Equipment list operational and

REMARKS OR EXCEPTIONS

(O) Either the pilot's or copilot's control wheel switch may

a) The autopilot is not utilized at less than initial approach altitude,

b) NWS is verified operational,

c) Pitch trim is verified operational, and

d) Pilot flying must have operational autopilot
Disengage switch.

OPERATIONAL PROCEDURES

1. Make appropriate discrepancy report entry.

2. Place placard forward of affected control wheel stating: "Autopilot Disconnect Switch INOP."

3. Crew briefings will include a reminder of the

4. Verify operation of Pitch Trim Control and Disconnect Function on left and right control wheel:

(a) Pilot side: Verify that Stabilizer follows up and
down Primary Pitch Trim inputs and will Disconnect using A/P Disconnect Switch.

(b) Repeat 4. (a) for Copilot's Pitch Trim Control and

5. Verify operation of Nose Wheel Steering and

(a) Pilot side: With Nose Wheel Steering on, verify

(b) Repeat 5. (a) using Copilot's A/P Disconnect

REMARKS OR EXCEPTIONS

1) Passenger Configuration

(O) May be inoperative while conducting operations that require two LRC’s provided:

a) SATCOM Voice or Data Link operates normally.

b) Alternate procedures are established and used.

c) SATCOM coverage is available over the intended route of flight.

d) Prior coordination with the appropriate ATC facility is required when INMARSAT codes for SATCOM Voice are not available.

communications unless otherwise authorized by the

appropriate ATC facilities.

OPERATIONAL PROCEDURES

1. Make appropriate discrepancy report entry.

2. Place a placard next to the HF radio controller stating, “HF RADIO INOPERATIVE.”

3. Prior to each flight a crewmember will use either the SATCOM Data Link or Voice system to transmit and receive information from a ground station to ensure that one of the systems are operational.

4. Prior to each flight a crewmember will review SATCOM system User’s Guide or Manual to ensure that coverage exists for the intended route of flight.

(O) May be inoperative provided:

a) Alternate, normal, and emergency procedures, and/or operating restrictions are established and used.
(O) May be inoperative provided:

a) PA not required by FAR, and

b) Alternate, normal and emergency procedures, and/or operating restrictions are established and used.

NOTE: Any station function (s) that operate normally may be used.

OPERATIONAL PROCEDURES

1. Before entering the cockpit, a crewmember will orally brief the passengers on the items for which he/she

2. During normal, abnormal or emergency conditions, a crewmember shall face the passengers from the

3. Place placards stating “PA SYSTEM INOP” next to

4. Make appropriate discrepancy report entry.

REMARKS OR EXCEPTIONS

2) Cargo Configuration (Courier or Supernumerary Address System)

(O) May be inoperative provided alternate procedures are established and used.

OPERATIONAL PROCEDURES

1. Before entering the cockpit, a crewmember will orally brief the passengers on the items for which he/she

2. During normal, abnormal or emergency conditions, a crewmember shall face the passengers from the

3. Place placards stating “PA SYSTEM INOP” next to

4. Make appropriate discrepancy report entry.

(O) May be inoperative provided alternate procedures are used for required passenger briefings.

OPERATIONAL PROCEDURES

1. Before entering the cockpit, a crewmember will orally brief the passengers on the items for which he/she

2. During normal, abnormal or emergency conditions, a crewmember shall face the passengers from the

3. Place placards stating “PA SYSTEM INOP” next to

4. Make appropriate discrepancy report entry.

REMARKS OR EXCEPTIONS

b) Flight Deck to Ground Function

(O) May be inoperative provided:

a) Flight deck to cabin and cabin to flight deck interphone functions operate normally on at least fifty percent of the cabin handsets.

OPERATIONAL PROCEDURES

1. Before entering the cockpit, a crewmember will orally brief the passengers on the items for which he/she

2. During normal, abnormal or emergency conditions, a crewmember shall face the passengers from the

3. Place placards stating “COCKPIT-CABIN INTERPHONE SYSTEM INOP” next to each audio control panel.

4. Make appropriate discrepancy report entry.

(O) May be inoperative provided alternate procedures are established and used.

OPERATIONAL PROCEDURES

1. Before entering the aircraft, a crewmember will orally brief the ground crew on the items for which he/she

2. During ground operation the flight crew will use voice commands and/or hand signals to communicate with the ground crew

3. Place placards stating “FLIGHT DECK TO GROUND INTERPHONE SYSTEM INOP” next to each audio control panel.

4. Make appropriate discrepancy report entry.

REMARKS OR EXCEPTIONS

a) Flight Deck to Cabin, Cabin to Flight Deck Functions

b) Flight Deck to Ground Functions

10. Recorded Passenger Briefing System

(O)May be inoperative provided:

alternate, normal and emergency procedures, and/or operating restrictions are established and used.

OPERATIONAL PROCEDURES

1. Before entering the cockpit, a crewmember will orally brief the occupants on the items for which he/she would normally use the Interphone System.

2. During normal, abnormal or emergency conditions, a crewmember shall face the occupants from the
cockpit and perform such announcements and/or give such instructions as are appropriate to the situation.

3. Place placards stating “XXXX INTERPHONE SYSTEM INOP” next to each audio control panel.

4. Make appropriate discrepancy report entry.

(O) May be inoperative provided alternate procedures are established and used.

OPERATIONAL PROCEDURES

1. Before entering the aircraft, a crewmember will orally brief the ground crew on the items for which he/she would normally use the Interphone System.

2. During ground operation the flight crew will use voice commands and/or hand signals to communicate with the ground crew

3. Place placards stating “COCKPIT-GROUND INTERPHONE SYSTEM INOP” next to each audio control panel.

4. Make appropriate discrepancy report entry.

(O) May be inoperative provided alternate procedures are used for required passenger briefings.

OPERATIONAL PROCEDURES

1. Before entering the cockpit, a crewmember will orally brief the passengers on the items for which he/she would normally use the Cabin Briefer System.

2. During normal, abnormal or emergency conditions, a crewmember shall face the passengers from the
cockpit and perform such announcements and/or give such instructions as are appropriate to the situation.

3. Place placards stating “CABIN BRIEFING SYSTEM INOP” adjacent to the control panel.

4. Make appropriate discrepancy report entry.

REMARKS OR EXCEPTIONS

(O) May be inoperative provided:

a) Affected speaker(s) is not required for procedures
or aural warnings, and

b) A headset is installed, operative, and used for each cockpit position.

OPERATIONAL PROCEDURE

1. Crew will test operation of aural warning systems, including but not limited to GPWS, TCAS, to ensure that sufficient flight deck speakers are operative for crew to hear aural warnings from all affected systems.

2. Place placard stating “XXXXX SPEAKER IS INOPERATIVE” next to the appropriate audio control panel, “XXXXX” being location of the inoperative speaker.

3. Make appropriate discrepancy report entry.

(O) May be inoperative provided:

a) Remaining RMU is verified to operate normally, and

b) Auxiliary Com/Nav Control Display Unit is verified to operate normally.

OPERATIONAL PROCEDURE

1. Prior to each flight a crewmember will use the Auxiliary Com/Nav Control Display Unit to tune at least one com channel and at least one navigational aid, checking for proper reception and transmission.

2. Place placard stating “RMU INOPERATIVE” on the inoperative RMU.

3. Make appropriate discrepancy report entry.

a) Paper Checklist is available and

b) Alternate normal, abnormal, and emergency operations briefing procedures are established and used.

OPERATIONAL PROCEDURE

1. Crewmembers will ensure that the standard checklist is available and be briefed on its use.

2. If cabin briefer is installed and inoperative,
crewmembers will brief passengers.

3. Make appropriate entry on discrepancy report.

REMARKS OR EXCEPTIONS

(O) May be inoperative provided procedures do not require its use.

(i.e. see item 23-2, HF Comm)

OPERATIONAL PROCEDURE

1. Prior to each flight a crewmember will use either the SATCOM Data Link or Voice system to transmit and receive information from a ground station to ensure that one of the systems are operational.

2. Prior to each flight a crewmember will review SATCOM system User’s Guide or Manual to ensure that coverage exists for the intended route of flight.

3. Make appropriate discrepancy entry.

4. Place placard over SATCOM Controller stating “ SATCOM INOP”.

REMARKS OR EXCEPTIONS

3. Engine Driven Generators (Aircraft with Parallel Electrical System)

(Aircraft with Split Bus Electrical System)

(M) One may be inoperative provided:

a) The affected battery is disconnected and the connector is stowed,

b) The APU is running and the APU generator is verified operating,

c) The maximum altitude is FL310, and

d) The affected battery switch remains in the OFF position.

MAINTENANCE PROCEDURES

1. Locate the affected battery on either the left or right side fuselage access panel just aft of the wing fairing.

2. Disconnect affected battery connector and cover with a plastic bag and secure with tie wrap.

3. Secure battery connector to prevent movement within compartment.

4. Place placard next to the Battery switch stating which battery has been disconnected and secured.

5. Make appropriate discrepancy report entry.

a) The APU is running and the APU generator is

b) The maximum altitude is FL310.

(M) LH GEN may be inoperative provided:

a) DC POWER XTIE Switch – CLOSED,

b) The APU is running and the APU generator is
verified operating by selecting RH GEN to OFF,
verify that load is picked up, then turn RH GEN
to ON, and

c) the maximum altitude is FL310.

a) DC POWER XTIE Switch – OPEN,

b) The APU is running and the APU GEN verified operating, and

c) the maximum altitude is FL310.

MAINTENANCE PROCEDURES

NOTE: The following procedure is to be used for all three generator relief items above. For all three, APU is to be left running for duration of flight to provide generator redundancy.

2. If the generator is not sound or does not rotate freely, it must be repaired or replaced before dispatch of the aircraft.

3. Place a placard near the appropriate generator switch stating, "LEFT/RIGHT GENERATOR INOP."

4. Make appropriate discrepancy report entry.

REMARKS OR EXCEPTIONS

3) Armrest

11. Pilot seat or Copilot Seat

3) Armrest

(O) May be inoperative provided:

a) Baggage is not stowed under seat with inoperative restraining bar,

b) Associated seat is placarded “DO NOT STOW BAGGAGE UNDER THIS SEAT”, and

c) Procedures are established to alert Cabin Crew of inoperative restraining bar.

OPERATIONAL PROCEDURE

1. Make appropriate entry in discrepancy report.

2. A crewmember shall brief cabin crew or passengers. Briefing will specify which seats are affected, and that baggage should not be stored under those seats.

3. Using a folded paper or other method that will not damage chair, hang or attach a placard to the seat-back stating “DO NOT STORE BAGGAGE ITEMS BENEATH THIS SEAT.”

(O) May be inoperative and occupied provided:

a) Seat does not block an Emergency Exit, and

b) Seat does not restrict any passenger from the main aircraft aisle.

OPERATIONAL PROCEDURE

1. Make appropriate entry in discrepancy report.

2. A crewmember shall brief cabin crew or passengers. Briefing will specify which seats are affected.

3. Using a folded paper or other method that will not damage chair, hang or attach a placard to the seat-back stating “ ARMREST INOP”.

(M) May be inoperative provided:

a) Affected armrest is stowed in the retracted position, and

b) Seat is acceptable to the affected crewmember.

MAINTENANCE PROCEDURES

1. Make appropriate entry in discrepancy report

2. Obtain tie wrap or equivalent material of twelve inches in length.

3. Place armrest in the stowed position.

4. Secure armrest to the exposed bungee material between the folds of the map pocket behind the crew seat.

REMARKS OR EXCEPTIONS

(M) May be inoperative provided:

a) Procedures are established to secure the compartment closed,

b) The compartment is not used for the storage of emergency equipment, and

c) The affected compartment (s) is not used for the storage of any item except those that are permanently affixed.

MAINTENANCE PROCEDURES

1. Make appropriate entry in discrepancy report.

2. A crewmember shall close and secure the affected compartment utilizing tape as appropriate to insure the compartment will not come open in flight.

3. A crewmember will ensure the compartment does not contain any items, including emergency equipment except for items that are permanently affixed.

4. A crewmember will brief the passengers as to the location of the emergency equipment, if move from the standard location.

5. Place placard over affected compartment (s) stating “ COMPARTMENT INOP”.

REMARKS OR EXCEPTIONS

3. APU Fire Detection and Extinguishing System

1) APU FIRE PUSH Illuminated Switch

(O) May be inoperative provided:

a) No baggage is carried.

b) The baggage isolation valve is closed, and

c) Procedures are established to log the pressurization cycles and flight hours when the baggage isolation valve is closed.

OPERATIONAL PROCEDURES

1. Record each pressurization cycle event during the time the baggage isolation valve is closed.

2. Make appropriate discrepancy report entry.
NOTE: One pressurization cycle is defined as one flight and may be used synonymous with landings.

(M) May be inoperative provided the APU is secured and other procedures do not require the use of the APU.

MAINTENANCE PROCEDURES

1. Disengage and tie wrap master circuit breaker located

2. Place placard on APU control panel stating, "APU

3. Make appropriate entry in discrepancy report.

(O) May be inoperative provided the APU FIRE CAS message, Master Warning Lights, APU System Master, and Aural Warnings are verified to operate normally.

OPERATIONAL PROCEDURES

1. Utilize the APU test switch on the APU panel to verify the items listed above are operational.

2. Make appropriate discrepancy entry.

3. Place placard over APU FIRE PUSH switch stating “ APU FIRE PUSH SWITCH INOP”.

REMARKS OR EXCEPTIONS

2. Control Lock T-handle (Units –0001 to –0062)

(O) Individual components of the synoptic wing display

a) The affected system is visually checked for proper operation prior to each takeoff, and

b) The affected aspects of the NO TAKEOFF warning system are verified to be operational.

OPERATIONAL PROCEDURES

1. Prior to departure, a crewmember will visually verify

2. Verify a NO TAKEOFF advisory (Cyan) CAS message

(b) Speed brakes extended.

3. Place a placard adjacent to the EICAS display stating which individual component of the synoptic wing display is inoperative.

4. Make appropriate discrepancy report entry.

(M) May be inoperative provided the system is secured unlocked.

MAINTENANCE PROCEDURES

1. Remove co-pilot seat and pedestal forward kick-panel on co-pilot side.

2. Remove floorboard 142BT (floorboard surrounding co-pilot's control yoke).

3. Ensure that control lock system is unlocked. Torque-tube arm connected to control-lock control cable should be at full aft travel, with striker plate/latch assembly pulled inboard, away from left hand secondary elevator stop arm.

4. (Refer to 750 Maintenance Manual Detail A, Figure 201, chapter 27-70-00) Using a loop of safety wire through the inboard anchor point for the forward striker plate/latch assembly spring, around the striker plate/latch assembly, and through the inboard anchor point for the aft striker plate spring, secure the striker plate/latch assembly in the retracted (unlocked, inboard) position.

5. (Refer to same section of Maintenance Manual, Figure 202) Secure rudder-lock portion of system at the top of the co-pilot's rudder pedal torque-tubes by installing tie-wrap from the front of the catch, just beneath the cable clevis, around the aft side of the bracket where the springs are anchored, and tightening the tie-wrap.

(Continued Next Page)

REMARKS OR EXCEPTIONS

6. Operate controls to verify that elevator and rudder pedals will operate smoothly through their full travel, with no interference.

7. Reinstall the pedestal kick-panel with a maintenance tag stating “Elevator and Rudder Control Lock Disabled.”

8. Re-install co-pilot seat.

9. Safety wire the Control Lock T-Handle in the stowed position.

10. Make an appropriate entry on the discrepancy report.

11. Place a placard on the LH control yoke stating, “FLIGHT CONTROL LOCK INOP.”

REMARKS OR EXCEPTIONS

(M) One may be inoperative provided:

a) Fuel Low Level message is operative.

b) Both Fuel Flow Indicators are operative,

c) The FMS fuel quantity function is operative and utilized,

d) Both Wing Tanks are completely filled with fuel, or

e) The fuel quantity in both wing tanks is determined by a reliable means.

MAINTENANCE PROCEDURES

1. Start the engines to ensure both fuel flow indicators and the FMS fuel quantity indicators are operative.

3. Verify the EICAS low fuel message is operative as follows:

(a) While observing the EICAS display unit, transfer

4. Ensure both wing tanks are completely filled with fuel

(Continued Next Page)

REMARKS OR EXCEPTIONS

3. Center Fuel Quantity Display

NOTE: Add 10% of the dipstick indication for gross weight computations, and subtract 10% of the dipstick indication (15% for JP4/JetB) for range computations.

FUEL TANK QUANTITY DISPLAY INOP.” Total Fuel Quantity Display will also be inoperative.

7. Make appropriate discrepancy report entry.
(M) May be inoperative provided:

a) Both Fuel Flow indicating systems are operative.

b) The FMS fuel quantity function is operative and utilized,

c) The center tank is verified empty, or

d) The quantity in center tank is verified by other
reliable means.

MAINTENANCE PROCEDURES

that the center tank is empty. Total Fuel Quantity Display will also be inoperative.)

2. Make appropriate discrepancy report entry.

3. Start the engines to ensure the FMS fuel quantity and fuel flow indicators are operative.

4. Shut down the engines.

5. Defuel and verify the center fuel tank is empty as follows: Defuel Single Point Method.
NOTE: Defueling may be slow or not possible if the ground equipment does not have enough suction or the hose is collapsed. Boost pump operation may speed wing tank defueling.
(a) Gain access to the refuel/defuel control panel by opening the access door located on the right side of the fuselage fairing forward of the wing leading edge.

(b) Ensure that the airplane and defueling equipment are properly grounded together and to an approved static ground.

(c) Remove the adapter (receptacle) cover.

(d) Insert the nozzle into the receptacle; turn clockwise and latch in place; open nozzle.

REMARKS OR EXCEPTIONS

5. Fuel Low Level Message

NOTE: Each fuel tank (left wing, right wing and center wing) incorporates a defueling shutoff valve.

(f) Start defueling equipment and monitor the operation.

(g) When the tank(s) are empty, shut down defueling equipment and remove the nozzle from the receptacle.

(h) If opened, close the manual select shutoff valve (return valve handle to stowed/horizontal position. Close manual defuel select shutoff valve access door.

(i) Install receptacle cap and close refuel/defuel control panel access door. Remove grounding cables and move airplane or vehicle from the area.
OR

MAINTENANCE PROCEDURES

1. Verify the center tank fuel quantity by lowering the magnetic fuel level indicator (dipstick) located between the forward and center (main) spar, inboard of the WS 18.35 sealed rib.

2. Place a placard on the instrument panel stating, "CENTER FUEL QUANTITY DISPLAY INOP."

3. Make appropriate discrepancy report entry.

MAINTENANCE PROCEDURES

1. Verify on preflight check, the associated fuel quantity indicator is operative.

2. Place placard on the instrument panel stating, "LEFT/RIGHT FUEL LOW LEVEL MESSAGE INOP."

3. Make appropriate discrepancy report entry.

REMARKS OR EXCEPTIONS

3. Static Heat L-R

13. Drain Mast Heaters

(M) One may be inoperative provided:

a) All Pitot Heater components are verified operative before each flight, and

b) Aircraft is not operated into known or forecast icing conditions.

MAINTENANCE PROCEDURES

1. Refer to AFM, Section III, Normal Procedures (Preflight Inspection and Exterior Inspection), to verify pitot heat operation.

2. Place a placard adjacent to the EICAS display stating, "LEFT/RIGHT PITOT HEAT "MESSAGE" INOP".

3. Make appropriate discrepancy report entry.

(M) One may be inoperative provided:

a) All Static Port Heater components are verified operative before each flight, and

b) Aircraft is not operated in known or forecast icing conditions.

MAINTENANCE PROCEDURES

1. Refer to AFM, Section III, Normal Procedures (Preflight Inspection and Exterior Inspection), to verify static port heat operation.

2. Place a placard adjacent to the EICAS display stating, "LEFT/RIGHT STATIC PORT HEAT "MESSAGE"
INOP."

3. Make appropriate discrepancy report entry.

(M) May be inoperative provided:

a) Associated galley service basin and lavatory basin are not used, and

b) Any remaining ice is removed from the galley service basins.

MAINTENANCE PROCEDURES

1. Gain access to the interior power junction box typically located in the aft port lavatory closet.

2. At the interior junction box, disengage DRAIN HEATER circuit breaker.

3. Place tie wrap around circuit breaker and placard “ DRAIN HEATER INOP”.

4. Make appropriate discrepancy report.

REMARKS OR EXCEPTIONS

OPERATIONAL PROCEDURES

1. Flight crew member will note and record takeoff and landing times using reliable time keeping instrument.

2. Place a placard adjacent to the Hobbs meter
stating, "HOBBS METER INOP."

3. Make appropriate discrepancy report entry.

REMARKS OR EXCEPTIONS

12. Cabin Interior Lighting System (including Cabin Indirect Lighting System and Cabin Reading Lights)

(O) May be inoperative provided alternate procedures are used for notifying passengers.

OPERATIONAL PROCEDURES

1. A crew member shall brief the passengers regarding the lack of FASTEN SEAT BELTS and NO SMOKING signs and shall ask them to be alert during movement on the surface and before takeoff and landing for a crew member announcing, by direct voice or passenger address system from the cockpit, that seat belts should be fastened and that smoking materials shall be extinguished.

2. Place an "INOP" placard next to the SEAT BELT/PASS SAFE switch.

3. Make appropriate discrepancy report entry.

(O) Individual lights may be inoperative provided:

a) All Cabin Emergency Lighting is verified operative,

b) Sufficient lighting is operative for the crew to perform required duties, and

c) Lighting configuration is acceptable to the flight

OPERATIONAL PROCEDURES

1. Make appropriate discrepancy report entry.

2. Place a placard next to the appropriate lighting control stating: “(appropriate light) INOPERATIVE.”

3. Position the Emergency Light switch, located on the pilot’s instrument panel to the ARM position.

4. Select main ship batteries to OFF. Cabin Emergency Lighting should illuminate, including: 4overhead head lights (3 in the cabin, 1 in the lav), 1 “EXIT” sign above, and 2 adjacent to the door, 1 “EXIT” sign above, and one below the cabin escape hatch, 2 sections of dropped aisle lights (RH aft, LH fwd).

5. Select Emergency Light switch to OFF.

REMARKS OR EXCEPTIONS

9. Class A TAWS Required by FAR

a) Current Aeronautical Charts are used to verify Navigational Fixes prior to dispatch,

b) Procedures are established and used to verify status and suitability of Navigation Facilities used to define route of flight, and

c) Approach Navigation Radios are manually tuned and identified.

OPERATIONAL PROCEDURES

1. Place placard adjacent to VHF Controller stating: "Navigation Database is not current."

2. Crewmember shall verify the type, suitability, and operational status of each Navigational Facility to be
used during route of flight, either by a current Aeronautical Chart, or Airport Facilities Directory, or verbally with FAA personnel, such as through a Flight Service Station briefer.

3. Once tuned, each Navigational Facility shall be

a) Alternate procedures are established and used, and

b) Repairs are made within two flight days.

OPERATIONAL PROCEDURES

1. Make appropriate entry on discrepancy report.

2. Install placard on the instrument panel stating “GPWS INOPERATIVE”

3. Crew briefings will include aural callouts through use of appropriate aircraft equipment to ensure obstacle and terrain clearance. Flight crew will review MEA, MSA, DH, MDA, as appropriate of the route being flown. Flight Manual and Operating Manual can be consulted for climb gradients available for the phase of flight being approached, and the ambient conditions (weight, temp, altitude). 2 engine climb is in Section VII of the Operating Manual Climb Tables and the AFM Landing Gross Climb Gradient table. For single engine climb capability, consult AFM Section IV, Second Segment Net Climb, Enroute Net Climb and Approach Gross Gradient Tables.

(Continued on next page
.

REMARKS OR EXCEPTIONS

1) Ground Proximity Warning System (GPWS) (Continued)

a) Modes 1 - 4

d) Advisory Callouts

(O) May be inoperative provided:

a) Alternate procedures are established, used, and

b) Repairs are made within two flight days.

OPERATIONAL PROCEDURES

1. Make appropriate entry on discrepancy report.

2. Install placard on the instrument panel stating “[Specific affected mode] INOPERATIVE”

3. Crew briefings will include aural callouts through use of appropriate aircraft equipment to ensure obstacle and terrain clearance. Flight crew will review MEA, MSA, DH, MDA, as appropriate of the route being flown. Flight Manual and Operating Manual can be consulted for climb gradients available for the phase of flight being approached, and the ambient conditions (weight, temp, altitude). 2 engine climb is in Section VII of the Operating Manual Climb Tables and the AFM Landing Gross Climb Gradient table. For single engine climb capability, consult AFM Section IV, Second Segment Net Climb, Enroute Net Climb and Approach Gross Gradient Tables.

---------------------------------- Or --------------------------

(O) May be inoperative provided:

a) Advisory callout not required by FAR, and

b) Alternate procedures are established and used.

OPERATIONAL PROCEDURES

2. Place “GPWS Advisory Callouts INOP” placard on the instrument panel.

3. Crew briefings will include aural callouts during approach, through the use of appropriate aircraft equipment to ensure obstacle and terrain clearance. Briefing should include MDA or DH, and procedure for one flight crew member to call out 500 feet above airport elevation, plus any other call outs agreed upon by the flight crew.

REMARKS OR EXCEPTIONS

2) Terrain System- Forward Looking Terrain Avoidance (FLTA) and Premature Descent (PDA) Functions

(O) May be inoperative provided:

a) Alternate procedures are established and used, and

b) Windshear Detection and Avoidance System (Predictive) operates normally.

OPERATIONAL PROCEDURES

(O) May be inoperative provided

a) Alternate procedures are established and used, and

b) Takeoffs and landings are not conducted in known or forecast windshear conditions.

OPERATIONAL PROCEDURES

2. Place “GPWS WINDSHEAR MODE INOP” placard on instrument panel.

3. Prior to each takeoff and prior to each approach, crew will obtain available weather reports to ensure windshear conditions are neither reported nor forecast in the aircraft flight path.

4. Crew briefings will include aural callouts through use of appropriate aircraft equipment i.e., airspeed, IVSI etc., and available weather reports for detection and prompt resolution of windshear encounter.

OPERATIONAL PROCEDURES

1. Make appropriate entry on discrepancy report.

2. Install placard on the instrument panel stating “GPWS Forward Looking Terrain Avoidance and Premature Descent Functions INOPERATIVE.”

3. Crew briefings will include

(a) Review of significant terrain expected to be encountered and obstacles in the airport area.

(b) Aural callouts to be used through use of appropriate air-craft equipment to ensure obstacle and terrain clearance.

(Continued Next Page)

REMARKS OR EXCEPTIONS

9. Class B TAWS Required by FAR

1) Ground Proximity Warning System (GPWS)

(c) Review of MSA and step-down fixes of the approach, and means to verify and call out passage of these points.

4. Flight Manual and Operating Manual can be consulted for climb gradients available for the phase of flight being approached, and the ambient conditions (weight, temp, altitude). 2 engine climb is in Section VII of the Operating Manual Climb Tables and the AFM Landing Gross Climb Gradient table. For single engine climb capability, consult AFM Section IV, Second Segment Net Climb, Enroute Net Climb and Approach Gross Gradient Tables.

(O) May be inoperative provided

a) Alternate procedures are established and used, and

b) Repairs are made within two flight days.

OPERATIONAL PROCEDURES

1. Make appropriate entry on discrepancy report.

2. Install placard on the instrument panel stating “GPWS INOPERATIVE”

3. Crew briefings will include aural callouts through use of appropriate aircraft equipment to ensure obstacle and terrain clearance. Flight crew will review MEA, MSA, DH, MDA, as appropriate of the route being flown. Flight Manual and Operating Manual can be consulted for climb gradients available for the phase of flight being approached, and the ambient conditions (weight, temp, altitude). 2 engine climb is in Section VII of the Operating Manual Climb Tables and the AFM Landing Gross Climb Gradient table. For single engine climb capability, consult AFM Section IV, Second Segment Net Climb, Enroute Net Climb and Approach Gross Gradient Tables.

REMARKS OR EXCEPTIONS

a) Modes 1 and 3

d) Advisory Callouts

(O) May be inoperative provided

a) Alternate procedures are established, used, and

b) Repairs are made within two flight days.

OPERATIONAL PROCEDURES

2. Place “GPWS Mode [1 or 2] INOP” placard on instrument panel.

3. Takeoff and approach crew briefings will include the lost of GPWS Mode, and steps to accommodate the loss.

4. During initial climbout, and during approaches, one flight crew member should monitor Altitude and Vertical speed, with appropriate callouts, to ensure that climb and descent rates are appropriate to phase of flight, and all altitude targets are met.

(O) May be inoperative provided alternate procedures are established and used.

---------------------------------- Or ----------------------------------

(O) May be inoperative provided:

a) Advisory callout not required by FAR, and

b) Alternate procedures are established and used.

OPERATIONAL PROCEDURES

1. Make appropriate entry on discrepancy report.

2. Place “GPWS Advisory Callouts INOP” placard on the instrument panel.

3. Crew briefings will include aural callouts during approach, through the use of appropriate aircraft equipment to ensure obstacle and terrain clearance. Briefing should include MDA or DH, and procedure for one flight crew member to call out 500 feet above airport elevation, plus any other call outs agreed upon by the flight crew.

REMARKS OR EXCEPTIONS

2) Terrain System Forward Looking Terrain Avoidance (FLTA) and Premature Descent (PDA) Functions

(O) May be inoperative provided alternate procedures are established, used.

OPERATIONAL PROCEDURES

2. Place “GPWS WINDSHEAR MODE INOP” placard on instrument panel.

3. Prior to each takeoff and prior to each approach, crew will obtain available weather reports to ensure windshear conditions are neither reported nor forecast in the aircraft flight path.

4. Crew briefings will include aural callouts through use of appropriate aircraft equipment i.e., airspeed, IVSI etc., and available weather reports for detection and prompt resolution of windshear encounter.

(O) May be inoperative provided alternate procedures are established and used.

OPERATIONAL PROCEDURES

1. Make appropriate entry on discrepancy report.

2. Install placard on the instrument panel stating “GPWS Forward Looking Terrain Avoidance and Premature Descent Functions INOPERATIVE.”

3. Crew briefings will include

(a) Review of significant terrain expected to be encountered and obstacles in the airport area.

(b) Aural callouts to be used through use of appropriate aircraft equipment to ensure obstacle and terrain clearance.

(c) Review of MSA and step-down fixes of the approach, and means to verify and call out passage of these points.

4. Flight Manual and Operating Manual can be consulted for climb gradients available for the phase of flight being approached, and the ambient conditions (weight, temp, altitude). 2 engine climb is in Section VII of the Operating Manual Climb Tables and the AFM Landing Gross Climb Gradient table. For single engine climb capability, consult AFM Section IV, Second Segment Net Climb, Enroute Net Climb and Approach Gross Gradient Tables.

REMARKS OR EXCEPTIONS

(M)(O) May be inoperative provided:

a) System is deactivated and secured, and

b) Enroute or approach procedures do not require

MAINTENANCE PROCEDURES

1. Make appropriate entry on the discrepancy report.

2. Install “INOP” placard on or adjacent to TCAS control
unit on instrument panel.

3. Disengage and secure TCAS circuit breaker.

OPERATIONAL PROCEDURES

1. When filing flight plans, crew will delete the “T” prefix from the Aircraft Equipment Code.

2. Flight crew will review all appropriate enroute and approach procedure charts appropriate to the flight to ensure TCAS is not required.

(M)(O) May be inoperative provided:

a) System is not required by FAR,

b) System is deactivated and secured, and

c) Enroute or approach procedures do not require
its use.

MAINTENANCE PROCEDURES

1. Make appropriate entry on the discrepancy report.

2. Install “INOP” placard on or adjacent to TCAS control
unit on instrument panel.

3. Disengage and secure TCAS circuit breaker.

OPERATIONAL PROCEDURES

1. When filing flight plans, crew will delete the “T” prefix from the Aircraft Equipment Code.

2. Flight crew will review all Equipment Requirements
listed in the FAR governing their operation, including
but not limited to Part 91, Part 135, RVSM (where applicable), etc.
(Continued Next Page)

REMARKS OR EXCEPTIONS

1) Combined Traffic Alert (TA) and Resolution Advisory (RA)

(M)(O) May be inoperative provided:

a) System is deactivated and secured, and

b) Enroute or approach procedures do not require

MAINTENANCE AND OPERATIONAL PROCEDURES

a) System is not required by FAR,

b) System is deactivated and secured, and

c) Enroute or approach procedures do not require

MAINTENANCE AND OPERATIONAL PROCEDURES

(O) May be inoperative on the non-flying pilot side

a) TA and RA visual display is operative on the flying pilot’s side and

b) TA and RA audio functions are operative on the
flying pilot side.

OPERATIONAL PROCEDURES

NOTE: This item refers to dual dedicated TCAS displays located on the RH and LH instrument panels, which are not part of the Citation X standard equipment. This item does not refer to the RA displays shown on the VSI portion of the PFD, nor to the TA/RA display shown on the MFD.

2. Place a placard on the instrument panel in front of the non-flying pilot side stating: “TCAS RA and TA display INOP.”

3. Utilizing the system self-test, crew will verify that TA
and RA advisory display on flying pilot side is
operational, and audio functions are operational.

4. The pilot with the operational TA and RA elements and audio functions shall conduct any subsequent maneuvering command by the RA (Resolution Advisory).

REMARKS OR EXCEPTIONS

3) Traffic Alert Display System(s)

(O) May be inoperative on the non-flying pilot side.

OPERATIONAL PROCEDURES

1. Make appropriate entry on the discrepancy report.

2. Place a placard on the instrument panel in front of the non-flying pilot side stating: “TCAS RA display
INOP.”

3. The pilot with the operational RA display shall conduct any subsequent maneuvering commanded by the RA (Resolution Advisory).

4. The non-flying pilot shall monitor the flying-pilot’s
vertical speed indicator/RA display during any TCAS-commanded maneuvers.
OR
(O) May be inoperative provided:

a) Traffic Alert (TA) visual and audio functions are

b) TA only mode is selected by the crew.

c) Enroute or approach procedures do not require
its use.

OPERATIONAL PROCEDURES

1. Make appropriate entry on the discrepancy report.

2. Place a placard on the instrument panel on or near the TCAS control unit stating: TCAS RA display INOP.

3. Using Test function, confirm that Traffic Alert display elements and voice command audio functions are operative.

4. Select TA only mode of operation.

(O) May be inoperative provided:

a) RA visual display and audio functions are operative, and

b) Enroute or approach procedures do not require its use.

OPERATIONAL PROCEDURES

1. Make appropriate entry on discrepancy report.

2. Place placard stating, “TCAS TA Display INOP” on the instrument panel.

3. Using test function, confirm that RA display elements (including VSI “fly to” and “do not fly” areas) and voice command audio functions are operative.

4. Prior to departure, flight crew will review enroute charts and approach procedures at destination to determine whether or not TA alerting is required.

5. Monitor PFD VSI for RA commands.

REMARKS OR EXCEPTIONS

12. Display Units (DU’s)

(O) May be inoperative provided:

a) Autopilot with altitude hold is operative, and

b) Enroute operations do not require its use, and

c) Repairs are made within three flight days.

OPERATIONAL PROCEDURES

1. Crew briefings will include aural callouts by crewmembers for appropriate altitudes.

2. On the Remote Instrument Controller located on the co-pilot’s pedestal, install placard next to the Altitude Select knob stating “ALTITUDE ALERT INOPERATIVE.”

3. Make appropriate entry in aircraft discrepancy report.

(O)(M) One display unit may be inoperative provided:

a) The inoperative DU is in the center position,

b) Both pilots' PFDs are operative and are in the #1 and #5 positions,

c) One DU displays EICAS, and

d) One DU displays a MFD.

MAINTENANCE PROCEDURES

(a) Ensure BATT, AVIONICS MASTER, EICAS

(b) Remove bezel controller by turning captive screws on outboard edges of bezel controller counterclockwise.

(c) Carefully pull bezel controller away from display
unit to disengage electrical connector.

(d) Insert hex key in mounting screw at bottom center

(e) Turn hex key counterclockwise, unlocking unit

(f) Use the display unit extraction tool, P/N CJMD234-108, to unseat unit from mounting rack.

(g) Pull display unit out of instrument panel and set aside.

2. Repeat steps 1.a-g to remove the center display unit to replace positions with the operative unit.

(a) Carefully slide display unit into mounting rack in instrument panel, ensuring proper mating of electrical connectors.

REMARKS OR EXCEPTIONS

19. Flight Guidance Controller

(b) Insert hex key in mounting screw at bottom center of display unit.

(c) Turn hex key clockwise until display is secured in mounting rack and flush with instrument panel.

(d) Carefully place bezel controller into position on display unit, ensuring proper mating of the connector on bezel controller with connector on the display unit.

4. Repeat steps 3.a - e installing operative display unit.

OPERATIONAL PROCEDURES

1. Verify one display unit displays EICAS and one unit displays MFD.

2. Verify both pilots' PFDs are operative.

3. Install placard over affected display stating, “DISPLAY UNIT INOP.”

4. Make appropriate discrepancy report entry.
(O) May be inoperative provided flight crew verifies that
the selected functions are properly displayed on the PFD/MFD.

OPERATIONAL PROCEDURES

1. Make appropriate entry on discrepancy report.

2. Install placards above both PFD’s stating, “XXX, XXX
FD Mode Annunciators INOP”, where “XXX, XXX” are
the specific Flight Director Mode Annunciators which
are inoperative.

3. During flight, crewmember selecting a flight director mode will verbalize the mode selected.

4. Second crewmember will respond by verbalizing the flight director mode displayed on the PFD.

REMARKS OR EXCEPTIONS

(M) Individual components may be inoperative provided:

a) Associated components are deactivated or isolated, and

b) Associated system components are verified not to have leaks.

a) System is drained, and

b) Procedures are established to ensure that the system is not serviced.

MAINTENANCE PROCEDURES

2. Place placard near the inoperative water system

3. Disengage and tie-wrap the water heater circuit

4. Open/remove access panels from lower vanity or

5. Remove quick-disconnect fitting.

6. Remove canister, inspect it and plumbing for leaks and dampness and empty canister.

7. Tape over canister lid and install placard on tank

8. Re-install canister and access panels

3. Remove access panels from Refreshment Center as needed to access tank.

4. Slide tank out of its compartment, disconnect and cap any electrical connectors.

5. Inspect tank and plumbing for leaks and dampness.

6. Drain tank, and remove any plumbing lines.

7. Replace tank without reconnecting any removed electrical or plumbing connections.

8. Reinstall access panels.