Limitations Flashcards
Vmo (Maximus Operating Speed): ______
Vmo (Maximus Operating Speed): 188 KIAS
Vo (Maximum Operating Maneuvering Speed): ______
Vo (Maximum Operating Maneuvering Speed): 127 KIAS
Vfe (Maximum Flaps Extended Speed):
10˚: ______
20˚: ______
36˚: ______
Vfe (Maximum Flaps Extended Speed):
10˚: 168 KIAS
20˚: 135 KIAS
36˚: 118 KIAS
Vle (Maximum Landing Gear Extended Speed): ______
Vle (Maximum Landing Gear Extended Speed): 168 KIAS
Vlo (Maximum Landing Gear Operating Speed)
Extension: ______
Retraction: ______
Vlo (Maximum Landing Gear Operating Speed)
Extension: 168 KIAS
Retraction: 129 KIAS
AIRSPEED INDICATOR MARKINGS (Garmin PFD):
RED LINE: _______ SIGNIFICANCE: ______
WHITE ARK: _______ SIGNIFICANCE: ______
GREEN ARK: _______ SIGNIFICANCE: ______
RED LINE: _______ SIGNIFICANCE: ______
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.
AIRSPEED INDICATOR MARKINGS (STBY Airspeed Indicator):
RED LINE: _______ SIGNIFICANCE: ______
WHITE ARK: _______ SIGNIFICANCE: ______
GREEN ARK: _______ SIGNIFICANCE: ______
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
POWER PLANT LIMITATIONS, MAX ITT ˚C: Take Off: \_\_\_\_\_\_\_\_\_ Max Cont.: \_\_\_\_\_\_\_ Min. Idle: \_\_\_\_\_\_\_\_\_ Starting: \_\_\_\_\_\_\_\_\_ Transient: \_\_\_\_\_\_\_\_ Max Reverse: \_\_\_\_\_
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
POWER PLANT LIMITATIONS, OIL PX PSI: Take Off: \_\_\_\_\_\_\_\_\_ Max Cont.: \_\_\_\_\_\_\_ Min. Idle: \_\_\_\_\_\_\_\_\_ Starting: \_\_\_\_\_\_\_\_\_ Transient: \_\_\_\_\_\_\_\_ Max Reverse: \_\_\_\_\_
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
POWER PLANT LIMITATIONS, OIL TEMP ˚C: Take Off: \_\_\_\_\_\_\_\_\_ Max Cont.: \_\_\_\_\_\_\_ Min. Idle: \_\_\_\_\_\_\_\_\_ Starting: \_\_\_\_\_\_\_\_\_ Transient: \_\_\_\_\_\_\_\_ Max Reverse: \_\_\_\_\_
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
Total fuel capacity: ______
Unusable Fuel: ___________
Total fuel capacity: 1160 LBS/ 173 USG
Unusable Fuel: 20 LBS/ 3 USG (At critical Flight attitudes)
Total usable fuel: ______
Each wing: ____________
Total usable fuel May be reduced by _____ if the engine driven fuel boost pump fails
Maximum allowable fuel imbalance: ______
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
Total Oil system capacity: ______
Oil tank capacity: _____________
Total Oil system capacity: 12 USqt
Oil tank capacity: 9,2 USgt
PROPELLER BLADE ANGLES
Low Pitch Stop Min./Max.: ______
Feather Min./Max.: ____________
Reverse Min./Max.: ____________
PROPELLER BLADE ANGLES
Low Pitch Stop Min./Max.: 18,9˚/19,1˚
Feather Min./Max.: 84˚/85˚
Reverse Min./Max.: -9,5˚/-10,5˚
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
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
GENERATOR/ ALTERNATOR LIMITATIONS
Max Continuous Load
Starter/Generator: ______amps
Alternator Ground Operation: ______ amps
Aternator In Flight: ______amps
GENERATOR/ ALTERNATOR LIMITATIONS
Max Continuous Load
Starter/Generator: 170 amps
Alternator Ground Operation: 120 amps
Aternator In Flight: 130 amps
POWER CONTROL LEVER OPERATION
Power Lever Position operation aft of the flight idle detent is not permitted:
1.: ______________
2.: ______________
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.
Takeoff is not approved with _________ annunciator illuminated
Takeoff is not approved with CHIP DETECT annunciator illuminated
POWERPLANT INSTRUMENT MARKINGS Propeller Speed (Np) Red Line: \_\_\_\_\_ Green Arc: \_\_\_\_ Red Line: \_\_\_\_\_
POWERPLANT INSTRUMENT MARKINGS Propeller Speed (Np) Red Line: 2000 Green Arc: 1200-2000 Red Line: 1200
POWERPLANT INSTRUMENT MARKINGS
Engine Speed (Ng)
Red Line: _____ (_____ RPM)
Green Arc: ____
POWERPLANT INSTRUMENT MARKINGS
Engine Speed (Ng)
Red Line: 101,7 (38.100 RPM)
Green Arc: 0-101,7
POWERPLANT INSTRUMENT MARKINGS
Fuel Flow PPH:
Green arc: ______
POWERPLANT INSTRUMENT MARKINGS
Fuel Flow PPH:
Green arc: 0-600
POWERPLANT INSTRUMENT MARKINGS Oil Pressure - PSI Red Line: \_\_\_\_\_ Yellow Arc: \_\_\_\_ Green Arc: \_\_\_\_ Yellow Arc: \_\_\_\_ Red Line: \_\_\_\_\_
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.
POWERPLANT INSTRUMENT MARKINGS Oil Temperature - ˚C Red Line: \_\_\_\_\_ Green Arc: \_\_\_\_ Yellow Arc: \_\_\_\_ Red Line: \_\_\_\_\_
POWERPLANT INSTRUMENT MARKINGS Oil Temperature - ˚C Red Line: 99˚C Green Arc: 0 - 99˚C Yellow Arc: -40 - 0˚C Red Line: -40˚C
POWERPLANT INSTRUMENT MARKINGS ITT - ˚C Red Line: \_\_\_\_\_\_ Yellow Arc: \_\_\_\_\_ Green Arc: \_\_\_\_\_
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.
POWERPLANT INSTRUMENT MARKINGS
Torque - Ft - Lb
Red Line: ____ Ft. Lb.
Green Arc: ____ Ft. Lb.
POWERPLANT INSTRUMENT MARKINGS
Torque - Ft - Lb
Red Line: 1313 Ft. Lb.
Green Arc: 0-1313 Ft. Lb.
WEIGHT LIMITATIONS MRW: \_\_\_\_\_ MTOW: \_\_\_\_\_ MLW: \_\_\_\_\_ MZFW: \_\_\_\_\_ Max. Weight Bag.: \_\_\_\_\_
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)
MANEUVER LIMITS
This is a ______ Category airplane. No ______ ______ including spins approved.
MANEUVER LIMITS
This is a NORMAL Category airplane. No ACROBATIC MANEUVERS including spins approved
FLIGHT LOAD FACTOR LIMITS Positive Load Factor: Flaps Up: \_\_\_\_\_\_ Flaps Down: \_\_\_\_\_\_ Negative Load Factor: \_\_\_\_\_ Note: \_\_\_\_\_\_\_
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
Takeoff and landing operations must be conducted from ______, ______ ______
Takeoff and landing operations must be conducted from PAVED, HARD SURFACES
OAT LIMITS
Starting: ____˚C to ____˚C
In-Flight: ____˚C to ____˚C
OAT LIMITS
Starting: -34˚C to 46˚C
In-Flight: -54˚C to 46˚C
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
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
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
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
GARMIN G1000
Operating single pilot - BARO SYNCH must be ____
Operating two pilot - BARO SYNCH must be ____
GARMIN G1000
Operating single pilot - BARO SYNCH must be ON
Operating two pilot - BARO SYNCH must be OFF
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.
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.
Max. Operating altitude: ______
Max. Operating altitude: 30.000 ft pressure altitude
Minimum oxygen required for flight above 25.000 ft: ____
Minimum oxygen required for flight above 25.000 ft: 800 psi
CABIN PRESSURERIZATION LIMITS
Maximum cabin differential pressure: ____
CABIN PRESSURERIZATION LIMITS
Maximum cabin differential pressure: 5,5 psi
Pressurized landing not approved
VORTEX GENERATORS
If a total of more than _____ vortex generators are damaged or missing, the aircraft is not airworthy
VORTEX GENERATORS
If a total of more than 5 vortex generators are damaged or missing, the aircraft is not airworthy