GoJet Limitation Flashcards

1
Q

MIN FLIGHT CREW

A

PILOT & CO-PILOT

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2
Q

A/C APPROVED OPERATIONS

A

VFR, IFR, ICING

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3
Q

FMS IS APPROVED FOR

A

ENROUTE, TERMINAL, & NP APPROACH

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4
Q

MAX TAXI/RAMP WEIGHT

A

75,250 LBS

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5
Q

MAX TAKEOFF WEIGHT

A

75,000 LBS

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6
Q

MAX LANDING WEIGHT

A

67,000 LBS

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7
Q

MAX ZERO FUEL WEIGHT

A

62,300 LBS

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8
Q

MIN FLIGHT WEIGHT

A

42,000 LBS

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9
Q

MIN OPERATING EMPTY WEIGHT

A

39,835 LBS

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10
Q

MAX PRESSURE ALT FOR T/O & LDG

A

8,000 FEET

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11
Q

MAX OPERATING ALTITUDE

A

41,000 FEET

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12
Q

MAX AMBIENT AIR TEMP FOR T/O & LDG

A

ISA +35C

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13
Q

MIN AMBIENT AIR TEMP FOR T/O

A

-40C

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14
Q

MAX RUNWAY SLOPES

A

+2 (UPHILL), -2 (DOWNHILL)

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15
Q

MAX TAILWIND COMPONENT

A

10 KNOTS

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16
Q

MAX MACH # IN RVSM AIRSPACE

A

0.83 MACH

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17
Q

FLIGHT SPOILERS IN FLIGHT < 300 FT

A

PROHIBITED

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18
Q

ENROUTE USE OF SLATS/FLAPS

A

PROHIBITED

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19
Q

EXTENDED SLATS/FLAPS >15,000 FT

A

PROHIBITED

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20
Q

VFE 1°

A

230 KIAS

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21
Q

VFE 8°

A

230 KIAS

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22
Q

VFE 20°

A

230 KIAS

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23
Q

VFE 30°

A

185 KIAS

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24
Q

VFE 45°

A

170 KIAS

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25
VLE
220 KIAS
26
VLO FOR RETRACTION
200 KIAS
27
VLO FOR EXTENTION
220 KIAS
28
MAX TIRE SPEED
182 KNOTS (210 MPH)
29
MAX SPEED FOR ADG OPERATION
VMO/MMO
30
MAX AIRSPEED WINDSHIELD WIPERS
250 KIAS
31
TURBULENCE PENETRATION SPEED
280 KIAS OR .75 MACH (WHICHEVER IS LOWER)
32
THRUST REVERSER USE IN FLIGHT
PROHIBITED
33
THRUST REVERSER DEPLOYED
GO-AROUNDS PROHIBITED
34
THRUST REVERSER EICAS MSG
TAKEOFF PROHIBITED
35
THRUST REVERSER POWERBACKS
PROHIBITED
36
THRUST REVERSER MAX % N1 >75 KTS
MAX N1
37
THRUST REVERSER MAX % N1 <75 KTS
60%
38
LOAD FACTOR LIMITS FLAPS UP
+2.5G / -1G
39
LOAD FACTOR LIMITS FLAPS DOWN
+2G / 0G
40
MAX DIFFERENTIAL PRESSURE
8.7 PSI
41
MAX DIFFERENTIAL NEG. PRESSURE
-0.5 PSI
42
DURRING TAXI, T/O, AND LDG DIFERENTIAL MUST NOT EXCEED
0.1 PSI
43
MAX ALTITUDE FOR SINGLE PACK
31,000 FEET
44
INFLIGHT ICING CONDITIONS
 10 C VISABLE MOISTURE
45
WING ANIT-ICE ON
WHEN ICE IS ANNUNCIATED OR IN ICING CONDITIONS < 230 KIAS
46
Do you Hold or extend Flap or Slats in Icing Condition
DO NOT HOLD IN ICING CONDITION WITH FLAPS/SLATS EXTENDED
47
AIRCRAFT ENGNINES
GE CF34-8C5B1 [CF34-8C1]
48
N1 RED LIMIT
99.5%
49
N2 RED LIMIT
99.4%
50
ITT RED LIMIT
VARIABLE
51
OIL TEMP RED LIMIT
164C
52
OIL PRESS RED LIMIT
0 to 24 PSI
53
OIL TEMP AMBER
156 to 163C
54
OIL PRESS AMBER
VARIABLE
55
N1 GREEN LIMIT
0 to 99.4%
56
N2 GREEN LIMIT
0 to 99.3%
57
ITT GREEN
VARIABLE
58
OIL TEMP GREEN LIMIT
-40 to 155C
59
OIL PRESS GREEN LIMIT
VARIABLE
60
MAX ELEC LOAD MAIN GEN
40kVA
61
MAX ELEC LOAD EACH TRU
120 AMPS
62
MAX TIME FOR DC POWER USE (GROUND)
5 MINUTES
63
CIRCUIT BREAKER RESET
LIMITED: PIC FOR SAFETY OR AFM ONLY
64
ENGINE GRD START ATTEMPT 1 - 2
90 SEC ON, 10 SEC COOL DOWN
65
ENGINE GRD START ATTEMPT 3 - 5
90 SEC ON, 5 MIN COOL DOWN
66
ENGINE FLT START OR MOTOR 1
120 SEC ON, 10 SEC COOL DOWN
67
ENGINE FLT START OR MOTOR 2 - 5
60 SEC ON, 5 MIN COOL DOWN
68
ENGINE GRD MOTORING 1
90 SEC ON, 5 MIN COOL DOWN
69
ENGINE GRD MOTORING 2 - 5
30 SEC ON, 5 MIN COOL DOWN
70
DO NOT USE ENGINE STARTER
> 45% N2
71
THRUST LEVER SHUT OFF TO IDLE (GRD)
ITT  120C
72
THRUST LEVER SHUT OFF TO IDLE (AIR)
ITT  90C
73
AUXILARY POWER UNIT
ALLIED SIGNAL RE220(RJ)
74
MIN TEMP FOR START (GROUND)
-40C
75
MAX APU EGT (START)
692C TO 1038C (DEPENDANT ON TEMP AND ALT)
76
MAX APU EGT
1038 C
77
MAX APU RPM
106%
78
MAX APU START CYCLES
3 STARTS/ATEMPTS IN 1 HOUR
79
APU STARTER COOLDOWN
2 MINUTES BETWEEN ATTEMPTS
80
MAX ALT APU BLEED
25,000 FEET
81
MAX ALT APU GROUND START
15,000 FEET
82
MAX ALT APU AIR START
37,000 FEET
83
MAX ALT APU GEN LOADING
41,000 FEET
84
MAX LOAD ON APU GEN
40 kVA
85
APU EGT RED LIMIT
807C
86
APU RPM RED LIMIT
107%
87
APU EGT GREEN LIMIT
0 to 806C
88
APU RPM GREEN LIMIT
0 to 106%
89
MAX WING FUEL IMBALANCE
800 LBS
90
MAX WING FUEL IMBALANCE T/O
300 LBS
91
FUEL WEIGHT
6.75 LBS / GAL (2.2046 LBS / KG)
92
FUEL QTY WING PRESSURE REFUEL
7,492 LBS / WING
93
FUEL QTY WING GRAVITY REFUEL
7,290 LBS / WING
94
FUEL QTY CENTER TANK
4,610 LBS
95
MAX FUEL QTY PRESSURE
19,594 LBS
96
MAX FUEL QTY GRAVITY
14,580 LBS
97
MIN FUEL GO AROUND
600 LBS / WING (MAX 10 NOSE UP)
98
MIN ENGINE FUEL TEMP FOR T/O
5C
99
FUEL GRADES & MIXING
ALLOWED SEE AFM & GOM
100
FUEL ADDITIVES
ALLOWED SEE AFM
101
FUEL CROSSFLOW (POWERED/GRAVITY)
OFF FOR TAKE-OFF
102
JET A
MIN TEMP T/O -30C FREEZING POINT -40C
103
JET A1
MIN TEMP T/O -37C FREEZING POINT -47C
104
JP-5
MIN TEMP T/O -36C FREEZING POINT -46C
105
JP-8
MIN TEMP T/O -37C FREEZING POINT -47C
106
NO.3 JET
MIN TEMP T/O -37C FREEZING POINT -47C
107
CIS-RT
MIN TEMP T/O -40C FREEZING POINT -40C
108
MAX OIL CONSUMPTION (PER ENGINE)
189 CC/HR (6.4 OZ/HR = .05 GAL/HR)
109
MIXING OF DIFFERENT OIL GRADES
PROHIBITED
110
APPROVED ENGINE OIL
TYPE I, TYPE II, CASTROL 4000
111
MAX ENGINE OIL SERVICE
36 HRS*
112
How aften the engine oil must be checked?
It need to checked between 3 min & 2Hrs aften every engine Shutdown
113
IF OIL REPLENISH SYSTEM USED
ENGINES REPLENISHED 15 MIN - 2 HRS
114
MAX REFILL WITHOUT DRY MOTORING
2 QTS
115
IF REPLENISHED AND PERIOD EXCEEDED
ENGINE(S) MUST BE DRY MOTORED
116
VMO 0-8,000 FEET
330 KIAS
117
VMO 8,000-25,000 FEET
335 KIAS
118
MMO 27,000-32,000 FEET
0.80 MACH
119
VMO 27,000-32,000 FEET
315 KIAS
120
MMO 32,000-41,000 FEET
0.85 MACH