Equipment list operational and



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SYSTEM & SEQUENCE NUMBERS

REMARKS OR EXCEPTIONS

26 FIRE PROTECTION
1. Portable Fire Extinguishers


(O) Any in excess of those required by FAR may be inoperative or missing provided:

a) The inoperative fire extinguisher is tagged inoperative, removed from the installed location, and placed out of sight so it can not be mistaken for a functional unit.

b) Required distribution is maintained.



OPERATIONAL PROCEDURES

1. Install a tag or placard on the inoperative fire extinguisher stating “INOPERATIVE.”

2. Remove fire extinguisher from its holder, cover it with a bag, and place it in a storage area or baggage area within the airplane.

3. Use the following formula to calculate the new empty CG of the airplane:


∆ Empty CG = (Extinguisher Wt) X (∆ Extinguisher location) / Aircraft Empty Weight
4. Make appropriate entry on the discrepancy report.




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SYSTEM & SEQUENCE NUMBERS

REMARKS OR EXCEPTIONS

27 FLIGHT CONTROLS
1. Electric Elevator Trim



DELETED: REVISION 2. AFM Limitations require the Electric Elevator Trim to be operative for takeoff.



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SYSTEM & SEQUENCE NUMBERS

REMARKS OR EXCEPTIONS

30 ICE & RAIN PROTECTION
3. Engine Anti-Ice Systems


(M) One may be inoperative provided:

a) Engine Anti-Ice Valve remains OPEN, and

b) Takeoff and landing field temperatures are not in excess of 10 degrees C.


(M) May be inoperative provided:

a) Engine Anti-Ice Valve is failed closed,

b) The flight is conducted in day VMC, and

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


NOTE: See AFM Performance Data.

MAINTENANCE PROCEDURES



CAUTION: ENGINE ANTI-ICE SWITCHES OPERATE BOTH THE WING LEADING EDGE AND ENGINE INLET SYSTEMS. DO NOT OPERATE THE SYSTEM LONGER THAN FIVE (5) MINUTES. FOLLOW TEST WITH A THIRTY (30) MINUTE COOLING PERIOD.
1. With engines shut down, make note of the temperature of the Engine Inlets (use of hand touch is sufficient).

2. Position the aircraft in a suitable run-up area.

3 Verify LH and RH ENG ANTI-ICE circuit breakers are engaged.

4. To verify whether the affected valve has failed open or closed:

a) Verify the AIR SOURCE SELECT switch, and WINDSHIELD BLEED (Anti-Ice) switch, are OFF.

b) Verify WING/ENGINE ANTI-ICE switches are OFF.

c) Set the parking brake and start both engines. Refer to AFM Normal Checklist for engine start.
NOTE: LH and RH ENG ANTI-ICE, LH and RH WING ANTI-ICE, and both MASTER CAUTION lights will illuminate at low engine power settings as a normal condition.
d) Gradually increase both throttles to achieve 70% N2.

e) After approximately 15 seconds, select Engine Anti-Ice ON for both engines. Verify both ENG ANTI-ICE annunciators illuminate.

f) As soon as each ENG ANTI-ICE annunciator extinguishes, immediately select Engine Anti-Ice OFF on that engine and gently retard the associated throttle to idle.

g) If the annunciator on the affected side extinguishes immediately, or substantially sooner than the unaffected side, the valve has failed open.

h) If the annunciator for the affected side does not extinguish within 20 seconds of the unaffected
side, retard the affected throttle to idle. The associated valve is failed closed.

i) Select both WING/ENGINE ANTI-ICE switches to OFF.

j) Shut down engines.

(Continued Next Page)






SYSTEM & SEQUENCE NUMBERS

REMARKS OR EXCEPTIONS

30 ICE & RAIN PROTECTION (Continued)
3. Engine Anti-Ice Systems (Continued)

4. Wing Anti-Ice

k) Exercising extreme caution, verify that the Engine Inlet remains cool to the touch, confirming that the Engine Anti-Ice Valve is closed. If the inlet is extremely hot to the touch, and if ENG ON was selected only momentarily, this is a further indicator that the valve failed open. If any doubt remains, repeat the engine run on the affected engine only, and DO NOT select any Anti-Ice system to ON. Then following shutdown, if inlet is hot, valve is definitely failed open.

5. Pull and secure the affected ANTI-ICE ENGINE c/b with tie-wrap.

6. Place a placard stating, “(LH/RH – as appropriate) Engine Anti-Ice INOP – failed (OPEN/CLOSED)” next to appropriate Wing/Engine Anti-Ice switch ENG ON position.

7. Make appropriate entry on the discrepancy report.

(O) One may be inoperative provided:

a) The Wing Anti-Ice Valve is failed closed, and

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


OPERATIONAL PROCEDURES
CAUTION: ENGINE ANTI-ICE SWITCHES OPERATE BOTH THE WING LEADING EDGE AND ENGINE INLET SYSTEMS. DO NOT OPERATE THE SYSTEM LONGER THAN FIVE (5) MINUTES. FOLLOW TEST WITH A THIRTY (30) MINUTE COOLING PERIOD.
1. Tape a lightweight streamer immediately aft of vent louver on the affected wing’s wingtip bottom.

2. Prior to starting engines, ensure both Precooler Doors are closed.

3. Verify L and R ENGINE ANTI-ICE and aft J-box L and R WING ANTI-ICE circuit breakers are engaged.

4. Verify AIR SOURCE SELECT is in OFF position.

5. Verify WING XFLOW switch is selected OFF.

6. Verify WINDSHIELD BLEED switch is selected OFF.

7. Verify non-affected WING/ENG ANTI-ICE switch is selected OFF.

8. Start the affected engine and run at idle.


NOTE: ENG ANTI-ICE LH or RH, WING ANTI-ICE LH or RH annunciators, as well as the MASTER CAUTION will illuminate at low throttle settings as a normal condition.
9. Gradually increase engine throttle to above 70 percent N2. Any observed airflow at the wingtip streamer indicates valve has failed open.

10. Place appropriate WING/ENG ANTI-ICE switch to WING/ENG position.

11. Observe wingtip streamer. Lack of airflow indicates the Wing Anti-Ice Valve has failed closed. Constant illumination of the appropriate WING ANTI-ICE annunciator also indicates that the valve has failed closed. Presence of airflow at the wing tip vent or annunciator extinguishing indicates valve has not failed closed.

(Continued Next Page)




SYSTEM & SEQUENCE NUMBERS

REMARKS OR EXCEPTIONS

30 ICE & RAIN PROTECTION (Continued)
4. Wing Anti-Ice (Continued)

12. Select appropriate WING/ENG ANTI-ICE switch to OFF.

13. Shut engine down.

14. Using extreme caution, feel the affected Wing Leading Edge. Ambient temperature (same as unaffected wing) is a further indicator that the Wing Anti-ice Valve has failed closed.

15. Place a placard stating, “(LH/RH – as appropriate) Wing Anti-Ice INOP – failed (OPEN/CLOSED)” next to the appropriate WING/ENG ANTI-ICE switch WING/ENG position.

16. Make appropriate entry on the discrepancy report.

17. Remove lightweight streamer from affected wing.



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