Falcon limitations Flashcards
1
Q
Baggage compartment limit
A
2866 Ibs (1300 kgs)
Not to exceed 123 IB/Sq ft (600 kg sq m)
2
Q
Max T/O Weight
A
46,500 lbs
3
Q
Max Ramp Weight
A
46,700 lbs
4
Q
Max Landing Weight
A
42,000 lbs
5
Q
MZFW
A
30,870 lbs
6
Q
Average BOW (basic operating weight)
A
26.500 lbs
7
Q
Minimum Operating Weight (or Min Flight Weight)
A
20,700 lbs
8
Q
CG Limit
A
14% MAC Forward - 31% MAC Aft.
MAC (Mean Aerodynamic Chord)
9
Q
Datum
A
25% MAC
10
Q
Max Approved Operating Altitude
A
51,000 ft
11
Q
Min/Max Altitude for T/O and Landing
A
-1,000 ft to 14,000 ft
12
Q
Min/Max Temperature for T/O and Landing
A
-54°C to +50°C
13
Q
Max Altitude for Operating Flaps or Slats
A
20,000 ft
14
Q
Vmo
A
350 KIAS below 10,000ft
370 KIAS at or above 10,000 ft
15
Q
Mmo > 35K
A
ABOVE 35,000 lbs
25,000 ft to 33,000 ft .87 Mach
33,000 ft to 37,000 ft .87 to .84 Mach
above 37,000 ft .84 Mach
16
Q
Mmo < 35K
A
BELOW 35,000 lbs
25,000 ft to 37,000 ft .87 Mach
37,000 ft to 42,000 ft .87 to .84 Mach
above 42,000 ft .84 Mach
17
Q
Va
A
228 KIAS
18
Q
Turbulent Air Penetration Speed
A
280 KIAS / .76 Mach
19
Q
Vlo (landing gear operation)
A
190 KIAS
VLO/MLO is the maximum speed at which it
is safe to extend or retract the landing gear.
20
Q
Mlo (landing gear operation)
A
.70 Mach
VLO/MLO is the maximum speed at which it
is safe to extend or retract the landing gear.
21
Q
Vle (landing gear extended)
A
245 KIAS
22
Q
Mle (landing gear extended)
A
.75 Mach
23
Q
Vwwo (windshield wipers operation)
A
215 KIAS
24
Q
D.V. Window
A
215 KIAS
25
Cracked or Bubbled Windshield Max Speed
7.5 psi max press diff.
| 230 KIAS
26
Vabo (air brakes operation)
No Limitation
27
Vabe (air brakes extended)
No Limitation
28
Vfe Slats+Flaps 7° (SF-1)
| Operating or Extended Speed
200 KIAS
29
Vfe Slats+Flaps 20° (SF-2)
| Operating or Extended Speed
190 KIAS
30
Vfe Slats+Flaps 40° (SF-3)
| Operating or Extended Speed
180 KIAS
31
Vmcg (minimum control on ground)
No Vmcg
32
Vmin (minimum selectable)
90 KIAS
33
Vmca (minimum control in air)
85.5 Kias
34
Demonstrated Crosswind
30 Knots
35
Max Tailwind
-1,000 to 10,000 ft - 10 Knots
above 10,000 ft - 4 Knots
10 Knots with 195kt (225mph) tires
36
Max Runway Slope
+/- 2.5%
37
Max Tire Rotation Speed
195 KIAS (225 mph tires)
38
Vp Hydroplanning Speed
89 KIAS
39
Max Speed for Total Hydraulic Loss
260 KIAS / .76 Mach
40
Wing Root Lights On Ground
15 min followed by 45 min cool down
41
Load Factor CLEAN
+2.53 G to -1G
42
Load Factor FLAPS EXTENDED
+2G to 0G
43
Engines Model:
Tell Flight engineer at 731- to bring 5 black rats and 1 chair
TFE731-5BR-1C
44
Engine Computers Limitation
Must be operative for Takeoff
45
Takeoff Thrust
4750 lbs
46
Max Continuous Thrust
4634 lbs
47
N1/N2 Max limits:
ToF:
Transient:
Takeoff:
100% - 100.8%
Transient (5 sec max):
103% - 103%
48
ITT TRANSIENT (5 SEC):
1006°C
49
ITT START
978°C
50
ITT TAKEOFF (5 MIN):
978°C
51
ITT MAX CONTINUOUS (30 MIN):
968°C
52
ITT RPR OPERATING
(5 MINUTES): 996°C
53
Starting Limitations:
N2 10% to lightoff ground or started assisted
Lightoff to idle:
Windmilling air start:
N2 10% to lightoff ground or started assisted:
10 seconds
Lightoff to idle (60% N2): 60 seconds
Windmilling air start: 45 seconds max
54
Starter Limitations
40 sec on - 3 min off
30 sec on - 3 min off
30 sec on - 30 min off
Double times btw 2 subsequent starts above 30°C
55
Oil Pressure Limitations
IDLE: Min + Max
TOF & MCT: Min + Max
Trasient: Max
Idle: 25-46 psi
T/O + MCT : 38-46 psi
Transient: 55 psi (less than 3 minutes)
56
Oil Temperature Limitations:
Sea level to 30,000 ft:
&
> 30K
Sea level to 30K 127°C
Above 30K > 140°C
57
Oil Temperature Limitations:
Transient abv 30K :
&
Minimum for exceeding idle:
Transient: 149°C (less than 2 minutes)
Minimum for exceeding idle: 30°C
58
Generator Limitations
<43K
>43K
Max Volts:
```
FL430 and below:
300 amp (350 amp 1 min)
```
Above FL430:
260 amp
Max system voltage: 32 volts
59
GTCP 36-150 - APU:
Max N1:
Star T5:
Stab T5:
Max Load:
N1: 110%
Start (less than 10 sec): 870°-985°C
Stabilized: 679° C
Generator: 300 amp (350 amp for 1 min)
60
Pressurization- Max and Normal Differential?
Max press diff: 9.6 psi
Normal press diff: 9.3 psi
61
Fuel
Total Useable:
Left Wing:
Right Wing:
Group 2 :
Min/ Max Refusing press:
Total Usable:
2,845 gl - 19,065 lbs
Left wing + G1:
904 gl - 6,058 lbs
Right wing + G3:
904 gl - 6,058 lbs
Front and Rear G2:
1,034 - 6,949 lbs
Min/Max refuelling press:
30-50 psi
62
Fuel Total Usable:
Total Usable:
| 2,845 gl - 19,065 lbs
63
Fuel Left wing + G1:
Left wing + G1:
| 904 gl - 6,058 lbs
64
Fuel Right wing + G3:
Right wing + G3:
| 904 gl - 6,058 lbs
65
Fuel Front and Rear G2:
Front and Rear G2:
| 1,034 - 6,949 lbs
66
Fuel Min/Max refuelling press:
Min/Max refuelling press:
| 30-50 psi
67
Autopilot Limitations
Radio altimeter operative:
Radio altimeter inoperative:
Decision height:
During FMS approach
(no approach) like Dep:
Min height Radio altimeter operative:
50 ft
Min height Radio altimeter inoperative:
150 ft
Min decision height:
200 ft
Min height during FMS approach:
300 ft
```
Minimum height (no approach):
1,000ft
```
68
Fuel Burn Rule
| constant cruise .78 Mach
First hour:
3,200 lbs
2nd hour:
2,200 lbs
Third hour and beyond:
2,000 lbs
69
Wingspan
63ft 5in
70
Height
24ft 9in without satcom
25ft 2in
71
Length
66ft 4in
72
Autopilot Limitations - Min height wt FMS approach:
300 ft
73
Autopilot Limitations- Min height RA operative:
50 ft
74
Autopilot Limitations- Min height RA inop :
150 ft
75
Autopilot Limitations - Min decision height:
Min decision height:
| 200 ft
76
Autopilot Limitations - Minimum height (no approach):
```
Minimum height (no approach):
1,000ft
```
77
MINIMUM TURNING RADIUS
| WITH NOSEWHEEL STEERING
47 FT. 9 IN.
78
Total usable fuel capacity is
19,065 lbs
| an additional 119 LBS unusable
79
Air Brakes Steady and flashing
Steady: AB not stowed
Flashing: Auto Stowed
80
Configuration Panel Black Arrow (Red)
Disagreement btwn slat/Flap VS Slats Postion
81
Main gear Red Lights
Main gear doors not closed
82
Oil Amber light
Low oil Pressure (<25 PSI)
Chip detected (metal)
83
#2 P BK Steady, Flashing
Steady: Num2 Brk Pressure > 230 PSI
Flashing:
The brake accumulator need to charge
< 1500 PSI PB Accumulator
84
Pitch Feel:
Dis aggrement : Elevator Arthur Position VS Hor Stab
85
TRANS Fire panel
Disagreement:
Btw Eng Fuel Shutoff Valve
VS
Fuel Shutoff Switch
86
Max Spd total hydraulic Loss
260 kts / 0.76 M
87
MZFW
30,870 LB
88
Bleed APU
Disagreement: Btwn APU Bleed Valve OPen Vs Apu bleed Switch
Or
PWL > 54 Degree and APU
Bleed Valve Not Closed
89
What causes T/O Config: "FATS'
Any PWR LVL >82D and:
Flaps <7D or 22D
AB not Stowed
Trim not in green
SLATS (Inboard not ext)
90
CABIN - Audio Warning and with Audio
With Audio : Cabin Altitude > 10K
Without "CABIN" Audio warning:
The main entry door is not locked or
Forward lav service panel not closed
91
Eng 2 Fail
GRD: PWL > 84D
ENG 2 N1< 85%
Grd or Flight: S Duct not closed
92
Windshield Cracked or Bubbles
230 kts
Max 7.5 PSI
93
BAG ISOL
The baggage compartment isolation valve is closed
94
BAG Access
Cabin baggage access door not closed
95
REV UNLOCK
DISagreement btw Thrus REV LVL Stowed Vs Thr Rev Claw locks not locked
96
Fueling
```
Refueling control panel door
refuel connnector door
Vent valve lever not stowed
Vent Valves 2 not closed
Gravity fueling switch on
Defueling switch on
REF/DEF valve open
B2 bus not powered
```
97
Ail Feel
Dis AileronArthur Q Position VS Airspeed (ADC1 or ADC2)
98
MACH TRIM
Mach trim sys not engaged
AP oon 0.80M max
99
AIL ZERO
Emergency aileron actuator not in the neutral position
