49. GPS (on Aircraft with C 2 0 (O) May be inoperative provided operations do | *** STC ST02970NY, not require its use. | ST01408WI-D, | ST01615WI-D, or | ST02967NY) | NOTE: ADS-B Out function will not be available | when both GPS are inoperative on | aircraft with STC ST02972NY or | ST02973NY. | 50. Cursor Control Display A 2 1 Copilot position may be inoperative provided: | *** (CCD) (Only on Aircraft Reversion Switch Panels (RSP) are | with STC ST03371NY) operative, and | Repairs are made within 3 flight days. | NOTE: If bezel buttons are used, displays will | revert back to legacy mode on aircraft | with ST03371NY. | 51. Incidence Meter D 1 0 (M) May be inoperative provided associated *** (M0051) circuit breakers are pulled and collared.
49. *** GPS (on Aircraft with STC ST02970NY, ST01408WI-D, ST01615WI-D, or ST02967NY) C 2 0 (O) May be inoperative provided operations do not require its use. | | | | | NOTE: ADS-B Out function will not be available when both GPS are inoperative on aircraft with STC ST02972NY or ST02973NY. | | | | 50. *** Cursor Control Display (CCD) (Only on Aircraft with STC ST03371NY) A 2 1 Copilot position may be inoperative provided: Reversion Switch Panels (RSP) are operative, and Repairs are made within 3 flight days. | | | | NOTE: If bezel buttons are used, displays will revert back to legacy mode on aircraft with ST03371NY. | | | 51. *** Incidence Meter (M0051) D 1 0 (M) May be inoperative provided associated circuit breakers are pulled and collared.
da-900_rev%2010.docx