Limitations Flashcards

1
Q

Vmo (Maximus Operating Speed): ______

A

Vmo (Maximus Operating Speed): 188 KIAS

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2
Q

Vo (Maximum Operating Maneuvering Speed): ______

A

Vo (Maximum Operating Maneuvering Speed): 127 KIAS

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3
Q

Vfe (Maximum Flaps Extended Speed):
10˚: ______
20˚: ______
36˚: ______

A

Vfe (Maximum Flaps Extended Speed):
10˚: 168 KIAS
20˚: 135 KIAS
36˚: 118 KIAS

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4
Q

Vle (Maximum Landing Gear Extended Speed): ______

A

Vle (Maximum Landing Gear Extended Speed): 168 KIAS

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5
Q

Vlo (Maximum Landing Gear Operating Speed)
Extension: ______
Retraction: ______

A

Vlo (Maximum Landing Gear Operating Speed)
Extension: 168 KIAS
Retraction: 129 KIAS

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6
Q

AIRSPEED INDICATOR MARKINGS (Garmin PFD):
RED LINE: _______ SIGNIFICANCE: ______
WHITE ARK: _______ SIGNIFICANCE: ______
GREEN ARK: _______ SIGNIFICANCE: ______
RED LINE: _______ SIGNIFICANCE: ______

A

AIRSPEED INDICATOR MARKINGS (Garmin PFD):
RED LINE: 188 KIAS SIGNIFICANCE: Vmo
WHITE ARK: 69 to 118 KIAS SIGNIFICANCE: Vfe (full flaps)
GREEN ARK: 79 to 188 KIAS SIGNIFICANCE: Normal Operating Speed
RED LINE: 69 KIAS SIGNIFICANCE: Stalling speed w. Ldg. Gear and flaps Extended @ Max weight.

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7
Q

AIRSPEED INDICATOR MARKINGS (STBY Airspeed Indicator):
RED LINE: _______ SIGNIFICANCE: ______
WHITE ARK: _______ SIGNIFICANCE: ______
GREEN ARK: _______ SIGNIFICANCE: ______

A

AIRSPEED INDICATOR MARKINGS (STBY Airspeed Indicator):
RED LINE: 188 KIAS SIGNIFICANCE: Vmo
WHITE ARK: 69 to 118 KIAS SIGNIFICANCE: Vfe w. Full flaps extended
GREEN ARK: 79 to 188 KIAS SIGNIFICANCE: Normal Operating Speed

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8
Q
POWER PLANT LIMITATIONS, MAX ITT ˚C:
Take Off: \_\_\_\_\_\_\_\_\_
Max Cont.: \_\_\_\_\_\_\_
Min. Idle: \_\_\_\_\_\_\_\_\_
Starting: \_\_\_\_\_\_\_\_\_
Transient: \_\_\_\_\_\_\_\_
Max Reverse: \_\_\_\_\_
A
POWER PLANT LIMITATIONS, MAX ITT ˚C:
Take Off: 800˚C
Max Cont.: 770˚C
Min. Idle: 750˚C (21.000-23.000 RPM)
Starting: 1000˚C (Limited to 5 Sec.)
Transient: 850˚C/ 880˚C (Limited to 20 Sec./ 4 Sec.)
Max Reverse: 770˚C
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9
Q
POWER PLANT LIMITATIONS, OIL PX PSI:
Take Off: \_\_\_\_\_\_\_\_\_
Max Cont.: \_\_\_\_\_\_\_
Min. Idle: \_\_\_\_\_\_\_\_\_
Starting: \_\_\_\_\_\_\_\_\_
Transient: \_\_\_\_\_\_\_\_
Max Reverse: \_\_\_\_\_
A
POWER PLANT LIMITATIONS, OIL PX PSI:
Take Off: 100-135 PSI
Max Cont.: 100-135 PSI
Min. Idle: 60 Min.
Starting: 0-200 PSI (Start blw. -17,7˚C, Oil px May reach 200 PSI)
Transient: 40-200 PSI
Max Reverse: 100-135 PSI
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10
Q
POWER PLANT LIMITATIONS, OIL TEMP ˚C:
Take Off: \_\_\_\_\_\_\_\_\_
Max Cont.: \_\_\_\_\_\_\_
Min. Idle: \_\_\_\_\_\_\_\_\_
Starting: \_\_\_\_\_\_\_\_\_
Transient: \_\_\_\_\_\_\_\_
Max Reverse: \_\_\_\_\_
A
POWER PLANT LIMITATIONS, OIL TEMP ˚C:
Take Off: 0-99˚C
Max Cont.: 0-99˚C
Min. Idle: -40˚C
Starting: -40˚C min (Limited by Oil Temp)
Transient: 99-104˚C (Limited to 10 Min.)
Max Reverse: 0-99˚C
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11
Q

Total fuel capacity: ______

Unusable Fuel: ___________

A

Total fuel capacity: 1160 LBS/ 173 USG

Unusable Fuel: 20 LBS/ 3 USG (At critical Flight attitudes)

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12
Q

Total usable fuel: ______
Each wing: ____________
Total usable fuel May be reduced by _____ if the engine driven fuel boost pump fails
Maximum allowable fuel imbalance: ______

A

Total usable fuel: 1140 LBS/ 170 USG
Each wing: 570 LBS/ 85 USG
Total usable fuel May be reduced by 13 LBS/ 2 USG if the engine driven fuel boost pump fails
Maximum allowable fuel imbalance: 125 LBS

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13
Q

Total Oil system capacity: ______

Oil tank capacity: _____________

A

Total Oil system capacity: 12 USqt

Oil tank capacity: 9,2 USgt

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14
Q

PROPELLER BLADE ANGLES
Low Pitch Stop Min./Max.: ______
Feather Min./Max.: ____________
Reverse Min./Max.: ____________

A

PROPELLER BLADE ANGLES
Low Pitch Stop Min./Max.: 18,9˚/19,1˚
Feather Min./Max.: 84˚/85˚
Reverse Min./Max.: -9,5˚/-10,5˚

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15
Q

STARTER LIMITATIONS
Use of the starter is limited to ___sec ON, ___min. OFF, ___sec ON, ___min. OFF, ___sec ON, ___min. OFF before a fourth start may be attempted

A

STARTER LIMITATIONS
Use of the starter is limited to 30 sec ON, 1 min. OFF, 30 sec ON, 1 min. OFF, 30 sec ON, 30 min. OFF before a fourth start may be attempted

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16
Q

GENERATOR/ ALTERNATOR LIMITATIONS
Max Continuous Load

Starter/Generator: ______amps
Alternator Ground Operation: ______ amps
Aternator In Flight: ______amps

A

GENERATOR/ ALTERNATOR LIMITATIONS
Max Continuous Load

Starter/Generator: 170 amps
Alternator Ground Operation: 120 amps
Aternator In Flight: 130 amps

17
Q

POWER CONTROL LEVER OPERATION
Power Lever Position operation aft of the flight idle detent is not permitted:
1.: ______________
2.: ______________

A

POWER CONTROL LEVER OPERATION
Power Lever Position operation aft of the flight idle detent is not permitted:
1.: When the engine is shut down
2.: During flight

WARNING:
Positioning the power lever aft of the flight idle stop in flight is prohibited. Such positioning May cause loss of airplane control or may result in an engine overspeed condition and consequent loss of engine power.

18
Q

Takeoff is not approved with _________ annunciator illuminated

A

Takeoff is not approved with CHIP DETECT annunciator illuminated

19
Q
POWERPLANT INSTRUMENT MARKINGS
Propeller Speed (Np)
Red Line: \_\_\_\_\_
Green Arc: \_\_\_\_
Red Line: \_\_\_\_\_
A
POWERPLANT INSTRUMENT MARKINGS
Propeller Speed (Np)
Red Line: 2000
Green Arc: 1200-2000
Red Line: 1200
20
Q

POWERPLANT INSTRUMENT MARKINGS
Engine Speed (Ng)
Red Line: _____ (_____ RPM)
Green Arc: ____

A

POWERPLANT INSTRUMENT MARKINGS
Engine Speed (Ng)
Red Line: 101,7 (38.100 RPM)
Green Arc: 0-101,7

21
Q

POWERPLANT INSTRUMENT MARKINGS
Fuel Flow PPH:
Green arc: ______

A

POWERPLANT INSTRUMENT MARKINGS
Fuel Flow PPH:
Green arc: 0-600

22
Q
POWERPLANT INSTRUMENT MARKINGS
Oil Pressure - PSI
Red Line: \_\_\_\_\_
Yellow Arc: \_\_\_\_
Green Arc: \_\_\_\_
Yellow Arc: \_\_\_\_
Red Line: \_\_\_\_\_
A
POWERPLANT INSTRUMENT MARKINGS
Oil Pressure - PSI
Red Line: 200
Yellow Arc: 135-200
Green Arc: 100-135
Yellow Arc: 60(85*)-100
Red Line: 60(85*)
*When torque is above 1100 ft.lb.
23
Q
POWERPLANT INSTRUMENT MARKINGS
Oil Temperature - ˚C
Red Line: \_\_\_\_\_
Green Arc: \_\_\_\_
Yellow Arc: \_\_\_\_
Red Line: \_\_\_\_\_
A
POWERPLANT INSTRUMENT MARKINGS
Oil Temperature - ˚C
Red Line: 99˚C
Green Arc: 0 - 99˚C
Yellow Arc: -40 - 0˚C
Red Line: -40˚C
24
Q
POWERPLANT INSTRUMENT MARKINGS
ITT - ˚C
Red Line: \_\_\_\_\_\_
Yellow Arc: \_\_\_\_\_ 
Green Arc: \_\_\_\_\_
A
POWERPLANT INSTRUMENT MARKINGS
ITT - ˚C
Red Line: 800˚C (1000˚C*)
Yellow Arc: 770 - 800˚C 
Green Arc: 0-770˚C
*ITT red line while the engine is OFF and during engine START is 1000˚C. Red line changes to 800˚C after engine START.
25
Q

POWERPLANT INSTRUMENT MARKINGS
Torque - Ft - Lb
Red Line: ____ Ft. Lb.
Green Arc: ____ Ft. Lb.

A

POWERPLANT INSTRUMENT MARKINGS
Torque - Ft - Lb
Red Line: 1313 Ft. Lb.
Green Arc: 0-1313 Ft. Lb.

26
Q
WEIGHT LIMITATIONS
MRW: \_\_\_\_\_
MTOW: \_\_\_\_\_
MLW: \_\_\_\_\_
MZFW: \_\_\_\_\_ 
Max. Weight Bag.: \_\_\_\_\_
A
WEIGHT LIMITATIONS
MRW:  5134 LBS (2328,7 Kg)
MTOW: 5092 LBS (2309,7 Kg)
MLW:  4850 LBS (2199,9 Kg)
MZFW: 4850 LBS (2199,9 Kg)
Max. Weight Bag.: 100 LBS (45,3 Kg)
27
Q

MANEUVER LIMITS

This is a ______ Category airplane. No ______ ______ including spins approved.

A

MANEUVER LIMITS

This is a NORMAL Category airplane. No ACROBATIC MANEUVERS including spins approved

28
Q
FLIGHT LOAD FACTOR LIMITS
Positive Load Factor:
Flaps Up: \_\_\_\_\_\_
Flaps Down: \_\_\_\_\_\_
Negative Load Factor: \_\_\_\_\_
Note: \_\_\_\_\_\_\_
A
FLIGHT LOAD FACTOR LIMITS
Positive Load Factor:
Flaps Up: 3,7 g
Flaps Down: 2 g
Negative Load Factor: -1,48 g
Note: NO INVERTED MANEUVERS APPROVED
29
Q

Takeoff and landing operations must be conducted from ______, ______ ______

A

Takeoff and landing operations must be conducted from PAVED, HARD SURFACES

30
Q

OAT LIMITS
Starting: ____˚C to ____˚C
In-Flight: ____˚C to ____˚C

A

OAT LIMITS
Starting: -34˚C to 46˚C
In-Flight: -54˚C to 46˚C

31
Q

FUEL TEMPERATURE LIMITS
Jet A
Starting: ____ ˚C to ____˚C
In-Flight: ____ ˚C to ____ ˚C

Jet A-1
Starting: ____ ˚C to ____ ˚C
In-Flight: ____ ˚C to ____ ˚C

A

FUEL TEMPERATURE LIMITS
Jet A
Starting: -34˚C to 50˚C
In-Flight: -34˚C to 50˚C

Jet A-1
Starting: -34˚C to 50˚C
In-Flight: -41˚C to 50˚C

32
Q

GARMIN Auto Pilot Limitations:
Minimum approved Operating speed: ____
Maximum approved Operating speed: ____
Minimum airspeed for autopilot coupled approaches: ____
Category __ Precision instrument approaches and ______ approaches only

A

GARMIN Auto Pilot Limitations:
Minimum approved Operating speed: 90 KIAS
Maximum approved Operating speed: 170 KIAS
Minimum airspeed for autopilot coupled approaches: 100 KIAS
Category 1 Precision instrument approaches and NON-PRECISION approaches only

33
Q

GARMIN G1000
Operating single pilot - BARO SYNCH must be ____
Operating two pilot - BARO SYNCH must be ____

A

GARMIN G1000
Operating single pilot - BARO SYNCH must be ON
Operating two pilot - BARO SYNCH must be OFF

34
Q

RADAR LIMITATIONS

  • Do NOT Operate the radar When trucks or containers accommodating flammable or explosives Arne within ____ ft.
  • Do NOT allow personnel within ____ ft. Of area Bering scanned whe. System is TX.
  • Radar images approximately ____NM should not be relief upon.
A

RADAR LIMITATIONS

  • Do NOT Operate the radar When trucks or containers accommodating flammable or explosives Arne within 15 ft.
  • Do NOT allow personnel within 15 ft. Of area Bering scanned whe. System is TX.
  • Radar images approximately 130 NM should not be relief upon.
35
Q

Max. Operating altitude: ______

A

Max. Operating altitude: 30.000 ft pressure altitude

36
Q

Minimum oxygen required for flight above 25.000 ft: ____

A

Minimum oxygen required for flight above 25.000 ft: 800 psi

37
Q

CABIN PRESSURERIZATION LIMITS

Maximum cabin differential pressure: ____

A

CABIN PRESSURERIZATION LIMITS
Maximum cabin differential pressure: 5,5 psi

Pressurized landing not approved

38
Q

VORTEX GENERATORS

If a total of more than _____ vortex generators are damaged or missing, the aircraft is not airworthy

A

VORTEX GENERATORS

If a total of more than 5 vortex generators are damaged or missing, the aircraft is not airworthy