King Air 350ER Flashcards
1
Q
Minimum Speed for Reverse?
A
40 kts
2
Q
Vmca (Flaps Approach) ?
A
98 kts
3
Q
Vmca (Flaps Up) ?
A
101 kts
4
Q
Vsse (Intentional One Engine Inop) ?
A
135 kts
5
Q
Vyse ?
A
135 kts
6
Q
Vx ?
A
135 kts
7
Q
Maximum Glide Range Speed ?
A
135 kts
8
Q
Vy ?
A
135 kts
9
Q
Minimum Speed in Flight in Sustained Icing ?
A
140 kts
10
Q
Vfe (Landing Flaps) ?
A
158 kts
11
Q
Vlo (Retraction) ?
A
164 kts
12
Q
Vb (Turbulence Penetration) ?
A
170 kts
13
Q
Va (Flaps Up) ?
A
182 kts
14
Q
Vlo (Extension) ?
A
182 kts
15
Q
Vfe (Flaps Approach) ?
A
202 kts
16
Q
Maximum Air Speed for Windshield De-Icing?
A
226 kts
17
Q
Vmo (Below 24,000 ft) ?
A
245 kts
18
Q
Mmo (Above 24,000 ft) ?
A
.58 Mach
19
Q
Maximum Ramp Weight?
A
16,600 lbs
20
Q
Maximum Takeoff Weight?
A
16,500 lbs
21
Q
Maximum Landing Weight?
A
15,675 lbs
22
Q
Maximum Zero Fuel Weight?
A
13,000 lbs
23
Q
Maximum Baggage Compartment Weight?
A
550 lbs
24
Q
Maximum Persons on Airstair Door?
A
One Person
25
Rudder Boost Limitation?
Must be operational for all phases of flight
26
Starter Limitations?
30 seconds On, 5 minutes Off
30 seconds On, 5 minutes Off
30 seconds On, 30 minutes Off
27
Propeller De-Ice Ammeter Limits?
26 to 32 amps (Normal Range)
28
Cabin Altimeter and Differential Limits?
6.6 psig (Maximum Cabin Differential)
29
Maximum ITT Limit Low Idle?
750°C
30
Maximum Reverse ITT Limit?
760°C
31
Recommended Cruise Climb ITT Limit?
785°C
32
Maximum Cruise ITT Limit?
820°C
33
Takeoff and Maximum Continuous ITT Limit?
820°C
34
Maximum Transient ITT Limit?
850°C for 20 seconds
35
Maximum ITT during Starting?
1000°C for 5 seconds
36
Oil Temperature Limit during Starting and Low Idle?
-40°C to 110°C
37
Normal Oil Temperature Limits?
0°C to 99°C
38
Maximum Oil Temperature Limit?
110°C
39
Maximum Transient Oil Temperature Limit?
99°C to 110°C for 10 minutes
40
Recommended Oil Temperature for Fuel Heater Operations at Takeoff?
55°C
41
Minimum Oil Pressure at Low Idle?
60 psi
42
Oil Pressure Caution Range?
60 to 90 psi (Torque Limited to 62%)
43
Normal Oil Pressure Operating Range?
90 to 135 psi
44
Maximum Starting Oil Pressure Limit?
200 psi
45
Normal Pneumatic Pressure Operating Range?
12 to 20 psi
46
Maximum Pneumatic Pressure Limit?
20 psi
47
Normal Torque Operating Range?
0 to 100% (1000 to 1700 rpm)
48
Maximum Transient Torque Limit?
156% (for 20 seconds)
49
Maximum Torque Limit with Props Above 1700 rpm?
96%
50
Inadvertent Torque Excursions up to _______% are time limited to _____ minutes?
102%
| 7 minutes
51
Minimum N1 Turbine Tach Speed at Low Idle?
62%
52
Maximum N1 Turbine Tach Speed?
104%
53
Maximum Transient N1 Turbine Tach Speed?
104%
54
Maximum DC Power Limit between 62% and 70% Torque?
75%
55
Maximum DC Power Below 34,000 feet?
100%
56
Maximum DC Power Above 34,000 feet?
95%
57
Normal Volts DC Power?
27.5 to 29 VDC
58
Minimum Prop RPM Limit at Idle?
1050 RPM
59
Normal Prop RPM Operating Range?
1450 to 1700 RPM
60
Maximum Prop RPM in Reverse?
1650 RPM
61
Maximum Prop RPM ?
1700 RPM
62
Maximum Prop RPM Transient?
1870 RPM for 5 seconds
63
Prop RPM range to avoid during Ground Operations?
400 to 1050 RPM
64
Maximum Fuel Imbalance?
300 lbs
65
Minimum Fuel in each Main for Takeoff?
265 lbs
66
Maximum Operating Time with the Fuel Press Light Illuminated?
10 hours
67
Maximum Usable Fuel Quantity?
775 gallons/5192 lbs
68
Approximate Range with Full Fuel?
2300 NM
69
Approximate Endurance with Full Fuel?
8 hours
70
Maximum Operating Altitude?
35,000 feet
71
ENGINE FIRE/FAILURE IN-FLIGHT
1 CONDITION LEVER - CUTOFF
2 PROPS - FEATHER
3 FIREWALL VALVE - CLOSE
4 EXTINGUISHER (IF FIRE WARNING PERSISTS) - ACTUATE
72
ENGINE FIRE ON THE GROUND
1 CONDITION LEVER - CUTOFF
2 FIREWALL VALVE - CLOSE
3 STARTER - STARTER ONLY
4 EXTINGUISHER (IF FIRE WARNING PERSISTS) - ACTUATE
73
EMERGENCY ENGINE SHUTDOWN ON THE GROUND
```
1 CONDITION LEVERS - CUTOFF
2 PROPS - FEATHER
3 FIREWALL VALVES - CLOSE
4 MASTER SWITCH - OFF
5 BATT BUS - EMER OFF
6 ESIS - OFF
```
74
TAKEOFF ABORT
1 POWER- GROUND FINE
| 2 BRAKES - AS REQUIRED
75
ENGINE FAILURE TAKEOFF CONTINUED
```
1 Vr - ROTATE
2 POWER - MAX ALLOWABLE
3 GEAR - UP
4 AIRSPEED - V2 TO ACCEL HEIGHT (400FT MIN AGL)
5 PROP (INOP ENG) - VERIFY FEATHERED
```
76
ENGINE FAILURE IN FLIGHT BELOW MINIMUM CONTROL SPEED (Vmca)
1 POWER - REDUCE AS REQUIRED TO MAINTAIN CONTROL
| 2 NOSE - LOWER TO ACCELERATE ABOVE Vmca
77
ELECTRICAL FIRE OR SMOKE
1 OXYGEN MASK(S) - DON
2 MASK SELECTOR SWITCH - EMER
3 MIC SWITCH(ES) - OXY
78
ENVIRONMENTAL SMOKE/FUMES
1 OXYGEN MASK - DON
2 MASK SELECTOR SWITCH - EMER
3 MIC SWITCH - OXY
79
AIRSTAIR DOOR/CARGO DOOR UNLOCKED
1 ALL OCCUPANTS - SEATED WITH SEATBELTS SECURELY FASTENED
80
EMERGENCY DESCENT
```
1 POWER LEVERS - IDLE
2 PROPS LEVERS - FULL FORWARD
3 FLAPS (202 KTS MAX) - APPROACH
4 LANDING GEAR (182 KTS MAX) - DOWN
5 AIRSPEED - 182 KTS MAX
```
81
GLIDE
1 LANDING GEAR - UP
2 FLAPS - UP
3 PROP LEVERS - FEATHERED
4 AIRSPEED - 135 KTS
82
USE OF OXYGEN
1 OXYGEN MASK(S) - DON
| 2 MIC SWITCH(ES) - OXY
83
PRESSURIZATION LOSS
1 OXYGEN MASK(S) - DON
2 MIC SWITCH(ES) - OXY
3 PASSENGER MANUAL DROPOUT - PULL ON
4 DESCEND - AS REQUIRED
84
HIGH DIFFERENTIAL PRESSURE
1 BLEED AIR VALVES - ENVIR OFF
2 OXYGEN (CREW AND PASSENGERS) - AS REQUIRED
3 DESCEND - AS REQUIRED
85
AUTO DEPLOYMENT OXYGEN SYSTEM FAILURE
1 PASSENGER MANUAL DROPOUT - PULL ON
86
DUAL GENERATOR FAILURE
1 INSTRUMENT EMERGENCY LIGHTS (IF REQUIRED) - ON
2 MISSION POWER SWITCH - OFF
3 NEBULA POWER SWITCH (IF INSTALLED) - OFF
4 GENERATORS - RESET, THEN ON
If either generator will reset
5 OPERATING GENERATOR LOADMETER - MONITOR
If neither generator will reset
6 ECS MODE - OFF
7 COCKPIT/CABIN BLOWER - AUTO
8 NON-ESSENTIAL EQUIPMENT - OFF
87
BLEED AIR FAIL
1 BLEED AIR VALVE (AFFECTED ENGINE) - PNEU & ENVIR OFF
88
SPINS
1 CONTROL COLUMN - FULL FORWARD, AILERONS NEUTRAL
2 FULL RUDDER - OPPOSITE THE DIRECTION OF THE SPIN
3 POWER LEVERS - IDLE
4 RUDDER - NEUTRALIZE WHEN ROTATION STOPS
5 EXECUTE A SMOOTH PULLOUT
89
UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION
1 AIRPLANE ATTITUDE - MAINTAIN USING ELEVATOR CONTROL
| 2 AP/TRIM DISCONNECT - DEPRESS FULLY AND HOLD [TRIM] ILLUMINATED
90
UNSCHEDULED RUDDER BOOST ACTIVATION
1 AP/TRIM DISCONNECT - DEPRESS TO 1ST LEVEL AND HOLD
2 RUDDER BOOST - OFF
If condition persists
3 YD/AP DISC (ON FLIGHT GUIDANCE PANEL) - PULL DOWN
91
AUTOPILOT MISTRIM [E] OR [A]
1 FLIGHT CONTROLS - HOLD FIRMLY
| 2 AP - DISENGAGE
92
AUTOPILOT TRIM FAIL [TRIM]
1 FLIGHT CONTROLS - HOLD FIRMLY
| 2 AP - DISENGAGE
93
AUTOPILOT AUTOMATIC DISENGAGEMENT
1 MAINTAIN AIRPLANE CONTROL
| 2 AP/TRIM DISCONNECT - DEPRESS TO 1ST LEVEL TO CANCEL HORN
94
EGPWS TERRAIN WARNING
```
In IMC or at night
1 WINGS - LEVEL
2 POWER - MAX ALLOWABLE
3 PITCH - INCREASE, ADJUST TO MAINTAIN 135 KIAS
4 GEAR AND FLAPS - UP
```
95
Max Temperature Limit Sea Level to 25,000' ?
ISA +37°C
96
Max Temperature Above 25,000' ?
ISA +31°C
97
Pneumatic Boot Limit?
No Operations Below -40°C
98
G Load Limitations Flaps Up?
-1.21 to 3.01
99
G Load Limitations Flaps Down?
0.0 to 2.0
100
DC Power Limitation at 62% to 70% Tach N1 Speed?
75% Maximum
101
Maximum DC Power Below 34,000' ?
100%
102
Maximum DC Power Above 34,000' ?
95%
103
Normal VDC ?
27.5 to 29.0 VDC
104
Maximum Crosswind for Takeoff?
35 kts
