ERJ-170/175 LIMITATIONS Flashcards

(100 cards)

1
Q

TYPE OF OPERATIONS

A
  1. VFR
  2. IFR
  3. Icing Conditions
  4. CAT I & CAT II
  5. Extended Overwater Operations
  6. RVSM
  7. RNP
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2
Q

APU MAX ROTOR SPEED

A

108%

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3
Q

APU MAX ITT START

A

1032 °C

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4
Q

APU MAX CONTINUES

A

717 °C

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5
Q

APU MAX ALTITUDE FOR START

A

33,000 Feet

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6
Q

APU MAX ALT ELECTRICS & PNEUMATICS

A

15,000 feet

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7
Q

APU MAX ALTITUDE ELECTRICS ONLY

A

33,000 Feet

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8
Q

APU MAX ALT to ASSIST ENG START

A

21,000 Feet

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9
Q

APU MIN OPERATION TEMPERATURE

A

- 62 °C

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10
Q

APU MAX OPERATION TEMPERATURE

A

ISA + 35 °C

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11
Q

APU DUTY CYCLE

A
  • 1st & 2nd Start………60 seconds ON/60 seconds OFF
  • 3rd Start………………..60 seconds ON/5 minutes OFF
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12
Q

PNEUMATIC

MAX DIFF PRESSURE to 37,000 Feet

A

7.8 psi

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13
Q

PNEUMATIC

MAX DIFF PRESSURE 37,000 - 41,000 Feet

A

8.4 psi

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14
Q

PNEUMATIC

MAX DIFFERENTIAL OVERPRESSURE

A

8.8 psi

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15
Q

PNEUMATIC

MAX DIFFERENTIAL NEGATIVE PRESSURE

A

- 0.5 psi

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16
Q

PNEUMATIC

MAX DIFFERENTIAL PRESSURE TAKEOFF AND LANDING

A

0.20 psi

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17
Q

PNEUMATIC

MAX ALT SINGLE PACK OPERATION

A

31,000 Feet

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18
Q

MAX OPERATION AIRSPEED VMO/ MMO

A

320 KIAS/0.82M

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19
Q

MAX AIRSPEED FOR RAT OPERATIONS

A

VMO/MMO 320 KIAS/0.82M

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20
Q

TURBULENT AIR PENETRATION BELLOW 10,000 Feet

A

250 KIAS

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21
Q

TURBULENT AIR PENETRATION ABOVE 10,000 Feet

A

270 KIAS/ 0.76 M

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22
Q

MAX TIRE LIMIT GROUND SPEED

A

195 KTS

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23
Q

MAX SPEED to Open DIRECT VISION WINDOW

A

160 KIAS

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24
Q

MAX WINDSHIELD WIPER OPERATION SPEED

A

253 KIAS

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25
ALL LANDING GEAR SPEEDS Limits
**250 KIAS**
26
DESIGN MANEUVERING SPEED
**240 KIAS**
27
FLAPS 1
**230 KIAS**
28
FLAPS 2
**215 KIAS**
29
FLAPS 3
**200 KIAS**
30
FLAPS 4
**180 KIAS**
31
FLAPS 5
**180 KIAS**
32
FLAPS FULL
**165 KIAS**
33
MAX OPERATING SPEED SL to 8,000 Feet
**300 KIAS**
34
MAX OPERATING SPEED 8,000 Feet to 10,000 Feet
**300 KIAS to 320 KIAS**
35
MAX OPERATING SPEED 10,000 Feet to FL 290
**320 KIAS**
36
MAX OPERATING SPEED FL 290 to FL 410
**Mach 0.82**
37
AUTO FLIGHT/AUTOPILOT MIN ENGAGEMENT HEIGHT ON TAKEOFF
**400 Ft**
38
AUTO FLIGHT/AUTOPILOT MIN USE HEIGHT ON APP FOR COUPLED ILS
**50 ft**
39
AUTO FLIGHT/AUTOPILOT MIN USE HEIGHT ON NON-PRECISION APP
**LEAVING THE MDA/DA**
40
BRAKES DO NOT TAKEOFF WITH BRAKE TEMPERATURE
**IN THE AMBER RANGE**
41
THE MAX N1 WITH BRAKE APPLIED
**60% N1**
42
MAX TAKEOFF & LANDING TAILWIND COMPONENT
**15 KTS**
43
MAX CROSSWINDS RECOMMEND FOR TAKEOFF & LANDING (DRY RUNWAY)
**38 KTS**
44
MAX CROSSWINDS RECOMMEND FOR TAKEOFF & LANDING (WET RUNWAY)
**31 KTS**
45
MAX CROSSWINDS RECOMMEND FOR TAKEOFF & LANDING (COMPACTED SNOW)
**20 KTS**
46
MAX CROSSWINDS RECOMMEND FOR TAKEOFF & LANDING (STANDING WATER/SLUSH/WET SNOW/ DRY SNOW)
**18 KTS**
47
MAX CROSSWINDS RECOMMEND FOR TAKEOFF & LANDING - ICE (INCLUDING WET ICE)
**12 KTS**
48
MAX ALT FLAPS EXTENDED
**20,000 feet**
49
LIMITATIONS ON THRUST REVERSER
1. **GROUND USE ONLY** 2. **FULL STOP LANDINGS ONLY** 3. **DO NOT ATTEMPT GO-AROUND AFT DEPLOYMENT** 4. **IDLE REVERSE BELOW 60 KTS** 5. **REV MUST BE IN GREEN OR AMBER BEFORE SELECTING FORWARD THRUST**
50
AIRCRAFT MAX FUEL CAPACITY
**20,935 lbs**
51
MAX FUEL USABEL PER TANK
**10,932 lbs**
52
UNUSABLE FUEL QTY PER TANK
**75 lbs**
53
MAX FUEL IMBALANCE
**800/794 lbs**
54
CROSSFEED (XFEED) OPERATION SET TO OFF
**FOR TAKEOFF AND LANDING**
55
CONDITION FOR ANTI-ICE TO BE SET TO ALL
**TEMP +10 °C AND BELOW AND VISIBLE MOISTURE**
56
MAXIMUM WINDSHIELD OPERATION SPEED
**253 KTS**
57
TAS/TAT/SAT VALID ABOVE
**60 KTS**
58
MAGNETIC COMPASS NOT VALID
**TRANSMITTING ON VHF #1**
59
ALL CAT I APPROACHES
**MUST USE BARO ALTIMETER MINIMUM**
60
PILOTS ARE AUTHORIZED TO DEVIATE FROM ATC
**RA ON TCAS**
61
BACK COURSE ILS IS PROHIBITED
**On IESS (Integrated Electronic Stby System)**
62
MINIMUM CREW
**2 PILOTS**
63
MAX RUNWAY SLOPE
**+/- 2.0%**
64
RUNWAY SURFACE TYPE
**PAVED**
65
FLAPS UP MANEUVERING G LOAD
**-1.0 G to +2.5 G**
66
FLAPS DOWN MANEUVERING G LOAD
**0.0 G to +2.0 G**
67
MAX OPERATING ALTITUDE
**41,000 feet**
68
MIN/MAX TAKEOFF & LANDING ALTITUDE
**- 1000 ft/8000 ft** **(Pressure altitude, not density altitude)**
69
MAX AMBIENT TEMP TAKEOFF/LANDING
**+52 °C**
70
MAX FLIGHT OPERATING LATITUDE
**78° N to 78° S**
71
MINIMUM AMBIENT TEMP FOR TAKEOFF
**- 40 °C**
72
MINIMUM AMBIENT TEMP FOR OPERATIONS
**- 54 °C**
73
MAINTENANCE INSPECTION REQUIRED
**LANDING BELOW - 40 °C**
74
MAX N1%
**99.5% N1**
75
MAX N2%
**99.4% N2**
76
MIN N2%
**58.5% N2**
77
MAX ITT START
**815 °C**
78
MAX ITT CONTINUOS
**960 °C**
79
MIN OIL PRESSURE
**25 psi**
80
MAX OIL PRESSURE
**95 psi**
81
MAX OIL TEMP | (CONTINUOUS)
**155 °C**
82
MAX OIL TEMP - TRANSIENT
**163 °C** ## Footnote (TRANSIENT Operation Above 155 °C is **limited to 15 MINUTES**)
83
EICAS
1. **RED - MAX AND MIN LIMITATIONS** 2. **AMBER - CAUTION RANGE** 3. **GREEN - NORMAL OPERATING RANGE**
84
MAX THRUST REDUCTION with **FLEX**
**25%**
85
**FLEX** PROHIBITED
**ON WET AND CONTAMINATED RUNWAYS**
86
**ATTCS** MUST BE ON
**FOR ALL TAKEOFFS**
87
ENGINE STARTER DUTY CYCLE ## Footnote **(GROUND)**
* *1st and 2nd START* **90 SECONDS ON/10 SECONDS OFF** * *3rd to 5th START* **90 SECONDS ON/5 MINUTES OFF**
88
ENGINE STARTER DUTY CYCLE ## Footnote **(FLIGHT)**
* *1st and 2nd START* **120 SECONDS ON/10 SECONDS OFF** * *3rd to 5th START* **120 SECONDS ON/5 MINUTES OFF**
89
ENGINE STARTER **DRY** MOTORING
* *1st START* **90 SECONDS ON/5 MINUTES OFF** * *2nd to 5th START* **90 SECONDS ON/15 MINUTES OFF** **​​**(AFTER **5** SEQUENTIAL MOTORING **15 MINUTES 0FF**)
90
**ITT** FOR ENGINE **R**ESTART
**120 °C OR LESS**
91
MAX RAMP WEIGHT (MRW)
**85,450 LBS**
92
MAX TAKEOFF WEIGHT (MTOW)
**85,098 LBS**
93
MAX LANDING WEIGHT (MLW)
**74,957 LBS**
94
MAX ZERO FUEL WEIGHT (MZFW)
**69,467 LBS**
95
**FWD** Baggage Compartment Capacity
**3,306 LBS**
96
**AFT** Baggage Compartment Capacity
**2,535 LBS**
97
ENGINE
**CF34-8**
98
MINIMUM FUEL TANK TEMPERATURE
**- 37 °C**
99
MAXIMUM ITT for TAKEOFF
**1006 °C** * **5** Minutes **all ENG** Operatives * **10** Minutes **one ENG** Inoperative
100
MAXIMUM ITT - GO AROUND
**990 °C** (Can be Exceed UP to 1006 °C for the First 2 Minutes)