5. Autothrottle Engage /
Disengage Switches
(On Thrust Lever
Stem)
|
C
|
2
|
1
|
(O) One may be inoperative provided functionally of remaining Autothrottle Engage/Disengage Switch is checked prior to each departure.
|
None required.
|
With both engines running, taxi the airplane to an area where engine run-ups are allowed on airport. Prior to performing the test, access the TRS menu on the Display Controller. Select Manual EPR and set a target of 1.30. Once in position, increase thrust on both engines to 1.10 EPR. Engage autothrottle in the standard manner. Once engaged, use the operative engage/disengage switch to disengage autothrottle. Verify that autothrottle is disengaged by listening for disconnect tone and retard both throttles to idle. Again, increase thrust on both engines to 1.10 EPR. Engage autothrottle in the standard manner. Once engaged, manually override autothrottle by pulling forcefully (approximately 25 lb of force is required) aft on throttles. Verify that autothrottle is disengaged by listening for disconnect tone and retard both throttles to idle.
|
An Inoperative Placard will be placed on Thrust Lever Stem and will be noted on ADLS.
|
6. Touch Control
Steering Switches
(TCS)
|
D
|
2
|
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.
|
7. Flight Guidance
Computer (FGC)
(Autopilots/Flight
Directors)
|
C
|
2
|
1
|
(M) (O) Except for ER operations or where en route operations or approach minimums require its use, may be inoperative provided airplane is operated in accordance with AFM Limitations.
NOTE: FGC is required for MNPS, RVSM, RNP and PRNAV operations.
|
Maintenance will pull and reset the affected IAC (GV) or MAU Channel (GV-SP/GIV-X) and Guidance Panel circuit breakers in attempt to reset the FGC. If FGC does not recover, no further action required.
|
Flight crew will observe AFM limitations in the event the operative FGC fails and the Yaw Damper is inoperative.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
8. Yaw Damper Systems
|
C
|
2
|
1
|
(O) Except for ER operations, may be inoperative provided airplane is operated in accordance with AFM Limitations.
|
None required.
|
Flight crew will ensure airplane is operated in accordance with AFM Limitations in the event the operative Yaw Damper fails.
|
AN Inoperative Placard will be displayed in a prominent position to be viewed by the flight crew and will be noted on the ADLS.
|
9. Takeoff/Go-Around
(TO/GA) Buttons (on
Power Lever Handles)
|
C
|
2
|
1
|
May be inoperative provided approach minimums do not require its use.
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be viewed by the flight crew and will be noted on ADLS.
|
|
C
|
2
|
0
|
(O) May be inoperative provided:
a) Both power levers are operated manually for takeoff and go-around, and
b) Autopilot and Flight Director are not used below 500 feet or MDA, whichever is higher.
NOTE: Flight Director Takeoff and Go-Around guidance and Autothrottles are not available with both TO/GA switches inoperative.
|
None required.
|
Flight Director and Autothrottle are not available for Takeoff or Go-Around with both TO/GA buttons inoperative. Flight crew shall use raw data and manual throttles for takeoff and go-around. For takeoff, once airborne and above 500 ft AGL, pilot-not-flying (PNF) shall select desired lateral mode (HDG or LNAV) on guidance panel as directed by pilot-flying (PF). Additionally, PNF shall select desired vertical mode (FLCH or VS or FPA) and engage autothrottle as directed by PF. For go-around, after flaps and landing gear have been retracted and airplane is above 500 ft AGL, PNF shall select desired lateral mode (HDG or LNAV) and vertical mode (FLCH or VS or FPA) on guidance panel and engage autothrottle at direction of PF.
|
An Inoperative Placard will be displayed in a prominent position to be viewed by the flight crew and will be noted on ADLS.
|
10. Mach Trim Systems
(GV-SP/GIV-X only)
|
C
|
2
|
1
|
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be viewed by the flight crew and will be noted on ADLS.
|
|
|
|
|
|
|
|
|
1. Radio Communications
|
|
|
|
|
|
|
|
1) VHF Communications
|
C
|
-
|
1
|
Any in excess of one, and not powered by an emergency bus, may be inoperative provided flight is conducted under VFR over routes navigated by reference to visual landmarks.
|
None required.
|
None required.
|
An Inoperative Placard will be placed adjacent to affected Radio Frequency Management Unit (GV) or MCDU (GVSP/GIV-X) and will be noted on ADLS.
|
|
C
|
-
|
2
|
Any in excess of two, and not powered by an emergency bus, may be inoperative.
NOTE: Comm 1 is powered by the Emergency Bus.
|
None required.
|
None required.
|
An Inoperative Placard will be placed adjacent to affected Radio Frequency Management Unit (GV) or MCDU (GVSP/GIV-X) and will be noted on ADLS.
|
*** a) Frequency
Transer
Light
|
C
|
-
|
0
|
One or more may be inoperative.
|
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) Frequency
Transfer
Switch
|
C
|
-
|
0
|
One or more may be inoperative.
|
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.
|
*** c) Frequency
Selector
Knob
|
C
|
-
|
2
|
Any in excess of two may be inoperative.
|
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.
|
*** d) Frequency
Indication
|
C
|
-
|
2
|
Any in excess of two may be inoperative.
|
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. Cockpit Voice A
Recorder System
|
A
|
-
|
0
|
One ore more may be inoperative provided:
-
Not more than 72 hours have elapsed since cockpit voice recorder was found to be unserviceable,
-
Airplane does not exceed 8 further consecutive flights with cockpit voice recorder unserviceable, and
-
Any flight data recorder required to be carried is operative.
NOTE: This alleviation is not applicable to combined CVR/FDR. For those combined systems refer to JAR-OPS 1 MEL Policy Document.
|
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. Selective Call
*** System (SELCAL)
|
C
|
-
|
0
|
(O) May be inoperative provided alternate procedures are established and used.
|
None required.
|
One crew member shall monitor the appropriate frequency.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
|
D
|
-
|
0
|
May be inoperative provided 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.
|
1) Channels
|
C
|
-
|
0
|
(O) May be inoperative provided alternate procedures are established and used.
|
None required.
|
Flight crew will ensure:
a) SELCAL decoder monitors audio from the VHF and HF communications transceivers,
b) Recognizes receipt of the tone set assigned to the airplane, and
c) Provides the flight compartment with call alert signals.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
|
D
|
-
|
0
|
May be inoperative provided 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.
|
4. Emergency Locator
Transmitters (ELT)
|
|
|
|
|
|
|
|
*** 1) Survival
Type ELTs
|
D
|
-
|
-
|
(M) Any in excess of those required may be missing or inoperative provided inoperative equipment is placarded inoperative, removed from installed location, and placed out of sight so it cannot be mistaken for a functional unit.
|
Maintenance will ensure to placard inoperative survival type ELT and remove from airplane for servicing.
Flight crew may accomplish this task if properly qualified and authorised.
|
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) Fixed ELTs
|
A
|
-
|
0
|
May be inoperative for a maximum of 6 flights or 25 flying hours, whichever occurs first.
|
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.
|
|
D
|
-
|
-
|
Any in excess of those required may be missing.
|
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. Crewmember
*** Interphone System
|
|
|
|
|
|
|
| -
Passenger
Configuration
|
|
|
|
|
|
|
|
a) Flight Deck to Cabin, Cabin to
Flight Deck
Functions
|
B
|
-
|
-
|
(O) May be inoperative provided:
-
Alternate procedures are established and used for communications with flight deck, and
-
PA system is operative.
|
None required.
|
Flight crew may use the PA to communicate with the cabin crew or speak to the cabin crew directly in either the cockpit or cabin to pass information.
|
An Inoperative Placard will be placed on Interphone System and will be noted on ADLS.
|
|
|
|
|
NOTE: Any station function(s) that is operative may be used.
|
|
|
|
b) Cabin to Cabin
Functions
|
C
|
-
|
0
|
(O) May be inoperative provided:
-
Alternate, normal and emergency procedures are established and used, and
-
PA system is operative.
|
None required.
|
Cabin crew may use the PA to communicate with the cabin crew or speak to the cabin crew directly in either the cockpit or cabin to pass information.
|
An Inoperative Placard will be placed on Interphone System and will be noted on ADLS.
|
|
|
|
|
NOTE: Any station function(s) that is operative may be used.
|
|
|
|
c) Flight Deck to
Ground
|
C
|
-
|
0
|
May be inoperative provided alternate, normal and emergency procedures are established and used.
|
None required.
|
None required.
|
An Inoperative Placard will be placed on Interphone System and will be noted on ADLS.
|
|
D
|
-
|
0
|
May be inoperative provided procedures do not require its use.
|
None required.
|
None required.
|
An Inoperative Placard will be placed on Interphone System and will be noted on ADLS.
|
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