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62 Cards in this Set
- Front
- Back
ERJ-170
Maximum Ramp Weight (MRW) |
82,364 lbs.
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ERJ-170
Maximum Takeoff Weight (MTOW) |
82,011 lbs.
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ERJ-170
Maximum Landing Weight (MLW) |
72,310 lbs.
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ERJ-170
Maximum Zero Fuel Weight (MZFW) |
65,256 lbs.
66,446 lbs.* * Refer to the Flight Release to confirm the applicable MZFW. |
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ERJ-175
Maximum Ramp Weight (MRW) |
85,870 lbs.
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ERJ-175
Maximum Takeoff Weight (MTOW) |
85,517 lbs.
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ERJ-175
Maximum Landing Weight (MLW) |
74,957 lbs.
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ERJ-175
Maximum Zero Fuel Weight (MZFW) |
69,886 lbs.
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Max. takeoff and landing tailwind component
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10 knots
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Max. runway slope
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+/- 2.0%
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Runway Surface Type
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PAVED
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Flap maneuvering load acceleration limits. Flaps...
Up DOWN |
-1.0 G to +2.5 G
0.0 G to +2.0 G |
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Max. operating altitude
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41,000 feet
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Max. takeoff and landing altitude
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8,000 feet (ERJ 170/175 only)
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Max. ambient air temperature for T/O and landing
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52°C
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Max. flap extension altitude
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20,000 feet
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Max. flight operating latitude
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78N to 78S
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Min. ambient temperature approved for takeoff
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-40°C
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Min. ambient temperature for operation
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-54°C
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The maximum demonstrated crosswind for takeoff and landing is:
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28 Knots
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Maximum crosswinds for takeoff and landing will be—
(1) Dry Runway (2) Wet Runway (3) Runway with Compacted Snow (4) Runway with Standing Water/Slush (5) Runway with Wet Ice (no melting) |
(1) 28 knots
(2) 28 knots (3) 20 knots (4) 18 knots (5) 12 knots |
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TURBULENT AIR PENETRATION
(1) Below 10,000 MSL (2)At or above 10,000 MSL |
(1) 250 KIAS
(2) 270 KIAS/0.70M (ERJ 170/175) Use whichever speed is lower |
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Maximum gear extension speed (VLO)
Maximum gear retraction speed (VLO) Maximum gear extended speed (VLE) |
250 KIAS
250 KIAS 250 KIAS |
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MAXIMUM TIRE GROUND SPEED
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195 KIAS
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MAXIMUM FLAP OPERATING SPEEDS - VFE
FLAP 1 FLAP 2 FLAP 3 FLAP 4 FLAP 5 FLAP FULL |
FLAP 1---230
FLAP 2---215 FLAP 3---200 FLAP 4---180 FLAP 5---180 FLAP FULL----165 |
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MAXIMUM SPEED TO OPEN THE DIRECT VISION WINDOW
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160 KIAS
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MANEUVERING SPEED ENVELOPE
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Full application of rudder and aileron controls, as well as maneuvers that
involve angles of attack near the stall, must be confined to speeds below 240 KIAS (R). |
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Maximum airspeed for windshield wiper operation is
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250 KIAS (R)
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(1) Maximum usable quantity per tank
(2) Unusable quantity per tank (3) Aircraft maximum fuel capacity (usable + unusable fuel) |
(1) 10392.5 lbs
(2) 75 lbs (3) 20,935 lbs |
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MINIMUM FUEL TANK TEMPERATURE
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- 40°C
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Maximum fuel imbalance between tanks
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794 lbs
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The XFEED Selector must be set to ______during takeoff and landing.
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OFF
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Maximum Differential Pressure
Up to 37,000 feet (1)____ Above 37,000 feet (2)___ Maximum Differential Overpressure (3)____ Maximum Differential Negative Pressure (4)___ Maximum Differential Pressure for Takeoff and Landing (5)_____ |
(1) 7.8 psi
(2) 8.3 psi (3) 8.7 psi (4) -0.5 psi (5) 0.2 psi |
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The maximum altitude for single pack operation is
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31,000 feet
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BRAKES
Cooling Limitation |
do not takeoff with amber brake temperature
indicators. (R) |
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FLAPS
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A. Maximum Altitude with Flaps Extended ......... 20,000 feet.
B. Enroute use of flaps is prohibited. (R) C. Do not hold in icing conditions with Flaps extended. (R) |
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THRUST REVERSERS (R)
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A. Approved for ground use only.
B. Intended for use during full stop landings. C. Do not attempt a go-around maneuver after deployment of the thrust reversers. D. Power back operations using thrust reversers are prohibited. E. Landing rollout below 60 KIAS: 1) Application of maximum reverse thrust is not permitted. 2) Reduce reverse thrust to IDLE. |
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NAVIGATION
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A. TAS, TAT and SAT are only valid above 60 KIAS.
B. Standby magnetic compass indication is not valid while transmitting on VHF #1. C. Barometric altimeter minimums must be used for all CAT I approaches. D. LOC Backcourse approaches using IESS is not authorized. |
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RVSM MINIMUM EQUIPMENT REQUIRED
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2 RVSM Compliant Air Data Systems
1 Autopilot with Altitude Hold Mode operative 1 Altitude Alerter 1 Transponder B. The ADS1, ADS2 and ADS3 are compliant with RVSM operation. C. The IESS must not be used for RVSM operation. |
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AUTO FLIGHT CONTROL SYSTEM
Minimum Engagement Height .......... Minimum Use Height- Coupled ILS Approach........... |
400 ft AGL
50 ft AGL |
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PROHIBITED MODES
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The VOR and VNAV flight director modes are prohibited
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POWER PLANT
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Two General Electric CF34-8E5 (ERJ 170/175 Only)
Aircraft Type ERJ170/175 ERJ 170/175 Parameter Minimum Maximum Engine Speed N1 99.5% 100% N2 58.5% 99.4% ITT Ground Start -------- 815ºC Inflight Start -------- 815ºC Normal Takeoff & Go Around --------- 965ºC a --------- 949ºC b Maximum Takeoff and Go Around ---------- 1006ºC a ---------- 990ºC b Maximum Continuous --------- 960ºC Oil Pressure Operating Range 25 psi 95 psi Oil Temperature Continuous ---------- 155ºC Transient ---------- 163ºC c a. Time limited to the first 2 minutes of the total 5 minute limit. b. Time limited to the remaining 3 minutes of the total 5 minute limit. c. Time limited to 15 minutes for transient operation above 155ºC. d. Time limited to 5 min. e. ITT transients above the nominal ITT limits are allowed to Normal and Maximum takeoff, up to 5.5°C for 2 s, 4.4°C for 5 s, 3.6°C for 15 s and 2.4°C for 30 s. f. During starts with oil temperature below -22°C the minimum oil pressure is 5 psi, time limited to 2 min. |
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ENGINE STARTER DUTY CYCLE LIMITS
|
Number of Start Maximum Time Followed by
Cool Down of 1st and 2nd 90 seconds ON (ground)a 10 seconds OFF 120 seconds ON (in flight)b 3rd through 5th 5 minutes OFF a.For ground starts, the maximum cumulative starter run time per start attempt is 90 seconds (monitoring plus start time). b.For in-flight starts, the maximum cumulative starter run time per start attempt is 120 seconds (monitoring plus start time). |
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ENGINE STARTER DRY MOTORING DUTY CYCLE LIMITS
|
Number of Start Maximum Time Followed by
Cool Down of 1st 90 Seconds ON 5 minutes OFF 2 through to 5a 30 Seconds ON 5 minutes OFF a.After 5 sequential motorings, cycle may be repeated following a 15 minute cool down period. |
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APU STARTER DUTY CYCLE
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Start Cycle Maximum Followed By
1st and 2nd 60 seconds ON 60 seconds OFF 3rd cycle 60 seconds ON 5 minutes OFF |
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APU LIMITS
TYPE OPERATIONAL LIMITS |
Sundstrand APS 2300
Parameter Min Max Start Temperature -54ºC ISA + 35ºC Altitude --------- 30,000 ft Operation Temperature -62ºC ISA + 35ºC Altitude Electrical --------- 33,000 ft Bleed ---------- 15,000 ft To Assist Engine Start ---------- 21,000 ft Rotor Speed ---------- 108% EGT Start ---------- 1032ºC Continuous ---------- 717ºC |
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EMERGENCY EVACUATION
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Captain:
1.Parking Brake .................................................ON 2.Flaps.............................................................5 3.Thrust Levers...............................................IDLE 4.START/STOP 1 & 2................................... STOP 5.Evacuation Command..............................Initiate • Initiate the evacuation by using the passenger address system. “Evacuate, Evacuate”. 5.Captain Evacuation Checklist complete. First Officer: 1.ATC .............................................................Notify 2.Fire Handles...............PULL & ROTATE (1L and 2R) 3.APU EMER STOP...................................PUSH IN 4.APU FIRE EXTINGUISHER ...................PUSH IN 5.PRESSURIZATION DUMP.....................PUSH IN 6.First Officer Evacuation Checklist complete. As the last step before leaving the cockpit: • The last crewmember leaving the flight deck will turn the batteries off. 1.Batteries......................................................OFF |
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ENGINE ABNORMAL START
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1.#___START/STOP .......................STOP
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DUAL ENGINE FAILURE
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1.Airspeed..........................................265 KIAS MIN
2.RAT MANUAL DEPLOY Lever.................... PULL |
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ENGINE FIRE (1 or 2), SEVERE DAMAGE
OR SEPARATION |
1.Autothrottles .......................................Disengage
2.#__ Thrust Lever ....... Confirm.....................IDLE 3.#__ START/STOP ...... Confirm................... STOP 4.#__ Fire Handle ......... Confirm....................PULL |
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APU FIRE
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1.APU EMER STOP .............................. PUSH IN
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BATT (1 or 2) OVERTEMP
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1.Associated BATT 1 or BATT 2....................OFF
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SMOKE / FIRE / FUMES
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1.Oxygen Masks............. Verify ............... ON, 100%
2.Crew Communication...........................Establish |
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CARGO FORWARD (AFT) SMOKE
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1.Associated Cargo Fire
Extinguisher Button..........................................PUSH |
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SMOKE EVACUATION
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1.Oxygen Masks............. Verify ............... ON, 100%
2.Crew Communication...........................Establish 3.Pressurization Dump Button ................ PUSH IN |
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JAMMED CONTROL COLUMN - PITCH
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1.ELEVATOR DISCONNECT Handle ..............PULL
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JAMMED CONTROL WHEEL - ROLL
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1.AILERON DISCONNECT Handle .................PULL
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PITCH TRIM RUNAWAY
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1.AP/TRIM DISC Button............ PRESS and HOLD
2.PITCH TRIM SYS 1 & 2 CUTOUT Button ..................................... PUSH IN 3.AP/TRIM DISC...................................... .RELEASE |
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ROLL (YAW) TRIM RUNAWAY
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1.AP/TRIM DISC Button ............ PRESS and HOLD
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STEERING RUNAWAY
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1.STEER DISC SWITCH ...............................PRESS
2.Steer the airplane using differential braking and rudder. |
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CABIN ALTITUDE HI
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1.Oxygen Masks........... Verify ................ ON, 100%
2.Crew Communication.......................... Establish 3.Altitude....................... 10,000 ft or MEA (whichever is higher) 4.Thrust Levers ...............................................IDLE 5.SPEED BRAKE Lever ......................FULL OPEN 6.Airspeed............................. MAX/APPROPRIATE 7.Transponder ................................................. 7700 8.ATC...........................................................NOTIFY |
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EMERGENCY DESCENT
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1.Seat Belts...................................................... ON
2.Altitude. 10,000 ft or MEA (whichever is higher) 3.Thrust Levers ............................................ IDLE 4.Speed Brake Lever........................ FULL OPEN 5.Airspeed...........................MAX/APPROPRIATE 6.Transponder ...............................................7700 7.ATC........................................................ NOTIFY |