問題一覧
1
18 deg C indicates
cabin temp is 18*
2
Aircraft is cruising at FL250
all pressurization parameters are normal
3
Exhaust fault indicates
extract fan is failed or over temp is detected in the avionics
4
Fuel Xfeed operations is complete
no, left electropump must be switched off
5
Fuel Xfeed steady “ON” on VCP indicates
fuel Xfeed is in progress
6
Anti Icing Level
only 1 horn is unserviceable
7
Fault amber light indicates
aircraft performance monitoring (APM) system is faulty
8
CRZ SPD Lo indicates
aircraft speed is below expected performance (-10kts)
9
TLU LO Speed indicates
full rudder deflection is available
10
Current vertical speed is
-900 Fpm
11
LNAV on FMA indicates
Pilot uses FMS as primary navigation system
12
Yellow symbol “ADC2” displayed on PFD
ADC 1 is failed and information are coming from ADC2
13
T/O data are confirmed and speed auto mode is engaged. Which climb speed will be targeted on initial climb
115 kts
14
Pilot can tune on IESI
VHF 1
15
Propeller brake (without specific failure)
does not receive sufficient pressure to operate
16
Main blue pump OVHT
opening the cross feed restores the blue hydraulics
17
ACW gen 1 has failed
the BTC has closed automatically
18
The power levers are set to the “RAMP”
for Go Around
19
Condition levers are set from AUTO TO 100% OVRD
forces the propeller NP to 100%
20
OAT -10*, 10 KTS HDWND, QNH 1003, icing conditions, RTOW?
d. 22 800kg or 23,000 kg (according to customer options)
21
OAT -10*, 10 KTS HDWND, QNH 1003, you take off at 21 T, icing conditions: V1, VR, V2?
b. 117, 117, 121
22
OAT -10*, 10 KTS TLWND, QNH 1003, icing conditions, RTOW?
d. 23,000kg
23
Taking off at 21 T in icing conditions, VFTO?
a. 125kt
24
Landing at 21 T in NORMAL conditions, VFGA?
d. 136 kt
25
Landing at 16 T in normal conditions, VFGA ?
c. 118kt
26
Landing at 16T in icing conditions, VFGA?
d. 111kt
27
Landing at 16T in normal conditions, Zp=2000 ft, OAT + 30, VGA?
a. 104kt
28
Landing at 17T in normal conditions HDWND 29G40 kt, OAT +30C, Vapp ?
b. 107kt
29
Take off at 21 T in icing conditions Headwind 25 kt, OAT -2C, VFTO ?
d. 125kts
30
What is the Maximum demonstrated X wind on dry runway ?
a. 35 kts
31
What is the tailwind limit ?
c. 15 kts
32
What is the maximum mean runway slope ?
a. +\- 2%
33
Engine fails is cruise. You expect?
d. nothing. ATPCS is not available during cruise
34
Engine fails on final approach, you expect ?
d. nothing. ATPCS not available at low power during approach (only in case of go- around)
35
In flight, PEC “FAULT” light illuminates
b. propeller stopped is automatically protected (by the propeller speed governor)
36
In case of amber Loop light on
c. according to procedure, pilots turn off the faulty loop (to recover fire detection)
37
Oxygen system is
a. available for flight crew and passengers
38
To access the cockpit emergency hatch
a. integrated steps are available
39
In flight, “Master Caution” and EEC flashes
b. You look for the checklist, a flashing EEC is NEVER RESET
40
In case of Dual Gen loss
b. An automatic switching makes the batteries to supply some DC buses
41
In flight:
c. DC bus 2 has failed
42
DC generators
c. are not connected as long as GPU is on (external power priority)
43
Without any failures, looking to this hydraulic page indicates that propeller brake
a. does not receive sufficient pressure to operate
44
In this situation, what have you lost?
b. AHRS
45
Amber CTK indicates
b. FMS 1&2 are working in independent mode (crosstalk unserviceable)
46
Amber DISCH light indicates
b. extinguisher bottle is discharged
47
White Squib lights indicate
d. squibs are armed
48
What happens when the fire handle is pulled?
a. LP fuel valve is closed, squibs are armed,DC and ACW generators are disconnected, affected engine is feathered, affected DeIce valve is closed and affected bleed valve is closed
49
Is it possible to discharge a fire bottle from the side where fire handle is not pulled?
b. No not possible