• Home
  • Download PDF
  • Order CD-ROM
  • Order in Print

Home > Aviation Maintenance and Training Volume 2 > > Fig 6:  HYD 2 Pump Failure
Fig 5:  HYD 1 Pump Failure
Fig 7:  Total Hydraulic Failure

Emergency Flight Procedures - index
Page Navigation
  86    87    88    89    90  91  92    93    94    95    96  
T-45C TS, ADV & IUT EMFP-04
Engine and Hydraulic Emergency Procedures
NOTE: If the failure of HYD 2 results from an
engine-driven pump (EDP) failure (with no leak),
then pressure is supplied by the RAT through the
Emergency Hydraulic system. If the failure
includes a complete or continuing loss of fluid,
then cycling pressure (indicative of RAT
operation) may be only temporary, if it occurs at
all.
d.
RAT continues to operate normally--i.e., gauge
Overlay 3
continues to fluctuate between approx 2,500 and
3,000 psi
Figure 6: HYD 2 PUMP FAILURE
Original (9-98)
Page 4-14






Western Governors University
< Previous Page
Index ^
Next Page >

Privacy Statement
Press Release
Contact

© Copyright Integrated Publishing, Inc.. All Rights Reserved. Design by Strategico.