Hawker 125 (Series 1 through 900XP)


Integrated Flight Information System (Pro Line 21 IFIS-5000)



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20

Integrated Flight Information System (Pro Line 21 IFIS-5000)


















1)

File Server Unit (FSU)

(FSU INOP) Message)
C

1

0










***




C

2

0

(O) One or both may be inoperative provided alternate procedures are established and used to ensure all information associated with the flight is available at the pilot station in current and appropriate form.
Note
If alternate source is electronic, dual redundancy is required for operation.

Traditional paper data will be carried and used for intended flight, or

Operations are to be conducted in accordance with FAA approved EFB Policy and Procedures Manual.



2)

Cursor Control Panel (CCP)

C

2

0

(O) One or both may be inoperative provided alternate procedures are established and used to ensure all information associated with the flight is available at the pilot station in current and appropriate form.

Traditional paper data will be carried and used for intended flight, or

Operations are to be conducted in accordance with FAA approved EFB Policy and Procedures Manual.






3) ***

Communications Management Unit (CMU)

C

1

0

(O) May be inoperative provided alternate procedures are established and used for Aircraft Communication Addressing and Reporting System (ACARS) and Universal Weather Radar (WX) inoperative.




Weather data for the intended flight path including alternates shall be obtained prior to departure.

4) ***

Third VHF Comm Radio

C

1

0

(O) May be inoperative provided alternate procedures are established and used for ACARS and Universal WX inoperative.




Weather data for the intended flight path including alternates shall be obtained prior to departure.

5) ***

XM Satellite Weather System

C

1

0













Maintenance and Operational Procedures
for Federal Aviation Administration Master Minimum Equipment List - No: 7 - 09/07/2007

1. SYSTEM,
Sequence Numbers & Item

Repair Category




2. Number Installed







3. Number Required for Dispatch

MAINTENANCE
PROCEDURES

OPERATIONAL
PROCEDURES

49 - AIRBORNE AUXILIARY POWER









4. Remarks and Exceptions

00-1

Auxiliary Power Unit (APU)


C

1

0

May be inoperative provided APU is not used.






10-1

APU Air/Load Control Valve
C

1

0

(M) (O) May be inoperative provided:

  1. Air valve is secured closed, and

  2. APU air switch remains OFF.

Note

If APU and APU Generator operate normally, APU may be used to provide electric power.

  1. Locate APU air valve in Rear Equipment Bay. Check valve mechanical indicator CLOSED.

  2. Disconnect electrical connections, bag and stow.

  3. In cockpit locate APU Air Valve Switch and insure that it is OFF.

  4. Place Inoperative ‘INOP’ Placard at APU air valve switch.

  1. Do not use APU bleed air.

  2. If APU and APU generator are operational, they may be used.







C

1

0

May be inoperative provided APU is not used.







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