EFTA00277580Set 9
2002-10-16387p87,076w
master avionics switch) is on.
Symptom 1 Power is not available to ASE
be illuminated when power is O Verify that the ASE system circuit breaker is closed.
System
Handset ... inspect the displays of all installed handsets in the system. If all handsets
not illuminated arc off, proceed to the next bullet in this list. If most handsets are illuminated ... system. Repair or
displays are handset display(s) are not reconnect any obvious problems.
illuminated) illuminated, the user/operator should O If needed, ring out the power lines per the system
https://www.justice.gov/epstein/files/DataSet%209/EFTA00277580.pdf
EFTA01122646Set 9
78p28,263w
cold position, and the duct
overheat light next to the associated temperature controller will illuminate.
If the automatic temperature regulator and the duct overheat protection both
fail, to prevent ... valves will close, both pack fans will stop and
both pack trip lights will illuminate. In addition, an engine fail light will
illuminate on each side of the pilot ... temperature. Should the aft cabin ducting overheat an amber light
on the panel will illuminate. Both zone control valves will close and the needle
will centre. The flight engineer
https://www.justice.gov/epstein/files/DataSet%209/EFTA01122646.pdf
EFTA01331032Set 10
2012-02-06403p85,460w
master avionics switch) is on.
Symptom I Power is not available to ASE
be illuminated when power is O Verify that the ASE system circuit breaker is closed ... inspect the displays of all installed handsets in the system. If all handsets
not illuminated Because the failure of a handset are off, proceed to the next bullet in this ... list. If most handsets arc illuminated, but
display is unlikely, a 'dead' display one is not, then proceed to Symptom 2.
(One or more suggests that there is a problem
https://www.justice.gov/epstein/files/DataSet%2010/EFTA01331032.pdf
EFTA01329414Set 10
2019-08-27310p50,053w
IIDS — Press to test all three displays. Observe parameter slewing, test results,
and illumination of these auxiliary warning lights:
Master Warning Panels
Engine control lights, press to dim
Landing gear ... affected.
If using battery power, depressing the copilots display test button will not illuminate
the auxiliary warning lights.
Document Number 213941-FMS-01
FAA APPROVED DATE: APR./27/2016 Revision ... Annunciators only indicate loss of GPS
position information for the transponders and will not illuminate with an ADC failure.
Document Number 21394-FMS-01
FAA APPROVED DATE: APR/27/2016 Revision
https://www.justice.gov/epstein/files/DataSet%2010/EFTA01329414.pdf
EFTA01105909Set 9
22p6,179w
overhead panel. BLEED AIR section)
opens the isolation valve. A 'bar in the switch illuminates to fill in the
crossover manifold line engraved on the BLEED AIR panel, signifying that ... displayed on CAS. On SPZ-
8000 equipped airplanes, an amber BLEED CONFIG light illuminates
above each navigation display. See Figure 5. After a five second delay,
risplay of the annunciation ... load control valve and the
isolation valve. The ON legend in the switch illuminates. APU bleed air then
flows through a check valve in the APU bleed air duct into
https://www.justice.gov/epstein/files/DataSet%209/EFTA01105909.pdf
EFTA01186744Set 9
22p6,179w
overhead panel. BLEED AIR section)
opens the isolation valve. A 'bar in the switch illuminates to fill in the
crossover manifold line engraved on the BLEED AIR panel, signifying that ... displayed on CAS. On SPZ-
8000 equipped airplanes, an amber BLEED CONFIG light illuminates
above each navigation display. See Figure 5. After a five second delay,
risplay of the annunciation ... load control valve and the
isolation valve. The ON legend in the switch illuminates. APU bleed air then
flows through a check valve in the APU bleed air duct into
https://www.justice.gov/epstein/files/DataSet%209/EFTA01186744.pdf
EFTA01199853Set 9
2014-07-0131p8,945w
selected Satcom ON using Pedestal
switch and monitored sequence, found "NOT RDY" light remained illuminated for
approx 20 mins but did not hear relay "clack" a second time after inital ... GENEVA < DRAFT >
Workorder No.: GVBBJ239
boot-up. After approx 20 mins of "NOT RDY" illuminated, found system remained on
and "clack" as descibed by crew not apparent.
Gained access ... Cargo Compartment.
Carried out self-test on SDU, found SDU PASS. SYS FAIL illuminated in addition
and following fault displayed:
HI GAIN ANT (TOP/L)
Connected maintenance Laptop to SDU using
https://www.justice.gov/epstein/files/DataSet%209/EFTA01199853.pdf
EFTA00285909Set 9
2016-12-16336p96,026w
Standard Model and the Higgs boson and beyond,
with lucid detail and insight, illuminating vividly not only the achieve-
ments themselves but also the joy of creative thought and discovery ... section, the Allegory of the Cave.
But in spite of its early provenance, it illuminates more directly and more
clearly both the potential necessity and the potential perils of searching ... blank wall. Their only view of the real world is that wall,
which is illuminated by a fire behind them, and on which they see shad-
ows moving. The shadows
https://www.justice.gov/epstein/files/DataSet%209/EFTA00285909.pdf
EFTA02705525Set 11
22p6,232w
overhead panel, BLEED AIR section)
opens the isolation valve. A "bar in the switch illuminates to fill in the
crossover manifold line engraved on the BLEED AIR panel, signifying that ... displayed on CAS. On SPZ-
8000 equipped airplanes, an amber BLEED CONFIG light illuminates
above each navigation display. See Figure 5. After a five second delay.
display of the annunciation ... load control valve and the
isolation valve. The ON legend in the switch illuminates. APU bleed air then
flows through a check valve in the APU bleed air duct into
https://www.justice.gov/epstein/files/DataSet%2011/EFTA02705525.pdf