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Embraer 170 > Limitations > Flashcards

Limitations Flashcards

(57 cards)

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1
Q

ERJ-170 Max Ramp Weight

A

82,364

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2
Q

ERJ-170 Max Takeoff Weight

A

82,011

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3
Q

ERJ-170 Max Landing Weight

A

72,310

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4
Q

ERJ-170 Max Zero Fuel Weight

A

65,256 lbs or

66,446 (refer to flight release)

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5
Q

Method 1 & 2

A

1 - aircrafts has capability to clear all obstructions 5SM either side of intended route by 1,000ft until destination.
2 - (driftdown) clear all obstructions 5SM either side of the route of flight by 2,000ft until reaching the diversion airport.

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6
Q

ERJ-175 Max Ramp Weight

A

85,870 lbs

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6
Q

ERJ-175 Max Takeoff Weight

A

85,517 lbs

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7
Q

ERJ-175 Max Landing Weight

A

74,957 lbs

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8
Q

ERJ-175 Max Zero Fuel Weight

A

69,886 lbs

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9
Q

Max Cargo Compartment Loads

A

FWD AFT
E170 3020 2271
E175 3307 2535

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10
Q

Max Runway Slope

A

+|- 2.0%

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11
Q

Runway Surface Type

A

Paved

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12
Q

Flap Maneuvering Acceleration Limits

Up and Down

A

Up: -1.0 G to +2.5 G
Down: 0 G to +2.0 G

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13
Q

Max Takeoff and Landing Altitude

A

8,000 ft

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14
Q

Max Ambient Air Temp for Takeoff and Landing

A

52°C

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15
Q

Min Ambient Air Temp for Takeoff and Landing

A

-40°C

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17
Q

Min Flight Crew

A

Pilot and Copilot

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18
Q

Max Recommended Crosswind:

DRY

A

38 kts

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19
Q

Max Recommended Crosswind:

WET

A

31 kts

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20
Q

Max Recommended Crosswind:

Compacted SNOW

A

20 kts

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21
Q

Max Recommended Crosswind:

Standing WATER/SLUSH

A

18 kts

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22
Q

Max Recommended Crosswind:

Wet ICE

A

12 kts

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23
Q

Max Altimeter Difference:

-2,000 up to 10,000

24
Q

Max Altimeter Difference:

10,000 up to 20,000

25
Max Altimeter Difference: 20,000 up to 41,000
180 ft
26
Max Airspeed for RAT operation:
VMO/MMO
27
Max Speed to Open the Direct Vision Window:
160 KIAS
28
Max Useable Fuel Quantity per Tank:
10,393 lbs | 1,536 Gallons
29
Unusable Fuel Quantity per Tank:
75 lbs | 11 Gallons
30
Aircraft Max Fuel Capacity | usable + unusable
20,936 lbs | 3,094 Gallons
31
Fuel Density lbs/Gal
6.767 lbs/gal
32
Approved Fuels:
``` Primary Jet A (ATSM D1655) Jet A-1 (ATSM D1655) Alternate JP-8 (MIL-T-83133A) Brazilian Spec QAV1 ```
33
Max Differential Pressure -Up to 37,000 ft
7.8 psi
34
Max Differential Pressure -Above 37,000 ft
8.3 psi
35
Max Differential Overpressure
8.7 psi
36
Max Differential Negative Pressure
-0.5 psi
37
Max Differential Pressure for Takeoff and Landing
.2 psi
38
Brakes Cooling Limitation
Do not takeoff with amber brake temperature indicators.
39
Landing Gear Retraction Limitation
Activation of the landing gear down lock release button is prohibited for all takeoffs unless obstacle clearance is required.
40
Thrust Reverser Limitations
1. Approved for ground use only. 2. Intended for use during rejected and full stop landings. 3. Do not attempt a go-around maneuver after deployment of the thrust reversers. 4. Power back operations using the thrust reversers are prohibited. 5. Must be stowed below 60 kts. 6. After Selecting Reverse Thrust, do not move the thrust levers into the forward thrust range until the REV icon on the EICAS is amber or green.
41
Instrument Limitations
1. TAS, TAT, and SAT are only valid above 60 kts. 2. Standby Magnetic Compass indication is not valid while transmitting on VHF #1. 3. Barometric Altimeter mins must be used for all CAT 1 approaches.
42
Navigation Limitations
1. LOC Backcourse approaches using IESS are not authorized. 2. The Captain must ensure displayed guidance from non usable stations is not used for navigation purposes by the flight crew.
43
TCAS Limitation
Pilots are authorized to deviate from their current ATC clearance to the extent necessary to comply with a Resolution Advisory (RA).
44
RVSM Min Equipment
- 2 RVSM compliant Air Data Systems - 1 Autopilot, engaged, with Altitude Hold Mode Operative - 1 Altitude Alerter - 1 Transponder - The ADS1, ADS2, ADS3 are compliant with RVSM operation. - The IESS must not be used - Should any of the equipment fail prior to entering RVSM airspace, the pilot should request a new clearance to avoid entering this airspace.
45
RVSM ADS 3
The ADS3 is not considered RVSM compliant in case of loss of sideslip compensation. (EICAS message ADS3 SLIPCOMP FAIL displayed)
46
Max Flight Operating Latitude
78°N to 78°S
47
Max Altitude with Flaps Extended
20,000 ft
48
Flaps Prohibited:
2. Enroute Use of Flaps prohibited. 3. Do not hold in icing conditions with Flaps extended 4. The use of Flaps 4 during approach and landing is prohibited.
49
FMS speeds:
May only be used during normal flight operations.
50
Autopilot Min Engagement Height
400 ft AGL
51
Autopilot Min Use Height (ILS Approach) (Non-Precision Approach)
Precision - 50 ft AGL | Non precision - MDA(DA)
52
Warm UP / Cool Down
1. Before applying takeoff thrust, allow the engines to warm up for a minimum of 2 minutes. 2. A 2 minute cool down must be observed prior to shutting down an engine.
53
After Power-up
Ensure airplane is not moved until IESS is initialized. Initialization occurs within 90 seconds after power-up. To allow the flight controls built-in test, wait three (3) minutes after power up to turn any hydraulic pump on.
54
Ground pneumatic start cart caution:
Do not operate air conditioning packs to avoid cabin air contamination. Pack 1 & 2 pushed out
55
Fly By Wire Power Up Built-In Test (PBIT)
1. Electric - lasts 3 min 2. Hydraulic - lasts 1 min ``` 1. Don't turn on hydr pump Cycle flight controls mode switches AC power supply interrupted 2. Don't move flight controls Steer Off annunciated Below 250psi & above 10°C Turn on pumps 1,2, 3A Wait 60 seconds Expired msg gone then pumps off ```
56
No FLEX takeoff if...
Runway is contaminated Windshear advisories are in effect Runway performance does not allow it
57
Types of Operations
1. VFR 2. IFR 3. Icing Conditions 4. CAT l 5. CAT ll 6. RVSM

Embraer 170 (5 decks)

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