Hawker 125 (Series 1 through 900XP)


-5 Non-Stabilized Magnetic Compass (Standby)



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9-5

Non-Stabilized Magnetic Compass (Standby)


B

1

0

May be inoperative provided any combination of three gyro or INS (IRU) stabilized compass systems are operative.













B

1

0

(O) May be inoperative provided:

  1. Any combination of two gyro OR INS (IRU) stabilized compass systems are operative, and

  2. Airplane is operated with dual independent navigation capability and under positive radar control by ATC, on the enroute portion of the flight.




  1. Confirm any combination of three gyro or INS (IRU) stabilized compass systems are operative,
    OR

  2. Confirm any combination of two gyro or INS (IRU) stabilized compass systems are operative, and

  3. Airplane is operated with dual independent navigation systems, and

  4. Airplane is operated under positive enroute ATC RADAR control.







B

1

0

(O) May be inoperative for flights that are entirely within areas of magnetic unreliability provided at least two stabilized directional gyro systems are operative and used in conjunction with approved free gyro navigation techniques.




Flights that are entirely within areas of magnetic unreliability may be flown provided at least two stabilized directional gyro systems are operative and used in conjunction with approved free gyro navigation techniques.

10-1

VMO/MMO Aural Warnings


B

2

1
















B

2

0

(O) May be inoperative provided:

  1. Both Mach/Airspeed indicators at both pilot positions are operative,

  2. If installed, Ventral Tank is either empty or EMPTY/FULL indicator is operative, and

  3. VMO/MMO Aircraft Flight Manual (AFM) limitations are observed.




  1. For air data computer driven indicators, confirm that both left and right Mach/Airspeed indicators are not flagged, and

  2. For aircraft equipped with Ventral Fuel Tank, tank must either not be filled or EMPTY/ FULL indicator must be verified operative.

  3. Observe AFM VMO/MMO limitations.

10-2

Altitude Alerting System


A

-

0

(O) May be inoperative provided:

  1. Autopilot with altitude capture and altitude hold is operative,

  2. Enroute operations do not require its use, and

  3. Repairs are made within three flight days.

Note

RVSM is not authorized.






  1. Autopilot with altitude capture and altitude hold is operative.

  2. Flight planning must avoid use of RVSM airspace.

1)

Aural Alert

C

-

0

May be inoperative provided:

Visual alert is operative, and

Autopilot with altitude capture and hold is operative.








2)

Visual Alert

C

-

0

May be inoperative provided:

Aural alert is operative, and



Autopilot with altitude capture and hold is operative.






10-3

Altimeter Vibrators




















1)

Servo Pneumatic

C

2

1

One may be inoperative provided associated air data computer is operative.







2)

Pneumatic

C

2

1

One may be inoperative provided VMC exists at departure and arrival airports.







3)

One Pneumatic and One Servo Pneumatic

C

2

1

Servo Pneumatic may be inoperative provided:

  1. Associated air data computer is operative, and

  1. VMC exists at departure and arrival airports.







4)

Standby Altimeter Vibrator (With Electric Altimeters Installed)

C

1

0

May be inoperative provided VMC exist at both departure and arrival airports.







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