When will the NG digital readout appear on the power pod?
- When NG increases above 100%,
- the difference between NG1 and NG2 exceeds 5%,
- or one either engine is out
When will TGT be indicated on the power pod?
- When TGT indications are above 793°C,
- there is a difference of 75°C or more between TGT1 and TGT2,
- or when an engine is out
Why do we avoid operation of NP between the 20 to 40 and 60 to 90 range?
Because vibrations at the input module can contaminants, tracked by IVHMS
What does FMDS (flight mission display system) include?
- reversionary switch panel -electronic flight information system (EFIS boxes) junction boxes
- MFSCs (Multifunction and collective slew controllers)
What are the pilot and copilot revisionary switch panels used for?
ATT Is for selecting either... HDG Is for selecting either... ADC Is for selecting either... FMS Is for selecting either... DCU Is for selecting either...
Used to select a secondary data source.
ATT Is for selecting either EGI attitude source
HDG Is for selecting either EGI heading source
ADC Is for selecting either Air Data Computers
FMS Is for selecting either the pilot or copilot FMS as the navigation source
DCU Is for selecting either DCUs for EICAS (DCU) data
On the ADI (Attitude direction indicator) magenta cross pointer, what does a dot represent for: VOR TACAN LOC BC FMS Enroute
VOR: 5° /dot
TACAN: 5° /dot
LOC BC; 2.5° /dot
FMS Enroute: 2 NM /dot
ILS course and glideslope guidance cues are represented by magenta diamonds. The ILS lateral deviation scale is expanded to provide more precise course guidance.
ILS lateral scaling is still…
Glideslope scale is standard at…
ILS lateral scaling is still 1.25°/dot
Glideslope scale is standard at 0.25°/dot
The radar altimeter read out range is from… to …, and is removed above…. It’s redisplays below…
The radar altimeter read out range is from-20 to 1500, and is removed above 1500. It’s redisplays below 1400
If the winds are less than… they will not be displayed.
Wind display read out will always be yellow when the IAS < …
What do the following mean:
Receiver autonomous integrity monitoring
I failure of EGI would result in what two major items being removed from the primary flight display?
ADI & HSI
The course points are can be a trusted by the OBS knob for all navigation sources except?
Strikes are indicated with a…
And cells are indicated with a…
The B/U pump will come on when:
- RSVR 1 LOW
- HYD PUMP 1 FAIL
- T/R SERVO 1 FAIL
- HYD PUMP 2 FAIL
- APU ACCUM LOW
The #1 Hydraulic pump supplies hydraulic pressure to…
- the first stage (fore, aft, lateral) primary servos
- first stage tail rotor servo