLEX MAIN DRIVE SHAFT |
| View/Download | IL_212-21-73.pdf | 04-Feb-21 | TAIL ROTOR BLADES 212-010-750-ALL LEAK CHECK. |
| View/Download | IL_212-20-72.pdf | 16-Oct-20 | INTRODUCTION OF BELL MISSIONLINK WEB SITE AND MISSIONLINK
EDGE SOFTWARE |
| View/Download | IL_212-20-71.pdf | 20-Aug-20 | MAIN TRANSMISSION SUPPORT CASE MOUNTS, NEW INSPECTION REQUIREMENTS |
| View/Download | IL_212-20-70.pdf | 16-Jul-20 | GLOBAL ALTERNATE METHOD OF COMPLIANCE (AMOC) FOR AIRWORTHINESS DIRECTIVE (AD) 2020-12-10. |
| View/Download | IL_212-20-69.pdf | 13-Jul-20 | INSTALLATION OF ALPINE AEROTECH LP (AAL) CREW BARRIER KIT |
| View/Download | IL_212-14-68.pdf | 25-Jul-14 | GLOBAL ALTERNATE METHOD OF COMPLIANCE (AMOC) FOR AIRWORTHINESS DIRECTIVE (AD) 2014-12-04. |
| View/Download | IL_212-14-67.pdf | 10-Jul-14 | MAIN ROTOR GRIPS 204-011-121-009/-121 LIFE LIMITATION PER FAA AD 2014-12-04. |
| View/Download | IL_212-13-66.pdf | 07-Jan-13 | REMOVAL OF ZINC CHROMATE PRIMER STRIPES AS AN OVERHEAT CONDITION INDICATION. |
| View/Download | IL_212-12-65.pdf | 10-Sep-12 | ENGINE NII (NF) GOVERNOR POSSIBLE ANOMALY |
212 Information Letters