Hawker 125 (Series 1 through 900XP)

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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
45 - CENTRAL MAINTENANCE COMPUTER					4. Remarks and Exceptions	MAINTENANCE PROCEDURES	OPERATIONAL PROCEDURES
00-1	Maintenance Diagnostic Computer (MDC) (Pro Line 21 only)	D	1	0

Hawker 125 (Series 1 through 900XP) Maintenance and Operational Procedures for Federal Aviation Administration Master Minimum Equipment List - No: 8 - 02/18/2008
1. SYSTEM, Sequence Numbers & Item		Repair Category
			2. Number Installed
				3. Number Required for Dispatch		MAINTENANCE PROCEDURES	OPERATIONAL PROCEDURES
46 - INFORMATION SYSTEMS					4. Remarks and Exceptions	MAINTENANCE PROCEDURES	OPERATIONAL PROCEDURES
10 ***	Electronic Flight Bag System (EFB)	C	-	0	(O) May be inoperative provided alternate procedures are established and used to ensure all information associated with the flight is available in current and appropriate form. Note If alternate source is electronic, dual redundancy is required for operation. Any function, program or document which operates normally may be used.		Operations are to be conducted in accordance with FAA approved EFB Policy and Procedures Manual.
1) ***	Power Connection (Class 1 & 2)	C	-	0	(O) May be inoperative provided alternate procedures are established and used.		Operations are to be conducted in accordance with FAA approved EFB Policy and Procedures Manual.
2) ***	Mounting Device (Class 2)	C	-	0	(M) (O) May be inoperative provided: The associated EFB and hardware is secured by an alternate means or removed from the aircraft, and Alternate procedures are established and used.	Remove or secure EFB mounting device to assure the device does not interfere with Normal or Emergency crew duties.	Operations are to be conducted in accordance with FAA approved EFB Policy and Procedures Manual.
3) ***	Data Connectivity (Class 2)	C	-	0	(O) May be inoperative provided alternate procedures are established and used.		Operations are to be conducted in accordance with FAA approved EFB Policy and Procedures Manual.
4) ***	EFB Printer	C	-	0	(O) May be inoperative provided all affected pertinent flight information is printed and available prior to departure.		Operations are to be conducted in accordance with FAA approved EFB Policy and Procedures Manual.

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