Limitations Flashcards

(58 cards)

1
Q

STRUCTURAL LIMITATIONS ERJ 175LL

A

Max. Ramp Wt. - 85,450 lb

Max. T/O Wt. - 85,098 lb

Max. Lnd. Wt. - 74,957 lb

Max. Zero Fuel Wt. - 69,467 lb

Min. Runway Width - 100ft (SW)

Min. Taxiway Width - 50ft (SW)

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2
Q

STRUCUTURSL LIMITSTIONS ERJ 175 LR

A

Max. Ramp Wt. - 85,870lb

Max. T/O Wt. - 85,517 lb

Max. Lnd. Wt. - 74,957 lb

Max. Zero Fuel Wt. - 69,866

Min. Runway Width - 100ft (SW)

Min. Taxiway Width - 50ft (SW)

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3
Q

EXTERNAL DIMENSIONS

A

WING SPAN - 93’ 11’’

AIRCRAFT LENGTH - 103’ 11’’

TAIL HEIGHT - 31’ 4’’

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4
Q

MAX OPS. ALT.

A

41,000’

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5
Q

MAX T/O & LND

A

10,000’

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6
Q

MAX. TEMP. T/O LND

A

ISA +35°C (52°C)

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7
Q

MIN. TEMP. T/O LND

A

-40°C

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8
Q

RWY SLOPE

A

+/- 2%

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9
Q

MAX. TAILWIND

A

15KT

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10
Q

MAX SINGLE PACK OPERATIONS

A

31,000’

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11
Q

VMO SL - 8,000’

A

300

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12
Q

VMO 10,000 - Mach Transition

A

320

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13
Q

MMO

A

.82

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14
Q

VA

A

240

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15
Q

VLO EXT

A

250

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16
Q

VLO RET

A

250

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17
Q

VLE

A

250

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18
Q

V TIRE

A

195

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19
Q

V RAT DEPLOY MAX

A

VMO/MMO

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20
Q

VMIN( TO PROVIDE ELECTRICAL POWER

A

130

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21
Q

VB (BELOW 10,000’)

A

250

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22
Q

VB (10,000’ AND ABOVE)

A

270/.76M (WHICHEVER IS LOWER)

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23
Q

V WIPER OPS MAX

A

250 (SW)

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24
Q

V WINDOW

25
VFE 1
230
26
VFE 2
215
27
VFE 3
200
28
VFE 4
180
29
VFE 5
180
30
VFE FULL
165
31
MAX ALT. FLAPS/SLAPS EXTENDED
20,000'
32
FLAPS CAT II APPROACH
MANDATORY FLAPS 5
33
GO-AROUND LANDING FLAPS FULL
GO-AROUND FLAPS 4
34
GO-AORUND LANDING FLAPS 5
GO-AROUND FLAPS 2
35
BATTERY MIN. VOLATGE
22.5V
36
MAX ITT START
815°C
37
STARTER CRANKING LIMITS (GROUND)
ATTEMPTS 1 & 2 - 90 SEC ON - 10 SEC OFF ATTEMPTS 3-5 - 90 SEC ON - 5 MIN OFF
38
STARTER CRANKING LIMITS (AIR)
ATTEMPTS 1 & 2 - 120 SEC ON - 10 SEC OFF ATTEMPTS 3-5 - 120 SEC ON - 5 MIN OFF
39
CRY MOTORING CYCLE LIMITS
MOTORING 1 - 90 SEC ON - 5 MIN OFF MOTORING 2-5 - 30 SEC ON - 5 MIN OFF AFTER MOTORING 5 CYCLES, PORCESS MAY BE REPEATED AFTER 15 MIN COOL DOWN
40
TAILWIND GROUND START
When it is necessary to perform an engine start with tailwind, monitor N1 indication. When there is no positive increase of N1 indication before starter cutout (50% N2), the engine start must be manually aborted.
41
ENGINE T/O THRUST LIMITAIONS
T/O WITH AUTOMATIC TAKEOFF THRUST CONTROL SYSTEM (ATTCS) OFF IS NOT AUTHORIZED
42
MAX FUEL CAPACITY
20,935 LB
43
MAX FUEL IMBALANCE
794 LB
44
MIN FUEL TANK TEMP
-37°C
45
CROSSFEED LIMITATIONS
MUST BE SELECTED OFF DURING T/O LND
46
GENERAL APU LIMITATIONS
WAIT 30 SEC AFTER EICAS IS ENERGIZED TO START APU DO NOT LEAVE AIRCRAFT UNATTENDED MORE THAN 5 MIN WITH APU RUNNING (SW) SIMUL. USE OF APU AND HP CART IS PROHIBITED
47
APU STARTER DUTY CYCLE
ATTEMPT 1&2 - 60 SEC OFF THIRD ATTEMPT - 5 MIN OFF
48
APU START LIMITATIONS
TEMPERATUR -54°C TO ISA +35°C ALTITUDE 30,000'
49
APU CONTINUOUS OPERATIONAL LIMITATIONS
TEMPERATUR - -54°C TO ISA +35°C ALTITUDE - 33,000' ELECTRICAL GENERATOR USE - 33,000' ENGINE START - 21,000' BLEED USE - 15,000'
50
PRESSURIZATIION LIMITATIONS
MAX DIFFERENTIAL PRESSURE - 8.4 PSI MAX DIFFERENTIAL OVERPRESSURE - 8.8 PSI MAX DIFFEERENTIAL NEGATIVE PRESSURE - -0.5 PSI MAX DIFFERENTIAL PRESSURE FO T/O AND LND - 0.2 PSI
51
MIN HYD RESERVOIR TEMP FOR ENG START
-18°C
52
BRAKE LIMITAION
BRAKE TEMP INDICATION MUST BE IN THE GREEN
53
THRUST REVERSER LIMITATIONS
* Do not attempt a go-around maneuver after deployment of the thrust reversers. * After selecting reverse thrust, do not move the thrust levers into the forward thrust range until the REV icon on the EICAS is shown in amber or green. * The use of thrust reversers during normal taxi operations is prohibited. * The use of thrust reversers for power back operations is prohibited.
54
AUTOPILOT USE LIMITATIONS
Min. Engagement Height - 400' Min. Use Height - 50' Min. Use Height - Non-precision Approach - MDA
55
TAS, TAT, and SAT LIMITATION
TAS, TAT, and SAT information are only valid above 60 kt.
56
VHF1 TRANSMISSION LIMITATION
THE STANDBY MAGNETIC COMPASS INDICATION IS NOT VALID
57
CAT I MINIMUM REQUIREMENT
BAROMETRIC ALTIMETER MINIMUMS MUST BE USED
58
FMS MINIMA LIMITATIONS
RNAV (GPS) LP MINIMA IS NOT AUTHORIZED