Hawker 125 (Series 1 through 900XP)


-2 Turn and Bank Indication



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20-2

Turn and Bank Indication




















1)

Rate of Turn Indication

C

-

1

Turn function of one instrument may be inoperative provided flight is conducted in VMC conditions only.













C

-

0

May be inoperative provided standby attitude indicator is operative.






20-3

Attitude Heading Reference System (AHRS) / Inertial Reference System (IRS)




















1)

Primary AHRS/IRS

B

2

1

(O) One may be inoperative provided:

  1. Standby attitude reference system is selected and verified operative,

  2. AFM limitations are observed, and

  3. Autopilot (A/P) is not used.




  1. Select and confirm operation of Standby Attitude Reference System.

  2. Autopilot is not used.

2)

Standby AHRS/ IRS

C

1

0

(O) May be inoperative provided both primary AHRS/IRS systems are verified operative.




Select and confirm Primary Attitude Reference System.

20-4

Compass and Attitude/AHRS Changeover/ Reversion Switches


C

2

0

(O) May be inoperative provided:

  1. Associated instruments are operative from independent sources, and

  2. Inoperative switches are not moved during flight.




  1. Confirm associated instruments are operative from independent sources, and

  2. Inoperative switches are placarded ‘INOP’ and not moved during flight.

  3. Confirm the switch is not in the cross transfer position, and in the event of an AHRS failure the pilot with the operative instruments will be the flying pilot. No attempt should be made to cross transfer data.

1)

AHRS Reversion Switch Lights (Honeywell)

C

6

0

(O) Switch backlight and annunciation, left and right, may be inoperative provided associated annunciation on the PFD is operative.




Confirm PFD annunciation each time affected switch is moved.

2)

AHS REV Transfer Switch Lights

(Pro Line 21)



C

4

0

(O) Switch backlight and annunciation, left and right, may be inoperative provided associated annunciation on the PFD is operative.




Confirm PFD annunciation each time affected switch is moved.

20-5


***

Angle of Attack System (Series 1 thru 700)


C

-

0










***

Teledyne AOA System (BAe-125-800 & Hawker 800 Only)


C

1

0









20-6

Standby Attitude Indicator











Incorporated into Item 34-20-9, Revision 6.







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