EJet Limits Flashcards
1
Q
Maximum Ramp Weight (MRW)
A
85,870
2
Q
Maximum Takeoff Weight (MTOW)
A
85,517
3
Q
Maximum Landing Weight (MLW)
A
74,957
4
Q
Maximum Zero Fuel Weight (MZFW)
A
69,886
5
Q
Max Operating Airspeed
A
VMO
6
Q
Max Operating Mach Number
A
MMO (.82M)
7
Q
Maximum Airspeed for RAT Operation
A
VMO/MMO
8
Q
Turbulent Airspeed: Below 10,000 feet
A
250 KIAS
9
Q
Turbulent Airspeed: At or Above 10,000 feet
A
270 KIAS/.76M
10
Q
Maximum Tire Limit Ground Speed
A
195 Knots
11
Q
Maximum Windshield Wiper Operation Speed
A
253 KIAS
12
Q
Maximum Gear Speed: Extension (VLOE)
A
250 KIAS
13
Q
Maximum Gear Speed: Extended (VLE)
A
250 KIAS
14
Q
Maximum Gear Speed: Retraction (VLOR)
A
250 KIAS
15
Q
Minimum Flight Crew
A
Pilot and Copilot
16
Q
Max Takeoff and Landing Tailwind Component
A
10 knots
17
Q
Max Runway Slope
A
+/-2%
18
Q
Runway Surface Type
A
Paved
19
Q
Flap Maneuvering Load Acceleration Limits:Flaps Up
A
-1.0 G to +2.5 G
20
Q
Flap Maneuvering Load Acceleration Limits:Flaps Down (1, 2, 3, 4, 5, and FULL)
A
-0.0 G to +2.0 G
21
Q
Max Operating Altitude
A
41,000 feet
22
Q
Max Takeoff and Landing Altitude
A
8,000 feet
23
Q
Min Takeoff and Landing Altitude
A
-1,000 feet
24
Q
Max Ambient Air Temperature for Takeoff and Landing
A
52°C
25
Max Flap Extension Altitude
20,000 feet
26
Maximum latitude for stationary alignment
78.25°N to 78.25°S
27
Min Ambient Temperature Approved for Takeoff
-40°C (SAT)
28
Min Ambient Temperature for Operation
-54°C (SAT)
29
Flaps Operating Speed: Flaps 1
230 KIAS
30
Flaps Operating Speed: Flaps 2
215 KIAS
31
Flaps Operating Speed: Flaps 3
200 KIAS
32
Flaps Operating Speed: Flaps 4
180 KIAS
33
Flaps Operating Speed: Flaps 5
180 KIAS
34
Flaps Operating Speed: Flaps Full
165 KIAS
35
Up to 8,000 feet
300 KIAS
36
Max speed 8,000 to 10,000 feet
300 to 320 KIAS (Increases Linearly)
37
Max speed 10,000 feet to FL290
320 KIAS (VMO)
38
Max speed FL290 to FL410
.82M (MMO)
39
Max Fuel Capacity (Total)
20,935 lb. (10392.5 lb. or 1535.5 US Gal per tank)
40
Unusable Quantity per Tank
75 lbs. / 11 US Gal per tank
41
Maximum Fuel Imbalance
794 lb.
42
Minimum Fuel Tank Temperature
-37°C
43
Max Differential Pressure
8.4
44
Max Differential Overpressure
8.8 psi
45
Max Differential Negative Pressure
-0.5 psi
46
Max Differential Pressure for Takeoff and Landing
0.2 psi
47
Max altitude for single pack operation
Flight Level 310
48
Engine Name
General Electric CF34-8E5 (A-10/S-2)
49
Engine Limits: N1
[-] to [99.5%]
50
Engine Limits: N2
[58.5%] to [99.4%]
51
Engine Limits: ITT (Start)
[-] to [815℃]
52
Engine Limits: ITT (Max T/O & Go Around) {Notes 1 & 2}
[-] to [990℃ (Time limited to 10 min.) (Can be exceeded up to 1006℃ during the first 2 min.]
53
Engine Limits: ITT (Max Continuous)
[-] to [960℃]
54
Engine Limits: OIL PRESSURE
[25 psi] to [95 psi]
55
Engine Limits: OIL TEMPERATURE: (Continuous)
[-] to [155℃]
56
Engine Limits: OIL TEMPERATURE: (Transient) {Note 3}
[-] to [163℃ (Transient operation above 155℃ limited to 15 min.)]
57
Red on EICAS
Max & Min Limitations
58
Amber on EICAS
Caution Range
59
Green on EICAS
Normal Operating Range
60
NOTE: For FLEX - reduction must not exceed: ___ of the ___ ____ ____
25% of the full takeoff thrust
61
NOTE: FLEX is prohibited: on _____ _____
on contaminated runways
62
NOTE: ATTCS must be ____ for all T/O and landings
ON
63
Engine Starter Duty Cycle: Attempts 1 & 2 GROUND
90 Sec ON / 10 sec OFF
64
Engine Starter Duty Cycle: Attempts 1 & 2 AIR
120 Sec ON / 10 sec OFF
65
Engine Starter Duty Cycle: Attempts 3, 4 & 5 GROUND
90 Sec ON / 10 sec OFF
66
Engine Starter Duty Cycle: Attempts 3, 4 & 5 AIR
120 Sec ON / 5 min OFF
67
Dry Motoring Duty Cycle Limits: Attempt 1
90 Sec ON / 5 min OFF
68
Dry Motoring Duty Cycle Limits: Attempts 2, 3, 4, & 5
30 Sec ON / 5 min OFF (After 5 sequential motorings, cycle may be epeated following a 15 min cool down)
69
APU Started Duty Cycle: Attempts 1 & 2
1 min ON / 1 min OFF
70
APU Started Duty Cycle: Attempt 3
1 min ON / 5 min OFF
71
APU Type?
Hamilton Sundstrand APS 2300
72
Min START Temp & ALT
[-54℃] & [-]
73
Max START Temp & ALT
[APU temp matches the Airplane Operational Envelope temp] & [30,000 ft]
74
Min Operational Temp
APU temp matches the Airplane Operational Envelope temp
75
Max Operational Temp
APU temp matches the Airplane Operational Envelope temp
76
Min Operational ALT
[-]
77
Max Operational ALT
33,000 ft
78
Min Operational ELE GEN
[-]
79
Max Operational ELE GEN
33,000 ft
80
Min Operational BLEED
[-]
81
Max Operational BLEED
15,000 ft
82
Min Operational TO ASSIST ENGINE START
[-]
83
Max Operational TO ASSIST ENGINE START
21,000 ft
84
Min ROTOR SPEED
[-]
85
Max ROTOR SPEED
108%
86
MAX EGT *NOTES*
[In-flight, there is no automatic shutdown if EGT exceeds the limits.] [There is no time limitation for operating the APU on ground or in flight in the amber range between662°C and 717°C.]
87
Min EGT: START AND CONTINUOUS
[-] to [1032℃]
88
Max EGT: START AND CONTINUOUS
[-] to [717℃]
89
TAS, TAT, SAT valid above…
…60 KIAS
90
Standby Mag Comp NOT VALID while transmitting on…
…VHF #1
91
Min A/P useage (T/O)?
400' AGL per Flight Manual & 1000' AGL per Mesa
92
Min approach height (Coupled ILS)
50' AGL
93
X-feed MUST be OFF…
…during T/O and Landing
94
If brake temp is in the AMBER
…DO NOT T/O
95
Icing conditions
ground OAT or inflight TAT is 10℃ or below with visible moisture
96
Max FWD Cargo Weight
3,306 lbs.
97
Max AFT Cargo Weight
2,535 lbs.
98
Dimensions: Nose to Tail
103'11'
99
Dimensions: Wing tip to Wing tip
93'11'
100
Dimensions: Height of Tail
32'4"
101
Trun Radius
59'2"
102
Max x-wind Limit: DRY
38 knots
103
Max x-wind Limit: WET
31 knots
104
Max x-wind Limit: compact SNOW
20 knots
105
Max x-wind Limit: standing water / SLUSH
18 knots
106
Max x-wind Limit: wet ICE
12 knots
107
Max x-wind Limit: Static T/O
25 knots
