Fokker 50 - Standby Altimeter Details; Standby Altimeter Altitude Display; Standby Altimeter Altitude Pointer; Standby Altimeter Pressure Controls

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Controls and indicators - For aircraft equipped with air data system type I, II, IV, V and VI

NOTE: Type II, the standby

altimeter is installed at the

RH main instrument panel

Fokker 50 - Flight Navigation Instruments

Page 49

Main Page

General1
Symbol Generator1
Display Units1
Primary Flight Displays1
EFIS Control Panel2
Avionics Panel2
Flight Mode Panel2
EFIS Test3
Functional Diagram4
Controls and Indicators5
Symbol Generator P/B5
Flight Mode Annunciators10
Comparator Display11
Flight Director Failure Display11
Excessive Deviation Display12
Navigation Display15
Heading Arrow16
Heading Display16
Range Display16
For Aircraft Equipped with Composite Mode25
Alerts26
Secondary Instruments27
Airspeed Indicator27
Radio Magnetic Indicator27
Altimeter28
Vertical Speed Indicator28
All29
Resolution Advisory29
Traffic Advisory29
Total Air Temperature System29
Traffic Advisory/Resolution Advisory Vertical Speed Indicator39
Standby Instruments47
Standby Horizon47
Standby Compass47
Standby Altimeter47
Terrain Awareness and Warning System (Type I)51
TAWS Display52
TAWS Display Information52
Depiction of Color Banding Within ROC Band Height52
Depiction of Color Banding above ROC Band Height53
ROC/RTC Relationship54
TAWS Graphical Symbols55
Terrain Threat55
Flight Plan55
Waypoint Idents56
Pop-Up Terrain Display56
Terrain Conflict and OFF-Flight Plan Maneuvering56
Terrain Envelope Off-Set57
System Alerts58
Forward Looking Terrain Alerts58
Required Terrain Clearance Alerts58
Imminent Terrain Impact Alerts58
Altimeter Setting Alert59
Premature Descent Alerts (PDA)60
Minimum Ground Clearance Boundary Envelope60
Basic Ground Proximity Alert Functions61
MODE 1: Excessive Rates of Descent61
MODE 2: Excessive Closure Rate to Terrain62
Operations to Plateau Airports62
Excessive Closure Rate to Terrain62
Mode 2A Envelope62
MODE 3: Negative Climb Rate or Altitude Loss after Take-Off64
MODE 4: Flight into Terrain When Not in Landing Configuration65
MODE 5: Excessive Downward Deviation from an ILS Glide Slope66
Glide Slope Inhibit66
Back Course Approaches66
MODE 6: Altitude Callouts67
Bank Angle Callouts67
Minimums & Approaching Minimums67
Aural and Visual Alert Messages67
Alert Priorities69
System Annunciators and Switches70
Display Inhibit Functions71
Navigation Display Inhibited Annunciations71
Operation72
Cold Temperature Correction72
Emergency Procedures72
Abnormal Procedures73
Build in Test74
Enhanced Ground Proximity Warning System (Type II)79
Mode Description80
BASIC GPWS Functions80
Inhibit Modes80
Steep Approach80
TAWS Functions81
Annunciation81
Excessive Bank Angle Alert81
Terrain Clearance Floor81
Geometric Altitude82
EGPWS/TAWS Alerts and Anuciations82
Taws Display Unit84
Conventional Mode Display84
Peaks Mode Display85
System Test85
System Failure86
General Switching Panel88
Altimeter Altitude Alert91
Inhibit Phases91

Fokker 50 - Standby Altimeter Details; Standby Altimeter Altitude Display; Standby Altimeter Altitude Pointer; Standby Altimeter Pressure Controls

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