3. Standby Flight
Displays (cont’d)
|
|
|
|
|
|
|
|
*** 3) 3-in-1 (Color Video Display) (GV Only) (cont’d)
|
|
|
|
|
|
|
|
*** c) Glideslope / Localizer Function
|
C
|
1
|
0
|
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
*** d) DME Displays
|
C
|
-
|
0
|
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
*** e) FMS Navigation
Functions
|
C
|
1
|
0
|
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
(continued)
|
|
|
|
|
|
|
|
3. Standby Flight
Displays (cont’d)
|
|
|
|
|
|
|
|
*** 4) 4-in-1 Standby
Attitude, Altitude,
Airspeed Indicator
Heading (Color Video Display) (GV-SP, GIV-X)
|
C
|
-
|
0
|
Except for ER operations, the Attitude position indicator may be inoperative provided not required by Operating Requirements.
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
|
B
|
-
|
0
|
Attitude Position indicator may be inoperative provided:
a) Operations are conducted in Day VMC only, and
b) Operations are not conducted into known or forecast VFR-on-Top Conditions.
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
*** a) Standby Air Data
Unit (Altitude and
Airspeed Function)
|
C
|
1
|
0
|
May be inoperative provided the airplane is operated in day VMC only.
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
*** b) Standby Heading
Display
|
C
|
1
|
0
|
May be inoperative provided all three (3) Heading Reference Systems are operative.
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
(continued)
|
|
|
|
|
|
|
|
3. Standby Flight
Displays (cont’d)
|
|
|
|
|
|
|
|
*** 4) 4-in-1 (Color Video Display) (GV-SP, GIV-X) (cont’d)
|
|
|
|
|
|
|
|
*** c) Glideslope/
Localizer Function
|
C
|
1
|
0
|
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
*** d) DME Displays
|
C
|
-
|
0
|
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
*** e) FMS Navigation
Functions
|
C
|
1
|
0
|
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
4. Weather Radar
Systems
|
C
|
-
|
-
|
Except for ER operations, one or more system(s) may be inoperative provided the weather reports or forecasts available to the commander indicate that cumuli-nimbus clouds or other potentially hazardous weather conditions, which could be detected by the system(s) when in working order, are unlikely to be encountered on the intended route of any planned diversion therefrom.
|
None required.
|
None required.
|
An Inoperative Placard will be placed on Radar Control Heads and will be noted on ADLS.
|
5. VOR/ILS
Navigation Systems
|
C
|
-
|
-
|
As required by Operating Requirements and no relief may be provided to an inoperative system or component if powered by an emergency bus.
|
None required.
|
None required.
|
An Inoperative Placard will be placed on affected RFMU and will be noted on ADLS.
|
6. Marker Beacon
Systems
|
B
|
-
|
0
|
One or more may be inoperative for IFR operations, provided approach procedures do not require marker fixes.
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
|
D
|
-
|
0
|
One ore more may be inoperative for VFR operations.
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
7. Automatic Direction
Finding Systems
|
-
|
2
|
-
|
As required by Operating Requirements.
|
None required.
|
None required.
|
An Inoperative Placard will be placed on or next to affected ADF Indicator and will be noted on ADLS.
|
8. SSR Transponder
|
|
|
|
|
|
|
|
1) Mode A/C Functions
|
C
|
-
|
-
|
Any in excess of those required for the route to be flown may be inoperative.
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
|
A
|
-
|
0
|
(O) May be inoperative for a maximum of 5 flights provided:
-
Permission is obtained from the Air Navigation Service Provider(s) along the route of any planned diversions, and
-
Flight is conducted under VFR over routes navigated by reference to visual landmarks.
NOTE: Mode C function is required to operate for RVSM operations.
|
None required.
|
Flight crew will coordinate with the appropriate ANSP for permission to fly with inoperative Mode A or C.
Flight crew will conduct the flight under VFR conditions over routes navigated by reference to visual landmarks to prevent getting lost.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
2) Mode S Function
|
D
|
-
|
0
|
Any in excess of those required for the route to be flown may be inoperative.
NOTE: A SSR transponder with an operative MODE S function is defined as a transponder which can provide at least elementary Surveillance capability.
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
| |
(continued)
|
C
|
-
|
0
|
One or more may be inoperative provided permission is obtained from the Air Navigation Service Provider(s) when required for the intended route.
NOTE 1: A SSR transponder with an operative MODE S function is defined as a transponder which can provide at least elementary Surveillance capability.
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
8. SSR Transponder
|
|
|
|
|
|
|
|
2) Mode S Function
(cont’d)
|
|
|
|
|
|
|
|
|
|
|
|
NOTE 2: Altitude reporting, provided by an SSR transponder Mode S function, is required for ACAS II operation. Refer to item 34-19 for flight with ACAS II inoperative.
NOTE 3: Altitude reporting, provided by an SSR transponder Mode S function, is required for flight into RVSM airspace.
|
|
|
|
3) Enhanced Surveillance Functions (if installed)
|
D
|
-
|
0
|
One or more Downlink Aircraft Parameters (DAP’s), which provided Enahnced Surveillance, may be inoperative when not required for the intended route.
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
|
C
|
-
|
0
|
One or more Downlink Aircraft Parameters (DAP’s), which provided Enahnced Surveillance, may be inoperative when required for the intended route.
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
9. Distance
Measuring Equipment
(DME) Systems
|
D
|
-
|
-
|
Except when en route operations or approach minimums require its use, any in excess of those required by Operating Requirements may be inoperative.
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
10. Standby RMI
*** (Electro-Mechanical)
|
C
|
1
|
0
|
May be inoperative provided all three (3) IRS's are operative.
|
None required.
|
None required.
|
An Inoperative Placard will be placed on Standby RMI (GV) and will be noted on ADLS.
|
*** 1) Standby Navigation
Display (Color Video)
|
C
|
1
|
0
|
May be inoperative provided all three (3) IRS’s are operative.
|
None required.
|
None required.
|
An Inoperative Placard will be placed on the EBDI (GV-SP/GIV-X) and will be noted on ADLS.
|
*** 2) DME Displays
|
C
|
2
|
0
|
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
11. Radio Altimeter
Systems
|
C
|
2
|
0
|
May be inoperative provided:
a) Landing weather minimums or operating procedures do not require its use, and
b) Other systems affected (E/GPWS, ACAS, Flight Director, Autopilot, Autothrottle, Altimeter Ground Awareness Display, Synthetic Vision Primary Flight Dispaly) are considered.
|
None required.
|
None required.
|
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
|
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