Memory Items

Front 1

ERJ-170
Maximum Ramp Weight
(MRW)

Back 1

82,364 lbs.

Front 2

ERJ-170
Maximum Takeoff Weight
(MTOW)

Back 2

82,011 lbs.

Front 3

ERJ-170
Maximum Landing Weight
(MLW)

Back 3

72,310 lbs.

Front 4

ERJ-170
Maximum Zero Fuel Weight
(MZFW)

Back 4

65,256 lbs.
66,446 lbs.*
* Refer to the Flight Release to confirm the applicable MZFW.

Front 5

ERJ-175
Maximum Ramp Weight
(MRW)

Back 5

85,870 lbs.

Front 6

ERJ-175
Maximum Takeoff Weight
(MTOW)

Back 6

85,517 lbs.

Front 7

ERJ-175
Maximum Landing Weight
(MLW)

Back 7

74,957 lbs.

Front 8

ERJ-175
Maximum Zero Fuel Weight
(MZFW)

Back 8

69,886 lbs.

Front 9

Max. takeoff and landing tailwind component

Back 9

10 knots

Front 10

Max. runway slope

Back 10

+/- 2.0%

Front 11

Runway Surface Type

Back 11

PAVED

Front 12

Flap maneuvering load acceleration limits. Flaps...
Up
DOWN

Back 12

-1.0 G to +2.5 G

0.0 G to +2.0 G

Front 13

Max. operating altitude

Back 13

41,000 feet

Front 14

Max. takeoff and landing altitude

Back 14

8,000 feet (ERJ 170/175 only)

Front 15

Max. ambient air temperature for T/O and landing

Back 15

52°C

Front 16

Max. flap extension altitude

Back 16

20,000 feet

Front 17

Max. flight operating latitude

Back 17

78N to 78S

Front 18

Min. ambient temperature approved for takeoff

Back 18

-40°C

Front 19

Min. ambient temperature for operation

Back 19

-54°C

Front 20

The maximum demonstrated crosswind for takeoff and landing is:

Back 20

28 Knots

Front 21

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)

Back 21

(1) 28 knots
(2) 28 knots
(3) 20 knots
(4) 18 knots
(5) 12 knots

Front 22

TURBULENT AIR PENETRATION
(1) Below 10,000 MSL

(2)At or above 10,000 MSL

Back 22

(1) 250 KIAS

(2) 270 KIAS/0.70M (ERJ 170/175)
Use whichever speed is lower

Front 23

Maximum gear extension speed (VLO)
Maximum gear retraction speed (VLO)
Maximum gear extended speed (VLE)

Back 23

250 KIAS
250 KIAS
250 KIAS

Front 24

MAXIMUM TIRE GROUND SPEED

Back 24

195 KIAS

Front 25

MAXIMUM FLAP OPERATING SPEEDS - VFE
FLAP 1
FLAP 2
FLAP 3
FLAP 4
FLAP 5
FLAP FULL

Back 25

FLAP 1---230
FLAP 2---215
FLAP 3---200
FLAP 4---180
FLAP 5---180
FLAP FULL----165

Front 26

MAXIMUM SPEED TO OPEN THE DIRECT VISION WINDOW

Back 26

160 KIAS

Front 27

MANEUVERING SPEED ENVELOPE

Back 27

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).

Front 28

Maximum airspeed for windshield wiper operation is

Back 28

250 KIAS (R)

Front 29

(1) Maximum usable quantity per tank
(2) Unusable quantity per tank
(3) Aircraft maximum fuel capacity
(usable + unusable fuel)

Back 29

(1) 10392.5 lbs
(2) 75 lbs
(3) 20,935 lbs

Front 30

MINIMUM FUEL TANK TEMPERATURE

Back 30

- 40°C

Front 31

Maximum fuel imbalance between tanks

Back 31

794 lbs

Front 32

The XFEED Selector must be set to ______during takeoff and landing.

Back 32

OFF

Front 33

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)_____

Back 33

(1) 7.8 psi
(2) 8.3 psi
(3) 8.7 psi
(4) -0.5 psi
(5) 0.2 psi

Front 34

The maximum altitude for single pack operation is

Back 34

31,000 feet

Front 35

BRAKES
Cooling Limitation

Back 35

do not takeoff with amber brake temperature
indicators. (R)

Front 36

FLAPS

Back 36

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)

Front 37

THRUST REVERSERS (R)

Back 37

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.

Front 38

NAVIGATION

Back 38

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.

Front 39

RVSM MINIMUM EQUIPMENT REQUIRED

Back 39

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.

Front 40

AUTO FLIGHT CONTROL SYSTEM

Minimum Engagement Height ..........

Minimum Use Height- Coupled ILS Approach...........

Back 40

400 ft AGL

50 ft AGL

Front 41

PROHIBITED MODES

Back 41

The VOR and VNAV flight director modes are prohibited

Front 42

POWER PLANT

Back 42

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.

Front 43

ENGINE STARTER DUTY CYCLE LIMITS

Back 43

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).

Front 44

ENGINE STARTER DRY MOTORING DUTY CYCLE LIMITS

Back 44

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.

Front 45

APU STARTER DUTY CYCLE

Back 45

Start Cycle Maximum Followed By
1st and 2nd 60 seconds ON 60 seconds OFF
3rd cycle 60 seconds ON 5 minutes OFF

Front 46

APU LIMITS
TYPE
OPERATIONAL LIMITS

Back 46

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

Front 47

EMERGENCY EVACUATION

Back 47

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

Front 48

ENGINE ABNORMAL START

Back 48

1.#___START/STOP .......................STOP

Front 49

DUAL ENGINE FAILURE

Back 49

1.Airspeed..........................................265 KIAS MIN
2.RAT MANUAL DEPLOY Lever.................... PULL

Front 50

ENGINE FIRE (1 or 2), SEVERE DAMAGE
OR SEPARATION

Back 50

1.Autothrottles .......................................Disengage
2.#__ Thrust Lever ....... Confirm.....................IDLE
3.#__ START/STOP ...... Confirm................... STOP
4.#__ Fire Handle ......... Confirm....................PULL

Front 51

APU FIRE

Back 51

1.APU EMER STOP .............................. PUSH IN

Front 52

BATT (1 or 2) OVERTEMP

Back 52

1.Associated BATT 1 or BATT 2....................OFF

Front 53

SMOKE / FIRE / FUMES

Back 53

1.Oxygen Masks............. Verify ............... ON, 100%
2.Crew Communication...........................Establish

Front 54

CARGO FORWARD (AFT) SMOKE

Back 54

1.Associated Cargo Fire
Extinguisher Button..........................................PUSH

Front 55

SMOKE EVACUATION

Back 55

1.Oxygen Masks............. Verify ............... ON, 100%
2.Crew Communication...........................Establish
3.Pressurization Dump Button ................ PUSH IN

Front 56

JAMMED CONTROL COLUMN - PITCH

Back 56

1.ELEVATOR DISCONNECT Handle ..............PULL

Front 57

JAMMED CONTROL WHEEL - ROLL

Back 57

1.AILERON DISCONNECT Handle .................PULL

Front 58

PITCH TRIM RUNAWAY

Back 58

1.AP/TRIM DISC Button............ PRESS and HOLD
2.PITCH TRIM SYS 1 & 2
CUTOUT Button ..................................... PUSH IN
3.AP/TRIM DISC...................................... .RELEASE

Front 59

ROLL (YAW) TRIM RUNAWAY

Back 59

1.AP/TRIM DISC Button ............ PRESS and HOLD

Front 60

STEERING RUNAWAY

Back 60

1.STEER DISC SWITCH ...............................PRESS
2.Steer the airplane using differential braking and
rudder.

Front 61

CABIN ALTITUDE HI

Back 61

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

Front 62

EMERGENCY DESCENT

Back 62

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