-10-02 Aileron Position Indication B 2 1 (O) One may be inoperative provided | aileron control is visually verified prior to | each flight. | -11-01 Aileron Trim Tab Position | Indicator / Indication | -02 Indicator Cover D 1 0 May be missing, or damaged provided | *** (Units -0001 thru -0182 aileron / rudder trim indicator is readable. | incorporating SB750-27-41 | and units -0183 thru -0500) | -20-01 Rudder Pedal Adjustment B 4 2 (M) (O) Two may be inoperative provided: | System Two pedal adjustments are not | inoperative at same pilot station, | Affected is positioned in a | detent and adjustment mechanism | is secured from movement, | Unaffected pedal is adjusted to | match affected pedal, and | Crewmember seated at affected | station verifies full control | movement and brake application is | available while restrained, prior to | each flight. | -20-02 Rudder Position Indication A 1 0 (O) May be inoperative provided: | (Lower rudder) Rudder control is visually verified | prior to each flight, and | Repairs are made within three | flight cycles. | -30-01 Elevator Position Indication B 2 1 (O) One may be inoperative provided | elevator control is visually verified prior to | each flight. | |
-10-02 Aileron Position Indication B 2 1 (O) One may be inoperative provided aileron control is visually verified prior to each flight. | | | -11-01 Aileron Trim Tab Position Indicator / Indication | | -02 *** Indicator Cover (Units -0001 thru -0182 incorporating SB750-27-41 and units -0183 thru -0500) D 1 0 May be missing, or damaged provided aileron / rudder trim indicator is readable. | | | | -20-01 Rudder Pedal Adjustment System B 4 2 (M) (O) Two may be inoperative provided: Two pedal adjustments are not inoperative at same pilot station, Affected is positioned in a detent and adjustment mechanism is secured from movement, Unaffected pedal is adjusted to match affected pedal, and Crewmember seated at affected station verifies full control movement and brake application is available while restrained, prior to each flight. | | | | | | | | | | | | | -20-02 Rudder Position Indication (Lower rudder) A 1 0 (O) May be inoperative provided: Rudder control is visually verified prior to each flight, and Repairs are made within three flight cycles. | | | | | -30-01 Elevator Position Indication B 2 1 (O) One may be inoperative provided elevator control is visually verified prior to each flight. | | | |