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(d) BLEED AIR, APU LCV
switch/light .......................................Press out to match APU load control
valve closed position.
No
(1) APU, PWR FUEL switch/light..........................Press out
(2) Do not restart APU.
END
EMERGENCY PROCEDURES
Auxiliary Power Plant
Vol. 1 03−07−4
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. BLEED AIR LEAKS
A. 10TH Stage, Left Bleed Duct Failure
Indication: L 10TH DUCT warning message and “BLEED AIR DUCT” aural on:
(1) BLEED AIR, 10TH STAGE, L
switch/light .......................................................Press out to close bleed air valve.
Check L 10TH STAGE
CLOSED light on.
(2) BLEED AIR, APU LCV switch/light..................Press out to close APU load control
valve.
Check APU LCV OPEN light
out.
(3) BLEED AIR, 10TH STAGE ISOL
switch/light .......................................................Press out to close ISOL valve.
Check 10TH ISOL OPEN light
out.
(4) AIR-CONDITIONING, L PACK
switch/light .......................................................Press out to shutdown pack.
Check L PACK OFF light on.
Above 40,000 feet:
Yes
(5) ANTI-ICE, L COWL
switch/light .................................................Press in to select left engine cowl
anti-ice system on.
Check L COWL A/ICE ON
advisory message on.
No
Warning message persists:
Yes
(5) Left thrust lever............................................ Retard to eliminate warning.
L 10TH DUCT warning message still persists (after 30 seconds):
Yes
(6) In-Flight Engine
Failure/Shutdown..........................Accomplish Refer to Chapter 5;
ABNORMAL PROCEDURES
– POWER PLANT – In-Flight
Engine Failure/Shutdown.
− END −
No
(5) No further action required.
END
EMERGENCY PROCEDURES
Bleed Air Leaks
Vol. 1 03−08−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. BLEED AIR LEAKS (CONT'D)
B. 10TH Stage, Right Bleed Duct Failure
Indication: R 10TH DUCT warning message and “BLEED AIR DUCT” aural on:
(1) BLEED AIR, 10TH STAGE, R
switch/light .......................................................Press out to close bleed air valve.
Check R 10TH STAGE
CLOSED light on.
(2) BLEED AIR, 10TH STAGE ISOL
switch/light .......................................................Press out to close ISOL valve.
Check 10TH ISOL OPEN light
out.
(3) AIR-CONDITIONING, R PACK
switch/light .......................................................Press out to shutdown pack.
Check R PACK OFF light on.
Above 40,000 feet:
Yes
(4) ANTI-ICE, R COWL
switch/light .................................................Press in to select right engine cowl
anti-ice system on.
Check R COWL A/ICE ON
advisory message on.
No
Warning message persists:
Yes
(4) Right thrust lever ......................................... Retard to eliminate warning.
R 10TH DUCT warning message still persists (after 30 seconds):
Yes
(5) In-Flight Engine
Failure/Shutdown..........................Accomplish Refer to Chapter 5;
ABNORMAL PROCEDURES
– POWER PLANT – In-Flight
Engine Failure/Shutdown.
− END −
No
(4) No further action required.
END
EMERGENCY PROCEDURES
Bleed Air Leaks
Vol. 1 03−08−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. BLEED AIR LEAKS (CONT'D)
C. 14TH Stage, Left/Right Bleed Duct Failure
Indication: L (R) 14TH DUCT warning message and “BLEED AIR DUCT” aural on.
Affected engine:
(1) BLEED AIR, 14TH STAGE L (R)
switch/light .......................................................Press out to close bleed air valve on
affected engine.
Check L (R) 14TH STAGE
CLOSED light on.
NOTE
1. Avoid icing conditions.
2. Cowl anti-icing will not be available on the affected engine.
3. The thrust reverser is inoperative on the affected engine.
Wing anti-ice required:
Yes
(2) BLEED AIR, 14TH STAGE
ISOL switch/light........................................Press in to open 14th-stage bleed air
isolation valve.
Check 14TH ISOL OPEN light
on.
No
Warning message persists:
Yes
(2) Affected thrust lever..................................... Retard to eliminate warning.
L (R) 14TH DUCT warning message still persists:
Yes
(3) In-Flight Engine
Failure/Shutdown..........................Accomplish Refer to Chapter 5;
　
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