Edu Dau-Fqp Data Page - Piper Malibu Meridian PA-46-500TP Airplane Maintenance Manual

(2) Procedure
CAUTION: DO NOT PERFORM TORQUE CALIBRATION WHEN THE ENGINE IS HOT. LET
(a) Prior to applying power to the Engine Display Unit (EDU), depress the "PAGE" switch on
the bezel of the primary EDU. While continuing to hold the "PAGE" switch depressed,
apply power to the EDU. Continue to hold the "PAGE" switch depressed until the EDU
displays the "Exceedance Data Page" in Test Mode. Release the "PAGE" switch.
(b) Depress and release the EDU "PAGE" switch until the "DAU/FQP DATA" page is displayed
(Refer to Figure 2).
(c) Pull both "DATA ACQUISITION" circuit breakers.
(d) Hold the SW-3 and SW-4 toggle switches on the DAU to either the "MIN MAX" or the
"CAL" position (Refer to Figure 3). Push in both "DATA ACQUISITION" circuit breakers
and keep holding the SW-3 and SW-4 toggle switches for a minimum of 5 seconds.
(e) On the "DAU/FQP DATA" page, verify that the mode is set to "CAL" (Refer to Figure 2).
DAU
S O F T WA RE KE Y /R EV:
CHAN NE L ID:
FQ P
S O F T WA RE K E Y/ REV:
77-10-00
PAGE 2
Apr 15/07
PIPER AIRCRAFT, INC.
PA-46-500TP, MALIBU MERIDIAN
MAINTENANCE MANUAL
THE ENGINE COOL DOWN FOR A MINIMUM OF ONE (1) HOUR PRIOR TO
PERFORMING TORQUE CALIBRATION.
DAU - F QP DATA
M OD E:
E QU IP ID :
FA IL F LAG S:
M O DE:

EDU DAU-FQP DATA Page

1 A
T EST
C10
CH 1
PASS
L EFT
1 A
CAL
TEST MODE
Figure 2
1 A
TEST
C10
C H 2
PASS
RIGHT
1 A
CAL
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