-00B (TAWS or TCAS II required) A 1 0 (M) May be inoperative provided: | (Units -0001 thru -0500) Radio altimeter is deactivated, | Approach minimums or operating | procedures do not require its use, | Basic TAWS modes are | considered inoperative (Refer to | item 34-44-03), | TCAS II is considered inoperative | (Refer to item 34-45-01), | Autothrottle system, if installed, is | considered inoperative, and | Repairs are made within two flight | days. | | NOTE 1: Landing gear warning system | will function differently without radio | altimeter input. Landing gear warning | may occur at higher altitudes above | ground with flaps extended. | | NOTE 2: Landing Operations Inhibit | (LOPI) operation will be affected. LOPI | may not activate during approach or | | (Continued) Radio Altimeter System -44-01 (Continued)
-00B (TAWS or TCAS II required) (Units -0001 thru -0500) A 1 0 (M) May be inoperative provided: Radio altimeter is deactivated, Approach minimums or operating procedures do not require its use, Basic TAWS modes are considered inoperative (Refer to item 34-44-03), TCAS II is considered inoperative (Refer to item 34-45-01), Autothrottle system, if installed, is considered inoperative, and Repairs are made within two flight days. NOTE 1: Landing gear warning system will function differently without radio altimeter input. Landing gear warning may occur at higher altitudes above ground with flaps extended. NOTE 2: Landing Operations Inhibit (LOPI) operation will be affected. LOPI may not activate during approach or | | | | | | | | | | | | | | | | | | | | | | | | (Continued) -44-01 Radio Altimeter System (Continued)
ce-750_rev%206.docx