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16. Navigation

Management

Systems

1) Navigation

Database(s)

(cont’d)

(O) One or more may be out of date for maximum of 10 calendar days provided:

Conventional (Non-RNAV) departure, arrival and approach procedures, when available, or ANSP assistance are used as an alternative to RNAV procedures which have been amended in current database cycle,
Before each flight, current aeronautical information is used to verify database Navigation Fixes. The coordinates, frequencies, status (as applicable) and suitability of Navigation Facilities required for intended route, and
Radio navigation aids, which are required to be flown for departure, arrival and approach procedures, and which have been amended in current database cycle are manually tuned and identified.

None required.

Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft.

Flight crew will verify navigation database information using current aeronautical information before each flight.

Flight Crew will manually tune and identify all radio navigation aids used throughout the flight.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

17. Lightning Sensor *** Systems (LSS)	D	-	0		None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
18. Stormscope ***	D	-	0		None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
19. Airborne Collision Avoidance System (ACAS)
1) ACAS System	A	-	0	(M)(O) May be inoperative for a maximum of 10 calendar days provided the system is deactivated and secured.	Maintenance or qualified flight crew will ensure system is deactivated by pulling and collaring ACAS Power circuit breaker.	Flight crew will follow flight plan to avoid airspace where an operating ACAS is required, e.g., RVSM airspace.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
2) Combined Traffic Alert (TA) and Resolution Advisory (RA) Dual Display System(s)	C	2	1	(O) May be inoperative on the non-flying pilot side provided: TA and RA visual display is operative on the flying pilot side, and TA and RA audio function is operative on the flying pilot side.	None required.	Flight crew will ensure the pilot flying has the operative TA and RA visual displays. Flight crew will perform an ACAS system test prior to first flight of the day.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
(continued)

19. Airborne Collision Avoidance System (ACAS)(cont’d)
3) Resolution Advisory (RA) Display System(s)	C	2	1	(O) May be inoperative on non-flying pilot side.	None required.	Flight crew will ensure that the pilot-flying has an operative RA display system.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
	C	-	0	(O) One may be inoperative provided: All Traffic Alert (TA) display elements and voice command audio functions are operative, and TA only mode is selected by the crew.	None required.	Flight crew will test the ACAS to ensure that the TA display and aurals are operative prior to first flight of the day. Flight crew will select TA only mode for the ACAS.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
4) Traffic Alert (TA) Display System(s)	C	-	0	(O) One or more may be inoperative provided all installed RA display and audio functions are operative.	None required.	Flight crew will test the ACAS to ensure that the RA display and aurals are operative prior to first flight of the day.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
5) Airspace Selection *** Function (Above / Normal / Below)	C	-	0		None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

20. Microwave Landing *** Systems (MLS)	D	-	-	As required by Operating Requirements.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
21. Symbol Generators (GV)	C	3	2	(M)(O) May be inoperative provided: a) EFIS displays at pilot’s and copilot's stations are operative from independent Symbol Generators, and b) Both EICAS displays are operative.	Maintenance should move inoperative SG to No. 3 position. Refer to AMM chapter 31-62-00. Maintenance will pull and collar the SG 3 circuit breaker. Flight crew may accomplish this task if properly qualified and authorised.	Flight crew will ensure EFIS Displays at pilot's and copilot's stations are operative from Independent Symbol Generators, and BOTH EICAS Displays (DU 3 and 4) are operative. Crew WILL select ALT for No. 3 SG to power EICAS displays.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
22. Guidance Panel Digital Indications and Mode Select Indications
1) Speed Display	C	1	0	May be inoperative provided the associated value is available in the Primary Flight Display.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
(continued)

22. Guidance Panel Digital Indications and Mode Select Indications (cont’d)
2) Heading Display	C	1	0	May be inoperative provided the associated value is available in the Primary Flight Display.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
3) VS/FPA Display	C	1	0	May be inoperative provided the associated value is available in the Primary Flight Display.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
4) Altitude Select Display	C	1	0	May be inoperative provided the associated value is available in the Primary Flight Display.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
5) LNAV	C	1	0	May be inoperative provided the associated value is available in the Primary Flight Display.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
6) VNAV	C	1	0	May be inoperative provided the associated value is available in the Primary Flight Display.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
(continued)

22. Guidance Panel Digital Indications and Mode Select Indications (cont’d)
7) FLCH	C	1	0	May be inoperative provided the associated value is available in the Primary Flight Display.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
8) Manual Speed	C	1	0	May be inoperative provided the associated value is available in the Primary Flight Display.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
9) Bank Select	C	1	0	May be inoperative provided the associated value is available in the Primary Flight Display.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
10) BC Select	C	1	0	May be inoperative provided the associated value is available in the Primary Flight Display.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
11) Heading Select	C	1	0	May be inoperative provided the associated value is available in the Primary Flight Display.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
(continued)

22. Guidance Panel Digital Indications and Mode Select Indications (cont’d)
12) VS/FPA Select	C	1	0	May be inoperative provided the associated value is available in the Primary Flight Display.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
13) Alt Hold Select	C	1	0	May be inoperative provided the associated value is available in the Primary Flight Display.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
14) Approach	C	1	0	May be inoperative provided the associated value is available in the Primary Flight Display.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
15) PFD Command	C	1	0	(O) May be inoperative provided the associated value is available in the Primary Flight Display.	None required.	On initial power up of the airplane, the default is PFD command left PFD. If button is pushed several times, PFD command to the left PFD can be established by pulling and resetting Guidance Panel circuit breakers.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

23. Altitude Alerting

System

(O) May be inoperative provided an autopilot with an altitude hold is operative.
NOTE: One altitude alerting system is required to be operative for RVSM operations.

None required.

Flight crew will ensure Autopilot with Altitude Hold is operable.
NOTE: Flight into RVSM airspace is not allowed with inoperative Altitude Alerting System.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

24. Display Units

(GV)

(M)(O) May be in operative provided:

a) The inoperative unit is located in the Copilot's Navigation Display Position (DU #5),

b) Standby Attitude Indicator is operative,

c) Standby RMI is operative, and

d) Alternate procedures are developed for operation without the Copilot's Navigation displays.

Maintenance will move the inoperative display unit to the Copilot's Navigation Display Position (DU #5). Refer to AMM chapter 31-63-03.

Maintenance will pull and collar the DU#5 circuit breaker.

Flight crew may accomplish this task if properly qualified and authorised.

Flight crew will ensure Standby Attitude Indicator and Standby RMI are operative. Alternate Procedures for operation without Copilot's Navigation Display (Pre-Takeoff and Pre-Arrival Crew Briefings) should include crew actions in the event of failure of another DU. Factors concerning abort criteria, takeoff continuance, deviation to alternate airfield and mission continuance should be included in there briefings.

For an approach with both copilot's PFD and ND inoperative, it is recommended that Compass Mode be selected on pilot's ND.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

(continued)

24. Display Units

(cont’d)

*** Display Units (GV)

For DU-885 Equipped

Airplanes

(continued)

(M)(O) May be inoperative provided:

The inoperative unit is located in the Copilot’s Navigation Display Position (DU #5),
Standby Attitude Indicator is operative,
Standby RMI is operative,
Alternate procedures are developed for operation without the Copilot’s Navigation displays, and
Terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft.

Maintenance will move the inoperative display unit to the Copilot's Navigation Display Position (DU #5). Refer to AMM chapter 31-63-03.
Manintenance will pull and collar DU#5 curcuit breaker.
Flight crew may accomplish this task if properly qualified and authorised.

Flight crew will ensure the following:

Standby Attitude Indicator and Standby RMI are operative,
Alternate Procedures for operation without Copilot's Navigation Display (Pre-Takeoff and Pre-Arrival Crew Briefings) should include crew actions in the event of failure of another DU,
Factors concerning abort criteria, takeoff continuance, deviation to alternate airfield and mission continuance should be included in their briefings, and
Terminal charts for origin, destination and alternate airports are verified to be current and onboard the aircraft.

For an approach with both copilot's PFD and ND inoperative, it is recommended that Compass Mode be selected on pilot's ND.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

24. Display Units (cont’d)
Display Units (GV-SP, GIV-X)	C	4	3	(M)(O) May be inoperative provided: a) The inoperative unit is located in the DU #3 position, and b) The pilot in the left seat flies the airplane.	Maintenance will move the inoperative display unit to the DU3 position. Refer to AMM Chapter 31-63-03 Maimtenance will pull and collar DU#3 circuit breaker. Flight crew may accomplish this task if properly qualified and authorised.	Flight crew will discuss alternate procedures for loss of a second display for all phases of flight including failures during takeoff, approach, landing, and go-around. It is required that the pilot in the left seat fly the airplane.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
25. Standby Magnetic Compass System (Flux Valve) (GV)	C	1	0	May be inoperative provided all three (3) Heading Reference systems are operative.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
*** Magnetometer (GV-SP, GIV-X)	C	1	0	May be inoperative provided all three (3) IRS’s are operative.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

26. Non-Stabilized *** Magnetic Compass	B	1	May be inoperative provided any combination of three (3) Gyro or INS (IRU) Stabilized Compass Systems are operative.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
	B	1	May be inoperative provided: Any combination of two(2) Gyro or INS (IRU) Stabilized Compass Systems are operative, and Airplane is operated with Dual Independent Navigation Capability and under Positive Radar Control by ATC on the en route portion of the flight.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
	B	1	May be inoperative for flights that are entirely within areas of magnetic unreliability provided at least two Stabilized Directional Gyro Systems are installed, operative, and used in conjunction with accepted Free Gyro Navigation Techniques.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

27. Head Up Display *** System	C	1	0	May be inoperative provided landing weather minimums or operating procedures do not require its use.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
28. Airborne Flight *** Information System (AFIS)	C	-	0	NOTE: The relief includes the datalink function (GV, GV-SP, GIV-X) and ADS-A/ADS-C function (GV-SP, GIV-X)	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
1) AFIS Printer	C	-	0		None required.	None required.	An Inoperative Placard will be placed on AFIS Printer and will be noted on ADLS.
29. Slip-Skid Indicator	B	2	1	May be inoperative provided: a) Third attitude indicator is installed and operative, and b) An operative slip indication is obtained by selecting another IRS source via the Display Controller.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
(GV Only)	B	2	1	(O) May be inoperative provided electronic slip indicator is replaced by a mechanical slip indicator.	None required.	Flight crew will ensure mechanical slip indicator is installed.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
	B	2	0	May be inoperative provided airplane is operated during day VMC conditions.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

30. Data Loader *** (GV)	D	1	0		None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
Data Management Unit (DMU) (GV-SP, GIV-X)	D	-	0		None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
31. Air Data Computers/ Systems
1) Micro Air Data Computers (GV)	C	3	2	(M) (O) May be inoperative provided: a) Manual Pressurisation Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, and e) Airplane is operated in accordance with AFM Limitations. NOTE: Two systems are required for operation in RVSM airspace.	Maintenance will pull and collar circuit breaker associated with inoperative Micro Air Data Computer. Flight crew may accomplish this task if properly qualified and authorised.	Flight crew will operationally check and assure that the items called out in provisos a) thru d) are operative. Flight crew will comply with all AFM limitations in Section 1-03-30, 1-03-40, and 1-21-10.	An Inoperative Placard will be placed on Micro Air Data Computers to be seen by flight crew and will be noted on ADLS.
(continued)

31. Air Data Computers/

Systems (cont’d)

1) Micro Air Data

Computers

(GV) (cont’d)

(continued)

May be inoperative provided airplane is operated in unpressurised configuration.

None required.

To operate the airplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section 3-21-60: Unpressurized Flight.
Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft.

An Inoperative Placard will be placed on Micro Air Data Computers to be seen by flight crew and will be noted on ADLS.

31. Air Data Computers/

Systems (cont’d)

2) Air Data Systems

(ADS)

(GV-SP, GIV-X)

(M) May be inoperative provided:

a) Manual Pressurisation Control System is operative,

b) Cabin Altitude and Differential Pressure Indicators are operative,

c) Cabin Rate of Climb Indicator is operative,

d) Autopilot is operative, and

e) Airplane is operated in accordance with AFM Limitations.

NOTE 1: Two systems are required for operation in RVSM airspace.

NOTE 2: If ADS 2 is failed, the WOW indications on the copilot’s flight control synoptic will be crosshatched. Dispatch is still allowed if the WOW indications on the pilot’s flight control synoptic are shown as valid.

Maintenance will pull and collar the ADM circuit breaker associated with the inoperative ADS.

Flight crew may accomplish this task if properly qualified and authorised.

None required.

An Inoperative Placard will be placed on Air Data Systems to be seen by flight crew and will be noted on ADLS.

(continued)

31. Air Data Computers/

Systems (cont’d)

(O) May be inoperative provided airplane is operated in unpressurised configuration.

None required.

An Inoperative Placard will be placed on Micro Air Data Computers to be seen by flight crew and will be noted on ADLS.

32. Integrated Avionics

*** Computers (IACs)

(GV)

May be inoperative provided two bus controllers are operative for dispatch.

NOTE: The FMS/PMS/Autothrottle function of the operative IACs may be inoperative as stated elsewhere in this section. The autopilot is addressed in ATA 22.

None required.

An Inoperative Placard will be will be placed on Integrated Avionics Computers (IACs) to be seen by flight crew and will be noted on ADLS.

33. Bus Controllers (GV)	C	-	2	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
34. Airshow Controller *** System	D	-	0	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
1) Cockpit Airshow *** Display System	D	-	0	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
2) Cabin Airshow *** Display System	D	-	0	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

35. Windshear Warning *** and Flight Guidance System (Reactive)	C	-	(O) May be inoperative provided alternate procedures are established and used.	None required.	Flight crew will comply with the AFM/AOM guidance on windshear conditions and the recommended procedures for windshear encounters.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
36. Windshear Detection *** and Avoidance System (Predictive)	C	-	(O) May be inoperative provided alternate procedures are established and used.	None required.	Flight crew will comply with the AFM/AOM guidance on windshear conditions and the recommended procedures for windshear encounters.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
37. Cockpit Voice *** Monitors	D	-		None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
38. Heads Up Checklist ***	D	-		None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

39. Enhanced Vision *** System (EVS)	D	1		None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
1) EVS Window *** Heat	D	1		None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
2) Secondary (non- *** HUD) EVS Display Repeater	D	1	May be inoperative provided procedures are not dependent on its use.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
40. Terrain Server Function/EGPWM Function/EGPWM Modules (GV-SP, GIV-X)	C	2	May be inoperative provided: GPWS functions are operative, and Repairs or replacements are carried out within 10 Calendar days. NOTE: Synthetic Vision PFD synthetic terrain will not be available with dual Terrain Server failures, but the full PFD may be used without restriction.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

41. Advanced Graphics

Modules (AGM)

(GV-SP, GIV-X)

(M)(O) May be inoperative provided:

a) The inoperative AGM is located in the AGM 3 position, and

b) Crew actions for subsequent failures are established.

Maintenance will move the inoperative AGM module to the AGM 3 position.
Flight crew may accomplish this task if properly qualified and authorised.

Flight crew will discuss the alternate procedures for sharing displays including if a display fails during all phases of flight including takeoff, approach, landing, and go-around.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

Advanced Graphics

Module (AGM)

(GV-SP, GIV-X)

(ASC 904 - Cert

Charlie and ASC 905 –

Cert Charlie II and Any later revision to the

Operating software)

(O) May be inoperative provided:

a) The inoperative AGM is electronically switched to the AGM 3 position resulting in DU3 Red Xing, and

b) Crew actions for subsequent failures are established.

None required.

Flight crew will ensure:

a) The failed AGM is electronically switched to the number 3 position,

b) Verify that DU 3 is Red X’ed prior to dispatch,

c) Dim DU 3 to eliminate the Red X, and

d) Discuss alternate procedures for sharing displays in the event a second AGM or DU fails during any phase of flight
NOTE: Refer to AFM Sections 2-08-260/261 and Section 3-16-11.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

42. Cockpit Printer

None required.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

43. Cursor Control Devices (GV-SP, GIV-X)	C	2	0	May be inoperative provided both Display Controllers, Weather Radar Controllers, and 2 MCDU’s are operative.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
*** Cursor Control Devices (GV Only)	C	2	0	(M)(O) May be inoperative provided: Both Display Controllers are operative, and Terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft.	Maintenance will pull and collar the circuit breaker for the inoperative CCD.	Flight crew will ensure that terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
44. Multifunction Control Display Units (MCDU) (GV-SP, GIV-X)	C	3	2	(M) May be inoperative provided: a) The FMS functions and Radio Tuning functions are operative on the remaining MCDU’s, and b) The inoperative MCDU is located in the No. 2 position. NOTE: MCDU 1 has Standby Engine instruments. MCDU 3 has Backup Radio Tuning functions.	Maintenance will perform procedures in accordance with AMM Chapter 34-60-03. The inoperative MCDU will be moved to the No. 2 position. Maintenance will pull and collar the circuit breaker for MCDU 2.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
1) Flight Management System (FMS) Functions (GV-SP, GIV-X) (continued)	B	3	1	Except where en route operations or approach minimums require its use, may be inoperative provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, and c) Procedures do not require its use. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. RNP RNAV including PRNAV and BRNAV only require a single FMS.	None required.	None required.	An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

44. Multifunction Control

Display Units (MCDU)

(GV-SP, GIV-X)

(cont’d)

a) Navigation Database(s)

Note: Database(s) which is/are out of date is/are considered to be inoperative

(O) One or more may be inoperative for the intended route where conventional (non-RNAV) navigation is sufficient provided:

a) Current aeronautical information (e.g. Charts) is available for the entire route and for the aerodromes to be used, and

b) Navigation databases information is disregarded.

None required.

Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft.

Flight crew will disregard navigation database information.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

Any in excess of one may be inoperative provided:

Operative database must be up to date for routes, departures, arrival and approach procedures that require use of navigation Database for RNAV, and
This up to date Database is readily available to flight crewmember(s) responsible for navigation.

None required.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

44. Multifunction Control

Display Units (MCDU)

(GV-SP, GIV-X)

(cont’d)

a) Navigation

Database(s)

Note: Database(s) which is/are out of date is/are considered to be inoperative

(O) One or more may be out of date for maximum of 10 calendar days provided:

a) Aero Navigation (RNAV) departure, arrival and approach procedures do not depend on data amended in current database cycle,

b) Before each flight, current aeronautical information is used to verify database Navigation Fixes, the coordinates, frequencies, status (as applicable) and suitability of Navigation Facilites required for intended route, and

c) Radio navigation aids, which are required to be flown for departure, arrival and approach procedures, which have been amended in current database cycle are manually tuned and identified.

None required.

Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft.

Flight crew will verify navigation database information using current aeronautical information before each flight.

Flight Crew will manually tune and identify all radio navigation aids used throughout the flight.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

(continued)

44. Multifunction Control

Display Units (MCDU)

(GV-SP, GIV-X)

(cont’d)

a) Navigation

Database(s)

Note: Database(s) which is/are out of date is/are considered to be inoperative

(O) One or more may be out of date for maximum of 10 calendar days provided:

a) Conventional (Non-RNAV) departure, arrival and approach procedure, when available, or ANSP assistance are used as an alternative to RNAV procedures which have been amended in the current database cycle,

b) Before each flight, current aeronautical information is used to verify database Navigation Fixes. The coordinates, frequencies, status (as applicable) and suitability of Navigation Facilites required for intended route, and

c) Radio navigation aids, which are required to be flown for departure, arrival and approach procedures, which have been amended in current database cycle are manually tuned and identified.

None required.

Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft.

Flight crew will verify navigation database information using current aeronautical information before each flight.

Flight Crew will manually tune and identify all radio navigation aids used throughout the flight.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

2) Radio Tuning Functions (GV-SP, GIV-X)

None required.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

45. Advanced Graphics

Module (AGM)

Databases

(GV-SP, GIV-X)

Note: Database(s)

which is/are out of date

is/are considered to be

inoperative

(O) One or more may be out out of date for maximum of 10 calendar days provided:

a) Before each flight, current aeronautical information is used to verify database Navigation Fixes. The coordinates, frequencies, status (as applicable) and suitability of Navigation Facilities required for intended route, and

b) Radio navigation aids, which are required to be flown for departure, arrival and approach procedures, and which have been amended in current database cycle are manually tuned and identified.

None required.

Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft.

Flight crew will verify navigation database information using current aeronautical information before each flight.

Flight Crew will manually tune and identify all radio navigation aids used throughout the flight.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

46. Charts Function

(GV-SP, GIV-X)

May be inoperative provided current aeronautical charts are carried onboard the airplane and available to the flight crew.

None required.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

1) Charts Database

May be out of currency provided the terminal charts for the origin, destination, and alternate airports are verified to be current.

None required.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

47. Video Function

(GV-SP, GIV-X)

May be inoperative provided alternate procedures are established for the use of the Enhanced Vision System (EVS) display function.

None required.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

48. Automatic Dependent

*** Surveillance-Broadcast

(ADS-B) System

Extended Squitter

(ADS-B Out)

Transmissions

One or more extended squitter transmissions may be inoperative when not required for the intended route.

None required.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

49. Right Side Display

Controller (GV Only)

(M) (O) May be inoperative provided:

a) The weather at the destination is forecast to be VFR (1,000 ft ceiling and three (3) miles visibility),

b) Weather forecast at the alternate airport meet the same requirements as specified for the destination (1,000 ft ceiling and three (3) miles visibility),

c) Both VOR and ADF navigation receivers are operative,

d) Flight is conducted based on short range navigation sources only being available,

e) Navigation suffix in the IFR flight plan clearly indicates that the airplane is not capable of any RNP required navigation capability,

f) Flight is conducted in airspace where the availability of navigation by short range navigation receivers (VOR/ADF) is assured,

g) One DBDI or Standby RMI or Secondary Navigation Display is operative,

h) Associated Display Controller circuit breaker is pulled and collared,

i) Alternate procedures are established and used, and

j) Repairs are made within one (1) flight day.

Maintenance will ensure associated Display Controller circuit breaker for the failed Display Controller is pulled and collared.

The flight crew shall prepare and display a TOLD (Takeoff and Landing Data) card pror to takeoff and prior to approach and landing.

An Inoperative Placard will be placed on the Right Side Display Controller and will be noted on ADLS.

49. Right Side Display

Controller

(GV-SP/GIV-X Only)

(M)(O) May be inoperative provided:

FMS is the navigation source on both PFD’s,
Destination and alternate airports have either LPV, GPS or FMS overlay approaches available without NOTAM restrictions for airplanes not equipped with Enhanced Navigation Package,
Destination and alternate airports have either LPV, GPS, FMS overlay, or ILS approach available without NOTAM restrictions for airplanes equipped with Enhanced Navigation Package,
No other display system failures exist,
Associated Display Controller circuit breaker is pulled and collared,
Alternate procedures are established and used, and
Repairs are made within two (2) flight days.

Maintenance will pull and collar associated Display Control circuit breaker.

Flight crew will verify the required approaches are available at the destination and alternate airports without being NOTAMed out of service or unusable. When weather conditions exist at the destination or alternate airport during the approach, the PNF will be prepared to announce approach minimums in the event the operative Display Controller fails en route.

An Inoperative Placard will be placed on the Right Side Display Controller and will be noted on ADLS.

50. Synthetic Vision

*** Primary Flight Display

(SV-PFD) Functions

None required.

An Inoperative Placard will be displayed in a prominante position to be seen by flight crew and will be noted on ADLS.

51. DDA (Digital to

*** Discrete Adapter)

(GV only)

May be inoperative provided approach minimums do not require its use.

None required.

An Inoperative Placard will be displayed in a prominante position to be seen by flight crew and will be noted on ADLS.

52. GNSSU WAAS (Wide

*** Area Augmentation

System or SBAS –

Space Based

Augentation System)

Function

WAAS function may be inoperative provided en route and approach procedures do not require its use.

None required.

An Inoperative Placard will be displayed in a prominante position to be seen by flight crew and will be noted on ADLS.

1. Passenger Oxygen System and Supply	-	-	-	As required by Operating Requirements.	None required.	None required.	An Inoperative Placard will be placed on affected Oxygen Control Panel or Mask Unit and will be noted on ADLS. Additionally, affected seats shall be blocked and placarded.
2. Cabin Oxygen ON Warning System	C	1	0	May be inoperative provided: Cabin Altitude and Differential Pressure Indicators are operative, and Cabin Altitude Pressure Warning System is operative.	None required.	None required.	An Inoperative Placard will be placed above "ON" position on Oxygen Control Panel and will be noted on ADLS.
	C	1	0	(O) May be inoperative provide airplane is operated in unpressurised configuration.	None required.	To operate the airplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section 3-21-60: Unpressurized Flight. Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft.	An Inoperative Placard will be placed above "ON" position on Oxygen Control Panel and will be noted on ADLS.

NOTE: Information regarding the oxygen system capabilities for each airplane can be found in the Airplane Flight Manual Supplement for Oxygen Systems. The following document number, G450/G350 – GC41453M000, G550/G500 – GC51453M004 or GV – GC52712M001 are associated with the Oxygen Flight Manual Supplements however, each operator must verify that the document number is applicable to the particular airplane.

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