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AFM Flashcards

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1
Q

ELECTRICAL SMOKE IN CABIN ON THE GROUND

A

“My Cockpit Totally Ignited, Fuel Pissed Everywhere, Abandon!”

  1. MASTER SWITCH OFF
  2. Cabin heat and defrost OFF
  3. Throttle Lever BOTH IDLE
  4. Ignitions ALL OFF
  5. Fuel Selector BOTH OFF
  6. Parking Brake ENGAGED
  7. Aircraft Evacuation carry out immediately
    Consider use of ditching emergency exit
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2
Q

ENGINE FIRE IN FLIGHT

A

CAFITPAHFAHLE

  1. Cabin heat and defrost BOTH OFF
  2. Autopilot OFF
  3. Fire affected engine Fuel Selector Confirm and OFF
  4. Fire affected engine Ignition Confirm and BOTH OFF
  5. Fire affected engine Throttle Lever Confirm and FULL FORWARD
  6. Fire affected engine Propeller Lever Confirm and FEATHER
  7. Fire affected engine Electrical fuel pump OFF
  8. Heading Keep control using rudder and ailerons
  9. Attitude Adjust as appropriate to keep airspeed
    over 62 KIAS
  10. Fire affected engine Field OFF
  11. Cabin ventilation OPEN
  12. Land as soon as possible applying one engine inoperative landing procedure.
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3
Q

Wingspan

A

11.4

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4
Q

Length

A

8.7

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5
Q

Height

A

2.58

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6
Q

Mean Chord

A

1.295

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7
Q

Engine displacement

A

1352

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8
Q

Engine max power

A

98.6 bhp @ 5800 (2388 prop) limited to 5 mins

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9
Q

Engine continuous power

A

92.5 bhp @ 5500 (2265 prop)

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10
Q

Prop diameter

A

1780mm

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11
Q

Tank capacity

A

2 X 100 L, of which 194.4 usable

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12
Q

Unusable fuel

A

5.6

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13
Q

Oil capacity

A

3 l

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14
Q

Wing loading

A

83 kg/m2

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15
Q

Vne

A

167 KIAS, 168 KCAS

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16
Q

Vno

A

135 KIAS, 133 KCAS

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17
Q

Va

A

118 KIAS, 117 KCAS

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18
Q

Vo

A

118 KIAS, 117 KCAS

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19
Q

VLE

A

122 KIAS

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20
Q

VLO

A

122 KIAS

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21
Q

VFE T/O

A

119 KIAS, 117 KCAS

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22
Q

VFE full

A

93 KIAS, 92 KCAS

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23
Q

VMC

A

62 KIAS, 62 KCAS

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24
Q

VYSE

A

84 KIAS, 84 KCAS

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25
Max CHT
135
26
Max CT
120
27
Oil temp min/max
50-130
28
Oil temp normal range
90-110
29
Oil pressure min/max
0.8 - 7
30
Oil pressure normal range
2-5
31
Fuel pressure min/max
2.2 - 5.8
32
Max operating altitude
14000
33
Acceptable operating temps
-25 ..... +50
34
Prop min RPM
580
35
Voltmeter min limit
10.5
36
Voltmeter normal range
12-14
37
Maneuver limiting load factors, flaps up
+3.8 .... -1.78
38
Maneuver limiting load factors, flaps extended
+2....0
39
Max baggage
80
40
Max floor loading
0.9 kg/dm2
41
Min pressure emergency landing gear actuator
20
42
Rear seats for TO and landing
Max low and aft position
43
Abort takeoff CHECKLIST
1. Throttle lever - BOTH IDLE 2. Rudder - KEEP HEADING CONTROL
44
Land as soon as possible means?
Land without delay at the nearest suitable area at which a safe approach and landing is assured
45
Land as soon as practical means?
Land at the nearest approved landing area where suitable repairs can be made
46
LH Gen Bus feeds
Pitot Heat Landing light Taxi light
47
Pitot heat is fed by?
LH Gen Bus
48
Landing light is fed by?
LH Gen Bus
49
LH Avionics Bus feeds?
DME Transponder Pressure Encoder Altimeter
49
Taxi light is fed by?
LH Gen Bus
50
DME is fed by?
LH Avionics Bus
51
Transponder is fed by?
LH Avionics Bus
52
Pressure Encoder Altimeter is fed by?
LH Avionics Bus
53
RH Avionics Bus feeds?
ADF Com2 Nav2 A/P A/P Pitch Trim
54
ADF is fed by?
RH Avionics Bus
55
COM 2 is fed by?
RH Avionics Bus
56
NAV 2 is fed by?
RH Avionics Bus
57
A/P is fed by?
RH Avionics Bus
58
A/P Pitch Trim is fed by?
RH Avionics Bus
59
RH Gen Bus feeds?
NAV lights Rudder trim Stall warning RH Attitude Indicator
60
Nav lights are fed by?
RH Gen Bus
61
Rudder trim is fed by?
RH Gen Bus
62
Stall warning is fed by?
RH Gen Bus
63
RH Attitude Indicator is fed by?
RH Gen Bus
64
Engine Securing Checklist
IIPPFF Alive On 1. Dead Throttle Lever IDLE 2. Dead Ignition BOTH OFF 3. Dead Propeller Lever FEATHER 4. Dead Fuel Selector OFF 5. Dead Electrical fuel pump OFF 6. Alive engine pump ON 7. Dead field OFF
65
Landing distance without flaps increases by?
25%
66
A fully charged battery can supply electrical power for up to ....... minutes?
30
67
Flap Up T/O increases take-off distance to 50ft by?
20%
68
Inflight Engine Restart Checklist
1. Carburettor heat ON if required 2. Electrical fuel pump ON 3. Fuel quantity indicator CHECK 4. Fuel Selector CHECK (Crossfeed if required) 5. FIELD OFF 6. Ignition BOTH ON 7. Operating engine Throttle Lever SET as practical 8. Stopped engine Throttle Lever IDLE 9. Stopped engine Propeller Lever FULL FORWARD 10. Start push-button inoperative engine PUSH 11. Propeller Lever inoperative engine SET at desired rpm 12. FIELD ON (check for positive ammeter) 13. Engine throttle levers SET as required If engine restart is unsuccessful 14. EMERG BATT switch 15. Repeat engine restart procedure ON (if starting battery installed) If engine restart is still unsuccessful: 16. Affected engine SECURE (see engine securing procedure Para. 3) 17. Land as soon as possible applying one engine inoperative landing procedure.
69
Engine failure before rotation MEMORY ITEMS
1. Throttle Lever BOTH IDLE 2. Rudder Keep heading control 3. Brakes As required
70
Engine failure after rotation MEMORY ITEMS
Ta-Pa-Ha-Da-Ga-Fa 1. Operating engine Throttle Lever FULL POWER 2. Operating engine Propeller Lever FULL FORWARD 3. Heading Keep control using rudder and ailerons 4. Attitude Reduce as appropriate to keep airspeed over 62 KIAS 5. Inoperative engine Propeller Lever FEATHER 6. Landing gear control lever UP 7. Airspeed VXSE/VYSE as required 8. Flaps 0°
71
Engine failure during en-route climb MEMORY ITEMS
1. Autopilot OFF 2. Heading Keep control using rudder and ailerons 3. Attitude Reduce as appropriate to keep airspeed over 62 KIAS
72
Engine failure in flight MEMORY ITEMS
Aha! Pilot Got Fucked! Check and kill. 1. Autopilot OFF 2. Heading Keep control using rudder and ailerons 3. Attitude Adjust as appropriate to keep airspeed over 62 KIAS 4. Both fuel pumps OFF 5. Gear UP 6. Flaps UP 7. Dead engine: Identify - Verify 8. Dead prop: Feather
73
Emergency landing gear extension operation takes?
20 secs
74
How long should you wait after turning the first lever of the emergency landing gear extension system?
20 secs
75
Engine fire on the ground MEMORY ITEMS
FIP CAMP Evacuated 1. Fuel Selectors BOTH OFF 2. Ignitions ALL OFF 3. Electrical fuel pumps BOTH OFF 4. Cabin heat and defrost OFF 5. MASTER SWITCH OFF 6. Parking Brake ENGAGED 7. Aircraft Evacuation carry out immediately Consider using the ditching exit
76
Engine fire during TO run MEMORY ITEMS before rotation
Remember to cool the cabin! BEFORE ROTATION: ABORT TAKE OFF 1. Throttle Lever BOTH IDLE 2. Rudder Keep heading control 3. Brakes As required With aircraft under control 4. Fuel Selector BOTH OFF 5. Ignitions ALL OFF 6. Electrical fuel pump BOTH OFF 7. Cabin heat and defrost OFF 8. MASTER SWITCH OFF 9. Parking Brake ENGAGED 10. Aircraft Evacuation carry out immediately Consider using the ditching exit
77
Engine fire during TO MEMORY ITEMS after rotation
1. Operating engine Throttle Lever FULL POWER 2. Operating engine Propeller Lever FULL FORWARD 3. Heading Keep control using rudder and ailerons 4. Attitude Reduce as appropriate to keep airspeed over 62 KIAS 5. Fire affected engine Propeller Lever FEATHER 6. Landing gear control lever UP 7. Airspeed VXSE/VYSE as required 8. Flaps 0° 9. Continue checklist
78
Engine fire in flight MEMORY ITEMS
Breathe. Take over. Secure. Pause. 1. Cabin heat and defrost BOTH OFF 2. Autopilot OFF 3. Fire affected engine Fuel Selector Confirm and OFF 4. Fire affected engine Ignition Confirm and BOTH OFF 5. Fire affected engine Throttle Lever Confirm and FULL FORWARD 6. Fire affected engine Propeller Lever Confirm and FEATHER 7. Fire affected engine Electrical fuel pump OFF 8. Heading Keep control using rudder and ailerons 9. Attitude Adjust as appropriate to keep airspeed over 62 KIAS 10. Fire affected engine Field OFF 11. Cabin ventilation OPEN 12. Land as soon as possible applying one engine inoperative landing procedure.
79
Electrical smoke in cabin on the ground MEMORY ITEMS
1. MASTER SWITCH OFF 2. Cabin heat and defrost OFF 3. Throttle Lever BOTH IDLE 4. Ignitions ALL OFF 5. Fuel Selector BOTH OFF 6. Parking Brake ENGAGED 7. Aircraft Evacuation carry out immediately Consider use of ditching emergency exit
80
Electrical smoke in cabin during flight MEMORY ITEMS
1. Cabin ventilation OPEN 2. Emergency light ON 3. Standby attitude indicator switch ON 4. Gain VMC conditions as soon as possible In case of cockpit fire: 5. Fire extinguisher use toward base of flames. 6. If smoke persists, shed electrical supply - CONTINUE CHECKLIST
81
Spin recovery MEMORY ITEMS
1. Both engines throttles idle 2. Flight Controls centralize 3. Rudder fully against rotation until it stops
82
Aircraft evacuation MEMORY ITEMS
Verify (if not yet performed): 1. Fuel Selectors BOTH OFF 2. Ignitions ALL OFF 3. Electrical fuel pumps BOTH OFF 4. MASTER SWITCH OFF 5. Parking Brake ENGAGED 6. Leave the aircraft using emergency exits
83
Suggested prop RPM drop during governor check
400-500 RPM, do not let prop RPMs drop below 1500
84
Order of actions, decreasing power
MAP then RPM
85
Order of actions, increasing power
RPM then MAP
86
Vr
65
87
Vx
72
88
Vy
84
89
Vapproach
90
90
V final approach
71
91
Va
122
92
VNE
171
93
Simulated feather power settings
13.5 MAP, 70-90 kts, 2000-4000 ft, RPM full forward
94
Safe simulated engine out speed
70
95
Speed on downwind
122
96
Stall speed, flaps up
66 KIAS, 64 KCAS
97
Stall speed, flaps TO
56 KIAS, 56 KCAS
98
Stall speed, flaps FULL
53 KIAS, 54 KCAS
99
TO distance to 50 ft (MTOW, ISA, Sea Level, Grass)
290
100
Ground roll decrease on a paved RWY
-6%
101
Max rate of climb at Vx, MTOW, ISA, Sea Level
1002
102
Max rate of climb, Vx, OEI, MTOW, ISA, Sea Level
203
103
65% cruise numbers, ISA
2250 RPM/26 MAP, 124 KTAS, 18.2 lt/hr
104
43% cruise numbers, ISA
2250 RPM/22 MAP, 103 KTAS, 12.1 ltr/hr
105
83% cruise numbers, ISA
2250 RPM/28 MAP, 136 KTAS, 23.2 ltr/hr
106
Landing from 50 ft., MTOW, Sea Level, ISA, grass
213
107
Datum for M&B calculations
Leading Edge
108
The fuel tank is located in?
The torque box
109
The torque box contains?
The fuel tank
110
The taxi and landing lights are in which wing?
Left
111
How many spars per wing?
Two
112
How many spars in the stabilator?
Two
113
Stabilator is actuated by?
Rods
114
Ailerons are actuated by?
A mixed system including cables and rods
115
How many flap actuators are there?
One
116
How do designers ensure that flap assymetry is impossible?
Single flap actuator
117
Rudder is actuated by?
Cables
118
How many cylinders per engine?
Four
119
Name these parts of the cooling system
1 - expansion tank 2 - radiator 3 - pressure cap with a pressure relief valve and return valve 4 - overflow bottle
120
What type of sump is installed?
Dry sump
121
Explain how the cooling system works
The coolant flow is forced by a water pump, driven from the camshaft, from the radiator to the cylinder heads. From the top of the cylinder heads the coolant passes on to the expansion tank (item 1, Figure below). Since the standard location of the radiator (2) is below engine level, the expansion tank, located on top of the engine, allows for coolant expansion. The expansion tank is closed by a pressure cap (3) fitted with pressure relief valve and return valve. At temperature rise and expansion of the coolant, the pressure relief valve opens and the coolant will flow via a hose at atmospheric pressure to the transparent overflow bottle (4). Once cooled down, the coolant will be sucked back into the cooling circuit.
122
The landing gear is powered by?
Electrics AND hydraulics
123
Generators are rated at how many AMPs?
40
124
Secondary electrical power is provided by?
A battery
125
The battery can provide?
38 AH in 20 hrs run time
126
How many electrical buses are there?
5
127
Name the electrical busses
Battery bus LH Gen Bus RH Gen Bus LH Avionics Bus RH Avionics Bus
128
What do Cross bus switches do?
Separate left busess from right busses
129
How many distribution busses are there?
One
130
Which bus supplies the most important loads?
The battery bus
131
How is the battery bus supplied?
From the battery and both generators, so a total of three sources
132
What devices are connected to the battery hot bus?
Emergency back-up attitude indicator Emergency light Chronometer
133
Which bus is the audio panel connected to?
Battery bus
134
Which bus is VHF Comm 1 connected to?
Battery bus
135
Which bus is NAV 1 connected to?
Battery bus
136
Which bus is GPS connected to?
Battery bus
137
Which bus are the fuel pumps connected to?
Battery bus
138
Which bus are fuel pressure indicators connected to?
Battery bus
139
Which bus are fuel quantity indicators connected to?
Battery bus
140
Which bus are oil pressure indicators connected to?
Battery bus
141
Which bus are oil temp indicators connected to?
Battery bus
142
Which bus are CHT indicators connected to?
Battery bus
143
Which bus are RPM indicators connected to?
Battery bus
144
Which bus are attitude indicators connected to?
Battery bus
145
Which bus are cabin and cockpit lights connected to?
Battery bus
146
Which bus are all internal lights connected to?
Battery bus
147
Which bus are strobe lights connected to?
Battery bus
148
Which bus are flaps connected to?
Battery bus
149
Which bus are door pressure switches connected to?
Battery bus
150
Which bus are OAT indicators connected to?
Battery bus
151
Which bus is the Turn Coordinator connected to?
Battery bus
152
Which bus are the LG hydraulic pumps connected to?
Battery bus
153
Which bus are the fire detectors connected to?
Battery bus
154
Which bus are the electrical power sources inside the cabin connected to?
Battery bus
155
What happens if you switch Cross Bus switches off?
The pertinent GEN bus is separated from the battery bus and from the opposite GEN bus
156
Engine starting battery is charged by?
LH Generator

P2006T (2 decks)

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