WorksheetsCJ3 - 16-17
Total questions: 27
Worksheet time: 14mins
Name
Class
Date
1.
1. The cockpit oxygen pressure gauge reads:
a)
A. The oxygen pressure which is present at the crew masks
b)
B. Electrically derived system low pressure
c)
C. Bottle pressure
d)
D. Electrically derived system high pressure
2.
2. Passenger masks are dropped when:
a)
A. The OXYGEN CONTROL VALVE knob is in the NORMAL position and cabin altitude exceeds 14,500 feet
b)
B. The cabin altitude exceeds 14,500 feet, regardless of OXYGEN knob position
c)
C. The OXYGEN CONTROL VALVE knob is in the MANUAL DROP position, regardless of altitude
d)
D. Both A and C
3.
3. If DC power fails, placing the OXYGEN CONTROL VALVE knob in:
a)
A. MANUAL DROP deploys the passenger masks, regardless of cabin altitude.
b)
B. MANUAL DROP deploys the passenger masks only if 14,500 feet cabin altitude is exceeded.
c)
C. CREW ONLY does not restrict oxygen to the crew only if the cabin altitude is above 14,500 feet.
d)
D. Any of the three operating positions does not route oxygen to the passengers—they have their own oxygen.
4.
4. The purpose of the altitude pressure switch is to:
a)
A. Bypass oxygen flow directly to the passengers regardless of OXYGEN CONTROL VALVE knob position.
b)
B. Open a solenoid at 14,500 feet cabin altitude, allowing oxygen flow to the passenger oxygen distribution system.
c)
C. Close a solenoid valve at 14,500 feet cabin altitude, stopping oxygen flow to the passengers.
d)
D. Restore cabin altitude to 8,000 feet so that oxygen is not required.
5.
5. If the OXYGEN CONTROL VALVE knob is in the CREW ONLY position:
a)
A. The passenger masks cannot be dropped automatically.
b)
B. The passenger masks do not deploy automatically, but they can still be dropped manually.
c)
C. The passengers still receive oxygen if the cabin altitude is above 8,000 feet.
d)
D. Normal DC power is removed from the passenger mask door actuators, thus pre- venting them from dropping the masks.
6.
6. If normal DC power is lost with the OXYGEN CONTROL VALVE knob in the NORMAL position:
a)
A. The passenger masks deploy immediately, regardless of the cabin altitude.
b)
B. The passenger masks cannot be dropped manually.
c)
C. The oxygen pressure gauge on the copilot panel is inoperative.
d)
D. Automatic dropping of the passenger masks does not occur.
7.
1. The standby HSI receives its heading data from:
a)
A. AHRS 1
b)
B. AHRS 2
c)
C. AHRS 3
d)
D. A self-contained directional gyro
8.
2. In order to fully function, the autopilot and yaw damper both require:
a)
A. One valid AHRS
b)
B. Two valid AHRS without attitude miscompares
c)
C. Three AHRS
d)
D. No AHRS
9.
3. Your PFD shows red flags of IAS, ALT, and VS. Which reversion control should you use?
a)
A. AHRS REV
b)
B. DADC REV
c)
C. Display REV TO MFD
d)
D. Display REV TO PFD
10.
4. Without normal aircraft DC power, the standby fight display battery should last:
a)
A. 10 minutes
b)
B. 30 minutes
c)
C. 60 minutes
d)
D. 88 minutes
11.
5. Normally needed FMS data entry items are indicated by:
a)
A. Boxes
b)
B. Dashes
c)
C. Blue brackets
d)
D. All the above
12.
6. Localizer-based approaches may be flown from the FAF to the runway using the Collins FMS as the lateral navigation source.
a)
A. True
b)
B. False
13.
7. If any data (other than messages) appear in yellow on any FMS CDU page:
a)
A. Some parameter is in error
b)
B. The FMS cannot enter the approach mode
c)
C. Not applicable; yellow is not used
14.
8. In order for the left PFDs NAV source to auto- swap from FMS to LOC:
a)
A. A localizer-based approach must be entered into the FMS
b)
B. The aircraft must be within 30 nm of that airport
c)
C. Either APPR or B/C on the mode select panel must be pushed
d)
D. All the above
15.
9. To enter airways into the fight plan:
a)
A. The airway designator is entered on the ROUTE line of the LEGS page
b)
B. The waypoints where you get on and of the airway must be on the FPLN page
c)
C. The airway designator can only be entered under the VIA column on the FPLN page, on the line immediately after the waypoint where you get on the airway
d)
D. Both B and C
16.
10. GPS approaches flown to an MDA usually use which mode select buttons?
a)
A. NAV and APPR
b)
B. NAV and VNAV
c)
C. APPR and VNAV
d)
D. GPS approaches using the FMS are not authorized
17.
11. To move the controlling FGC arrow from the left side to the right side:
a)
A. Select NAV 2 or FMS 2 as the active NAV source
b)
B. The aircraft can only be flown from the left side; you cannot move FGC to the right
c)
C. Press the AP XFR button on the autopilot panel and reprogram the fight director
d)
D. Get out of the left seat and move to the right (seat sensor installed)
18.
12. The FMS TUN page can be used to control ATC modes, TCAS test, and marker beacon sensitivity.
a)
A. True
b)
B. False
19.
13. For VNAV to fly a descent path, the Collins FMS must be the active NAV source and:
a)
A. An altitude constraint at a waypoint must be entered on the LEGS page
b)
B. VNAV must be on
c)
C. The altitude preselector must be lowered below the current cruising altitude (normally to the altitude cleared to by ATC)
d)
D. All the above
20.
14. A type 6 FMS is currently authorized for use to fly to which minima?
a)
A. LNAV (MDA)
b)
B. LNAV/VNAV (DA)
c)
C. LPV (DA)
d)
D. Both A and B
21.
15. The Collins FMS and the Garmin GPS receiver communicate with each other in all aspects.
a)
A. Always
b)
B. Sometimes
c)
C. Only for charts
d)
D. Never
22.
16. The left PFD is displaying a PPOS map from FMS 1. Which statement is correct?
a)
A. A PLAN map from FMS 1 may be shown on the MFD at the same time.
b)
B. TERR may be shown on the left PFD with weather radar at the same time.
c)
C. A PLAN map can be displayed on the MFD, but only after the left PFD is not displaying the PPOS map.
d)
D. NEXRAD radar images can be shown on the PPOS map.
23.
17. The IFIS panel displays charts and graphic weather on the:
a)
A. Left PFD only
b)
B. Right PFD only
c)
C. Left PFD and/or MFD
d)
D. MFD only
24.
18. Both PFDs and the MFD must be fully operational without any reversions prior to dispatch.
a)
A. True
b)
B. False
25.
19. The CE-525 is certified for Cat II ILS operations.
a)
A. True
b)
B. False
26.
20. The radar altimeter is tested:
a)
A. Once a year by maintenance
b)
B. When the ground proximity system (Honeywell or Landmark) is tested
c)
C. When the rotary test knob is in the ANNU position
d)
D. Never; that is why question 19 is FALSE
27.
21. A type 7 FMS may fly to LPV minima provided:
a)
A. WAAS is operational
b)
B. An appropriate approach has been executed in the FMS
c)
C. Airport temperature is within the limits shown on the chart
d)
D. Both A and B
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