All Flashcards
(221 cards)
0
Q
What is the function of the tensator motor
A
Counterbalance the main entrance door during opening and closing
1
Q
Where is the tensator
A
Top step of entry door
2
Q
Maximum certified number of occupants?
A
17 occupants
3
Q
Maximum air temperature for flight?
A
ISA +35c
4
Q
What is the minimum temperature for takeoff and landing?
A
-40c
5
Q
What is the minimum en route temperature?
A
-75C
6
Q
What is the maximum crosswind component for takeoff and landing?
A
30 knots
7
Q
What is Vmo below 12,000 feet with ventral tank empty?
A
335 KIAS
8
Q
What is Vmo with ventral tank full?
A
280 KIAS
9
Q
What is maneuvering speed Va?
A
196 KIAS
10
Q
What is the maximum speed to meet bird strike requirements?
A
280 KIAS up to 8,000 feet
11
Q
What is the maximum speed permitted with flaps15?
A
220 knots
12
Q
What are the maximum and minimum airport pressure altitudes for takeoff and landing?
A
+9000
-2000
13
Q
What is the maximum operating altitude?
A
41,000 feet
14
Q
What is the maximum taxi and ramp weight?
A
800 xp and modified -28,120 pounds
800 - 27,520 pounds
15
Q
What is the maximum landing weight?
A
23,350 pounds
16
Q
What is the maximum zero fuel weight?
A
800XP - 18,450 pounds
800 - 17,520 pounds
17
Q
What are the estimated flight planning fuel burns per hour?
A
Hour 1: 2,000 PPH
Hour 2 and sub: 1,500 PPH
18
Q
What is the estimated fuel burn for an instrument approach?
A
200 pounds
19
Q
What is the estimated true airspeed for planning?
A
420 Knots
20
Q
Which engine is the critical engine?
A
Windward side engine
21
Q
What is the required missed approach climb gradient at the destination airport?
A
Single engine miss: 2.1%
2-engine baulked landing: 3.2%
22
Q
What is the minimum flap retraction speed on single engine departure?
A
800XP - V2 + 10
800 - V2 + 9
23
Q
What is the maximum airport elevation for using tabulated takeoff data?
A
800 XP : 8,000
800: 6,000 feet
24
What is the Minimum Altitude for the Use of
| the Yaw Damper or Autopilot?
400 Feet AGL
25
How Often is the FMS NAV Database Updated?
Every 28 Days
26
Are Circling Approaches Supported by the
| NAV Database?
NO
27
What is the Maximum Bank Angle
Commanded by the FMS in Holding,
Procedure Turns, and Arc Segments?
27°
28
How Many Seconds Prior to a Lateral Course
| Change Does the Lateral Track Alert Appear?
30 Seconds
29
What is the Function of the CLR Key
| (Honeywell)?
Erase Information in the Scratch Pad
30
What is the Standard Course Intercept Used
| by the FMS?
45°
31
What Are the Electrical Requirements for
| Using a Ground Power Unit (GPU)?
28 Volts / 1500 Amps
32
All FMS Tasks May Be Accessed Through
| Which Three Menu Keys?
PERF
NAV
DIR
33
Where is the Switch for Emergency Lighting
| Located?
In the Cockpit on the Pilot’s Overhead Panel
34
Where Are the Inverter Switches Located?
Typically on the Overhead Panel
35
Where Are the Inverters Installed?
The Rear Bay
36
What is the Maximum Continuous Generator
| Load in Flight?
300 Amps
38
Approximately How Many Minutes of Battery
Power Do You Have With the Loss of All
Generated Power?
- 800 XP: 30 Minutes
| - 800: 60 Minutes (1 Hour)
38
What is the Minimum NiCad Battery
| Temperature for Takeoff?
-10°C
39
What Will Placing the Battery Switch to
| EMERGENCY Ensure?
- Both Batteries Supply Power to Close
Both Emergency Contactors
- Both Battery Charge Contactors Are
Opened
40
What is the Maximum Battery Charge Rate
| Before Takeoff?
20 Amps
41
Where Are the Engine and APU Fire
| Extinguisher Bottles Located?
Rear Bay
42
How Many Portable Fire Extinguishers MUST
| Be On the Aircraft?
2
43
What Are the Contents of the Sealed
| Stainless Steel Fire Loops?
- Helium
| - Hydrogen Gas-Saturated Metallic Core
44
Where is the Power Source for Shot 1 to
| Either Engine?
PE Bus
45
What is the Power Source for Shot 2 to Either
| Engine?
PS-2
46
How Many Lights Will Illuminate When
| Testing the Engine Fire Warning System?
5
47
What is the Maximum 15° Flap Speed?
220 KIAS
48
What is the 800XP Maximum Altitude Allowed
| With Landing Gear or Flaps Lowered?
20,000 Feet
49
What is the Power Source for the Rudder
| Bias System?
LP Bleed Air From Each Engine
50
How Many Channels May Be Used by the
| Stall Ident System?
3
51
How Many Channels Are Used by the Stall
| Ident System to Activate the Pusher?
At Least 2
52
How Long After Takeoff is the Stall Ident
| System Inhibited?
6 Seconds
53
What Controls the Speed of the Electric Trim
| System?
Flap Position
54
What is the Maximum Fuel Temperature?
+57°C
56
What is the Minimum Fuel Ambient
| Temperature With Jet A Fuel?
Takeoff: -35°C
| Flight: -38°C
56
How Many Fuel Tanks Are Installed on the
| Hawker 800/800XP?
13 with ventral
57
How Many Fuel Tanks Are Installed on the
| Hawker 800/800XP?
- 13 Total
- 6 in Each Wing (12)
- Ventral Tank
58
What is the Maximum Fuel Imbalance
| Between Wings Before and In Flight?
500 Pounds
59
When Can Fuel Transfer From the Ventral
| Tank to the Wing Tanks Be Initiated?
Fuel in Each Wing Reduced to 3,300 Pounds
60
How Long Does it Take to Transfer Fuel From
the Ventral Tanks to the Wing Tanks With
BOTH DC Boost Pumps Operating?
Approximately 20 Minutes
61
What it the MINIMUM Fuel Quantity in Each
Wing to Permit Takeoff With Fuel in the
Ventral Tank?
3,450 Pounds
62
What Fuel Pressure Does the Reducing Valve
| Establish During Single Point Refueling?
25 PSI
63
What is the Maximum Speed With Fuel in the
| Ventral Tanks?
280 KIAS
64
What is the Maximum Fuel Quantity in
| Pounds / Gallons?
10,000 lbs / 1,500 Gallons
65
What is Normal Hydraulic System Operating
| Pressure?
3,000 PSI
66
What is the Capacity of the Main Hydraulic
| System Reservoir?
2.4 US Gallons
67
What Type of Hydraulic Fluid is Approved
| For Use in the Hawker 800/800XP?
MIL-H-5606
68
The HYD 1 & LOW PRESS Lights Illuminate
| Below What Pressure?
1,500 PSI (After 57 Second Delay)
69
How Much Pressure is Trapped by the
Pressure Maintaining Valve for Normal
Braking and Stall Ident?
2,300 PSI
70
When Will the AUX HYD LOW LVL Light
| Illuminate?
Aux Hydraulic Reservoir Approximately
| ½ Pint Low
71
What Pressure Will Open the Full Flow Relief
| Valve to Relieve System Pressure?
800: 4000 PSI
72
What Temperature Will Illuminate the HYD
| OVHT Amber Light?
90°C
73
What is the Capacity of the Auxiliary
| Hydraulic System?
6 U.S. Pints
74
What is the Power Source For the Rotary Ice
| Detector Motor?
XS-2
75
```
Which System(s) Can Be Powered by the
Auxiliary Hydraulic System?
```
Landing gear
| Flap
76
Which Windscreen Panels Are Heated?
“A” and “B” Panels
77
Under What Conditions Should Engine
| ANTICE be Selected?
Operating in Visible Moisture to Include
Takeoff and Landing and Temperatures
At or Below:
78
How Much TKS Protection Time Remains
When the Amber ANTICE LO PRESS Light
First Illuminates?
30 Minutes
79
What De-Ices the Conical Spinners?
Centrifugal Force
80
How Much TKS Priming and Protection Are
| Available With a Full Reservoir Gauge?
30 minutes
81
What is VLO?
220 KIAS
82
What Operates the Nose Wheel Door During
| Extension and Retraction?
A Mechanical Linkage
83
What Pressure Illuminates the Emergency
| Brake Low Pressure Light?
2,250 PSI
84
The Brake Reducing Valve Reduces System
| Pressure to:
1,750 – 1,900 PSI
85
Which Hydraulic System(s) Power the Main
| Landing Gear Actuators?
Main & auxiliary
86
What Controls the Landing Gear Selector
| Baulk?
Weight-on-Wheels Switch
87
Which Flap Setting Will Activate the Landing
| Gear Warning Horn With the Landing Gear Up?
Greater Than 15°
88
What is Landing Gear Operating Speed
| (VLO)?
220 KIAS
89
At What Altitude Will the Passenger Masks
| Automatically Deploy if Armed?
12,000 ± 500 Feet
90
Where Are the Oxygen Bottles Located?
Rear Bay
91
At What Cabin Pressure Altitude Will the
Eros Crew Mask Automatically Provide
Pressure Breathing?
35,000 Feet
92
How Many Liters of Oxygen Are Contained in
| Each Fully-Charged Cylinder?
750 Liters @ 1,800 PSI
93
What is the Power Source for the Main Air
| Valves?
PE Bus
94
What is the Source of Bleed Air for
| FLT/DK HEAT?
Right Engine Bleed Air
95
What is the Power Source for the FLT/DK
| Heat Valve?
PE
96
What are the Selectable Positions of the Main
| Air Valves?
Closed
LP
Open
97
What Will Placing the DUMP VALVE Selector
| Handle DOWN Provide?
Smoke Removal
98
At Which Temperature Does the DUCT OVHT
| Annunciator Illuminate?
800: 116°C
99
Which Cockpit Window(s) Can Be Opened?
“C” Panel and ONLY On the Ground
100
What Cabin Altitude Can be Maintained With
the Dump Valve Open and FLT/DK Air Fully
Open?
9,000 ft. Cabin Altitude @ 40,000 ft.
101
What is the Maximum Cabin Pressure
| Differential During Normal Operations?
8.55 PSI
102
What Cabin Altitude Can Be Maintained At
| 43,000 Feet?
8,000 Feet
103
What is the Power Source For the Fan-
| Operated Venturi?
115 VAC From Inverter #2
104
What Controls the Operation of the Fan-
| Operated Venturi?
8,000 Feet
105
What is Used By the Pilot to Monitor Cabin
| Pressurization?
The CABIN Triple Needle Indicator
106
What is the Function of the Pneumatic
| Relays?
Controls Vacuum Applied to the Outflow Valves
107
How is the Ram Air Valve Controlled?
Electrically Through a Micro-Switch in the Base
| of the Dump Valve Lever Quadrant
109
Which Modes of Operation Are Available for
| the Cabin Temperature Control System?
Auto
| Manual
109
Where Does Air for Ram Air Heat Exchanger
Cooling Come From If the Dorsal Intake is
Plugged?
Rear Bay Through Spring-Loaded Door
110
What is done With the Water Extracted From
| the Water Separator?
800: Vented Overboard
111
```
What is the Function of the Fan in the Cold
Air Unit (CAU)?
```
Draw Air Through the Ram Air Duct
| During Ground Operations
112
What is the Minimum Oil Pressure for
| Ground Idle?
25 PSI
113
What Engines Are Installed on the
| Hawker 800/800XP?
800: TFE 731-5R-1-H
114
Which Fuel Pressure Value Illuminates the
| LOW FUEL PRESS Annunciator?
6 PSI
115
What Indication Will You Get if You Are On
the Ground, Thrust Reversers Are Selected,
and Rudder Bias is NOT Inhibited?
Amber REVERSER Annunciator
| Illuminates on the MWS Panel
116
How Are the Dee Howard Thrust
| Reversers Controlled and Powered?
Electrically Controlled
| Hydraulically Operated
117
What is the Maximum Altitude for a Starter-
| Assisted Relight?
20,000 Feet
118
What is Normal Operating Oil Temperature
| (Green Arc)?
30°C to 127°C
119
What is the Minimum Oil Temperature for
| Takeoff?
+30°C
120
What is the Minimum Oil Temperature for
| Starting?
-40°C
122
What is Takeoff, Climb, and Maximum
| Continuous Oil Pressure?
800: 38 PSI
122
What is the Maximum Continuous Generator
| Load for the Turbomach T-62T APU (800)?
300 Amps
123
The Maximum Permissible APU Overspeed
| Is?
Honeywell: 110%
Turbomach: 100%
124
What is the Maximum Continuous Generator
| Load for the GTCP-36-150 APU (800XP)?
250 Amps
125
Where Does the APU Receive Fuel From?
Left Wing Tank
126
What are the EGT Limitations for the
| Turbomach T-62T APU (800)?
Normal: 1080°F
Starting: 1380°F
127
APU FIRE red light
Illuminates to indicate an overheat or fire condition in the APU.. Fire bell will not cancel until the APU master switch is selected OFF.
Silence fire bell by depressing switch light.
1. MASTER Switch – OFF
2. FIRE EXT Switch - OPERATE
128
APU GEN FAIL amber light
Illuminates to indicate the APU generator line contactor is de-energized.
129
LOW OIL PRESS amber light
Illuminates to indicate oil pressure is less than 35
psig.
APU shuts down if operating.
130
HIGH OIL TEMP amber light
Illuminates to indicate temperature is above 325°F.
| APU shuts down if operating.
131
BLEED AIR VALVE FAIL amber light
Illuminates to indicate BLEED AIR switch is set to CLOSE, but Load Control Valve has failed to close.
132
BLEED AIR ON green light
Illuminates to indicate Load Control Valve is open.
133
READY TO LOAD green light
Illuminates to indicate APU has reached operating speed.
134
APU ON white light
Illuminates to indicate the APU master switch is ON.
135
ENG 1 FIRE (up) red light
Illuminates to indicate the temperature in a fire
zone in the associated engine exceeds a preset limit.
The fire bell also sounds.
136
OIL 1 LO PRESS red light
Illuminates to indicate the associated engine oil
| pressure is less than 23 PSI.
137
MAIN AIR VALVE 1 amber light
ON GROUND: Indicates the associated main air valve is open.
IN FLIGHT: Indicates that the associated main air
valve does not correspond with the
switch position.
138
ENG 1 A/ICE amber light
Indicates that the associated engine bleed air pressure is:
139
EXT DOOR UNLOCKED amber light
Illuminates to indicate the entry door is not fully locked.
140
HYD (up) amber light
Illuminates to indicate an amber hydraulic annunciator is illuminated on the overhead panel.
142
AUX HYD LO LEVEL amber light
Indicates that approximately ½ pint of fluid was withdrawn
from the tank.
Lit when the auxiliary system is used
142
AIR BRAKES - OPEN
Illuminates to indicate the airbrakes are extended from the shut position.
143
HYD 1 LO PRESS amber light
Illuminates to indicate the associated supply pressure fell to 1,500psi for more than 57 seconds.
Remains illuminated until pressure rises to 1,850 psi
144
CABIN ALTITUDE red light
Illuminates to indicate cabin altitude has reached 9,300 ± 300 feet.
146
REAR BAY OVHT red light
Indicates that any of six thermally operated switches has detected an overheat condition in the rear equipment bay.
Temperature exposure exceeds 100°C
147
REVERSER amber light
On ground with T/R selected indicates rudder bias inhibit failure
In flight without T/R selected indicates hydraulic isolation valve failure
147
ICE PROT SELECTED white light
ADVISORY: Illuminates to indicate either or both engine anti ice switches are ON
148
ICE PROT (up) amber light
Illuminates to indicate ananti-ice system failure Look up to the overhead panel to determine the affected system(s)
149
DUCT OVHT (up) amber light
Illuminates to indicate duct temperature exceeds:
150
RUDDER BIAS amber light
Illuminates to indicate one or both bias switches are OFF.
151
STALL IDENT amber light
ADVISORY: Illuminates to indicate a stall warning and identification annunciator is illuminated on the left or right instrument panel.
152
ELECT (up) amber light
Illuminates to indicate a DC fault is annunciated on the overhead panel.
153
GEN 1 FAIL amber light
Illuminates to indicate that the associated generator line contactor is de-energized.
154
MACH TRIM OFF amber light
Illuminates to indicate the
Mach trim function is not
available (800XP).
155
ENGINE FAILURE DURING TAKEOFF
| BELOW V1 SPEED – ABORT TAKEOFF
1. Thrust Levers - CLOSE
2. Anti-Skid Braking - APPLY
3. Airbrakes - OPEN
4. Thrust Reverser - DEPLOY
5. Reverse Power - APPLY
156
ENGINE FAILURE DURING TAKEOFF
| Above V1 SPEED – Continue TAKEOFF
```
1. Takeoff – CONTINUE
At Positive Rate of Climb:
2. LANDING GEAR Lever – UP
3. APR Switch – OVERRIDE (if required)
4. Speed – V2 MINIMUM
5. MAIN AIR VLVs (Both) - CLOSE
```
157
SINGLE ENGINE FAILURE
1. Affected Engine - IDENTIFY
2. HP Cock - CLOSE
3. LP Cock - CLOSE
4. GEN - TRIP
5. BUS TIE (if open) - CLOSE
If failure during initial climb:
6. MAIN AIR VLVs (1 & 2) - CLOSE
7. F/DK VLV - CLOSE
158
TWO-ENGINE FAILURE
1. ENG IGNITION 1 & 2 – ON
2. Thrust Levers – CLOSE
3. Crew Oxygen – DONN MASKS IF ABOVE 15,000 FEET
4. Engine Indications - MONITOR
159
ENGINE FIRE IN FLIGHT
1. Affected Engine - IDENTIFY
2. HP Cock - CLOSE
3. LP Cock - CLOSE
4. GEN - TRIP
5. BUS TIE (if open) - CLOSE
6. ENG EXT - SHOT 1
If fire warning during initial climb:
7. MAIN AIR VLVs (1 & 2) - CLOSE
8. F/DK VLV - CLOSE
160
ENGINE FIRE ON GROUND
1. Affected Engine - IDENTIFY
2. START PWR (starting only) - PUSH FOR ABORT
3. HP Cock - CLOSE
4. LP Cock - CLOSE
5. GEN - TRIP
6. BUS TIE (if open) - CLOSE
7. ENG EXT - SHOT 1
After 30 seconds, if ENG FIRE remains illuminated:
8. ENG EXT - SHOT 2
161
OIL LOW PRESSURE
1. Oil Pressure – CHECK GAUGE READING
If below 25 PSI:
2. HP Cock (affected engine) - CLOSE
162
APU FIRE
1. MASTER Switch - OFF
| 2. FIRE EXT Switch - OPERATE
163
RAPID DEPRESSURIZATION
1. Crew Oxygen - DONN MASKS
164
EMERGENCY DESCENT
1. Thrust Levers - CLOSE
2. Speed – MMO/VMO
(unless structural damage is suspected)
3. AIRBRAKE - OPEN
165
FUSELAGE FIRE OR SMOKE
1. Crew Oxygen - DONN MASKS (100% EMERG)
2. Smoke Goggles - DONN/VENT
3. Cabin Notices - ON
166
HIGH PRESSURE AIR OVERHEAT
1. MAIN AIR VLV - CLOSE
| 2. F/DK VLV - CLOSE
167
SMOKE FROM A/C DUCTING
1. Crew Oxygen - DONN MASKS, 100% EMERG
2. Smoke Goggles - DONN/VENT
3. Cabin Notices - ON
168
REAR EQUIPMENT BAY OVERHEAT
1. MAIN AIR VLVs (1 & 2) – CLOSE
| 2. F/DK VLV – OPEN FULLY
169
ELECTRICAL FIRE OR SMOKE
1. Crew Oxygen - DONN MASKS / 100% EMERG
2. Smoke Goggles – DONN / VENT
3. Cabin Notices - ON
170
BATTERY OVERHEAT
In Flight:
1. BATT - EMERG
On Ground:
1. BATT - OFF
171
WHEEL BRAKE FAILURE
1. Brake Pedals - RELEASED
2. WHEEL BRAKE Lever - EMERGY
3. Brake Pedals - APPLY GENTLY
Use one continuous application if possible
172
STALL IDENTIFICATION SYSTEM
1. Take Normal Recovery Action
173
EMERGENCY EVACUATION – PILOT ACTIONS
1. Airplane - STOP
2. WHEEL BRAKE Lever - PARK
3. HP Cocks - CLOSE
4. LP Cocks - CLOSE
5. PA - ORDER EVACUATION
174
EMERGENCY EVALCUATION – COPILOT ACTIONS
1. Dump Valve - OPEN
2. ENG 1 & ENG 2 Extinguishers - SHOT 1 (BOTH)
3. APU FIRE EXT (if installed) - OPERATE
4. Notify ATC on VHF COMM 1
175
ABORTED TAKEOFF
1. Anti-Skid Braking - APPLY
2. Thrust Levers - CLOSE
3. Airbrakes - DEPLOY
4. Thrust Reverser – DEPLOY (if installed)
176
ENGINE FAILURE DURING TAKEOFF
| Above V1 SPEED – Continue TAKEOFF
At Positive Rate of Climb:
1. LANDING GEAR Lever - UP
2. MAIN AIR VLV’s (both) - CLOSE
3. F/DK - CLOSE
177
TWO-ENGINE FAILURE
1. ENG IGNITION 1 & 2 - ON
2. Thrust Levers - CLOSE
3. Fuel Enrich (if required) - PUSH (up to 400°C)
If above 15,000 ft:
4. Crew Oxygen - DON MASKS
178
ENGINE FIRE IN FLIGHT
```
1. Thrust Lever (Affected Engine) - IDLE
If fire warning persists:
2. HP Cock (Affected Engine) - CLOSE
3. LP Cock (Affected Engine) - CLOSE
4. ENG EXT - SHOT 1
If engine shutdown occurs during initial climb:
5. MAIN AIR VLVs 1 & 2 - CLOSE BOTH
6. F/DK VLV - CLOSE
```
179
ENGINE FIRE ON GROUND
1. START PWR (Starting Only) - PUSH FOR ABORT
2. HP Cock (Affected Engine) - CLOSE
3. LP Cock (Affected Engine) - CLOSE
4. ENG EXT (Affected Engine) - SHOT 1
180
THRUST REVERSER INADVERTENT
| DEPLOYMENT – IN FLIGHT
1. HP Cock (affected engine) - CLOSE
181
APU FIRE [GARRETT GTCP 3092C (A)]
1. APU MASTER – OFF
Units With Doors: Wait 10 Seconds
If Warning Persists:
2. APU FIRE EXT – OPERATE
182
APU FIRE (TURBOMACH)
1. APU MASTER - OFF
| 2. APU FIRE EXT - OPERATE
183
RAPID DEPRESSURIZATION
1. Crew Oxygen - DON MASKS
184
EMERGENCY DESCENT
1. Thrust Levers - CLOSE
2. Speed – MMO/VMO
(unless structural damage is suspected)
3. AIRBRAKE - OPEN
185
FUSELAGE FIRE OR SMOKE
1. Crew Oxygen - DONN MASKS (100% EMERG)
2. Smoke Goggles - DONN/VENT
3. Cabin Notices - ON
186
SMOKE FROM AIR CONDITIONING DUCTS
1. Crew Oxygen - DONN MASKS, 100% EMERG
2. Smoke Goggles - DONN/VENT
3. Cabin Notices - ON
187
HIGH PRESSURE AIR OVERHEAT
1. Associated MAIN AIR VLV - CLOSE
| 2. F/DK VLV - CLOSE
188
REAR EQUIPMENT BAY OVERHEAT
1. MAIN AIR VLVs (both) - CLOSE
| 2. F/DK VLV - OPEN FULLY
189
FIRE IN FLIGHT COMPARTMENT / PASSENGER CABIN
1. Crew Oxygen – DONN MASKS – 100% EMERGENCY
2. Smoke Goggles – DONN & VENT
3. Cabin Notice - ON
190
ELECTRICAL FIRE OR SMOKE
1. Crew Oxygen - DONN MASKS/100%
2. Smoke Goggles - DONN/VENT
3. Cabin Notices - ON
191
BATTERY OVERHEAT
In Flight:
1. BATT - EMERG
On Ground:
1. BATT - OFF
192
WHEEL BRAKE FAILURE
1. Brake Pedals - RELEASE
2. WHEEL BRAKE Lever - EMERGY
3. Brake Pedals - APPLY GENTLY
Use one continuous application If possible
193
EMERGENCY EVACUATION
1. Aircraft - STOP
2. WHEEL BRAKE Lever - PARK
3. HP Cocks - CLOSE
4. LP Cocks - CLOSE
5. PA - ORDER EVACUATION
6. Dump Valve – OPEN
7. ENG 1 & 2 Extinguishers – SHOT 1 (BOTH)
8. APU FIRE EXT (if fitted) – OPERATE
9. Notify ATC on VHF COMM 1
194
Where Does the DME Indicator Have the Greatest Error Between Ground and Displayed Distance?
At High Altitude – Close to the VORTAC
196
Which Checks/Inspections of Flight Instruments or Systems MUST Be Accomplished Before IFR Flight?
VOR Within Preceding 30 Days
| Altimeters/Transponders Within Preceding 24 Months
196
What is the Maximum Speed to be Used
| in a Procedure Turn?
200 Knots
197
What are the Required Items to be Recorded
| When Performing a VOR Check?
Date
Place
Bearing Error
Signature in Aircraft Log or Other Record
198
When is a Procedure Turn Required?
When Necessary to Reverse Direction to
Establish the Aircraft Inbound On an
Intermediate or Final Approach Course
199
If Straight-In Minimums Are NOT Published, May a Pilot Land Straight-In?
YES
201
Does ATC Retain Wake Turbulence Separation When the PIC Has Accepted Visual Separation From Traffic?
NO – Acceptance Also Means the Pilot
Accepts Responsibility for Wake
Turbulence Separation
202
What is the Minimum Climb Gradient to be Maintained Whenever NO Climb Gradient is Specified on a DP (Departure Procedure)?
200 Feet per Nautical Mile
203
How Does the LDA Differ From a LOC Course?
LDA is Not Aligned Within 3° of Runway
204
Which Normally Changes When Crossing a Front – Pressure, Temperature, Dew Point, or
Wind?
Wind
205
What Conditions Would Be Most Favorable For the Formation of Rime Ice?
Light Drizzle
Strataform Clouds
Temperatures At/Below Freezing
205
What Information Can be Obtained From
| the 250 Milibar Chart?
Winds Aloft at 39,000 Feet
206
What Conditions Would Be Most Favorable For the Formation of Fog?
```
Light Wind (3-5 Knots)
Narrow Temperature/Dew Point Spread (2°C)
```
207
Which Atmospheric Factor Causes Rapid
| Movement of Surface Fronts?
Upper Winds Blowing Across the Front
208
What Condition is Indicated Whenever Ice
| Pellets Are Encountered During Flight?
Freezing Rain at Higher Levels
209
Which Type of Precipitation Indicates
| the Presence of Supercooled Water?
Freezing Rain
210
Which Conditions Are Most Likely to
| Produce a Microburst?
Convective Activity in Very Dry Air
211
What is an Indication That a
Thunderstorm Has Reached the Mature
Stage?
Precipitation
212
What Are the Major Hazards of Flying
| Under the Anvil of a Thunderstorm?
Hail
Severe Turbulence
Lightning
213
What is a Squall Line and Where Does It
| Develop?
A Non-Frontal, Narrow Band of Active
Thunderstorms Which Often Develops
Ahead of a Cold Front in Moist, Unstable
Air
214
What kind of storms are most likely to
| generate tornadoes?
Steady state thunderstorms associated with
| cold fronts or squall lines
216
Which Conditions are Necessary for a Low-
| Level, Temperature Inversion Windshear?
Calm/Light Wind Near Surface
| Relatively Strong Wind Just Above Inversion
216
How Long is a Convective Outlook Valid?
24 Hours
217
What Conditions Are Necessary For a Squall
| to be Reported?
Sudden Increase of Wind Speed By At Least 15 Knots
| Winds Peaking to 20 Knots or More / Lasting a Minute or Longer
218
What Tops Level of a Thunderstorm
| Would Qualify It as Severe?
35,000 Feet
219
How Far Should You Avoid a Thunderstorm?
20 Nautical Miles
221
How Far Away From Mountains Could
You Expect to Find Clear Air Turbulence
Associated With Mountain Wave?
5,000 Feet Above the Tropopause
| 100 Miles or More Downwind From Mountains
