Hawker 125 (Series 1 through 900XP)


-5 VHF Navigation (VOR/ILS) System



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50-5

VHF Navigation (VOR/ILS) System


C

-

-

As required by FAR.






50-6


***

Global Positioning System (GPS)


C

-

0

As required by FAR.






50-7


***

Traffic Advisory System (B.F. Goodrich Skywatch/ SKY-497)


D

1

0









50-8

Automatic Dependent Surveillance- Broadcast (ADS-B) System


D

-

0

May be inoperative provided it is not required by 14 CFR.

Note

If ADS-B is installed in lieu of or as a replacement for 14 CFR required equipment, the repair category in the operator’s Minimum Equipment List (MEL) will be the same as that of the 14 CFR required equipment.









1)

Link and Display Processor Unit (LDPU)

D

-

0

Note

Cockpit Display Traffic Information (CDTI) display of data from other aircraft systems may be used.









2)

Cockpit Display and Traffic Information (CDTI)

D

-

0

Note

ADS-B data transmissions may continue.









3)

CDTI Control Panel

D

-

0

May be inoperative provided:

  1. Flight Identification (ID) can be set, and

  2. Screen Display is acceptable to the flight crew.







4)

Data Link Transmitters

D

-

0










5)

Data Link Receivers

D

-

0









60-1

Traffic Collision and Avoidance System (TCAS I)


B

-

0

(M) May be inoperative provided:

  1. System is deactivated and secured, and

  2. Enroute or approach procedures do not require its use.

  1. Pull TCAS circuit breaker and tie-wrap.

  2. Install “TCAS INOP” placards on both RMU’s for Honeywell equipped aircraft and near the FMS-CDU for Collins equipped aircraft.

  1. Confirm the associated (M) procedure has been completed to deactivate and secure the system.

  2. Plan flight so enroute and approach procedures do not require use of TCAS.

  3. Use ATC on (modes S and A) or ATC ALT (modes A, C, S).







C

-

0

(M) May be inoperative provided:

  1. System not required by FAR,

  2. System is deactivated and secured, and

  3. Enroute or approach procedures do not require its use.

  1. Pull TCAS circuit breaker and tie-wrap.

  2. Install “TCAS INOP” placards on both RMU’s for Honeywell equipped aircraft and near the FMS-CDU for Collins equipped aircraft.

  1. Confirm the associated (M) procedure has been completed to deactivate and secure the system.

  2. Plan flight so enroute and approach procedures do not require use of TCAS.

  3. Use ATC on (modes S and A) or ATC ALT (modes A, C, S).

Note

TCAS is not required on any aircraft with a seating configuration of less than 10 seats, excluding any pilot seat, per FAR 135.180, and it is not required by FAR 91.






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