Oil temp 30 min…………run up procedure (60% N1)

Limitations Flashcards by Peter Euler

MLM

E190-E2: 49050kg
E195-E2: 54000kg

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MTOM

E190-E2: 54000kg
E195-E2: 61500kg

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MZFM

E190-E2: 46700kg
E195-E2: 51850kg

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Gear

Vlo. 220
Vle. 250
V. 265

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Max speed flap extended

Flaps1. 220kts
Flaps2. 215kts
Flaps3. 200kts
Flaps4. 180kts
Flaps5. 180kts
Full. 165kts

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Flap manouver speed (1.3 g margin to shaker = 40 bank for max t/o mass w/o ice)

Up. 210
1. 180
2. 160
3. 150
4. 140
5. 140
Full. 130

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Ice Speed reset

SAT > 5
no ice accretion
no ice condition

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Engine Start

Starter Limit………………….4 min
Fuel on to idle……………….max 120 sec
After N2 pos. Oil press….10 sec
Ignition and fuel…………….20-27% N2
Starter Cut Out………………55% N2

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Engine

Oil temp<24………………….no t/o
OAT<= 3 + vis. moist/ ground Time > 30 min…………run up procedure (60% N1)

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Cold soak fuel frost area

No prec/visible moisture
OAT > 0
Frost layer inside marked area

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LMC

5 pax
1 Crew Member
350kg
+/- 2% CG
fuel discrepancies up to 100 kg may be accepted w/o LMC
only one LMC

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TOLD

+/- 1kts
+/- 0.5 units

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Fuel Uplift

2% of FOB + 140 kg

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Water Drain in flight

ground time > 4h
OAT < 5

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Dispatch Landing Performance

required if:
Cat II/III
malfunctions reading landing distance
tailwind > 10kts
airport elevation > 3000ft
runway contaminated
runway < 2200m

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Wind Limitations Autoland

Max headwind: 25kts
Max x-wind: 15 kts
Max Tail-wind: 15kts

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Rolling Take Off

advance TL to 40% w/o brake - then move TL forward
TOD and ASD increase in 275m

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Normal Take Off

advance TL to 40% with brakes on - then move TL forward
TOD and ASD increase by 30m

Static Take Off

advance TL to 40%, and then to TOGA with brakes on

Take OFF with x-wind>30kts and/or tails wind >13 its

AT disarmed
TL to 60%
release brakes
when GS 20kts arm AT and make sure TL advance to TOGA
A

Take OFF with x-wind>30kts and/or tails wind >13 its

AT disarmed
TL to 60%
release brakes
when GS 20kts arm AT and make sure TL advance to TOGA
ASD and TOD increase by 150 bzw 170m

Take Off OAT < 3 and visible moisture and gnd time > 30’

TL to 60% N1, hold at that thrust level for 10” and then back to idle or until fan vibration stops

Conversion of visibility to CMV

not applicable for:

RVR values for take off (except first part=90m segment)
when measured values available
for the purpose of continuation of an LVO approach
use factor 1 for flight planning purposes

Engine Start Protection

Hot Start
Hung Start
Failure of N1 to rotate
Failure to light up
Inabiity to control igniter or fuel flow

Engine Airstart Envelope

AES: from 130 kts - 260kts and 20000ft from 200kts - 260kts and 30000ft WML: from 260kts - 320kts and 25000ft for WML N2>15 for AES N2 < 8

LSA Tape

functon of: Airspeed Slat/Flap AoA Spoiler position Landing Gear Icing Condition top of band Vs1g, bottom Vshaker (factor K from 1.054 to 1.13)

Turbulent airspeed

250 < 8000ft 270 > 10000ft - 33000ft M0.76 up to 40000ft

Autopilot

available @ 200ft minimum use height NPA = 190ft minimum use height PA = 80ft

MAX Reverse should be taken into account when considered with ePerf

Wet Slippery Contaminated

Best Beta

Gear not locked down Flaps less than 5 TLA > 57 FCS in normal mode

RNP (track limitations)

Departure/Enroute/Arrival …..track deviation < half RNP value Approach…half scale deflection (= 1 dot for angular approach; +/- 75ft for linear approach)

ADDNAR

5000m vis 2000ft ceiling or circling alt+500ft mnm 1 non RNP approach 2 separate RWY with independant approach aids no adverse WX no gusts BA mnm medium

Airplane Approach Category

E-Jets flaps 5 /Full…………………..C E195-E2 flaps 5 >52000………….D

Conversion VIS to RVR (planning)

Conversion factor of 1 shall be used

Wind Limitations Planning

For x-Wind and tailwind limits gust shall be considered taking respective runway condition into account.If OM-B does not state a gust limit the mean crosswind limit plus 5 kts is applicable Departure/Destination…..50kts mean Wind/x-and tail wind acc OM-B Alternate………40kts mean wind/x-and tail wind acc OM-B-10kts/5kts

APU Start/Operation Limit

39000ft (start) 39000ft (elec supply) 15000ft (bleed supply) 20000ft (to assist engine start, see QRH table)

Starter Limitation (until 55%N2) (Engine Starter Limit)

4 min if full duty cycle was used 30 min cool down time

Wind limitations Cat II

Headwind: 25kts Crosswind: 18kts Tailwind:15kts

Stabilisation criteria lateral

Linear Approach/ILS…..half scale deflection Angular Approach……..+/-5

Stabilisation criteria vertical

Conventional 3D…….half scale deflect. 2D…….+/-100ft of CDFA path SMA (Segment mnm alt)…..-0/+100ft

3 basic fuel scheme

Basic Procedure Procedure without alternate Procedure with closed destination

Basic procedure (Fuel Planning)

Taxi Fuel Trip Fuel Contingency Fuel Alternate Fuel Final Reserve Fuel Additional Fuel (if required e.g ADDNAR , ADDE, MEL required) Extra Fuel (e.g SWIFAT)

Procedure without alternate

Taxi Fuel Trip Fuel Contingency Fuel Final Reserve Fuel ADDNAR Extra Fuel

Procedure with closed destination

Taxi Fuel Trip Fuel Contingency Fuel Final Reserve Fuel Additional Fuel (if required) Alternate Fuel 2 (furt away alternate) extra fuel