Limitations Flashcards
(104 cards)
1
Q
Maximum Design Ramp Weight
A
17,030
2
Q
Maximum Design Takeoff Weight
A
16,830 lbs
3
Q
Maximum Design Landing Weight
A
15,200 lbs
4
Q
Maximum Design Zero Fuel Weight
A
12,600 lbs
5
Q
Takeoff Weight is limited by the most restrictive of what requirements?
A
- Max Certified Takeoff Weight - 16,830 lbs.
- Max takeoff Weight permitted by climb requirements.
- Landing distance.
6
Q
Landing Weight is limited by the most restrictive of what requirements?
A
- Max certified landing Weight - 15,200 lbs.
- Max landing Weight permitted by climb requirements or brake energy.
- Landing distance.
7
Q
Maximum Nose Baggage Compartment Weight?
A
310 lbs.
8
Q
Maximum tail baggage compartment Weight?
A
Forward: 300
Aft: 200
9
Q
What is normal oil pressure at N2 speeds above 60%?
A
45 to 140 psi
10
Q
Oil pressure below what psi is undesirable, and should be tolerated only for the completion of the flight, preferably at a reduced power setting?
A
45 psi.
11
Q
Oil pressure may be in what range for up to 400 seconds?
A
> 140 PSI, but <= 270 PSI
12
Q
When may takeoff ratings, which are nominally limited to 5 minutes be used for up to 10 minutes without adverse effects on engine airworthiness?
A
One engine inoperative operations
13
Q
Max Observed ITT - Takeoff
A
700 C
14
Q
Max Observed ITT - Max Continuous
A
700 C
15
Q
Max Observed ITT - Starting / Transient
A
740 C
16
Q
Max N2% - Takeoff
A
100
17
Q
Max N2% - Maximum Continuous
A
100
18
Q
Max N2% - Ground Idle
A
49.1
19
Q
Max N2% - Flight Idle
A
52.9
20
Q
Max N2% - Transient
A
102
21
Q
Max N1% - Takeoff
A
100
22
Q
Max N1% - Maximum Continuous
A
100
23
Q
Max N1% - Transient
A
102
24
Q
Starter Limitations
A
- 3 engine starts per 30 minutes
- 3 cycles of operation with a 90 second rest period between cycles is permitted
25
Battery Limitations
3 engine starts per hour
26
What conditions may damage the starter when using external power?
- Voltage in excess of 28 VDC or
| - Current in excess of 1000 amps
27
Minimum amps for start
800 amps
28
Pitot Static Ground Operation Limits
2 minutes ON with 2 minutes OFF between cycles to preclude system damage
29
Electrical Load Limit - Ground Operations
- 125 amps per generator @ ground idle
| - 225 amps per generator @ high idle
30
Electrical Load Limit - Transient
Up to 300 amps are permissible for 4 minutes
31
Single Point Refueling Pressure Range Limit
10 psi to 50 psi
32
Single Point Defueling Pressure Range Limit
-10 psi max
33
Maximum Asymmetrical Fuel Differential for Normal Operations
200 pounds
34
Flight characteristics requirements were not demonstrated with unbalance fuel above how many pounds?
200 pounds
35
How many pounds was a lateral fuel imbalance demonstrated for emergency return?
600 pounds
36
MMO (Above 28,907 feet)
.755 mach (indicated)
37
VMO (Between 8,000 and 28,907 feet)
292 KIAS
38
VMO (Below 8,000 feet)
262 KIAS
39
Maximum Flaps Extended Speed (VFE):
| Full Flaps - LAND Position (35 degrees)
173
40
Maximum Flaps Extended Speed (VFE):
Partial Flaps - T.O. (7 degrees) and
T.O. & APPR Position (15 degrees)
200
41
Maximum Landing Gear Extended Speed (VLE)
250
42
Maximum Landing Gear Operating Speed (VLO)
| Extending
250
43
Maximum Landing Gear Operating Speed (VLO)
| Retracting
200
44
Maximum Speed Brake Operation Speed (VSB)
No Limit
45
Maximum Airspeed for Autopilot Operation
292 KIAS or .755 MACH
46
Minimum Speed Sustained Flight in Icing Conditions (Except Takeoff, Approach and Landing)
160 KIAS
47
Takeoff and Landing Limitations:
| Maximum Altitude
14,000 feet
48
Takeoff and Landing Limitations:
| Maximum Tailwind Component
10 knots
49
Takeoff and Landing Limitations:
| Minimum Ambient Temperature
-54 C
50
Takeoff and Landing Limitations:
| Maximum Water/Slush on Runway
0.5 inches
51
Takeoff and Landing Limitations:
| Maximum Tire Ground Speed
165 KIAS
52
Takeoff and Landing Limitations:
| At what setting must the autopilot and yaw damper be for takeoff and landing?
OFF
53
Takeoff and Landing Limitations:
| At what setting must the ENGINE SYNC knob be for takeoff and landing?
OFF
54
Takeoff and Landing Limitations:
| When must the Vertical Navigation System be turned off during takeoff and landing?
Below 500 ft. AGL
55
Takeoff and Landing Limitations:
| Takeoff with antiskid inoperative is....
Prohibited
56
Takeoff and Landing Limitations:
| What must be in contact with the ground prior to extending/deploying the thrust reversers?
The nose wheel
57
Which critical areas (with frost adhered to) prohibit takeoff?
- Wing leading edge
- Upper wing surface
- Windshield
58
Which critical areas (with ice, snow, or slush adhered to) prohibit takeoff?
- Wing leading edge and upper wing surface
- Flight control surfaces including all hinge gaps
- Horizontal stabilizer
- Vertical stabilizer
- Engine inlets
- Top of engine pylons
- Top of fuselage
- Windshield
- All static ports
- Angle of Attack Vanes
- Upper surface of nose forward of windshield
59
A ____ and ____ check of the wing leading edge and wing upper surface must be performed to make sure the wing is free from ___________ when outside air temperature is less than _______ or if it cannot be determined that the wing fuel temperature is above ______ and any of the following exist: (4 items)
A visual and tactile check...
...free from frost, ice, snow, or slush...
...temperature is less than 10 C / 50 F...
...temperature is above 0 C / 32 F...
...the following exist:
a. There is visible moisture present (rain, drizzle, sleet, snow, fog, etc.,
b. Water is present on the upper wing surface,
c. The difference between the dew point and OAT is 3C (5F) or less, or
d. The atmospheric conditions have been conducive to frost formation.
60
What should the anti-ice switches be selected to when operating in visible moisture, and the indicated RAT is +10C (50F) or below?
Wing / Engine - ON
61
When should Tail de-ice be turned on?
When in visible moisture, and the indicated RAT is between +10C and -35C(-31F) / -40C(-40F) as applicable.
62
How long is the ground operation of pitot-static heat limited to preclude damage to the pitot tubes and angle of attack vanes?
2 minutes
63
Can anti-ice systems be used to deice surfaces prior to takeoff?
No. They must not be used for that purpose.
64
Minimum airspeed for sustained flight in icing (except takeoff, approach, and landing)
160 KIAS
65
In icing conditions, operating the airplane at other than flaps at 0 for an extended period of time (except takeoff, approach, and landing) is what?
Prohibited.
66
Severe icing may result from environmental conditions outside of those for which the airplane is what?
For which the airplane is certified.
67
Flight in _________ or _________ (super cooled liquid water and ice crystals) may result in ice build-up on ________ surfaces exceeding the capability of the _________ or may result in forming _____ of protected surfaces.
Flight in freezing rain, freezing drizzle, or mixed icing conditions...
...build-up on protected surfaces...
...capability of the ice protection system...
...forming aft of the protected surfaces.
68
Runback ice extending approximately ______ aft of the heated __________ on the _______of the wing is _______ in some icing conditions, has been evaluated to ensure ________ performance and controllability, and is not an indication of _______.
```
...approximately 12 to 18 inches aft...
...heated leading edge on the upper surface...
...is normal in some icing...
...to ensure satisfactory performance...
...not an indication of severe icing.
```
69
During flight, severe icing conditions that exceed those for which the airplane is certified shall be determined by the following conditions:
1. Unusually extensive ice accumulation on the _____ and _____ in areas not normally observed.
2. Accumulation of ice on the upper surface of the wing aft of the _____ area extending more than ____ aft of the heated leading edge.
1. ...accumulation on the airframe and windshield...
| 2. ...aft of the protected area...more than 12-18 inches aft...
70
Maximum Operating Altitude
45,000 Feet.
71
Maximum Generator Load (Above idle)
300 Amps in Flight
72
Maximum Generator Load (Idle)
225 Amps in Flight
73
Load Limits (In Flight) - Flaps UP Position (0)
-1.44 to +3.6G @ 16,630 lbs.
74
Load Limits (In Flight) - Flaps T.O., T.O. & APPR, and Land Position (7 to 35 degrees).
0.00 to +2.0 @ 16,630 lbs.
75
Load Limits (Landing) - Flaps LAND Position (35 degrees)
+3.46G @ 15,200 lbs.
76
Load Factor. This acceleration limits the airplane to a maximum landing sink rate of ______.
600 FPM
77
Normal Cabin Pressurization Limitations
0.0 to 9.0 PSID.
78
Airplane must be ___________ before takeoff and landing.
depressurized
79
The angle-of-attack system may be used as a reference system, but ______ replace the airspeed display in the PFD as a ___________.
..., but does not replace...
| ...the PFD as a primary instrument.
80
The angle-of-attack system can be used as a reference for ______ (1.3 VS1) at all airplane weights and center-of-gravity locations at _________ flap positions. 1.3VS1 is indicated by approximately ____ on the AOA gage and by the ___________ on the pilots and copilot's airspeed indicators.
...reference for approach speed (1.3 VS1)...
...locations at zero, T.O. Approach and landing flap...
...approximately 0.6 on the AOA gage...
...and by the top of the white tape on the pilots...
81
The angle-of-attack and stall warning system must be _____________ must be performed.
...must be operable and a satisfactory preflight test must be performed.
82
________ must remain in his seat with the seat belt fastened during all autopilot operations.
One pilot must...
83
Autopilot operation is ___________ if any comparison monitor annunciator illuminates in flight.
...operation is prohibited if...
84
Minimum Autopilot Use Height (En route)
1000 AGL
85
Minimum Autopilot Use Height (Non-precision Approaches)
300 FT
86
Minimum Autopilot Use Height (ILS Approach (CAT I))
180 FT
87
Honeywell Primus-1000 Flight Guidance System:
| EFIS ground operation with the pilot's NOSE AVN FAN annunciator illuminated is limited to how long?
3 minutes.
88
Honeywell Primus-1000 Flight Guidance System:
| What mode must the pilot's and copilot's PFD's be installed and operational in for takeoff?
Normal (Non-Reversionary)
89
Honeywell Primus-1000 Flight Guidance System:
The P-1000 system must be verified to be _________ by a satisfactory preflight test as contained in the NORMAL procedures.
...operational...
90
Honeywell Primus-1000 Flight Guidance System:
| Dual PFD SG _____ to the MFD is ______.
...SG reversion to the MFD is prohibited.
91
Crew and passenger oxygen masks are not approved for use above _______ feet cabin altitude.
40,000
92
Prolonged operation of passenger masks above ______ feet cabin altitudes is not recommended.
25,000
93
Passenger masks are ______ for use in an ________descent to an altitude not requiring _______.
...masks are intended for use...
...in an emergency descent...
...not requiring supplemental oxygen....
94
The pressure demand crew oxygen mask must be ___________ in their containers to qualify as a quick-donning oxygen mask.
...must be properly stowed...
95
Cabin temperatures must be held at or above ______ for a minimum of ______ minutes prior to flight above ________ after a prolonged ground cold soak period of _________ at ambient temperatures of _______ or colder. This temperature ensures ___________ and operation of the _________ oxygen masks.
```
...at or above 0 degrees...
...for a minimum of 15 minutes...
...above FL250...
...period of 2 hours or longer...
...ambient temperatures of -10 C (+14F)...
...ensures proper deployment...
...of the passenger oxygen masks.
```
96
Reverse thrust power must be reduced to the __________ detent position at ______ on landing roll.
...to the idle reverse detent...
| ...at 60 KIAS on landing roll...
97
Maximum allowable thrust reverser deployed time is ____ minutes in any ____ minute period.
...time is 3 minutes in any 10 minute period.
98
Use of thrust reversers is _______ during touch and go landings.
prohibited
99
The thrust reversers must be checked ________ and the first flight after any _________ has been performed on the aircraft.
...checked on the 1st flight of the day...
| ...after any maintenance action has been...
100
The use of thrust reversers to _________ is prohibited.
...to back the plane...
101
Trim: The _______ system preflight must be accomplished in accordance with Section III, Normal Procedures prior _________.
The elevator trim system...
| ...prior to takeoff.
102
The GND IDLE switch must be in _____ position when conducting ________.
...in High position...
| ...when conducting touch & go landings.
103
Standby Flight Instruments:
| A satisfactory ______ must be accomplished on the standby gyro system.
preflight
104
Standby Flight Instruments:
| The standby flight display and standby HSI ________ prior to takeoff.
...HSI must be functioning prior to...
