5s & 9s Flashcards
1
Q
VMO Max Allowable Below 11,500 feet
Max Autopilot Operation
A
248 KIAS
2
Q
Brake Deice
A
- Max Temp +15°C
- 10 Minute Max Cycle
- Minimum 85% N1 for simultaneous use of wing and antenna boots
- Prohibited During Single Engine Operations
3
Q
Loss of Pressurization
Above 10,000 FT AGL
A
Crew oxygen masks –100% and don.
MIC switch – OXYGEN MASK
4
Q
Autofeather
A
Armed above 89% N1
20 to 14% Torque, Opposite Side Disarms
13 to 7% Torque, Failed Prop Feathers
5
Q
Electrical Fire
A
Oxygen masks EMERGENCY and don
MIC switch - OXYGEN MASK
6
Q
Bank Limits
A
60°
7
Q
Ground Power Unit Amps Limits
A
1000 Amps for 5 Seconds
500 Amps 2 minutes
300 Amps continuously
8
Q
Max if Windshield Icing
A
226 KIAS
9
Q
Max Altitude for Inoperative Yaw Damper
A
17,000 ft
10
Q
Wing Fire
A
- Perform engine shutdown on affected side.
2. Land as soon as possible.
11
Q
AC/DC Power
A
22 VDC Min Battery Start 28 VDC Max GPU Start AC Freq 394-406 AC Voltage 104-124 DC Voltage 28-28.5
12
Q
Weight Limitations (lbs)
A
Toilet Seat for Takeoff and Landing = 238 Airstair Door Limit = 300 Max Zero Fuel = 13,100 Max Landing Weight = 15,675 Max Takeoff = 16,500 Ramp Weight = 16,620
13
Q
Oil Temperature
A
-40° (Min) Starting
-40° to 110° Low Idle / Transient (10 min)
+10° to 105 Max Climb/Cont/Cruise/Norm/Reverse
+10° to 110° Takeoff (5 Minutes)
74° to 80°C Recommended
14
Q
TGT Limits
A
400-830°C Normal 750°C Max for Low Idle 760°C Max Reverse 800°C Normal Cruise and Climb 810°C Max Cruise and Climb 830°C Max Continuous 840°C for 5 Minutes Max for Takeoff 870°C for 20 Seconds Max Transient 1000°C for 5 Seconds Max for Starting
15
Q
Max for Approach Flap Extension
A
197 KIAS
16
Q
Landing Gear Retraction
A
160 KIAS
17
Q
Starter Limitations
A
40 Seconds On, 15 Minutes OFF
40 Seconds ON, 30 Minutes OFF
18
Q
Pitot Tube Limit
A
15 Minutes Maximum on the Ground
19
Q
Engine Failure After V1
A
- POWER — Maximum allowable.
- LDG GEAR CONTROL handle – UP
(two positive climb indications). - Propeller — Verify feathered.
- FLAPS — UP after Vyse/Venr, (130 KIAS).
20
Q
VB (Turbulence Penetration)
A
150 KIAS
21
Q
Max Operating Temperature to 25,000 ft
A
ISA +37°C
22
Q
Max Design Sink Rate
A
500 feet per minute
23
Q
Min Altitude for Autopilot Use
A
200’ AGL
24
Q
SPINS
A
Control Wheel - Full Forward, Ailerons Neutral
Full Rudder - Opposite the direction of spin
Power Levers - IDLE
Rudder - Neutralize when rotation stops
Execute a smooth recovery
25
Engine Fire In Flight
| Fire Pull Handle Illuminated
1. POWER Lever (affected engine) – IDLE.
2. PROP Lever (affected engine) – FEATHER
3. MISSION CONTROL switch - OFF
4. CONDITION lever (affected engine) – FUEL CUTOFF.
5. FIRE PULL handle – PULL.
6. PUSH TO EXTINGUISH switch – Push (if required)
26
G Loading with Flaps Beyond Approach
0 to 2.0
27
N1 Limits
```
62-104% Normal
62% Low Idle (Min)
72% High Idle (Approximately)
88% Max Reverse
104% Normal Cruise
104% Max Cruise
104% Max Continuous
```
28
Engine Ice Vanes
Extended +5°C or below and in visible moisture.
29
Pneumatic Limits
12-20 Normal
30
Max Operating Altitude
35,000 ft
31
Minimum Airspeed for using Reverse
40 KIAS
32
Fuel System Limitations
265 lbs Min for takeoff (Mains Only)
300 lbs Max Fuel Imbalance
540 gal Usable Capacity
549 gal Max Capacity (9 gal within fuel lines)
10 hrs With Fuel Press Annunciator On
150 hrs Operating with AVGAS
15,000 ft Standby Boost Pumps When Using AVGAS
30,000 ft Standby Boost Pumps When Using JP4
33
Propeller Failure (OVER 1802 RPM)
1. POWER lever (affected engine) – IDLE.
| 2. PROP lever (affected engine) – FEATHER.
34
VA Design Maneuvering Speed
167 KIAS
35
Pitch Limits
30°
36
Generator Load Limits
0 -95% load 65% N1
95-100% load 70% N1
37
Oil Pressure
+/- 10 Fluctuations Authorized
40 (Min) Starting
60 (Min) Low Idle
60-90 Torque Limited to 54%
90 Undesirable
90 to 135 All Flight Conditions
90 to 135 Takeoff (5 Minutes)
40 - 200 Transient (20 sec)
200 (Max) Starting
38
VLE Landing Gear Extension
179 KIAS
39
Windshield Heat Must be On
Freezing level or 10,000’ AGL
40
Min Speed During Icing
140 KIAS
41
Max 90° crosswind (Less than 13000 lbs)
20 KIAS
42
Engine/Nacelle Fire During Start or Ground Operations
1. PROP levers – FEATHER.
2. CONDITION levers – FUEL CUTOFF.
3. FIRE PULL handle (illuminated) – PULL.
4. PUSH TO EXTINGUISH switch – Push (if required).
5. MASTER SWITCH – OFF.
43
Engine Malfunction During Final Approach
1. POWER – As required.
| 2. GEAR – Recheck DN.
44
Propeller De-Ice Ammeter
26-32 Amps
45
Max Demonstrated Crosswind
20 or 25Kts @ 90 if below / above 13,000 lbs
46
VMCA (Red Line)
103 KIAS
(VMCA = the minimum flight speed at which the aircraft is directionally controllable. Certification conditions include one engine becoming inoperative and propeller feathered, up to a 5° bank toward the operative engine, takeoff power on the operative engine, landing gear up, flaps up, most rear-ward CG)
47
Gyro Suction
2.8 - 5.9 Normal
48
Overspeed Governor
1802 RPM
| Test: 1540 to 1580 RPM
49
De-Ice Boots
½ (.5) inch Ice Build Up Prior to Activating Surface Deice
¼ (.25)°inch Ice Build Up Prior to Activating Antenna Deice
16 psi min With One Bleed Air Source Inoperative
Below -40°C Operation Can Cause Permanent Damage
50
Engine Malfunction Prior to or at V1 (Abort)
1. POWER levers — GROUND FINE.
2. Braking – AS REQUIRED
^^^^^^^^^^^^^^^^^^^^
3. REVERSE THRUST - AS REQUIRED
if insufficient runway remains for stopping perform the following:
4. CONDITION LEVERS - FUEL CUTOFF
5. FIRE PULL HANDLES - PULL
6. MASTER SWITCH - OFF
51
Fuselage Fire
1. Fight the fire.
| 2. Land as soon as possible if fire continues.
52
VSSE (Safe One-engine Operating Speed)
115 KIAS
(The safe one engine inoperative speed selected to provide a reasonable margin against the occurrence of an unintentional stall when making intentional engine cuts)
53
Landing Gear Cycling
5 Complete Cycles (Extension and Retraction) in a 20 minute period.
10 to 15 minute cooling period Between 20 Minute Time Groupings.
Cycle rate should Not Exceed 10 cycles Equally Spaced in 1 Hour.
54
G Loading with Flaps Up or Approach
–1.21 to 3.02
55
Engine Malfunction (Second Engine)
1. Airspeed – As required.
2. POWER lever – IDLE.
3. PROP lever – As required.
56
Torque Limitations
```
54% With <1000 RPM (N2)
75% Max Reverse
83% Max at 1700 RPM (N2)
94% Max at 1500 RPM (N2)
100% Max for Takeoff
100% Continuous
138% for 20 Sec Max Transient
```
57
Max Cabin Differential
6.5 psi
58
Engine Malfunction During Flight
1. Autopilot/Yaw Damper – Disengage.
2. POWER – As required.
3. Dead engine – Identify.
4. Propeller – Verify feather.
59
VREF
111 KIAS
60
Max Operating Temperature above 25,000 ft
ISA +31°C
61
Emergency Descent
1. POWER levers – IDLE.
2. PROP levers – HIGH RPM.
3. FLAPS – APPROACH.
4. Gear– DN.
5. Airspeed – 179 KIAS maximum.
62
Max for FULL Flap Extension
151 KIAS
63
Max 90° crosswind (Greater than 13000 lbs)
25 KIAS
64
PROP RPM N2
```
1000 Minimum unless in Feather
1450-1700 Normal
1650 Max Reverse
1700 Max Continuous
1870 Max Transient (for 20 Sec)
```
65
Cruise Climb Airspeeds
```
SL to 10,000 ft at Pilot’s Discretion = 160
SL to 10,000 ft = 135
10,000 to 20,000 ft = 130
20,000 to 25,000 ft = 125
25,000 to 35,000 ft = 120
```
66
SINGLE ENGINE GO-AROUND
1. POWER – Maximum allowable.
2. LDG GEAR CONTROL HANDLE – UP.
3. FLAPS – UP.
4. Airspeed – VYSE
67
Smoke and Fume Elimination
Crew oxygen masks –EMG and Don.
MIC Switch - Oxygen Mask
^^^^^^^^^^^^^^^^^^^^^^^^^^^
3. “ENVIRO & PNEU BLEED AIR valve switches — PNEU ONLY.
4. FWD VENT BLOWER switch — AUTO.
5. AFT VENT BLOWER switch — Off.
6. CABIN AIR MODE SELECT switch — OFF.”
If smoke and fumes are not eliminated:
7. CABIN PRESS switch — DUMP.
NOTE Opening storm window (after depressurizing) will facilitate smoke and fume removal.
8. Engine instruments — Monitor.
68
VYSE
VENR
Recommended for Autopilot-Coupled Approaches
130 KIAS
69
In-Flight Starting Limitations
In-flight engine restarts shall be conducted within 2 minutes or after 10 minutes, except if the engine is required for safety.
(This is due to thermal expansion issues)
70
Wing Tip Pod Limitations
254 lbs Minimum Weight for Pods w/out Limits
14,000 lbs Maximum Gross Takeoff Weight
11,000 lbs Maximum Zero Fuel Weight
71
Common Missile Warning System Safety Pin Limitations
The Safe/Arm Control Panel SAFETY PIN shall be installed during all ground operations.
72
Use of A/P During Severe Icing is ____________
Use of A/P During Severe Icing is Prohibited
73
Sustained Flight in Icing w/ Flaps Extended is ____________
Sustained Flight in Icing w/ Flaps Extended is Prohibited
74
Cracked Or Shattered Windshield (One-Time Evac Mission)
25,000 ft Max Altitude
25 Hours Max
Continued Flight with Cracked WS Cracks must NOT impair visibility
Cracks must NOT interfere with windshield wipers
Windshield anti-ice REQUIRED for flights into icing
2.0-4.6 PSID Required Cabin Diff until Landing
75
Crack in Any SIDE Window (One-Time Evac Mission)
25 Hours Maximum
Pressurized flight is PROHIBITED due to cracked side window.
Conduct flight w/ the cabin pressure switch in DUMP position
76
Vmo between 11,500-35,000ft
0.472 Mach
77
Spins, Aerobatics, Abrupt Maneuvers above 167KIAS
Prohibited
78
Do not attempt an airstart if N1 indicates ____, if there was a ____ ____ or there was a ____. Starting an engine under these conditions may have catastrophic results. Loss of aircraft control, damage to equipment, injury, and/or loss of life may occur.
0
Fuel Leak
Fire
