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K. Landing Gear Manual Extension (Cont’d)
No
Any landing gear fails to lock in the down position:
(6) Gear DN Disagree Procedure ..................... Accomplish Refer to Chapter 3;
EMERGENCY
PROCEDURES – LANDING
GEAR, WHEEL AND BRAKE
SYSTEM – Gear DN
Disagree.
END
ABNORMAL PROCEDURES
Landing Gear, Wheel and Brake System
Vol. 1 05−16−11
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
ABNORMAL PROCEDURES
Landing Gear, Wheel and Brake System
Vol. 1 05−16−12
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
THIS PAGE INTENTIONALLY LEFT BLANK
1. MISCELLANEOUS SYSTEMS
A. Emergency Lighting System Selected Off
Indication: EMER LTS OFF caution message on.
(1) EMER LTS switch ................................................Check status of EMER LTS.
END
B. Crew Oxygen Low Pressure
Indication: OXY LO PRESS caution message on.
OXY pressure readout indicates less than 800 psi:
Yes
(1) Descent ....................................................... Initiate to a safe altitude.
− END −
No
(1) Crew oxygen masks ................................................Test and check pressure readout.
NOTE
If pressure remains unchanged (one bottle closed), oxygen
quantity will be one half of that indicated on the crew oxygen
consumption data chart in the Operating Manual.
(2) Oxygen quantity .................................................Monitor
OXY pressure readout drops to 0 psi (bottle(s) closed):
Yes
(3) Descent ....................................................... Initiate to a safe altitude.
− END −
No
(3) No further action required.
END
C. Passenger Oxygen Deployed and Activated (If Installed)
Indication: PAX OXY ON caution message.
(1) Passenger oxygen................................................Check status.
END
ABNORMAL PROCEDURES
Miscellaneous Systems
Vol. 1 05−17−1
REV 69, Jun 04/07
CL−604 Operating Manual
PSP 604−6
1. MISCELLANEOUS SYSTEMS (CONT'D)
D. Radio Tuning Unit Failure
Indication: Blank screen on affected RTU, or inability to tune all radios from affected
RTU.
(1) Affected RTU INHIBIT switch/light
(centre pedestal) ...............................................Press in to inhibit failed RTU.
Check RTU 1 (2) INHIB light
on.
(2) Operable RTU ...................................................... Utilize to tune cross-side radios.
END
E. Dual HF Transmission Failure
Indication: No HF transmission. Dashes displayed for HF 1 and HF 2, on RTUs
(1) HF COMM 2 circuit breakers
(2E1, 2E2 and 2E3)............................................... Open
(2) HF 1................................................................... Attempt communication.
Transmission successful:
Yes
(3) No further action required.
− END −
No
(3) HF COMM 2 circuit breakers
(2E1, 2E2 and 2E3)...............................................Close
(4) HF COMM 1 circuit breakers
(1K5, 1K6 and 1K7)............................................... Open
(5) HF 2................................................................... Attempt communication.
END
F. Flight Management System Tuning Failure
Indication: Unreliable FMS tuning data.
(1) FMS TUNE switch/light (centre
pedestal)............................................................Press in to inhibit FMS radio tuning
operation.
Check FMS TUNE INHIB light
on.
END
ABNORMAL PROCEDURES
Miscellaneous Systems
Vol. 1 05−17−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. MISCELLANEOUS SYSTEMS (CONT'D)
G. Flight Management System CDU/FMC Failure
Indication: No data available on CDU.
(1) Reversionary panel, FMS 3 switch
(if installed) ............................................................... Set to failed FMS position.
On airplanes 5500 and subsequent and airplanes incorporating Service Bulletin
604–34–031:
(2) N1 setting value................................................Deselect active N1 thrust setting from
EICAS display. Use N1 thrust
setting value displayed on
CDU(s) only.
NOTE
The input parameters on the THRUST LIMIT, TAKEOFF REF and
APPROACH REF CDU pages must be re-confirmed by the pilot
following an FMS SYNC command, an FMS 3 reversion (if installed) or
an FMS cold start.
END
ABNORMAL PROCEDURES
Miscellaneous Systems
Vol. 1 05−17−3
　
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