SYSTEM & SEQUENCE NUMBERS
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REMARKS OR EXCEPTIONS
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34 NAVIGATION (Continued)
Traffic Alert and Collision Avoidance System (TCAS II) (Continued)
1) Combined Traffic Alert (TA) and Resolution Advisory (RA) Dual Display System(s)
2) Resolution Advisory (RA) Display System(s)
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(M)(O) May be inoperative provided:
a) Not required by FAR,
b) System is deactivated and secured, and
c) Enroute or approach procedures do not require its use.
MAINTENANCE PROCEDURES
Use the same procedures as for the first TCAS I item above.
(O) May be inoperative on the non-flying pilot side provided:
a) TA and RA elements and audio functions are operative on the flying pilot’s side and
b) TA and RA display indications are visible to the non-flying pilot.
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 standard CJ2 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..
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 and TA display INOP.”
3. Utilizing the system self-test, crew will verify that TA and RA advisory display on the 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).
NOTE: The current wording in Policy Letter PL-32, Rev 5 for this item is as follows (No Procedure Required):
“May be inoperative on the non-flying pilot side provided:
a) TA and RA visual display is operative on the flying pilot’s side, and
b) TA and RA audio function is operative on flying pilot side.” ( No procedure required)
(O) May be inoperative provided:
a) Traffic Alert (TA) visual display and audio functions are operative,
b) TA only mode is selected by the crew, and
c) Enroute or approach procedures do not require its use.
1. Using the Test function, confirm that Traffic Alert display elements and voice command audio functions are operative.
2. Select TA only mode of operation.
3. Place a placard on the instrument panel on or near the TCAS control unit stating: “TCAS RA display INOP”.
4. Make appropriate entry on the discrepancy report.
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SYSTEM & SEQUENCE NUMBERS
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REMARKS OR EXCEPTIONS
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34 NAVIGATION (Continued)
Traffic Alert and Collision Avoidance System (TCAS II) (Continued)
3) Traffic Alert (TA) Display System(s)
14. Class B TAWS
1) Ground Proximity Warning System (GPWS)
a) Modes 1&3
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(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. Using the Test function, confirm that RA display elements (including VSI “fly to” and “do not fly” areas) and voice command audio functions are operative.
2. Monitor PFD VSI for RA commands.
3. Place a placard on or near the TCAS control unit stating: “TCAS TA Display INOP”.
4. Make appropriate entry on the discrepancy report.
(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 the 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.
(O) May be inoperative provided:
a) Alternate procedures are established and used, and
b) Repairs are made within two flight days.
OPERATIONAL PROCEDURES
1. Crew briefings will include aural callouts through use of appropriate aircraft equipment to ensure obstacle and terrain clearance.
2. Make appropriate entry on the discrepancy report.
3. Install placard on the instrument panel stating which specific GPWS modes are inoperative.
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SYSTEM & SEQUENCE NUMBERS
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REMARKS OR EXCEPTIONS
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34 NAVIGATION (Continued)
d) Advisory Callouts
e) Windshear Mode (Reactive)
15. Navigation Databases
1) Flight Management Systems
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(O) May be inoperative provided alternate procedures are established and used.
OPERATIONAL PROCEDURES
1. Make appropriate entry on the discrepancy report.
2. Place “GPWS Advisory Callouts INOP” placard on the instrument panel.
3. Crew briefings will include aural callouts through use of appropriate aircraft equipment to ensure obstacle and terrain clearance.
(O) May be inoperative provided alternate procedures are established and used.
OPERATIONAL PROCEDURES
1. Make appropriate entry on the discrepancy report.
2. Place GPWS Windshear Mode “INOP” placard on instrument panel.
3. 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 out of currency provided:
a) Current Aeronautical Charts are used to verify navigation fixes prior to dispatch,
b) Procedures are established 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
NOTE: Although the 525A MMEL does not require one, Policy Letter PL-98 requires a procedure for this item, therefore one is shown here.
1. Place placard adjacent to FMS 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, Airport Facilities Directory, or verbally with FAA personnel, such as through a Flight Service Station Briefer.
3. Once tuned, each navigational facility shall be identified using the audible signal transmitted by the facility.
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SYSTEM & SEQUENCE NUMBERS
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REMARKS OR EXCEPTIONS
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34 NAVIGATION (Continued)
15. Navigation Databases (Continued)
2) Navigation Management Systems
16. Windshear Warning and Flight Guidance System
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(O) May be out of currency provided:
a) Current Aeronautical Charts are used to verify navigation fixes prior to dispatch,
b) Procedures are established 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
NOTE: Although the 525A MMEL does not require one, Policy Letter PL-98 requires a procedure for this item, therefore one is shown here.
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, Airport Facilities Directory, or verbally with FAA personnel, such as through a Flight Service Station Briefer.
3. Once tuned, each navigational facility shall be identified using the audible signal transmitted by the facility.
(O) May be inoperative provided:
a) Alternate procedures are established and used, and
b) Windshear Detection and Avoidance System operates normally.
(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
NOTE: Windshear Warning and Flight Guidance Systems, as well as Windshear Detection and Avoidance Systems are not offered as standard nor optional equipment on Citation CJ2’s. Windshear Warning is incorporated in the GPWS systems. See GPWS earlier in this Guide for required procedures.
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SYSTEM & SEQUENCE NUMBERS
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REMARKS OR EXCEPTIONS
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34 NAVIGATION (Continued)
16. Windshear Warning and Flight Guidance System (Continued)
17. Windshear Detection and Avoidance System
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NOTE: Items 34-16 and 34-17 are a result of Policy Letter PL-67, which addresses predictive and reactive airborne windshear systems required for Part 121 Air Carriers, and states in part.
“Title 14 Code of Federal Regulations (14 CFR) Section 121.358 sets forth requirements for the Part 121 operators to have their aircraft equipped with either an approved Airborne Windshear Warning And Flight Guidance System (reactive system), an approved Airborne Detection And Avoidance System (predictive system), or an approved combination of these systems. This policy letter provides for minimum equipment list relief for the Low-Altitude Windshear System on air carrier aircraft. Airborne Windshear Warning and Flight Guidance Systems (Reactive Windshear-RWS) have been integrated onto aircraft as part of the Ground Proximity Warning System (GPWS) Windshear Mode. Airborne detection and avoidance systems have been integrated onto aircraft as Predictive Windshear Systems.”
(O) May be inoperative provided:
a) Alternate procedures are established and used, and
b) Windshear Warning and Guidance System operates normally
(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
See the explanation in item 34-16 above.
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SYSTEM & SEQUENCE NUMBERS
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REMARKS OR EXCEPTIONS
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38 WATER/WASTE
1. Potable Water Systems
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(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.
NOTE: Any portion of the system that operates normally
may be used.
(M) May be inoperative provided:
a) System is drained, and
b) Procedures are established to ensure that the system is not serviced prior to repair.
MAINTENANCE PROCEDURES
NOTE: Potable water systems in the CJ2 include, but are not limited to water tanks and heated liquid tanks with spigots in the Refreshment Center. The following procedures cover either MMEL item above, for typical installations. Water tanks in the upper aft vanity plumbed and gravity-fed to a wash basin are not typical, but are addressed here for completeness.
1. Make appropriate discrepancy report entry.
2. Place placard near the inoperative water system (faucet or spigot) stating: “WATER SYSTEM INOPERATIVE”.
For Refreshment Center Liquid Storage Tanks:
3. Remove access panels from Refreshment Center as needed to access tank.
4. Slide tank out of its compartment, disconnect and cap/bag 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.
For Aft Vanity Water Storage Tank:
3. Remove access panels from vanity as needed to access tank.
4. On most installations, turn the fasteners that secure the tank and depress the collar on the quick-disconnect water line connection to release the tank.
5. Disconnect and cap/bag any electrical connections from the tank (heating circuit, pump, etc.).
6. Inspect tank and plumbing for leaks and dampness.
7. Drain tank, and put in place without reconnecting plumbing.
8. Reinstall access panels.
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SYSTEM & SEQUENCE NUMBERS
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REMARKS OR EXCEPTIONS
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38 WATER/WASTE (Continued)
2. Lavatory Waste Systems
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(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.
NOTE: Any portion of the system that operates normally may be used.
MAINTENANCE PROCEDURES
1. Clean all components with disinfectant.
2. Place bag over toilet seat or relief tube, as appropriate, with placard stating “TOILET IS INOPERATIVE”, or “RELIEF TUBE IS INOPERATIVE.”
3. Make appropriate discrepancy report entry.
For Flushing Toilet:
4. Lift seat assembly or remove access cover to gain access to wiring.
5. Disconnect ship wiring from toilet.
6. Insulate and label all exposed wires to prevent any shorts and to facilitate future re-connection.
7. Visually inspect tank and reservoir for any leaks. Correct any leaks prior to flight.
For Non-Flushing Toilet:
4. Dispose of receptacle bag, if needed.
5. Clean receptacle with disinfectant.
For Relief Tube:
No other action is needed.
Note: An alternate form of relief for this item, offered in PL-83, is omitted here because it requires that the lavatory door be secured closed. The CJ2 emergency escape hatch location in the lavatory prohibits such relief, because the lavatory door is required to be open during takeoff and landing.
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SYSTEM & SEQUENCE NUMBERS
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REMARKS OR EXCEPTIONS
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52 DOORS
1. CABIN DOOR Annunciator
2. BAGGAGE DOOR FWD Annunciator
3. BAGGAGE DOOR AFT Annunciator
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(O) May be inoperative provided:
a) The door is verified CLOSED and latched,
b) The 6 lock flags are visible in the sight glass locations in the door, and
c The interior door handle securing pin is verified engaged (unable to rotate the handle without depressing the push button in the handle grip).
OPERATIONAL PROCEDURES
1. Make appropriate entry in the discrepancy report.
2. Place placard below annunciator panel stating “CABIN DOOR ANNUNCIATOR LIGHT INOP”.
3. Have a member of the flight crew verify that all 6 cabin door pin flags are visible through the sight glass locations.
4. Have a member of the flight crew verify that the cabin door handle securing pin is engaged and will not rotate without depressing the push button.
(O) May be inoperative provided the forward baggage doors are verified CLOSED and locked.
OPERATIONAL PROCEDURES
1. Make appropriate entry in the discrepancy report.
2. Place placard below annunciator panel stating “BAGGAGE DOOR FWD ANNUNCIATOR LIGHT INOP”.
3. Have a member of the flight crew verify that the Aft Baggage door is closed and latch and the lock aligns with the lock indicators.
(O) May be inoperative provided the door is verified CLOSED and locked.
OPERATIONAL PROCEDURES
1. Make appropriate entry in the discrepancy report.
2. Place placard below annunciator panel stating “BAGGAGE DOOR AFT ANNUNCIATOR LIGHT INOP”.
3. Have a member of the flight crew verify that the Aft Baggage door is closed and latch and the lock aligns with the lock indicators.
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SYSTEM & SEQUENCE NUMBERS
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REMARKS OR EXCEPTIONS
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78 ENGINE EXHAUST
1. Thrust Attenuators (SN’s 1-299)
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(O) May be inoperative provided both attenuators are hydraulically locked in the stowed position. See AFM Limitations and Abnormal Procedure: Dispatch with Attenuator Stowed.
OPERATIONAL PROCEDURES
1. Make appropriate discrepancy report entry.
2. Place a “THRUST ATTENUATOR INOP” placard next to the THRUST ATTENUATOR STOW/AUTO/TEST switch.
3. Place the THRUST ATTENUATOR STOW/AUTO/TEST switch in the “STOW” position.
4. Visually verify the thrust attenuators are in the stowed position.
NOTE: See AFM limitations and abnormal procedures.
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COPYRIGHT © 1993
CESSNA AIRCRAFT COMPANY
WICHITA, KANSAS, USA
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16 JULY 2007
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525AMELM00
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