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1,800 psi, or pressure is rapidly decreasing:
Yes
(3) HYDRAULIC pumps 3A and
3B ................................................................................. OFF
(4) Land at the nearest suitable airport.
(5) Inoperative systems (see
below) .................................................................... REVIEW
• Inboard brakes inoperative (when system 3
accumulator pressure is depleted);
• Normal landing gear extension and retraction
inoperative;
• Nose door will remain open;
• Nose wheel steering inoperative (may have nose wheel
shimmy);
• Parking brake inoperative.
(6) ANTI-SKID..................................................LEAVE ARMED
(7) Landing Gear Manual
Extension procedure.....................................ACCOMPLISH
(See Page ABNORM 13–9)
(8) Actual landing distance...................................... INCREASE
as applicable by factor given below:
WITHOUT THRUST
REVERSERS
WITH THRUST
REVERSERS
1.70 (70%) 1.50 (50%)
NOTE
Maximize the use of reverse thrust.
− END −
No
(3) HYDRAULIC pump 3B ...............................................LEAVE ON
(4) Hydraulic pressure and fluid
quantity........................................................................MONITOR
END
ABNORM 10-4
REV 74, Nov 07/08
QUICK REFERENCE HANDBOOK
PSP 604-15
HYDRAULIC SYSTEM
MALFUNCTIONS
HYD 1 (2) HI TEMP
HYD 1 HI TEMP or HYD 2 HI TEMP
NOTE
Disregard HYD 1 (2) HI TEMP caution message if one
other hydraulic system has already failed (i.e. leave pumps
on).
During flight:
Temperature is less than 107°C (225°F):
Yes
(1) Affected HYDRAULIC pump......................................... OFF
(2) Affected system temperature...............................MONITOR
− END −
No
Temperature is less than 135°C (275°F):
Yes
(1) Affected HYDRAULIC pump......................................... OFF
(2) Affected system temperature...............................MONITOR
(3) Land at the nearest suitable airport.
− END −
No
(1) Affected HYDRAULIC pump ................................................ OFF
Affected engine:
(2) In-Flight Engine Failure/Shutdown .......................ACCOMPLISH
(See Page ABNORM 1–2)
(3) Inoperative systems ...................................................... REVIEW
(See Page ABNORM 10−2 to 10−3)
(4) Actual landing distance ............................................. INCREASE
as applicable by factor given below:
SYSTEM 1 FAILED SYSTEM 2 FAILED
1.60 (60%) 2.25 (125%)
END
ABNORM 10-5
REV 72, Jan 22/08
QUICK REFERENCE HANDBOOK
PSP 604-15
HYDRAULIC SYSTEM
MALFUNCTIONS
HYD 3 HI TEMP
HYD 3 HI TEMP
During flight:
(1) HYDRAULIC pumps 3A and 3B ........................................... OFF
(2) System No. 3 temperature ..........................................MONITOR
Temperature is more than 107°C (225°F):
Yes
(3) Land at the nearest suitable airport.
No
Prior to landing:
(3) HYDRAULIC pumps 3A and 3B ............................................. ON
END
HYD EDP 1A (2A)
HYD EDP 1A or HYD EDP 2A
(1) Affected HYDRAULIC pump .................................................. ON
(2) Hydraulic pressure and fluid
quantity............................................................................CHECK
System quantity low:
Yes
(3) Affected HYDRAULIC pump......................................... OFF
NOTE
The engine-driven pump has been operating without
hydraulic fluid. Log length of time that engine-driven
pump has been running dry. Monitor fluid temperature
readouts.
− END −
No
(3) No further action required.
END
ABNORM 10-6
REV 72, Jan 22/08
QUICK REFERENCE HANDBOOK
PSP 604-15
HYDRAULIC SYSTEM
MALFUNCTIONS
HYD PUMP 1B
HYD PUMP 1B
(1) HYDRAULIC pump 1B ........................................................... ON
HYD PUMP 1B caution message persists:
Yes
(2) HYDRAULIC pump 1B ................................................. OFF
− END −
No
(2) No further action required.
END
HYD PUMP 2B
HYD PUMP 2B
(1) HYDRAULIC pump 2B ........................................................... ON
HYD PUMP 2B caution message persists:
Yes
(2) HYDRAULIC pump 2B ................................................. OFF
− END −
No
　
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