Lana'i Flashcards
1
Q
7.1 Airspeed Limitations
- Vmo
- Mmo
- Vo
- Vfe
- Vlo
- Vle
A
- Vmo: 240 KIAS (Maximum operating speed is the speed limit that may not be
exceed at any time) - Mmo: .48 MACH (Maximum operating limit speed is the speed limit that may not be deliberately exceeded in normal flight operations)
- Vo: 166 KIAS (10450lbs) 123 KIAS (5730lbs) (Maximum Operating Maneuvering airspeed is the maximum speed at which application of full available aerodynamic control will not overstress the airplane)
- Vfe: 15° 165 KIAS 30°/40° 130
- Vlo: 180 KIAS (Maximum landing gear operating speed is the maximum speed at which the landing gear can be safely extended or retracted)
- Vle: 240 KIAS
2
Q
7.2 Powerplant Limitations
Oil:
Capacity
Operating range
Takeoff NOT approved with _______ CAS Message
A
Capacity: 3.6Gal
Operating range: 1Gal
Inside green range
Takeoff not approved with ENGINE OIL LEVEL CAS message
3
Q
Fuel:
Approved Fuel Grades
When Anti Ice additive must be used
Total Fuel Capacity
Total Usable Fuel
Total Unusable
Maximum Fuel Imbalance
___ LCD segments on fuel indicator
Fuel can safely be used during _______________
Do not allow fueling with ________________
A
Approved fuel grades: JET A, JET A-1, JET B, JP-4
▪ Any other fuel that complies with latest revision of Pratt and Whitney Service Bulletin
o Anti-Ice additive must be used for all flight operations in ambient temperatures below 0° C
o Total Fuel Capacity: 406.8 Gal
o Total Usable Fuel: 402 Gal
o TotalUnusable:4.8Gal
o Maximum Fuel Imbalance 26.4 Gal
- 3 LCD segments on fuel indicator
o Fuel can be safely used during all Normal Category airplane maneuvers.
o Do not allow fueling with electrical busses powered or external power connected.
4
Q
Propeller:
4 Blade / 5 Blade
▪ Max Normal RPM:
▪ Max Transient RPM:
▪ Max Reverse RPM:
▪ Stabilized operation on the ground between _______ is not permitted.
A
Propeller
o4 Blade / 5 Blade
▪ Max Normal RPM: 1700 (+/- 30)
▪ Max Transient RPM: 1870
▪ Max Reverse RPM: 1650
▪ Stabilized operation on the ground between 350 and 950 RPM is not permitted.
5
Q
Generator
Max Continuous Load/ Max Load for 2 minutes**
Generator 1:
Starter/Generator 2:
A
Max Continuous load/max load for 2 minutes:
Generator 1 - 300/450 amps
Starter/Generator 2 - 300/450 amps
** Max load permitted for 2-minute period per each one hour of operation
6
Q
PCL Operation
Power Control Lever operation aft of the idle detent is prohibited:
A
▪ When engine is not running.
▪ During flight. Such operation may lead to loss of airplane control and total
power loss.
▪ When engine is controlled by the Manual Override System. Such operation may lead to loss of airplane control or may result in an engine/propeller overspeed condition and consequent loss of engine power.
7
Q
Chip Detector
Takeoff is not approved with:
A
Takeoff is not approved with ENGINE CHIP caution annunciator illuminated.
8
Q
Power Plant Window Markings
A
Red Amber Green Amber Red
(min Limit) (Caution) (Normal) (caution) (max Limit)
Torque (psi) N/A. N/A. 0-36.95psi. 36.95psi. 44.34psi
ITT (°C) N/A N/A 400-820°C 820°C 850°C
Engine Speed N/A 60% 60 - 103.5% 103.5% 104%
(Ng%)
Oil Temp (°C) N/A 10°C 10° - 105°C 105°C 110°C
Oil Pressure 60psi 90psi 90 - 135psi N/A 135psi
(psi)
9
Q
Engine Operating Limitations
SHP -
Takeoff - 1200
max Cont. Max Climb - 1200
Cruise - 1000
Max Reverse - 900
A
SHP
Takeoff - 1200
max Cont. Max Climb - 1200
Cruise - 1000
Max Reverse - 900
10
Q
Torque limit applies within a range of ____ to ____ propeller rpm
A
Torque limit applies within a range of 1000 to 1700 propeller rpm
11
Q
Torque is limited to ___ psi below ____ propeller rpm.
A
Torque is limited to 23.9 psi below 1000 propeller rpm.
12
Q
Normal oil pressure is __ to __ psi at gas generator speeds above ___
A
Normal oil pressure is 90 to 135 psi at gas generator speeds above 72%
13
Q
With engine torque below ___ psi, minimum oil pressure is __ psi at normal oil temperature (__ - __° C).
A
With engine torque below 35.87 psi, minimum oil pressure is 85 psi at normal oil temperature (60 to 70° C).
14
Q
Oil pressures under __ psi are undesirable.
A
Oil pressures under 90 psi are undesirable.
15
Q
Under emergency conditions, to complete a flight, a lower oil pressure of __ psi is permissible at reduced power level not exceeding __ psi torque.
A
Under emergency conditions, to complete a flight, a lower oil pressure of 60 psi is permissible at reduced power level not exceeding 23.9 psi torque.
16
Q
Oil pressures below __psi are unsafe and require that either the engine be shut down or a landing be made as soon as possible using the minimum power required to sustain flight.
A
Oil pressures below 60 psi are unsafe and require that either the engine be shut down or a landing be made as soon as possible using the minimum power required to sustain flight.
17
Q
- This value is time limited to 5 seconds maximum.
- These values are time limited to 20 seconds maximum.
transient:
TORQUE __psi,
Max ITT ___°C,
Np RPM ____,
Oil Pressure __ - ___psi
A
- STARTING - Max ITT (1000°C)
- TRANSIENT - TORQUE 61psi,
Max ITT 870°C,
Np RPM 1870,
Oil Pressure 40 - 200psi
18
Q
These values apply over a speed range of 50.7% to 61.4% Ng rpm
A
Min idle - Max ITT 750°C
19
Q
For increased service life of the engine oil, an oil temperature of between __ to __° is recommended.
A
60° - 70°C
20
Q
Oil temperature limits are __° C to __° C with limited periods of __ minutes at __ to __°C.
A
Oil temperature limits are -40° C to 105° C with limited periods of 10 minutes at 105 to 110°C.
21
Q
100% gas generator speed corresponds to _____ rpm. 100% power turbine speed (N1) corresponds to _____ rpm which also corresponds to ____ rpm propeller speed.
A
100% gas generator speed corresponds to 37468 rpm. 100% power turbine speed (N1) corresponds to 29894 rpm which also corresponds to 1700 rpm propeller speed.
22
Q
Takeoff power is time limited to _ minutes
A
5
23
Q
regarding which values, during which steady state operations (phases of flight), operation from ___ rpm up to ___ rpm is permitted to allow for governing accuracy.
A
During steady state operation, operation from 1670 rpm up to 1730 rpm is permitted to allow for governing accuracy.
Takeoff
Max Cont./Max Climb
Cruise
24
Q
Weight Limitations
Max Ramp Weight = ____ lbs.
Max Takeoff Weight = ____ lbs.
Max Landing Weight = ____ lbs.
Max Zero Fuel Weight = ____ lbs.
A
Max Ramp Weight = 10495 lbs.
Max Takeoff Weight = 10450 lbs.
Max Landing Weight = 9921 lbs.
Max Zero Fuel Weight = 9039 lbs.
25
CG Limitations
## Footnote
At mat takeoff weight
CG Limitations
## Footnote
Weight. (lb) Foward Limit. (in) Aft Limit (in)
10450 232.2 240.43
26
It is the responsibility of the ___ to make sure the airplane is loaded properly using the
“PC-12 Calculator” (all managed iPads) or via reference to Section 6 of the Pilot’s Information Manual.
It is the responsibility of the captain to make sure the airplane is loaded properly using the “PC-12 Calculator” (all managed iPads) or via reference to Section 6 of the Pilot’s Information Manual.
27
This airplane is certificated in the ______ Category. Aerobatic maneuvers, including spins, are not approved.
This airplane is certificated in the Normal Category. Aerobatic maneuvers, including spins, are not approved.
28
Flight load limits with flaps up +\_\_\_ g - ___ g
Flight load limits with flaps down +\_\_\_ g - \_\_\_g
Flight load limits with flaps up +3.3 g - 1.32 g
Flight load limits with flaps down +2.0 g - 0.0g
29
The Pilatus PC-12 is approved for the following types of operation when the required equipment is installed and operational:
o VFRDay/Night
o IFR Day incl. CAT 1 approaches, single pilot
o IFR Night incl. CAT 1 approaches, single pilot
o Flight into Known Icing Conditions.
The Pilatus PC-12 is approved for the following types of operation when the required equipment is installed and operational:
o VFRDay/Night
o IFR Day incl. CAT 1 approaches, single pilot
o IFR Night incl. CAT 1 approaches, single pilot
o Flight into Known Icing Conditions.
30
Starter Operating Limitations
Sequence ............................................................................. ________ Off
Sequence ............................................................................. ________ Off
Sequence ............................................................................. ________ Off
Sequence ....................................................................................... 60 Seconds Off
Sequence ....................................................................................... 60 Seconds Off
Sequence ....................................................................................... 30 Minutes Off
31
The Company *does/doesnt* maintain RVSM compliance for the PC-12; therefore:
Maximum operating altitude with two pilots is \_\_\_\_; and
Maximum operating altitude with one pilot is \_\_\_\_.
See oxygen chart for operating requirements.
Operations with one pilot above FL\_\_\_ up to and including FL\_\_\_ is allowed if that pilot wears, secured and sealed, an oxygen mask providing supplemental oxygen at all times during operations at those altitudes.
The Company does NOT maintain RVSM compliance for the PC-12; therefore Maximum operating altitude with two pilots is FL280; and
Maximum operating altitude with one pilot is FL250.3 See oxygen chart for operating requirements.
Operations with one pilot above FL250 up to and including FL280 is allowed if that pilot wears, secured and sealed, an oxygen mask providing supplemental oxygen at all times during operations at those altitudes.
32
Cabin Pressurization Limitations
Maximum cabin pressure differential is ____ psi
Pressurized landing is approved, up to ___ psi
Maximum cabin pressure differential is 5.75 psi
Pressurized landing is approved, up to 0.7 psi
33
Outside Air Temperature Limitations
## Footnote
Minimum Outside Air Temperature -\_\_° C
Maximum Outside Air Temperature \_\_° C
Minimum Outside Air Temperature -55° C
Maximum Outside Air Temperature 50° C
34
Flight in icing conditions is only approved with \_\_\_\_\_\_\_\_\_\_\_\_, ________ \_ and _______ \_ serviceable.
Flight in icing conditions is only approved with all ice protection systems, generator 1 and generator 2 serviceable.
35
Flight in icing conditions is prohibited when the _______________ is active.
Flight in icing conditions is prohibited when the Propeller De Ice caution is active.
36
During flight in icing conditions, if there is a failure of \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_, then \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_. Immediately request _______________ to facilitate a ___________ to exit the icing conditions.
During flight in icing conditions, if there is a failure of any of the aircraft ice protection systems exit icing conditions. Immediately request priority handling from Air Traffic Control to facilitate a route or an altitude change to exit the icing conditions.
37
During flight in icing conditions or flight with any visible ice accretion on the airframe, the following flap maximum extension limits apply:
After failure of the airframe pneumatic deice boots, \_\_° FLAP; With operational airframe pneumatic deice boots, \_\_° FLAP;
In the event of a balked landing go-around with residual ice on the airframe, the flaps should not be retracted from the \_\_° position.
During flight in icing conditions or flight with any visible ice accretion on the airframe, the following flap maximum extension limits apply:
After failure of the airframe pneumatic deice boots, 0° FLAP;
With operational airframe pneumatic deice boots, 15° FLAP;
In the event of a balked landing go-around with residual ice on the airframe, the flaps should not be retracted from the 15° position
38
Flight in freezing rain, freezing fog, freezing drizzle and mixed conditions causing ice accretion beyond the protected areas of the pneumatic boots *is/is not* approved
Flight in freezing rain, freezing fog, freezing drizzle and mixed conditions causing ice accretion beyond the protected areas of the pneumatic boots is not approved.
39
The aircraft must be clear of all deposits of \_\_\_\_, \_\_\_\_\_, and ____ adhering to the lifting and control surfaces immediately prior to takeoff.
The aircraft must be clear of all deposits of snow, ice and frost adhering to the lifting and control surfaces immediately prior to takeoff.
40
In the event of a balked landing (go around) with residual ice on the airframe, the landing gear and flaps may not fully retract after selection.
In the event of a balked landing (go around) with residual ice on the airframe, the landing gear and flaps may not fully retract after selection.
41
The _________________ must be operative prior to flight into forecast icing conditions at night.
The left-wing inspection light must be operative prior to flight into forecast icing conditions at night.
42
During flight, severe icing conditions that exceed those for which the airplane is certificated shall be determined by the following visual cues.
If one or more of these visual cues exists, immediately request priority handling from ATC to exit the icing conditions:
If one or more of these visual cues exists, immediately request priority handling from ATC to exit the icing conditions:
Unusually extensive ice accumulation on the airframe and windshield areas not normally observed to collect ice
Accumulation of ice beyond the active portions of the wing pneumatic boots
43
Pneumatic Deicing Boot Limitations
The pneumatic deice system boots are *required/not required* to be installed for all flights.
Preflight function test *required/not required* before takeoff and flight into known icing conditions.
The system is *required/not required* to function properly for flight into known icing conditions.
Operation of the pneumatic de-ice boot system in ambient temperatures below \_\_°C and above \_\_°C may cause permanent damage to the boots.
The wing and tail leading edge pneumatic deicing boot system *must be/dont need to be* activated at the first sign of ice formation anywhere on the aircraft.
The wing and tail leading edge pneumatic deicing boot system may be/may not be deactivated only after leaving icing conditions and after the aircraft is determined to be clear of ice.
The pneumatic deice system boots are required to be installed for all flights.
Preflight function test required before takeoff and flight into known icing conditions.
The system is required to function properly for flight into known icing conditions.
Operation of the pneumatic de-ice boot system in ambient temperatures below -40°C and above +40°C may cause permanent damage to the boots.
The wing and tail leading edge pneumatic deicing boot system must be activated at the first sign of ice formation anywhere on the aircraft.
The wing and tail leading edge pneumatic deicing boot system may be deactivated only after leaving icing conditions and after the aircraft is determined to be clear of ice.
44
System and Equipment Limitations
## Footnote
Stall Warning / Stick Pusher:
Preflight function test *required/not required* before takeoff.
System is *required/not required* to function properly in normal mode for all flights and in ice mode for flight into known icing conditions.
Brakes:
To allow adequate cooling of the wheels and brakes the aircraft must remain onthe ground for at least __ min following the two events:
▪
▪
Trim Systems
o Stabilizer normal and alternate, and rudder trim systems *must/may not* function properly for all flights.
Stall Warning / Stick Pusher:
Preflight function test *required* before takeoff.
System is *required* to function properly in normal mode for all flights and in ice mode for flight into known icing conditions.
Brakes:
To allow adequate cooling of the wheels and brakes the aircraft must remain onthe ground for at least 45 min following the two events:
▪ Rejected takeoff with brake on speed greater than Vr - 20 kts and heavy brake usage.
▪ 0° flap full stop landing and heavy brake usage.
Trim Systems
o Stabilizer normal and alternate, and rudder trim systems must function properly for all flights.
45
Heated Windshield
o Left Hand and Right-Hand Heated Windshields *must/may not* function properly for all flights. Exception, for IFR flights conducted into no known or forecast icing conditions at least __ heating zone of the windshield on the side of the pilot in command must function properly.
Heated Windshield
o Left Hand and Right-Hand Heated Windshields must function properly for all flights. Exception, for IFR flights conducted into no known or forecast icing conditions at least one heating zone of the windshield on the side of the pilot in command must function properly.
46
Fire Detection System
o Preflight Function Test *is/is not* required for takeoff.
o System *must/may not* function properly for all flights.
Fire Detection System
o Preflight Function Test is required for takeoff.
o System must function properly for all flights.
47
+Oxygen System
A minimum oxygen supply of __ minutes duration for each occupant is required for dispatch for pressurized flight above FL\_\_\_.
The oxygen system shut-off valve handle in the cockpit must be selected to __ prior to engine start and throughout the duration of flight.
The oxygen masks for the crew must be ______ for all flights.
For aircraft with the Corporate Commuter sidewall paneling, oxygen masks must be connected and properly stowed for each passenger prior to takeoff when the aircraft is to be operated above \_\_\_\_\_\_
In the executive interior configurations, the oxygen masks are ______ connected.
• Oxygen System
o A minimum oxygen supply of 10 minutes duration for each occupant is requiredfor dispatch for pressurized flight above FL250.
o The oxygen system shut-off valve handle in the cockpit must be selected to on prior to engine start and throughout the duration of flight.
o The oxygen masks for the crew must be connected for all flights.
o For aircraft with the Corporate Commuter sidewall paneling ,oxygen masks must be connected and properly stowed for each passenger prior to takeoff when the aircraft is to be operated above 10,000 feet.
▪ In the executive interior configurations, the oxygen masks are permanently connected.
48
PROBE HEAT
Preflight function test *required/not required* before takeoff
The system is required to function properly for ___ flight and flight \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
PROBE HEAT
Preflight function test required before takeoff
The system is required to function properly for IFR flight and flight into known icing conditions.
49
Flap System Cycle Limits
A flap cycle is defined as movement from \_° to \_\_° to \_\_° and from \_° to \_\_° to \_\_°
to \_\_°.
▪ Maximum number of cycles per hour
Up to 25° C OAT = \_\_
25° C to 50° C OAT = \_\_
A flap cycle is defined as movement from 0° to 15° to 0° and from 0° to 15° to 40°to 0°.
▪ Maximum number of cycles per hour
Up to 25° C OAT = 10
25° C to 50° C OAT = 8
50
Primus Apex
o The Honeywell PRIMUS APEX Integrated Avionics System for the Pilatus PC-12NG Pilot’s Guide must *always/sometimes* be on board the aircraft.
Primus Apex
o The Honeywell PRIMUS APEX Integrated Avionics System for the Pilatus PC-12
NG Pilot’s Guide must always be on board the aircraft.
51
Primus Apex AFCS MUH
OpSpec C071 Autopilot Minimum Use Altitudes/Heights (MUH)
Minimum use heights:
Takeoff/initial climb
Enroute
Approach
Minimum use heights:
Takeoff/initial climb - 400'
Enroute - 1000'
Approach - APV/ILS 200'
Non-precision 400'
52
During autopilot operation, a pilot must be seated in a _______ with \_\_\_\_\_\_\_\_\_.
During autopilot operation, a pilot must be seated in a pilot position with seat belt fastened.
53
The ________ and _________ must be ___ during \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_. (AFC)
The autopilot (AP) and yaw damper (YD) must be OFF during takeoff and landing.
54
The system is approved for Category _ operation (Approach mode selected) and autopilot coupled go-arounds initiated at \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
The system is approved for Category 1 operation (Approach mode selected) and autopilot coupled go-arounds initiated at decision altitude or minimum descent altitude.
55
Maximum approved glideslope angle for all coupled approaches is \_\_°.
Maximum approved glideslope angle for all coupled approaches is 4°.
56
Maximum approved VNAV / VPATH coupled descent angle is \_\_°
Maximum approved VNAV / VPATH coupled descent angle is 8°
57
During normal operation do not overpower the autopilot to change ___ and ___ attitude.
During normal operation do not overpower the autopilot to change pitch and roll attitude.
58
In accordance with FAA recommendation (AC 00-24C), the use of “PITCH ATTITUDE HOLD” mode is recommended during operation in \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_.
In accordance with FAA recommendation (AC 00-24C), the use of “PITCH ATTITUDE HOLD” mode is recommended during operation in severe turbulence.
59
MAXIMUM PASSENGER SEATING LIMITATIONS
For take-off and landing the ______ and __________ must be fastened, the _______ tightened, and the __________ positioned to support the head.
For take-off and landing the seat lap and shoulder belts must be fastened, the lap belt tightened, and the seat headrest positioned to support the head.
60
Cargo Limitations
STD-9S - ____ lb
EX-6S-STD-2S - ___ lb
EX-4S-STD-4S - ___ lb
EX-6S-2 - ___ lb
EX - 4S - ___ lb
Cargo Limitations
STD-9S - 265lb lb
EX-6S-STD-2S - 265 lb
EX-4S-STD-4S - 265 lb
EX-6S-2 - 400 lb
EX - 4S - 400 lb
61
Maximum freight load
3300 lbs
62
Cargo must be arranged to permit free access to the _________ and the \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
Cargo must be arranged to permit free access to the passenger door and the right-hand emergency over-wing exit.
63
All cargo must be secured by approved Cargo Restraints as described in Section 6. Tie Down Straps with a breaking strength of at least ____ lbs. per strap must be used. All Cargo/Containers must be located against a Retaining Bar secured laterally to the seat rails.
All cargo must be secured by approved Cargo Restraints as described in Section 6. Tie Down Straps with a breaking strength of at least 1800 lbs. per strap must be used. All Cargo/Containers must be located against a Retaining Bar secured laterally to the seat rails.
64
Items up to a total weight of __ lbs. can be stowed in the cabin area without being strapped down providing a Cargo Net is installed in front of the items. Cargo Nets may only be installed on the attachments at Frames __ and \_\_. No passengers must be seated rearward of a Cargo Net.
Items up to a total weight of 66 lbs. can be stowed in the cabin area without being strapped down providing a Cargo Net is installed in front of the items. Cargo Nets may only be installed on the attachments at Frames 24 and 27. No passengers must be seated rearward of a Cargo Net.
65
If an extendable baggage net is used the tie down fittings and the cargo strap fittings must have a minimum space of __ inches between the fittings.
If an extendable baggage net is used the tie down fittings and the cargo strap fittings must have a minimum space of 5 inches between the fittings.
66
Smoking or vaping is prohibited in the _____ or _____ on any Company aircraft.
Smoking or vaping is prohibited in the cabin or lavatory on any Company aircraft.
67
PORTABLE ELECTRONIC DEVICE LIMITATIONS
The PC-12 NG is ________ tolerant.
The Safety Card instructs that handheld devices must be in _______ (non-transmitting) mode for \_\_\_\_\_\_, \_\_\_\_\_\_\_\_\_, and \_\_\_\_\_\_\_\_.
PORTABLE ELECTRONIC DEVICE LIMITATIONS
The PC-12 NG is Transmitting-PED tolerant.
The Safety Card instructs that handheld devices must be in airplane (non-transmitting) mode for taxi, takeoff, and landing.
68
Engine Operating Limitations
**_Torque_**
Takeoff -
Max Cont. Max climb. -
Cruise -
Transient -
Max. Reverse -
**_Torque_**
Takeoff - 44.34
Max Cont. Max climb. - 44.34
Cruise - 36.95
Transient - 61
Max. Reverse - 34.25
69
Engine Operating Limitations
**_Max ITT °C_**
Takeoff -
Max cont. Max Climb. -
Cruise -
Min Idle -
Starting -
Transient -
Max Reverse -
**_Max ITT °C_**
Takeoff - 850
Max cont. Max Climb. - 820
Cruise - 820
Min Idle - 750 (5)
Starting - 1000 (3)
Transient - 870 (4)
Max Reverse - 760
70
Engine Operating Limitations
**_NG %_**
Takeoff -
Max Cont. Max Climb. -
Cruise -
Min Idle -
Starting -
Transient -
Max Reverse -
**_NG %_**
Takeoff - 104
Max Cont. Max Climb. - 104
Cruise - 104
Min Idle - 60.7 (GI) 64 (FI)
Starting -
Transient - 104
Max Reverse -
71
Engine Operating Limitations
**_Np RPM_**
Takeoff -
Max Cont. Max Climb. -
Cruise -
Min Idle -
Starting -
Transient -
Max Reverse -
**_Np RPM_**
Takeoff - 1700 (10)
Max Cont. Max Climb. - 1700 (10)
Cruise - 1700 (10)
Min Idle -
Starting -
Transient - 1870 (4)
Max Reverse - 1650
72
Engine Operating Limitations
**_Oil Press PSI_**
Takeoff -
Max Cont. Max Climb. -
Cruise -
Min Idle -
Starting -
Transient -
Max Reverse -
**_Oil Press PSI_**
Takeoff - 90 - 135
Max Cont. Max Climb. - 90 - 135
Cruise - 90 - 135
Min Idle - 60 Min
Starting - 200 Max
Transient - 40 - 200 (4)
Max Reverse - 90 - 135
73
Engine Operating Limitations
**_Oil Temp °C_**
Takeoff -
Max Cont. Max Climb -
Cruise -
Min Idle -
Starting -
Transient -
Max Reverse -
**_Oil Temp °C_**
Takeoff - 10 - 110
Max Cont. Max Climb - 10 - 105
Cruise - 10 - 105
Min Idle - -40 - 110
Starting - -40 Min
Transient - -40 - 110
Max Reverse - 10 - 105
74
D073 - AAIP
\_\_\_hr/\_\_mo
\_\_\_hr / \_\_\_mo
300hr / 6mo
600hr / 12mo
75
D095 - MEL
## Footnote
Cat A: Must be repaired within...
Cat B: Must be repaired within...
Cat C: Must be repaired within
Cat D: Must be repaired within
Cat A: Must be repaired within the time interval specified in "remarks or exceptions" collumn of Certificate Holders FAA-Approved MEL
Cat B: Must be repaired within Repaired within 3 consecutive calender days (72hrs) excluding the calender day the malfunction was recorded in MX Logs
Cat C: Must be repaired within 10 consecutive calender days excluding the calender day the malfunction was recorded in MX Logs
Cat D: Must be repaired within 120 consecutive calender days excluding the calender day the malfunction was recorded in MX Logs
76
Positive transfer of controls
A
B
C
**A**dvise PM
**B**rief PM on current status (Atc Clearance, Automation, Flight path, etc...)
**C**hange - "You have the controls"
"I have the controls"
77
PIC Needs Immediate control - procedure
&
When may SIC exercise emergency authority to assume controls
"I have the Controls"
"You have the controls"
Brief reason for taking control as time permits
&
Sic may exercise emergency authority to assume controls only in the event of PIC Incapacitation
78
If AP is engaged, who makes all AFCS Inputs?
What if its disengaged?
Who must confirm all changes and what is said to confirm?
Who must confirm and announce AFCS mode change annunciations for initial arming or capturing of a lateral or vertical guidance?
PF
PM
Pilot not operating the AFCS, "Set/Checked"
PF
79
Who manages ATC communications unless busy with other duties?
If busy with other duties, what is said before leaving and upon return to ATC
PM
"I am off comm 1" & "I am back on Comm 1, any changes?"
80
Flap Setting Changes inflight
When commanded to change the flap setting by the PF, the PM will
1.
2.
3.
4.
what airspeed in relation to Vfe should flaps be operated and why
1. Ensure speed below Vfe (decreasing or stable)
2. Report "speed checks, flaps \_\_" after confirming correct speed
3. Visually confirm flap selector lever is in commanded position
4. Report "Flaps __ set" when flap movement ceases
Operate flaps 10KIAS below Vfe to prevent overspeed and required MX actions/inspections
81
Landing Gear Setting changes in flight
When commanded by PF to operate landing gear, PM will
1.
2.
3.
What airspeedinrelation to Vlo should the gear be operated and why?
1. Check speed is decreaseing or stable below 180KIAS
2. Announce "Speed checks, Gear down"
3. Report "Gear down, Three green"
Operate Gear 10KIAS below Vlo to prevent overspeed & MX actions/inspections
82
External Lights
\_\_ operates external lights for taxi and Takeoff
\_\_ operates external lights in flight and after landing
Prior to entering or crossing any runway, the ____ light, _____ lights, and _____ lights will be turned on
PF operates external lights for taxi and Takeoff
PM operates external lights in flight and after landing
Prior to entering or crossing any runway, the Taxi light, Landing lights, and Strobe lights will be turned on
83
When must the following lights be on
Taxi lights
Anytime the aircraft is in motion on the ground, day or night
one flash signals to marshaller that you are ready to taxi
84
When must the Navigation Nav lights be on
For all operations unless deferred per MEL for daytime operations
85
When must the Rotating beacon be on
Prior to engine start & will stay on for all operations until the engine is shut down
May be turned off if causing distraction due to weather (IMC at night...etc)
86
when must the Strobe lights be on
Just prior to takeoff & remain on during all flight operations exept when they may cause cockpit distractions in certain WX
87
When must the Recog/pulse lights be on?
Prior to entering or crossing any runway & remain on below FL180 until clearing the landing RWY
Pulse (day)
Steady (night)
88
When must the landing lights be turned on?
Prior to entering or crossing any runway
89
when must the Wing (ice detection) light be operative?
known or forecast icing conditions at night
90
\_\_ Operates the Icing protection panel unless otherwise noted
PM
91
When must the probes be on?
On at line-up check, until clearing runway at destination
92
When must the windshield heat be operated?
As required for visibility (high humidity with condensation, icing, etc...)
93
When should the Inertial Seperator be open?
During flight in icing or heavy Precip and during all taxi, takeoff, and landing operations
closed when not required to be open
94
When should the Deice Boots and Prop heat be on?
ON at the first indication of icing conditions & remain on until no residual ice remains on the airframe
95
when is the preflight test of ice protection equipment required?
First flight per crew and each flight into known or forecast icing conditions
96
Describe the Challenge/Response method of Checklist usage
1. PF calls for appropriate checklist
2. PM states challenge item
3. PF confirms item is complete and set appropriately
97
Describe the NON-Challenge method
1. PF calls for appropriate checklist
2. PM states each challenge item and confirms complete
98
Aircraft Acceptance flow
When is this performed
What, in addition to the flow, should be accomplished after each flight and maintinence
**_Cabin Check_**
## Footnote
1. Fire Extinguisher.......... INSTALLED BEHIND COPILOT SEAT
2. Briefing speaker............ CHARGED
3. Infant Life Vests............ FOR EACH INFANT PASSENGER
4. Life Vest..............................INSTALLED FOR EACH PASSENGER SEAT
5. Safety card...................... FOR EACH PASSENGER
6. Seatbelt.............................. ATTACHED TO EACH SHOULDER HARNESS
7. Heater Air Intake.......... ON BAGGAGE STEP, NO AIRFLOW OBST.
8. Baggage restraints.... AS REQUIRED (BAGGAGE/CARGO NET), STRAPS
9. Aircraft Bag............. (Engine inlet covers, tool bag (optional))
10. First Aid Kit........... Sealed. (Not required by rule)
11. Cleaning kit........... Main/leather, window, wipes, gloves, bags
performed after maintinence, and before each flight
Check for personal items left/company items taken after flights, especially between seats and sidewalls
99
Acceptance flow - Documents
1. Airworthiness........... SERIAL # CORRECT & IN PAX VIEW
2. Registration...............CURRENT & CORRECT TAIL & SERIAL #
3. POH Volumes1 & 2... BEHIND COPILOT SEAT
4. Primus Apex Pilots Guide... BEHIND PILOT SEAT
5. QRH....... PRINTED QRH ON BOARD (report worn or damaged to MX)
6. Aircraft binder.......
MX STATUS OVERVIEW - no inspections out of date/wont expire during flight.
LOGGING SHEET - Adequate space, & Hobbs entry matches current reading
OPEN MEL ITEMS - Binder cover shows MEL status. check for operational restrictions in current MEL & discuss
DISCREPANCY ENTRIES - must have corrective action or unexpired deferral. No open discrepancies permitted for flight (except specified MX flights)
VOR CHECKS - required within 30 days before use of each NAV Radio
WEIGHT & BALANCE FORM - Correct and in folder, matches weight, moment, & seating Config. used for calculations
7. IPads.......... CHARGED AND UPDATED. W&B DATA MATCHES OFFICIAL DATA IN BINDER
100
Acceptance Flow - Overhead Panel
1. Fuel Pumps............................................ AUTO
2. Ignition.................................................. AUTO
3. External Lights...................................... OFF
4. PAX Warnign signs............................... OFF
5. AV busses, Cabin Bus, Gen Busses....... ON
6. STBY Bus, BAT Busses........................ OFF
7. Bus Tie.................................................. CLOSED
8. EXT PWR............................................. CENTERED
9. Master Power & Gaurd......................... ON & GUARDED
10. EPS...................................................... OFF
101
Acceptance Flow - Pedestal
1. WX Radar........................................................ STBY (OFF used for MX only)
2. Main Oxygen lever.......................................... ON
3. Display Reversion Controls............................ NORMAL/SET
4. ELT.................................................................. ARMED/GUARDED
5. Trim & flap Interrupts..................................... NORM/GUARDED
6. MOR Lever..................................................... OFF & STOWED
7. Power Lever..................................................... IDLE
8. Condition Lever............................................... CUTOFF/FEATHER
9. ⇔Flap.............................................................. 0°
10. Cockpit/Instrument/Cabin light switches....... OFF
11. Fuel Firewall Shuttof lever............................. STOWED
12. Landing Gear Override Handle...................... STOWED
13. ACS Firewall Shutoff Lever........................... FULLY IN
102
Acceptance Flow - Cockpit Sweep
1. Crew Oxygen Masks............... 100% & CHECKED L/R
2. 110 Vac.................................... ON
3. Emerg Com 1........................... NORM
4. Aural Warn............................... ON
5. Mic Selects............................... MIC (L/R)
6. Oxygen Pressure....................... CHECKED
7. PAX Oxygen Selector............... AUTO
8. Circuit Breakers........................ CHECKED (L/R)
9. Parking Brake............................ SET/SIGN SET
10. ⇔Ice Protection....................... OFF
11. Inertial Seperator...................... OPEN
12. Landing Gear Handle............... DOWN
13. ACS, ECS, CPCS Switches....... AUTO
103
Before Start
Complete when ____ Pilots are present in Cockpit and approx __ Min or less from engine start
1. Preflight Checks........... COMPLETE
* Full external safety Inspection walkaround, cabin check, security inspection prior to first flight of day, after every crew change and after MX and before all other flights
2. Oxygen........... ON, CHECKED, SET 100% (L/R)
* Indication must be below red line and adequate for upcoming flights
* Oxygen Pressure Gauge - note reading
* OAT - note reading
* % of full bottle - determine from "oxygen available with partially full bottle" graph" and compute in MIN
* determine oxygen duration in MIN for a full bottle for the number of connected pax oxygen masks and pilots from the "oxygen duration with full bottle" graph
* Multiply the full bottle duration by the % of usable capacity to obtain the available oxygen duration in minutes
* company policy: the oxygen masks associated with each pax seat will always remain attached to its outlet
3. Circuit Breakers........ Checked (L/R)
* check if any circuit breakers have tripped since last check. Consult MX personnel for guidance before proceeding
4. WX & Clearance......... RECEIVED, ATIS \_\_\_
* obtain ATC Clearance and lcl WX/NTM info. review en route and dest WX if appropriate
Turn on STBY Bus (at a minimum) according to sequence below to operate radios and program FMS
5. FMS/ Fuel REM............ REVIEWED/\_\_.\_\_/FLT ID SET
* SIC programs FMS and PIC verifies FMS is correct
* after, both pilots must review FMS for correct data/routing
* check fuel rem box on waypoints pg displays appr #. REQUIRED for VNAV
* during INIT Programming: check databases will stay current for entire flight day & flt ID matches ATC callsign for upcoming flight. *Databases expire at 2400Z on the last day listed under each database heading*
* 6.* Takeoff Power Setting.............. ___ PSI
* Calculate takeoff torque setting from POH Static Takeoff torque chart (Speed Card or Foreflight documents). This will be the target torque setting for Takeoff. ACS must be inhibited before takeoff if target setting is below the flat portion of the chart
7. SEBB........... BUSSES ON/ARMED, EPS LIGHT OFF
* The electrical system must be powered up in the following sequence:
1. STBY BUS - ON
* FMS and radio tasks may be completed using only the STBY bus to conserve battery power, if desired
1. EPS bus - TEST for 5 sec (green TEST light must stay on during test), then. EPS bus - ARMED
* Red "EPS ON" light must illuminate until main batteries are on. **Wait until lower MFD displays map page and ESIS begins aligning before continuing**
1. ****BAT 1 - ON, BAT 2 - ON
* The red "EPS ON" light must extinguish once the main batteries are on
* When Completing before start checklist, Check*:
***_S_***tandby bus switch is on
***_E_***PS switch is armed
***_B_***attery 1 and ***_B_***attery 2 busses are on
Red "EPS ON" light has extinguished
8. EXT PWR............ ON (or NOT AVAILABLE)
* If using external Power, allow PFD 1 to display before selecting External power - ON
9. \*External Lights......... CHECKED
104
**_After Takeoff_**
Both pilots begin this flow after \_\_\_\_\_\_\* or \_\_\_\_\_\_\*.
\*LIFTOFF, \*GO-AROUND/MISSED APPROACH
## Footnote
**(PM CALLS)**"POSITIVE RATE"
**(PF CALLS, PM SETS)**"GEAR"
"YAW DAMPER"
"FLAPS"
"TAXI/LANDING LIGHT"
**(PF)**
ICE PROTECTION.......................................AS REQUIRED
**(PM)**
ACS BLEED AIR..........................................AUTO/PRESSURE CHECKED
**(PF)**
POWER..........................................................CLIMB POWER
105
**Cruise**
\_\_\_\_\* completes cruis flow after \_\_\_\_\_\* at intermediate and final cruising altitudes.
\*PF, \*LEVEL OFF
## Footnote
**(PF)**
ICE PROTECTION.....................................AS REQUIRED
POWER.......................................................SET [PER CRUISE CHART]
ENGINE INSTRUMENTS.........................GREEN
CPCS...........................................................CHECKED [▵P 5.75MAX, ADJUST A/C]
FUEL...........................................................CHECKED
106
**_Descent Flow_**
Begin descent flo no later than \_\_\_\_\_\_\* or \_\_\_\_\_\_\* (if cruising above FL180)
\*TOP OF DESCENT, \*PASSING BELOW TRANSITION ALTITUDE
## Footnote
**(PM)**
ATIS/WEATHER INFORMATION
**(PF/PM)**
ALTIMETERS............................................\_\_.\_\_ SET AND CROSSCHECKED
**(PM)**
LANDING FIELD......................................[LFE]\_\_\_\_SET
**(PF)**
APPROACH BREIFING/SET UP..............COMPLETE
**(PM)**
ICE PROTECTION....................................AS REQUIRED/SEPARATOR OPEN
RECOG LIGHTS/SIGNS...........................ON
107
**_Landing_**
Complete landing checklist prior to descending below ____ AGL\*. Autopilot may remain on until the minimum authorized altitude.
\*500'
## Footnote
LANDING GEAR................................DOWN THREE GREEN
FLAPS..................................................\_\_\_\_\_\_
EXTERNAL LIGHTS.........................ON
CABIN PRESSURE............................BELOW 0.7
AIRSPEED..........................................\_\_\_\_\_\_
AUTOPILOT/YAW DAMP.................OFF
*(Autopilot can be disconnected no lower than 200' on ILS/APV, and 400' on non-precision approach)*
108
**_After Landing Flows_**
Complete the after landing flows when \_\_\_\_\* of the runway after landing, exept item \_\_\_\_\* may be completed before exiting the runway.
\*CLEARED, \*#1
**_ON THE RUNWAY_**
**(PF)**
CONDITION LEVER............................GROUND IDLE [2MIN COOLDOWN]
**(PM)**
TIMER...................................................START
**_AFTER EXITING THE RUNWAY_**
**(PF)**
TRIMS...................................................GREEN RANGE
ICE PROTECTION...............................AS REQUIRED
**(PM)**
FLAPS...................................................0 ▶︎ 15
WX RADAR.........................................STBY
LIGHTS................................................AS REQUIRED
*(Normally, TAXI, BEACON, and NAV light will be on)
(Turn off all light exept NAV and BEACON when approaching ground marshaller or others to avoid blinding effect)*
109
**_Parking Flow_**
PIC completes the securing flow after the last flight of the day, before leaving the airplane unattended, or before towing.
Main oxygen lever..........................................OFF
Flight control lock..........................................INSTALLED
Instal the flight control lock after the last flight of the day and if wind or other aircraft may affect flight control movements while aircraft is parked on the ramp.
Parking brake.................................................RELEASED [if chocked or towing]
Release the parking brake if the aircraft is chocked or about to be towed. Never leave an aircraft unattended unless chocked or parking brake is set with brakes pressurized.
Brake sign......................................................DISPLAYED
Sunshades......................................................INSTALLED
Tail stand.......................................................AS REQUIRED
Tie downs......................................................AS REQUIRED
Wheel chocks................................................AS REQUIRED
Propeller anchor............................................INSTALLED
External covers.............................................INSTALLED
Cockpit dome light.......................................OFF
110
**_Shutdown Flow_**
Begin the shutdown flows once \_\_\_\_\_\* and PIC has \_\_\_\_\_\_\_\_\_\_\_\_.\*
\*STOPPED, \*CONTROL OVER THE AIRCRAFT
**_ABOVE THE LINE_**
**(PIC)**
PCL................................................IDLE
PARKING BRAKE.......................SET
ICE PROTECTION.......................OFF
**(SIC)**
Call out.........................................."2 minutes, ITT stable"
**(PIC)**
CONDITION LEVER....................CUTOFF
**(SIC)**
EXTERNAL LIGHTS/SIGNS.......OFF [EXEPT NAV]
CABIN...........................................DEPRESSURIZED
FLIGHT PLAN/TIMES.................CLOSED AND NOTED
* Verify items above line and wait at least 1 minute after shutdown before continuing.
- -----------------------------------------------------------------------------------------------------------------------------*
**_BELOW THE LINE_**
**(PIC)**
CAS OIL QTY WARNING............ABSENT [REFILL IF DISPLAYED]
EXT PWR.......................................AS REQUIRED
STBY BUS SWITCH.....................OFF ▶︎ ON
EPS.................................................OFF ▶︎ ARMED
BAT 1+2.........................................OFF ▶︎ ON
111
The PC-12 has a ___ Turbine Engine, meaning that..
Free Turbine, meaning that the compressor and power sections spin in opposite directions
112
Type of Engine & HP
Pratt and Whitney PT6A-67P
1600SHP flat rated to 1200
113
service ceiling
FL300
114
Glide Ratio
16:1
about 2.6NM per 1000'
115
when does the shaker activate?
The pusher?
about 8kt above stall
about 2kt above stall
116
How many fuel pumps and what drives each?
2 Motive flow, 2 Boost pump, and 2 engine driven pumps
117
5.75psi = \_\_\_mbar
400
118
Trim indications
green for ground/takeoff
white in the air
red for takeoff warning
white with green dot in lower right corner for autotrim
white with yellow box in lower corner for invalid autotrim
big X for invalid data
119
What activates Pusher ICE Mode?
What does Pusher ICE Mode do?
Seperator open and Propeller heat on
decreases pusher/shaker actions by 8°
120
When should the Ignition switch be set to ON?
Wind shear, Heavy Precip, turbulence
121
ITT stands for
Sensor is located
Inter-Turbine Temperature
T5 (station 5)
122
5 FAS messages
1. _Stall_
2. _Gear_
- Gear up with ASI below 130, power idle
- Flaps set to 30° or 40° with gear up
- Radar altitude below 200 & torque below 10PSI
3. _Speed_
- Exceedance of any V Speed
4. _No Takeoff_
- Trim out of green, flaps 0°, Ground idle
5. _Cabin_
- Oxygen: Cabin Pressure above 0.7 on the ground
123
recommended torque settings for
500fpm descent
cruise
slowing
150kts
500fpm descent - 10 PSI
cruise - 36.9 PSI
slowing - 30 PSI
150kts - 15 PSI
124
VFR Minimum Altitudes and Visibility
135. 203(a)(1)(2)
135. 205(a)
135.203(a)(1)(2)
Except for takeoffs and landings, Company pilots must not operate aircraft below the following heights:
1. During the day: 500' above the surface; and not less than 500' horizontally from any obstacle
2. At night: 1000' (2000' in designated mountainous terrain) above the highest obstacle within a horizontal distance of 5 miles from the course intended to be flown
135. 205(a)
(a) . Company pilots must not operate VFR in uncontrolled airspace when the ceiling is less than 1000' unless flight visibility is at leat 2 miles
125
VFR Fuel Supply
135.209(a)(1)(2)
Company pilots may not begin a flight under VFR unless, considering wind and forecast weather conditions, it has enough fuel to fly to the first point of intended landing and, assuming normal cruising fuel consumption:
1. During the day, to fly after that for at least 30 minutes; or
2. At night, to fly after that for at least 45 minutes
126
IFR Desination Airport Weather Minimums
135.219
Company pilots may not depart IFR or begin IFR or over the top operation, unless the latest weather reports or forecasts indicate that weather conditions at the estimated time of arrival at the destination airport will be at or above authorized IFR landing minimums
127
IFR Alternate Airport Requirements
135. 223(a)(1)(2)(3)
135. 223(b)(1)(2)(3)
Company pilots may not conduct a flight under IFR unless it carries enough fuel considering weather reports or forecasts, to:
1. Complete the flight to the destination airport; and
2. Fly from that airport to the alternate airport; and
3. Fly after that for 45 minutes at normal cruising speed.
The alternate, referenced above, is not required if there is a published standard instrument approach procedure for the destination airport and, for at least one hour before and after the estimated time of arrival, the appropriate weather reports or forecasts indicate that:
1. The ceiling will be at least 1500' above the minimum circling altitude; or
2. If circling is NA for the airport, the ceiling will be at least 1500' above the lowest published straight in minimum, or 2000' above the airport elevation, whichever is higher; and
3. Visibility for that airport is forecast to be at least 3 miles, or 2 miles more than the lowest applicable visibility minimums, whichever is the greater, for the instrument approach procedure to be used at the destination airport
128
IFR Alternate Airport Weather Minimums
14 CFR 119.43(b)(1)(2)
135.221
OpSpecs C055
14 CFR 119.43(b)(1)(2) - Certificate holder's duty to maintain operations specifications.
(b) Each certificate holder shall insert pertinent excerpts of its operations specifications, or references thereto, in its manual and shall -
(1) Clearly identify each such excerpt as a part of its operations specifications; and
(2) State that compliance with each operations specifications requirement is mandatory.
135. 221 - (a) Aircraft other than rotorcraft. No person may designate an alternate airport unless the weather reports or forecasts, or any combination of them, indicate that the weather conditions will be at or above authorized alternate airport landing minimums for that airport at the estimated time of arrival.
OpSpecs C055
a. The certificate holder is authorized to derive alternate airport weather minimums from table 1 below, according to the limitations and provisions of this operations specification
_For Airports with at least one operational navigational facility providing a straight in nonprecision approach procedure, or CAT I precision approach, or, when applicable, a circling maneuver from an IAP_
Ceiling - Add 400' to MDA(H) or DA(H), as applicable
Visibility - Add 1SM or 1600 m to the landing minimum
_For airports with at least 2 operational navigational facilities, each providing a straight-in approach procedure to different suitable runways_
Ceiling - Add 200' to higher DA(H) or MDA(H) of the two approaches used
Visibility - Add 1/2SM or 800 M to the higher authorized landing minimum of the two approaches used
b. Special Limitations and Provisions
1. The certificate holder must not use an alternate airport weather minimum other than any applicable minimum derived from table 1.
* The company must not designate an alternate airport unless the weather reports or forecasts indicate that the weather conditions will be t or above authoried alternate airport landing minimums for that airport at the estimated time of arrival*
* Alternate airport weather minimums may only be derived from the table in OpSpecs C055*
* Jeppesen Takeoff Minimums“FOR FILING AS AN ALTERNATE”section may include restrictions that limit use of one or more approaches or the airport entirely as an alternate airport under certain times or conditions (e.g., “Authorized Only When Twr Operating”or “Authorized Only When Local Weather Available”). Keep in mind such restrictions are alwaysbinding when using an alternate airport. That said, the alternate weather minimums (if the alternate is authorized) are derived from OpSpec C055.*
129
Unscheduled One and Two Pilot Crews - Flight time limitations
14 CFR 135.267(a-f)1.The Companywill not schedule, and no Company pilot will accept, any flight if that flight time, when added to any other commercial flyingtime, would cause them to exceed:
a. 500 hours in any calendar quarter.
b. 800 hours in any two consecutive calendar quarters.
c. 1,400 hours in any calendar year.
2. During any 24 consecutive hours,the total flight time for the assigned flight,when added to any other commercial flyingtimeby that pilot,may not exceed:
a. 8 hours for a flight crew consisting of one pilot.
b. 10 hours for a flight crew consisting of two pilots qualified under Part 135 for the operation being conducted.
3. A pilot's flight time may exceed the flight time limits of paragraph (2),above,if:
a. The assigned flight time occurs during a regularly assigned duty period of no more than 14 hours; and
b. This duty period is immediately preceded by and followed by a required rest period of at least 10 consecutive hours of rest; and
c. Any flight time is assigned during this period, when added to any other commercial flying time by the pilot,does not exceed:
i. 8 hours for a flight crew consisting of one pilot; or
ii. 10 hours for a flight crew consisting of two pilots;and
iii. The combined duty and rest periods equal 24 hours.
4. Each assignment under paragraph (3) above must provide for at least 10 consecutive hours of rest during the 24-hour period that precedes the planned completion time of the assignment.
5. When at pilot has exceeded the daily flight time limitations listed above, because of circumstances beyond the control of the Company or pilot(such as adverse weather conditions), that pilot must have a rest period before being assigned or accepting an assignment for flight time of at least:
a. 11 consecutive hours of rest if the flight time limitation is exceeded by not more than 30 minutes.
b. 12 consecutive hours of rest if the flight time limitation is exceeded by more than 30 minutes, but not more than 60 minutes.
c. 16 consecutive hours of rest if the flight time limitation is exceeded by more than 60 minutes.
6. Each pilotmust be provided at least 13 rest periods of at least 24 consecutive hours each in each calendar quarter.
7. The Company must not assign a pilot any duty during any required rest period.
130
When PAX oxygen is set to auto, it permits automatic pressurization of the passenger oxygen system when:
* The cabin Pressure Control System (CPCS) senses a cabin altitude above 13500' +/-500'
* In HI FIELD mode, the cabin altitude is sensed above takeoff/landing field elevation +2000' or 14500' +/-500'
131
Trim must be set to the _______ when CG is ___ of \_\_\_
Trim must be set to the diamond when CG is aft of 236
132
Steep turn flow
**Entry**
1. Cruise Checklist.......... Complete
2. Torque......................... As required to maintain ASI and ALT (~15 PSI)
3. Airspeed...................... 150 KIAS +/-10 KIAS
4. Bank Angle................. Roll Smoothly to 45°
5. Altitude....................... Maintain Constant +/-100'
**Exit**
1. Airspeed...................... 150 KIAS +/-10 KIAS
2. Bank Angle................. Roll Smoothly to wings level
3. Altitude....................... Maintain Constant +/-100'
4. Cruise Checklist......... Completed
133
Approach to Stall - Enroute Clean Configuration
Beginning of Maneuver
* Altitude 5000' AGL
* PCL Idle
* AP/YD/FD OFF
* Landing Gear up
* Flaps 0°
Stall and Recovery
At Stick Shaker Activation:
* Reduce AOA
* PCL Set Takeoff Torque
* As DSB Centers Initiate a Climb
* Verify Flaps 0°
* Landing gear retracted
Completion of Maneuver
* Level off at Starting Altitude +/-100'
* Airspeed 150 KIAS +/-10 KIAS
* Maneuver Complete
134
Approach to stall - Takeoff Configuration
Beginning of Maneuver
* Altitude 5000' AGL
* PCL Set 15 PSI
* AP/YD/FD Off
* Landing Gear Up
* Flaps 15°(\<165 KIAS)
* PCL Idle
* Commence Turn 15° Bank
Stall and recovery
At Stick Shaker Activation
* Reduce AOA
* Roll Wings Level
* PCL Set Takeoff Torque
* As DSB Centers Initiate a Climb
* When ASI is Greater Than 100 KIAS, Select Flaps 0°
Completion Of Maneuver
* Level off at Starting Altitude +/-100'
* ASI 150 KIAS +/-10KIAS
* Maneuver Complete
135
Approach To Stall - Landing Configuration
_Beginning of Maneuve_r
* Altitude 5000' AGL
* PCL Set 15 PSI
* AP/YD/FD OFF
* Landing Gear Down Below 180KIAS
* Flaps 40° (Below 130 KIAS)
_Stall and Recovery_
At Stick Shaker Activation
* Reduce AOA
* PCL Set Takeoff Torque
* As DSB Centers Initiate a Climb
* Flaps 15°
* Climbing - Landing Gear Up
* When ASI is Greater Than 100 KIAS, Select Flaps 0°
_Completion Of Maneuver_
* Level off at Starting Altitude +/-100'
* ASI 150 KIAS +/-10 KIAS
* Maneuver Complete
